NASA Technical Memorandum 4789

Flight Wing Surface Pressure

and Boundary-Layer Data

Report from the F- 111 Smooth

Variable-Camber Supercritical

Mission Adaptive Wing

Sheryll Goecke Powers and Lannie D. Webb

Dryden Flight Research Center

Edwards, California

National Aeronautics and

Space Administration

Office of Management

Scientific and Technical

Information Program

1997

CONTENTS

1

ABSTRACT ..............................................................................

.1

INTRODUCTION .........................................................................

NOMENCLATURE ........................................................................ 2

DESCRIPTION OF EXPERIMENT ........................................................... 4

INSTRUMENTATION ...................................................................... 55

Wing-Pressure Orifices ................................................................... 5

Boundary-Layer Rake .................................................................... 5

Flight Deflection Measurement System ...................................................... 6

Measurements ................................................... 6

Accuracy ..............................................................................

6

ANALYSIS TECHNIQUES .................................................................. 6

Pressure Data .............................................................. 7

Flight Detection Measurement System ................................ 7

Test Points .............................................................................

7

RESULTS AND DISCUSSION .............................................................. 8

Span Effects on Pressure Distribution ....................................................... 8

Mach Number Effects .................................................................... 8

Camber and Angle-of-Attack Effects .................................................... 9

Camber and Angle-of-Attack Effects on Normal Force Coefficient ................................. 9

Wing-Tip Twist Effects ...................................................................

10

CONCLUDING REMARKS ................................................................

APPENDIX A: Maw Airfoil Coordinates for a Wing Sweep of 26 ° at 24

Span Stations 0.93, 0.76, 0.59, and 0.40 ........................................................

APPENDIX B: General Listing of Available Wing Pressure and Boundary-Layer Data ................... 45

APPENDIX C: Wing Pressure Coefficients for Nominal Dynamic Pressure of 300 lb/ft 2

52

and Mach Number of 0.60 ...................................................................

APPENDIX D: Wing Pressure Coefficients for Nominal Dynamic Pressure of 300 lb/ft 2

140

and Mach Number of 0.70 ..................................................................

APPENDIX E: Wing Pressure Coefficients for Nominal Dynamic Pressure of 300 lb/ft 2

203

and Mach Number of 0.80 ..................................................................

APPENDIX F: Wing Pressure Coefficients for Nominal Dynamic Pressure of 300 lb/ft 2

300

and Mach Number of 0.85 ..................................................................

111
APPENDIX G: Wing Pressure Coefficients for Nominal Dynamic Pressure of 300 lb/ft 2

and Mach Number of 0.90 ....

" " ............................................ 381

APPENDIX H: Wing Pressure Coefficients for Dynamic Pressures From 300 to 800 lb/ft 2

and Mach Numbers From 0.61 to 1.41

........................................................ 456

APPENDIX I: Wing Pressure Coefficients for Dynamic Pressures From 80 to 300 lb/ft 2

and Mach Numbers From 0.28 to 0.59

...... ; ................................................. 571

APPENDIX J: Wing Pressure Coefficients for Dynamic Pressure From 250 to 800 lb/ft 2

and Mach Numbers From 0.60 to 0.90

........................................................ 07

APPENDIX K: Boundary-Layer Data

........................................................ 79

REFERENCES

.......................................................................... 49

TABLES

A°I.

A-2.

A-3.

A-4.

A-5.

A-6.

A-7.

A-8.

B.

C-I.

C-2.

D-1.

D-2.

E-I.

E-2.

Fol.

F-2.

G-1.

G-2.

H-1.

H-2.

I-1.

Full-scale wing-splash coordinates (_LE/TE = 0/2, 1"1= 0.93, c = 9.2276 ft) ........................ 24

Full-scale wing-splash coordinates (8/..F_E = 0/2, 1"1= 0.76, c = 9.9413 ft) ........................ 29

Full-scale wing-splash coordinates (_LF_/rE= 0/2, "1"1= 0.59, c = 10.8549 ft) ....................... 31

Full-scale wing-splash coordinates (SLE,TE = 5/10, rl = 0.76, c = 9.8570 ft) ....................... 35

Design coordinates (_LE//'E = 0/2, rl = 0.93, c = 9.1426 ft) .................................... 41

Design coordinates (SLEq.E = 0/2, 1"1= 0.76, c = 9.9827 ft) .................................... 42

Design coordinates (_iLF_/TE= 0/2, rI = 0.59, c = 10.8227 ft) ................................... 43

Design coordinates (SLF_/rE= 0/2, 1"1= 0.40, c = 11.8004 ft) ................................... 44

Nominal values for MINF, ALPT and QINF, with appendix letters

.............................. 45

Summary of Data

..................................................................... 2

Listing of Data

....................................................................... 5

Summary of Data.

................................................................... 40

Listing of Data.

..................................................................... 42

Summary of Data

.................................................................... 03

Listing of Data

...................................................................... 06

Summary of Data.

................................................................... 00

Listing of Data

...................................................................... 03

Summary of Data

.................................................................... 81

Listing of Data

...................................................................... 84

Summary of Data.

................................................................... 456

Listing of Data

...................................................................... 460

Summary of Data.

................................................................... 71

iv
I°2.

J-1.

J-2.

K-1.

K-2.

573

Listing of Data ......................................................................

607

Summary of Data ....................................................................

612

Listing of Data ......................................................................

779

Summary of Data ....................................................................

794

Listing of Data ......................................................................

FIGURES

1. AFrI/F- 11 ! MAW airplane in flight. Chordwise dark areas on the right wing indicate

the four semispan locations of pressure orifices (refs. 11, 12, and 27) ............................. 11

2. The MAW smooth, variable-camber flap shape (refs. 11, 12, and 27) ............................. 11

3. Wing-splash template preparation on the AFFI/F-111 MAW airplane (ref. 16) ..................... 12

4. Wing planform and airfoil shapes at design cruise condition (ref. 11 and 16) ....................... 12

5. Semispan locations of surface-pressure orifices, boundary-layer rake, pressure

instrumentation, and wingtip accelerometers for the right wing (ref. 12) .......................... 13

13

6. Boundary-layer rake (refs. 12 and 27) .....................................................

7. FDMS target locations on the lower surface of the left wing (ref. 12) ............................. 14

8. Time history of typical windup turn maneuver used to obtain wing pressure, FDMS,

and boundary-layer data; M**= 0.85, qoo = 300 lb/ft 2, and _)LE/TE = 0/2 (ref. 12) .................... 14

9. Steady chordwise pressure distributions at four semispan stations for M_ = 0.85,

q_ = 300 Ib/ft 2, and _SLEq-E = 0/2. No separation at OtT= 8 ° (ref. 12) ............................. 15

10. Steady chordwise pressure distributions at four semispan stations for Moo-- 0.85,

qoo ---300 lb/ft 2, and _LE/TE = 5/|0 (ref. 12) ................................................. 16

i 1 Steady chordwise pressure distributions for large and small ranges of Mach number; • 17

T1= 0.76, qoo -- 300 lb/ft 2, and otT = 8° (ref. 11) ..............................................

12. Chordwise pressure distributions and velocity profiles for different cambers (Moo = 0.80,

rl = 0.76, and qoo = 300 ib/ft 2) (ref. 27) ..................................................... 18

13. Section normal-force coefficient as a function of _T for different camber deflections at 21

Moo = 0.80, 11= 0.76, and q_, = 300 lb/ft 2 (ref. 27) ............................................

14. Comparison of FDMS measured wingtip delta twist with two pressure profiles for 22

Moo = 0.85 and qoo= 300 and 600 ib/ft 2 (ref. 12) .............................................

V

ABSTRACT

Flight tests were conducted using the advanced fighter technology integration F-Ill (AFTI/F-111) aircraft

modified with a variable-sweep supercritical mission adaptive wing (MAW). The MAW leading- and trailing-edge

variable-camber surfaces were deflected in flight to provide a near-ideal wing camber shape for the flight condition.

The MAW features smooth, flexible upper surfaces and fully enclosed lower surfaces, which distinguishes it from

conventional flaps that have discontinuous surfaces and exposed or semi-exposed mechanisms. Upper and lower

surface wing pressure distributions were measured along four streamwise rows on the right wing for cruise,

maneuvering, and landing configurations. Boundary-layer measurements were obtained near the trailing edge for

one of the rows. Cruise and maneuvering wing leading-edge sweeps were 26 ° for Mach numbers less than 1 and 45 °

or 58 ° for Mach numbers greater than 1. The landing wing sweep was 9° or 16". Mach numbers ranged from 0.27

to 1.41, angles of attack from 2° to 13°, and Reynolds number per unit foot from 1.4 × 106 to 6.5 × 106. Leadingedge cambers ranged from 0° to 20 ° down, and trailing-edge cambers ranged from 1° up to 19° down. Wing

deflection data for a Mach number of 0.85 are shown for three cambers. Wing pressure and boundary-layer data are

given. Selected data comparisons are shown. Measured wing coordinates are given for three streamwise semispan

locations for cruise camber and one spanwise location for maneuver camber.

INTRODUCTION

The wing for a tactical fighter airplane is typically designed for a few optimum or near-optimum flight

conditions such as a specific Mach number, altitude and load-factor combination, or 1-g cruise. However, the

airplane must operate over a wide range of flight conditions. To investigate advanced wing designs, the National

Aeronautics and Space Administration (NASA) and the United States Air Force (USAF) conducted a series of flight

tests on an F-111A airplane. The first flight test was the Transonic Aircraft Technology (TACT) program (refs. !

and 2), which combined a supercritical airfoil (ref. 3) with planform and twist changes to improve transonic cruise

and maneuver performance relative to the conventional F-111 wing (ref. 4). The second flight test, which was the

final research program conducted on the advanced fighter technology integration (AFFI)/F-111, was the mission

adaptive wing (MAW) concept.

The MAW concept had a supercritical wing configuration that allowed smooth camber changes throughout the

flight envelope to provide additional aerodynamic performance at all flight conditions. Previous supercritical wing

designs tended toward a fixed-geometry shape, which was a compromise for specific mission requirements. The

MAW design goals were to minimize penalties for off-design flight conditions through the combination of smooth

skin variable camber and variable sweep (ref. 5). On airplanes such as the F-16 and F-18 aircraft, the variable

camber is achieved through discrete flap positions. Better performance can be achieved with smooth variable

camber. Design studies (refs. 6 and 7) to develop a smooth, variable-camber supercritical wing resulted in the MAW.

The MAW consists of leading- and trailing-edge variable-camber surfaces that can be deflected in flight to provide

a near-ideal wing camber shape for any flight condition. These variable-camber surfaces feature smooth, flexible

upper surfaces and fully enclosed lower surfaces, distinguishing them from conventional flaps that have

discontinuous surfaces and exposed or semi-exposed mechanisms. The camber shape is controlled by either a

manual or automatic flight control system (ref. 8).

The wing and aircraft were extensively instrumented to evaluate the aerodynamic performance of the MAW

(refs. 9 and 10). Instrumentation for defining the wing characteristics included surface-pressures orifices, a

boundary-layer rake, and a flight deflection measurement system (FDMS). The MAW was flown on the AFTI/F-111

in a joint NASA/USAF/Boeing Advanced Systems (Seattle, Washington) flight research program at the NASA

Dryden Flight Research Center (DFRC).
Resultsfrom theMAWprogramweresummarizedat thesymposiumheldat NASA DFRCin April 1989

(ref.5). Aerodynamiccharacteristicsandperformanceevaluationsuchaswing-pressureresults,buffetresults,

andlift anddraghavebeendiscussedin separatesubdisciplinereports(refs.11-15).The dataindicatethat,

comparedto the basicF-111Aand TACTdesigns,the AFTI/F-Ill MAW aircraft significantlyimproved

aerodynamiccharacteristics.

Theprimarygoalofthispaperistodocumentwingpressureandboundary-layer dataobtainedduringtheMAW

flight program.Thedataareselectedfrom stableor near-stableflight conditionsfor cruise,maneuvering,and

landingconfigurations.ThecruiseandmaneuveringdataforMachnumberslessthan1areatawingleading-edge

sweepof 26°. ForMachnumbersgreaterthanl, thewingsweepsare45° or58°.Thelandingwingsweepsare9°

or 16°.TheReynoldsnumberperunitfoot(RNPU)isfrom1.4x l06 to6.5x l06.Machnumbersrangefrom0.27

to 1.41forthewingsurface-pressure dataandfrom0.48to0.95fortheboundary-layer data.Leading-edgecambers

rangefrom0° to20° down,andtrailing-edgecambersrangefrom1oupto 19° down.Anglesof attackvariedfrom

2° to 13°,anddynamicpressuresrangedfrom80to800Ib/ft2.

Thewing-pressuredistributionsarefromfourchordwiserows,andtheboundary-layer pofilesarefromnearthe

trailingedgeof oneof thepressurerows.PlotsofrepresentativedatanearthedesignMachnumberareshownand

discussed.Thewing-twistdeflectiondata(threecambersat a Machnumberof 0.85),whichwerepresentedin

reference12,arealsoincludedinthisreport.Computational fluiddynamicscomparisonswithMAWflightdataare

presentedinreferences11and16.Flightwing-pressuredistributionsarealsocomparedwithMAWwind-tunneldata

andwithTACTflightdatain reference11.

NOMENCLATURE

The values in brackets, [

edge sweepback angle of 26 ° scaled up, are from reference 17.

AFT/

ALPT

b

Beta or BETA

Cav

CMAC

c n

C

p

C *

p

], which are based on a trapezoidal planform with an aspect ratio of 5.14 and a leadingadvanced fighter technology integration

wing reference angle of attack, ct + Act, deg

wing span, ft [56.55 ft]

aircraft angle of sideslip, deg

streamwise local chord for sweepback angle of 26 °, ft

mean geometric chord, wing reference area, ft 2

wing span, ft [11.0 ft]

b/2

mean aerodynamic chord, (2/S) f c2dy [11.2 ft]

0

1

section normal force coefficient, f(ACp )d(x/c)

0

pressure coefficient, ( p - po_) / q,_

critical pressure coefficient, _-+

2
C

PLS.

Cpre

Cpus.

CN

CNWP

CP

DFRC

FDMS

H

L.S.

LOC

M.o

MAW

MINF

MTOP

NASA

P

P..

PCM

PSUR

q..

QINF

RNPU

S

TACT

THETA

TINF

U

U e

U.S.

USAF

UTOP

W

x

pressure coefficient on wing lower surface

pressure coefficient on wing upper surface at xlc = 0.96

pressure coefficient on wing upper surface

section normal force coefficient, '(ACp)d(x/c)

0

wing normal force coefficient calculated using CN values

pressure coefficient, ( p - p,o)/ q**

Dryden Flight Research Center

flight deflection measurement system

altitude, ft

lower wing surface

chord location

free-stream Mach number

mission adaptive wing

free-stream Mach number

local Mach number for boundary-layer rake at Y = 5 in.

National Aeronautics and Space Administration

local wing surface static pressure, lb/ft 2

free-stream static pressure, lb/ft 2

pulse code modulation

local surface static pressure for boundary-layer rake at x/c = 0.96 for rl = 0.76, lb/ft 2

free-stream dynamic pressure, lb/ft 2

free-stream dynamic pressure, lb/ft 2

Reynolds number per unit foot, ft -1

wing reference area, ft2 [622.0 ft 2]

Transonic Aircraft Technology

6, b

PU (1- U

momentum thickness, I _, _e )dy'in

0

free-stream temperature, °F

chordwise component of local velocity, ft/sec

chordwise component of local velocity at Y = 5 in. and x/c = 0.96 for rl = 0.76, ft/sec

upper wing surface

United States Air Force

chordwise component of local velocity at Y = 5 in. and x/c = 0.96 for 1"!= 0.76, ft/sec

spanwise component of local flow velocity, positive outboard direction, ft/sec

local streamwise coordinate (from wing leading edge) for sweepback angle of 26 °, ft
x/c

Y

Y

Z

z/c

(X

O_Pn wt

OLT

Y

Aa

SLE/rE

g)LFA,_O

.q

0

P

Pc

fraction of local streamwise chord (wing)

perpendicular distance above upper wing surface, in.

spanwise coordinate, ft

vertical component, ft

nondimensional vertical component

indicated angle of attack corrected to wing reference plane, deg

dynamic response of normal acceleration at wingtip, g

wing reference angle of attack, ct + Atx, deg

aircraft angle of sideslip, deg

ratio of specific heats ( 1.4 for this study)

angle-of-attack correction for pitch and upwash effects, deg

boundary-layer thickness, in.

leading- and trailing-edge camber deflection, down is positive, deg

leading-edge camber deflection/(inboard/midsparffoutboard trailing-edge flap deflections),

down is positive, deg

orifice row semispan locations, 2y/b

local wing-twist angle, deg

air density, slug/ft 3

air density at edge of boundary layer, slug/ft 3

DESCRIPTION OF EXPERIMENT

Figures 1 and 2 show the AFYI/F- 111 MAW airplane and camber shape of the wing. The airplane was initially

an F- 111A airplane that had its wings replaced for the TACT/F- 111 program (ref. 1). The TACT wing, except for

the wing box, was subsequently replaced with the MAW. Modifications (ref. 18) were made to the TACT wing

planform to accommodate the installation of the smooth skin leading- and trailing-edge variable-camber systems.

Figure 2 shows the variable-camber leading- and trailing-edge surfaces of the MAW, specifically, the flex panels for

the upper surfaces and the fixed-geometry (nonflexing) surfaces for the lower surfaces. (Note that the positive

direction is down.)

Three wing-splash templates were made to obtain the constructed wing geometry at semispan locations (rl)

of 0.93, 0.76, and 0.59 (which correspond to pressure orifice rows) for a leading- and trailing-edge camber (SLF_/TE)

of 0/2. One wing splash was made at 1"1= 0.76 for 5LE/TE = 5/10. Figure 3 shows a template fitted on a streamwise

airfoil section of the MAW. A discussion of the template construction technique and the method used to obtain the

wing coordinates from the template is found in reference 16. Appendix A lists the wing coordinates from the

templates and the wing design coordinates from 1/ 12 scale wind-tunnel model. The design coordinates are from

reference 17. Figure 4 shows airfoil shapes of the MAW model for a wing sweep of 26 ° and 6LF_/TE= 0/2 (refs. 11

and 16). Tables A-1 through A-3 list the as-built coordinates determined from the wing splashes for 5LE/TE = 0/2 at

= 0.93, 0.76, and 0.59. Table A-4 lists the as-built coordinates for SLE/rE= 5/10 at rI = 0.76. The final MAW wing

design coordinates (ref. 17), which were for a 1-g cruise condition at a leading-edge wing sweepback of 26 °

and CSLE/TE = 0/2, are listed in tables A-5 through A-8. The as-built coordinates for 6LE/TE= 0/2 and 1"1= 0.76 are

compared with the corresponding design coordinates in reference 16. This comparison indicates significant

differences on the upper surface for x/c of 0.50 to 0.70, where x/c is the ratio of chordwise distance from leading edge

4
to chord. The maximum disagreement, at x/c = 0.61, corresponds to a 0.24-in. difference between the design and

full-scale measurements. This comparison required a rotation of the design airfoil to account for the local twist angle

of 0 = 5.279 °. This rotation was accomplished by using the two-dimensional direction-cosine transformation of

Euler angles: x rotated = x cos0 + z sin0, and z rotated = z cos0 - x sin0.

INSTRUMENTATION

Wing-Pressure Orifices

For this study, the pressure instrumentation was located on the right wing of the AFTI/F- 111 airplane (fig. 5).

A detailed discussion of the static pressure instrumentation is found in reference 19. There were 152 flush-surface

static pressure orifices located on the upper and lower surfaces in four chordwise rows aligned with the free-stream

airflow at a leading-edge sweepback angle of 26 °. Figure 5 shows the number of upper and lower orifices at each

semispan station. Nine of the 10 pressure transducer boxes were located inside the flexible leading- and trailing-edge

flap surfaces, a fact which required connecting the leading- and trailing-edge surfaces with a flexible fluoro-silicon

tubing (0.07 in. inside diameter). The orifices located on the surface of the wing box were connected by stainlesssteel tubing (0.12 in. inside diameter). In most cases, the length of the pressure lines from the orifices to the

transducers was limited to less than 5 ft, thus minimizing pressure lag effects. Individual differential pressure

transducers (+_3 lb/in 2) mounted in the 10 boxes were used to measure the differential pressure between the wingsurface orifices and the reference pressure. A temperature-controlled variable-capacitance absolute pressure

(0 to 2200 ib/ft 2) transducer (labeled reference transducer in figure 5) measured the reference pressure.

Boundary-Layer Rake

The 36-probe flow-direction boundary-layer rake was installed on the upper-wing surface at 1"1= 0.76 (see figs. 5

and 6). The leading edge of the center probes was at x/c = 0.96, where x is the streamwise coordinate and c is the

streamwise local chord for a wing sweep of 26 °. Three impact pressures were measured at each probe height. For

3 flights, 31 upper surface orifice transducers from rows 1"1= 0.76 and 0.59 and 5 spare wing transducers were

connected to the boundary-layer rake shown in figure 6. Local flow direction was calculated using the pressures from

the two side probes (cut at 45 ° ) and the calibration technique in reference 20. Because of transducer problems, the

pressures at Y = 0.03 in. and 4.47 in. (see fig. 6) were not measured.

Flight Deflection Measurement System

The electro-optical FDMS used in this study (refs. 10 and 12) was an updated version of an earlier system

(refs. 21 and 22). The MAW FDMS consisted of a control unit, a receiver, a target driver, and 13 infrared lightemitting-diode targets (fig. 7). The targets were mounted on points of structural interest on the lower surface of the

left-hand wing. The receiver was mounted behind a window panel in the left side of the fuselage below the wing.

From this receiver location, all targets could be viewed for all camber settings when the wing was swept to 26 ° .

The control unit commanded the target driver to momentarily energize each target in order. Before each target

was illuminated, the control unit initiated a sequence within the receiver that involved clearing its linear diode array,

scanning the array to sample the background light signature, and scanning again with the target on. This process was

necessary to accomplish the automatic background light compensation. References 10 and 23 provide more

comprehensive information on the FDMS.
Measurements

Free-stream flight parameters, Mach number (M,_), static pressure (p.,), dynamic pressure (q_), wing reference

angle of attack (aT), and sideslip angle (_) were measured and derived from sensors installed on the APTI/F-111

airdata boom. Mach number data from a modified MA-1 type uncompensated pitot-static probe (ref. 24) were

corrected for position error. Angle of attack and sideslip angle were measured using a flight-path accelerometer vane

system (ref. 25). Angle of attack is referenced to the wing reference plane for consistency with the wind-tunnel data.

Because the noseboom is canted 2.5 ° down relative to the vehicle body axis and the MAW is set to an angle 1° up

relative to the vehicle body axis, a 3.5 ° correction was added to the indicated vane angle of attack to obtain the

indicated angle of attack, o_. This o_was corrected for pitch and upwash effects (ref. 14) to obtain o_T . Corrections

for boom bending were considered unnecessary because of the rigidity of the boom. This corrected angle of attack

was used for the wing-pressure data analysis.

All the instrumented parameters were recorded digitally on an airborne pulse code modulation (PCM) system.

The PCM system had a sampling rate of 20 to 800 samples/sec. Each of the wing surface and boundary-layer

pressures were sampled at 20 samples/sec. The system sampling rate for each FDMS target was 12.5 samples/sec.

Accuracy

Based on the repeatability of checkpoints used in the airspeed calibration, the accuracy of the corrected values

of M.o is estimated to be the same as that for the TACT program, +0.005 (ref. 1). The corrected values of angle of

attack and angle of sideslip have an estimated accuracy of-t-0.25 ° (ref. 1). The uncertainty in the determination of

Cp is a function of the uncertainties in q.,, p._, and p. The uncertainty in p is a function of the individual differential

pressure transducer and the absolute reference transducer. The transducer range for the individual differential

pressure transducers was _'f_3lb/in 2. The range for the absolute reference pressure transducer was 0-2200 lb/ft 2. For

the data in this report, Mach number ranges from 0.27 to 1.41 and dynamic pressure ranges from 80 to 810 lb/ft 2.

However, the majority of the data were obtained for Mach numbers of 0.60, 0.70, 0.80, 0.85 and 0.90 and a dynamic

pressure near 300 lb/ft 2, which corresponds to a nominal altitude of 32,000 ft. The uncertainty in Cp was calculated

for these latter conditions using the method of standard deviation outlined in reference 26. Estimated uncertainties

in the parameters were +4.8 lb/ft 2 for p, +1.3 lb/ft 2 for p._, and +0.005 for M. Using these standard deviations

resulted in a standard deviation of +0.02 for Cp These uncertainties in Cp occurred for trim flight conditions and

during wind-up turns where quasi-stable values of angle of attack, M, and altitude are maintained. The standard

deviation for data would be slightly less at dynamic pressures higher than 300 lb/ft 2 and slightly more at dynamic

pressure lower than 300 ib/ft 2.

ANALYSIS TECHNIQUES

Each time segment for the pressure, boundary-layer and FDMS data is for one point in time; in other words, the

data were not averaged for a time period. Thus the data for a given time, for example 9:34:25.500, represent a

snapshot of conditions at that time.

Pressure Data

To minimize concerns about pressure and sampling lag, the data used for the surface and boundary-layer

pressures were chosen from stabilized and quasi-stabilized flight conditions. When selecting data for analysis,

maximum deviations from the stabilized and quasi-stabilized flight conditions were 0.01 for M and 0.25 ° for ctT .

For the boundary-layer data, the Mach number and velocity calculations used the assumptionsthat the local static

pressure was constant through the boundary layer and that total temperature was constant through the boundary layer

6
andequaltothefree-streamvalue.Thelocalstaticpressurefortheboundary-layer data,PSUR,wasthesurfacestatic

pressureatx/c = 0.96 (directly ahead of the rake).

Flight Detection Measurement System

The data used for the FDMS analysis were from left-hand turns so that the lighted targets were against a

darkened background (dark compared to the sky). This contrast provided an optimum working environment for the

optical measurement system. Most of the data were obtained for stabilized or quasi-stabilized conditions.

Test Points

Flight data presented in this paper are for Mach numbers from 0.27 to 1.41 for the wing surface-pressure data

and from 0.48 to 0.95 for the boundary-layer data. The wing-twist deflection data are for a Mach number of 0.85.

Leading-edge cambers range from 0 ° to 20 ° down, trailing-edge cambers range from 1° up to 19° down, and angles

of attack range from 2 ° to 13°. Free-stream dynamic pressures range from 100 lb/ft 2 to 800 lb/ft 2. The majority of

the data were at 300 Ib/ft 2 or 600 lb/ft 2. All the boundary-layer and FDMS data and most of the wing surfacepressure data are for a wing sweep of 26 °. There are also wing surface-pressure data for wing sweeps 9 °, 16°, 45 °

and 58 °. Flight RNPU ranged from 1.4 x 106 to 6.5 x 106. Data for both the wing pressure and boundary-layer were

selected for analysis, in most cases, for angles of sideslip near 0 °. Appendices B through K contain the data from the

wing pressure and boundary-layer studies in table format. An overview of the available wing pressure and boundarylayer data is given in Appendix B where the wing camber and the nominal flight conditions for Mach number,

dynamic pressure, and angle of attack are listed. Appendix B also serves as an index to the wing-pressure data in

Appendix C through Appendix J. All the boundary-layer data are in Appendix K. The boundary-layer data are

limited to a maximum trailing-edge down camber of 7° because the flow was separating at the trailing edge for

cambers exceeding 7 ° down. The boundary-layer rake was not designed to measure separated flows.

To minimize concerns about pressure and system lag, wing pressure and boundary-layer data for the different

angles of attack were obtained during slow controlled windup turns. The aircraft was stabilized at the desired

Mach number and altitude before entering the windup turn. During an ideal slow windup turn, the aircraft was

stabilized for a few seconds or longer at each desired Mach number and angle of attack combination. Because of

thrust limitations, it was not possible to hold altitude and Mach number constant at the higher angles of attack

(>8 °) or flap settings. To correlate the FDMS and pressure data, the FDMS system data were obtained during the

pressure maneuvers.

Figure 8 illustrates the slow windup turn maneuver and the response of one pressure transducer and the dynamic

response of a wing-tip accelerometer. During the initial portion of this particular maneuver, the pilot was adjusting

altitude to achieve the desired conditions later in the maneuver. The initial part of the maneuver was unsteady in

nature but developed into a steady turn culminating at around 80 sec at the maximum aim angle of attack and dynamic

pressure values, and with the Mach number held constant. The wing pressure, boundary-layer, and FDMS data were

gathered using this type of windup turn. Soon after reaching the desired conditions, the onset of separation was

indicated by the traces for the wing-tip accelerometer and the trailing-edge pressure orifice at x/c = 0.96 and rl = 0.93,

and the maneuver was terminated.

RESULTS AND DISCUSSION

As can be seen in Appendices B through K, an extensive database was obtained. The purpose of this report is to

document the available data, so only a few results are presented in graphical form. The results presented in this

section were previously presented in references 11, 12, or 27.
Span Effects on Pressure Distribution

In figure 9 (ref. 12), the chordwise Cp distributions as a function of x/c are shown at the four semispan stations

for M.o = 0.85, q.o = 300 lb/ft 2, _LE/TE= 0/2 (baseline camber configuration), and CZT=8 ° and 10% These two angles

of attack were selected to show the effects of trailing-edge flow conditions on the pressure profiles. The critical

pressure coefficient (Cp*), the pressure coefficient corresponding to when the local Mach number equals 1, is also

shown. The czT = 8 ° data have good pressure recovery at the trailing edge, and the midspan profiles are typical of

supercritical airfoils (ref. 7) at or near the wing design conditions. All the upper surface-pressure profiles have a

strong negative pressure peak at the leading edge; however, for the midspan rows (r1 = 0.59 and 0.76) for (XT = 8 °,

the peak is followed by nearly constant Cp plateaus. For ctT = 8 °, the C profiles shock down from near x/c _=0.40

at 1"1= 0.93 to x,/c _--0.70 at 1"1= 0.40. Following the aft shocks, the Cp values indicate a region of recompression that

continues to the trailing edge. At the trailing edge, the pressures show good recovery for all the semispan stations.

The Cp profiles for otT = 10° also show strong leading-edge negative pressure peaks. The midspan Cp plateaus

disappear with the forward movement of the aft shock consequent to the separation of the boundary layer at the

trailing edge. The shading on the trailing edge of the wing represents an approximate region of separated flow

determined by analysis of the chordwise Cp profiles for ctT = 10°.

Figure 10 (ref. 12) illustrates the Cp profiles for _LE/TE = 5/10 and the same Mach number and angles of attack

as the Cp profiles in figure 5. The critical pressure coefficient is also shown. The leading-edge camber of 5° produces

a rounded leading-edge Cp profile. The midspan Cp profiles are semiflat followed by aft shock recompression near

the trailing-edge flap line (x/c _=0.70). The wing-tip row (rl = 0.93) is similar except for the large negative pressure

area aft of the trailing-edge flap line, resulting in a large secondary velocity peak. As shown in figure 9, the aft shock

moves toward the leading edge as ct T was increased to 10°. The larger trailing-edge deflection angle and angle of

attack, both 10°, combine to increase the approximate region of separated flow shown, which is indicated by the

shaded area.

Mach Number Effects

Figure 11 (ref. 11) compares the upper- and lower-surface Cp distributions at rl = 0.76, O_T= 8° and _)LF_/TE = 0/2

for large and small changes in Mach number. Figure 11(a) illustrates the development and rearward movement of the

expected shock in the upper surface Cp distributions with increasing Mach number (M._ = 0.60, 0.80, 0.85, to 0.90).

For M** = 0.85, the flattop supercritical pressure profile has developed. The lower surface Cp distributions show

small changes with increasing Mach number. Figure 11 (b) compares the Cp distribution for small changes in Mach

number. This comparison illustrates the sensitivity of the Cp distributions to Mach number near the wing design

cruise Mach number of 0.85. The flight data for the wing design cruise condition of Moo = 0.85, cxT = 5.6 ° and an

altitude of 35,000 ft (q._ -- 250 lb/ft 2) are found in Appendix J. The four sets of data shown in figure 1 l(b) are all from

the same flight test maneuver, during which the target Mach number was 0.85. The actual flight Mach numbers were

M., = 0.844, 0.852, 0.855 to 0.861. The critical pressure coefficient for M** = 0.85 is also shown. This excellent

agreement in the pressure distributions forward of x/c = 0.5 indicates that the respective angles of attack have been

matched to identical values. This fact means that the shock movement in the upper surface C distributions, rearward

with each small increase in M, is caused by the small variation in Mach number (retd. 28). As expected, the

separation between the shock locations is relatively proportional to the difference between the M.o values. This

sensitivity can be shown for differences in M as small as 0.003 for this maneuver.

Camber and Angle-of-Attack Effects

Figure 12 (ref. 27) shows the boundary-layer velocity profiles near the trailing edge and their associated pressure

distributions for rl = 0.76. The critical pressure coefficient is also shown with the pressure distribution data. These
dataareforfourcambersatMoo = 0.80 and angles of attack between 6° and 12°. The velocity profiles for Ot T = 6°

and _)LE/TE = 0/2, 5/2, and 10/2 are in good agreement (fig. 12(a)). The profile for _LE/TE= 0/2 shows larger losses;

thus, the momentum thickness and associated momentum loss are larger. The pressure distributions in figure 12(b),

except for _SLF_/TE-- 5/6, exhibit characteristics similar to the profiles discussed in figures 9-11. The pressure

distributions for _LE/TE = 5/6 and 10/2 show the most aft shock location. The pressure distribution for _LF/TE = 5/6

has a secondary velocity peak near x/c -_-0.65. All the cambers show good trailing-edge recovery.

Figures 12(c) and 12(d) show the data for O_T = 8°. The velocity profile for _)LE/TE = 0/2 is similar to the a T = 6°

profile in figure 12(a). The remaining profiles show larger losses than for O_T= 6°. The velocity profile for _LF_/TE =

5/6 indicates that flow separation is imminent. In figure 12(c), the pressure plateaus for all the distributions are more

fully developed then for the O.T = 6 ° case, and the aft shocks have moved rearward. The two trailing-edge cambers,

_)TE= 2° and 6 °, illustrate the effect on the movement of the aft normal shock with trailing-edge deflection. For all

four cambers, however, the trailing-edge pressure recovery indicates no separation (fig. 12(d)).

Figures 12(e) and 12(f) present only Cp data for _T = 100 and 12° because the velocity profiles showed that

separated flow existed near the trailing edge for all cambers. The pressure plateaus begin to weaken for the O_T= 10°

data (fig. 12(e)) and lose their well-defined shape for the O_T = 12° data (fig. 12(f)). The pressure distributions also

indicate that separated flow exists at the trailing edge. For t_T= 12°, the slope in the Cp data indicates that separated

flow could exist from x/c = 0.7 to the trailing edge (fig. 12(f)).

Camber and Angle-of-Attack Effects

on Normal Force Coefficient

Figure 13 (ref. 27) shows sample section normal-force coefficients, cn, at a Mach number of 0.80 for a range of

angle of attack at rl = 0.76 and for several _)LE/TEvalues. Figure 13(a) compares the cn characteristics for the three

leading-edge surface deflections of 8LE/T E = 0/2, 5/2, and 10/2. Curves for the data at _)LE/TE = 0/2 and _LE/TE =

5/2 are almost identical for the higher angles of attack. The _)LFJTE = 10/2 c n levels for aT > 8° are slightly lower

than for _SLF_/TE= 0/2 and _)LE/TE = 5/2. For C_T= 10°, the cn for _LE/FE = 10/2 is approximately 7 percent lower.

In general, the data for these conditions show that, with increasing angle of attack, lift decreases as the leading-edge

camber deflects to 10°.

Figure 13(b) compares the cn characteristics for the trailing-edge surface deflections of _)LE/TE -- 1O/10, 10/18,

and 5/15. The cn characteristics for cambers of 5LF_/TE= 0/2 and 10/2 are shown as reference values for comparison

with figure 13(a). (Note the change in cn scale between figure 13(a) and 13(b).) As expected for a given angle of

attack, cn increases with increasing trailing-edge surface deflection. The camber _LE, TE -- 5/15 data (dashed line)

provide some data for medium and large trailing-edge deflections (ref. 29). Figures 13(a) and 13(b) indicate the

benefits of judiciously selecting leading- and trailing-edge camber deflections. The variation in total aircraft drag

caused by the change in camber is discussed in references 30 and 31.

Wing-Tip Twist Effects

The incremental change in wing-tip twist caused by load (wing-tip delta twist) was calculated as the difference

between the changes in deflections of the forward and aft wing-tip targets. This wing-tip delta twist is the

incremental twist caused by load, not the total twist. Figure 14(a) (ref. 12) shows the wing-tip delta twist, in degrees,

as a function of free-stream dynamic pressure for three camber settings at a Mach number of 0.85. The trailing-edge

uptwist is negative. The close agreement between the data for _)LE/TE = 0/2 and _LE/TE = 10/2 shows that the effect

of leading-edge camber on wing twist is insignificant compared to the effect of trailing-edge camber. The

9
FLEXSTABpredictionsreportedbyNelsoninreference32showthesametrend.Onlyonedata point was available

for _LE/FE = 5/10, qoo = 600 ib/ft 2. The vertical spread in the groups of measured wing-tip twists is caused by the

variation in aircraft angle of attack. For a given dynamic pressure and Mach number, an increase in angle of attack

causes a corresponding increase in load factor, which in turn directly affects the wing-tip delta twist. Thus, an

increase in aircraft angle of attack causes more negative wing-tip twist, which is also referred to as washout. The

resulting local angle of attack that the wing-tip experiences is therefore less than the aircraft angle of attack for a

positive normal acceleration maneuver.

Figures 14(b) and 14(c) compares wing surface-pressure profiles at two span locations (1"1= 0.93 and 0.76) at M,,,

= 0.85, O_T= 8 °, _LF_/TE = 0/2, and q** ---300 and 600 lb/ft 2. The wing-tip delta twist is only 0.5 ° for _LE/FE = 0/2,

a fact that suggests that large effects would not be anticipated for the two dynamic pressures investigated. In figure

17, the wing-twist effects, if any, are minimal at the inboard row location, and the outboard row shows only a small

difference in the twist at the wing-tip for the two dynamic pressures.

CONCLUDING REMARKS

This report presented selected results from the wing-surface and boundary-layer pressures and the FDMS for the

AFFI/F- 111 MAW aircraft flight program, primarily for conditions near the wing design Mach number. The pressure

data represent a very small portion of the data available from the MAW program. Extensive tables listing wingpressure and boundary-layer data are included in this report for cruise, maneuvering, and landing wing cambers;

from Mach 0.27 to Mach 1.41; angles of attack from 2° to 13°; and dynamic pressures from 80 to 800 lb/ft 2.

Leading-edge cambers ranged from 0 ° to 20 ° down and trailing-edge cambers ranged from 1° up to 19° down. The

wing-pressure orifices were aligned with the free-stream flow for a wing sweep of 26 °. Wing-pressure data were also

obtained at wing sweeps of 9°, 16°, 45 °, and 56 °. For these wing sweeps, the wing-pressure orifices were not aligned

with the free-stream flow. The data provide a large research base for further analysis on smooth variable-camber

airfoils. Measured wing coordinates are also given for three streamwise semispan locations for the cruise camber and

one spanwise location for a maneuver camber. Results indicate

The pressure profiles had a distribution typical of a supercritical airfoil for the _LF_./TE = 0/2 and 8LE//'E =

5/ I0 cambers investigated in this paper. The midspan pressure profiles for both cambers illustrate the

nearly constant upper surface-pressure coefficient plateaus expected for supercritical wings. The wing-tip

twist measurements provide insight into how dynamic pressures for positive normal accelerations affect

the wing-tip pressure profiles.

The movement of the shock location on the upper surface of the wing chord is shown for large and small

changes in Mach number. These shock locations are very sensitive to small changes in Mach number near

a free-stream Mach number of 0.85.

The section normal-force coefficients for Mach 0.80 show that as angle of attack increases, an increase in

the leading-edge deflection produces a slight decrease in lift, but an increase in the trailing-edge flap

deflection results in an increase in lift.

The boundary-layer velocity profile data revealed that the flow near the trailing edge for a Mach 0.80 and

dynamic pressure of 300 lb/ft 2 separated for 10 ° and higher angles of attack. The wing-pressure data

supported these results.

Dryden Flight Research Center

National Aeronautics and Space Administration

Edwards, California, April 29, 1996

10
EC8533205-017

Figure1.AFTUF-111MAWairplanein flight.Chordwisedarkareasontherightwingindicatethefoursemispan

locationsof pressureorifices(refs.11,12,and27).

Flex panel V Wing box ..

\ rel'elrOllCO line

_-- Fixed.geometry TE

ieedlng edge

_29

Figure 2. The MAW smooth, variable-camber flap shape (refs. 11, 12, and 27).

11
E89 0208-004

Figure 3. Wing-splash template preparation on the AFrFF-I 11 MAW airplane (ref. 16).

Fuselal e/',_,,._ 26 °

glove /_ _ leading-edge

,,rcr., iJ.._i _ ! "_

centerllne _ : I""'_P',._ I I

I , :o,0-----...LI I 'q= o.s9

_ I I _ = o.7s

960330

Figure 4. Wing planform and airfoil shapes at design cruise condition (ref. 11 and 16).

12
S Aircraft

centerline

• Accelerometer locations "_"" ""- ... • Boundary-layer rake location

""_"r_ / 6° --_-- Trt:_i:du_fT::/:clatc:ti:ns

_,-; _ /-- Leading-edge

Reference I _'_ "

transducer-/ ! _ =T"-,,_

flaps 1] = 0.40 TI = 0.___

TI-0,76 1]=0.93

Number of J J I

pressure 16 31 40 15 Upper surface

orifices 12 14 14 10 Lower surface 960331

Figure 5. Semispan locations of surface-pressure orifices, boundary-layer rake, pressure instrumentation, and

wingtip accelerometers for the right wing (ref. 12).

f

Silver // _ />\

solder-_ /745 o \

"--.. -5.;-"

_/Stainless ste_ubing

0.03 in. outside diameter

/

/

/

/

/

/

/

/

/

/

Rake probe /

heights "'( \

\

\

\

\

\

\

\,

Y

4.96

4.47*

3.99

3.49

2.99

2,33

1.96

1,47

0.97

0.47

0.24

0.03*

!

--_ 1in. ._--

j' '

|

|

i

|

5 in.

i i

i |

i i

| |

| i

f ,

*Probes not functional

Figure 6. Boundary-layer rake (refs. 12 and 27).

0.16 in.

+

I I

/ I

960332

13
y Receiver

960333

Figure 7. FDMS target locations on the lower surface of the left wing (ref. 12).

IlnWT,

g

qo_p

Ib/ft 2

Moo

I f J I I

I I I I I I

.85

.84 r I I I

P, 62O L_-.

at 520

TI = 0.76

_°=o. ,20 I J J I i f I I I

0 10 20 30 40 50 60 70 80 90

Time, sec

960334

Figure 8. Time history of typical windup turn maneuver used to obtain wing pressure, FDMS, and boundary-layer

data; M._ ---0.85, q._ ---300 Ib/ft 2, and _SLF_E= 0/2 (ref. 12).

14
(XT=8 °

GT=10 °

/I

©

11 = 0.93

11 = 0.76

of separation

for (xT = 10 °

Cp

! /

I1 : 0.59

-.4

m.2

I l I n =0.40

0 .2 .4 .6 .8 1.0

/

Figure 9. Steady chordwise pressure distributions at four semispan stations for M

and _LE/rE = 0/2. No separation at C_T= 8° fief. 12).

960335

= 0.85, q,_ --- 300 lb/ft 2,

15
= 0.76

of separation

for OCT= 8° and 10 °

11 = 0.59

/

-.4 /

-.2 /

I I

O' .2 .4 .6 .8 1.0

/

Figure 10. Steady chordwise pressure distributions at four semispan stations for M

and 8LF_./r£= 5/10 (ref. 12).

11 = 0.40

960336

--- 0.85, q_ = 300 Ib/ft 2,

16
-2

-1

Cp 0

1 --

2

_°2

Flight

data

0

[]

Zl

I I I

Cpu.s.

CpL.S.

I

= open symbols

= solid symbols

I I

0 .2 .4 .6 .8

x/c

(a) Large Mach number range.

1.0

960337

Mo_ = 0.608

Moo = 0.797

M_ = 0.852

Moo = 0.901

-2 u

Cp 0

2

- .2 0 .2

I I t I

.4 .6

x/c

960338

(b) Small Mach number range.

Figure 11. Steady chordwise pressure distributions for large and small ranges of Mach number; 1"1= 0.76,

q=, = 300 lb/ft 2, and OtT = 8° (ref. 11).

17
Yl

In.

5LE/TE

C) 012

[] 512

10/2

Z_ 5/6

o I I I

.6 .7 .8 .9 1.0 1.1

U_ e

960339

(a) Velocity profiles, a T = 6°.

-2

I 8LEITE

C) 012

[] 512

1012

516

------ Cp*

Cp

0

1 I t f I I

o .2 ., ., ., 1.o

xJc

960353

(b) Chordwise pressure distributions, a T = 6 °.

Figure 12. Chordwise pressure distributions and velocity profiles for different cambers (M = 0.80, 1"1- 0.76, and

q_ = 300 lb/ft 2) (ref. 27).

18
Yl

in.

5 m

4 --

3 --

2 --

1 --

o I I I I

.6 .7 .8 .9 1.0 1.1

U_ e

960340

(c) Velocity profiles, O_T = 8 °.

8LE/TE

0 012

[] 512

<> lol2

516

-2

8LEITE

© 0/2

[] 512

_ 10/2

516

Cp

'------

1 I I l

0 .2 .4 .6 .8 1.0

x/c

960354

(d) Chordwise pressure distributions, O_T = 8°.

Figure 12. Continued.

19
Cp

-2

-1

_LEITE

© O/2

D 5/2

_ 10/2 5/6

Cp*

0

,I

1

0

I I I I I

.2 .4 .6 .8 1.0

x/c

(e) Chordwise pressure distributions, ot T = 10 °.

960341

Cp

-2

-1

1

0

(SLE/TE

012

512

1012

516

Cp*

I I I I I

.2 .4 .6 .8 1.0

x/c

960342

(f) Chordwise pressure distributions, ct T = 12 °.

Figure 12. Concluded.

20
.8

.7

.6

Cn .5 --

,4 --

• 3 --

.2

4

©

/

I L I I I I I I

5 6 7 8 9 10 11 12

a, deg

(a) Effects of leading-edge camber deflections.

13

960343

5LE/TE

© 0/2

[] 1012

0 512

1.2 --

Cn .6

1.0 --

• 8 --

o4 --

• 2 --

0

2

i,/'S

8LE/TE

C) 0/2

[] 1012

0 10110

A 10118

511 5

I I t I I I t I I I I

3 4 5 6 7 8 9 10 11 12 13

0_, deg 960344

(b) Effects of trailing-edge camber deflections.

Figure 13. Section normal-force coefficient as a function of ctT for different camber deflections at M = 0.80,

rl = 0.76, and q_ = 300 Ib/ft 2 (ref. 27).

21
0 --

Wlngtip

delta

twist,

deg

Trailing I edge

up

-1

-2

3

-4 --

-5

2OO

O_T,

deg

-- 4.3_. 3.5 ----_ __ _ 5.143.5

4.0_ 6.0 J L_ "_-., _" __ 4, 4.2

"_. 6

0

[]

8LE/I"E,

deg

O/2

10/2

5/10

t

3O0

_'A

_3.1

I I I I

4OO 5OO 6OO 7OO

q_,lb/ft 2

96O345

(a) FDMS wing-tip delta twist as a function of dynamic pressure for three cambers.

-.4

Cp - .2

.2

!t

0

I I I I I I I t I I

.1 .2 .3 .4 .5 .6 .7 .8 .9 1.0

x/c

960346

(b) _LF_/TE= 0/2, T1 = 0.93, (XT = 8°.

Figure 14. Comparison of FDMS measured wingtip delta twist with two pressure profiles for M.o = 0.85 and

q.o -- 300 and 600 lb/ft 2 (ref. 12).

22
- 1.2 r _ q_ = 300 Ib/ft 2

Cp - .2

"8 I L I I I I I I I 1

• 0L) .1 .2 .3 .4 .5 .6 .7 .8 .9 1.0

x/c

960347

(c) _LFJTE = 0/2, 11= 0.76, a T = 8 °.

Figure 14. Concluded.

23
APPENDIX A

Maw Airfoil Coordinates for a Wing Sweep of 26 °

at Span Stations 0.93, 0.76, 0.59, and 0.40.

Table A-1. Full-scale wing-splash coordinates (_LE/TE = 0/2,

rl = 0.93, c = 9.2276 ft).

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.0000E-00 0.2646E-03 0.0000E-00 0.9031E-05

0.3432E-04 0.7487E-03 0.6322E-04 -0.7884E-03

0.2953E-03 0.1616E-02 0.2068E-03 -0.1342E-02

0.5473E-03 0.2110E-02 0.3648E-03 -0.1739E-02

0.8281E-03 0.2539E-02 0.7071E-03 -0.2366E-02

0.1598E-02 0.3425E-02 0.1086E-02 -0.2905E-02

0.2593E-02 0.4228E-02 0.1852E-02 -0.3663E-02

0.3248E-02 0.4675E-02 0.2521E-02 -0.4104E-02

0.4258E-02 0.5299E-02 0.3759E-02 -0.4773E-02

0.5294E-02 0.5879E-02 0.5408E-02 -0.5518E-02

0.6246E-02 0.6359E-02 0.7115E-02 -0.6171E-02

0.7485E-02 0.6922E-02 0.8438E-02 -0.6606E-02

0.9648E-02 0.7787E-02 0.1090E-01 -0.7293E-02

0.1159E-01 0.8479E-02 0.1353E-01 -0.7888E-02

0.1408E-01 0.9148E-02 0.1643E-01 -0.8447E-02

0.1660E-01 0.9823E-02 0.1913E-01 -0.8879E-02

0.1954E-01 0.1051E-01 0.2138E-01 -0.9178E-02

0.2250E-01 0.1124E-01 0.2331E-01 -0.9407E-02

0.2579E-01 0.1189E-01 0.2624E-01 -0.9678E-02

0.2950E-01 0.1254E-01 0.2870E-01 -0.9870E-02

0.3251E-01 0.1298E-01 0.3182E-01 -O.IO06E-01

0.3557E-01 0.1345E-01 0.3617E-01 -0.1039E-01

0.3893E-01 0.1395E-01 0.3907E-01 -0.1078E-01

0.4193E-01 0.1436E-01 0.4221E-01 -0.1117E-O1

0.4533E-01 0.1481E-01 0.4533E-01 -0.1167E-01

0.4746E-01 0.1508E-01 0.4877E-01 -0.1207E-01

0.5177E-01 0.1561E-01 0.5206E-01 -0.1243E-01

0.5710E-01 0.1624E-01 0.5568E-01 -0.1287E-01

0.6326E-01 0.1692E-01 0.5913E-01 -0.1321E-01

0.6905E-01 0.1752E-01 0.6235E-01 -0.1350E-01

0.7523E-01 0.1814E-01 0.6476E-01 -0.1377E-01

24
TableA-1.Continued.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.8118E-01 0.1870E-01 0.6769E-01 -0.1410E-01

0.8598E-01 0.1915E-01 0.7106E-01 -0.1444E-01

0.9238E-01 0.1972E-01 0.7481E-01 -0.1481E-01

0.9986E-01 0.2036E-01 0.7855E-01 -0.1516E-01

0.1090E+00 0.2109E-01 0.8491E-01 -0.1570E-01

0.1204E+00 0.2195E-01 0.8808E-01 -0.1596E-01

0.1295E+00 0.2265E-01 0.9129E-01 -0.1621E-01

0.1417E+00 0.2347E-01 0.9583E-01 -0.1655E-01

0.1527E+00 0.2412E-01 0.9919E-01 -0.1676E-01

0.1619E+00 0.2464E-01 0.1034E+00 -0.1701E-01

0.1707E+00 0.2511E-01 0.1074E+00 -0.1723E-01

0.1815E+00 0.2562E-01 0.1114E+00 -0.1743E-01

0.1912E+00 0.2606E-01 0.1159E+00 -0.1765E-01

0.2023E+00 0.2657E-01 0.1205E+00 -0.1785E-01

0.2151E+00 0.2714E-01 0.1237E+00 -0.1798E-01

0.2268E+00 0.2767E-01 0.1277E+00 -0.1812E-O 1

0.2379E+00 0.2813E-01 0.1306E+00 -0.1822E-01

0.2505 E+00 0.2843E-01 0.1356E+00 -0.1837E-01

0.2620E+00 0.2879E-01 0.1395E+00 -0.1849E-01

0.2737E+00 0.2919E-O 1 0.1436E+00 -0.1860E-01

0.2877E+00 0.2959E-01 O.1482E+00 -0.1870E-01

0.3012E+00 0.2990E-01 0.1525E+00 -0.1877E-01

0.3167E+00 0.3025E-01 O. 1562E+00 -0.1880E-01

0.3265E+00 0.3047E-01 0.1604E+00 -0.1885E-01

0.3370E+00 0.3069E-01 0.1651E+00 -0.1895E-01

0.3494E+00 0.3093E-01 0.1706E+00 -0.1906E-01

0.3620E+00 0.3113E-01 0.1792E+00 -0.1924E-01

0.3745E+00 0.3134E-01 0.1874E+00 -0.1942E-01

0.3887E+00 0.3156E-01 0.1969E+00 -0.1968E-01

0.4016E+00 0.3171E-01 0.2044E+00 -0.1981E-01

0.4165E+00 0.3186E-01 0.2143E+00 -0.1988E-01

0.4282E+00 0.3199E-01 0.2237E+00 -0.1996E-01

0.4385E+00 0.3208E-01 0.2331E+00 -0.2005E-01

0.4479E+00 0.3217E-01 0.2437E+00 -0.2007E-01

0.4607E+00 0.3225E-01 0.2553E+00 -0.2009E-01

0.4732E+00 0.3233E-01 0.2631E+00 -0.2007E-01

25
TableA-I. Continued.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.4859E+00 0.3239E-01 0.2715E+00 -0.2008E-01

0.4916E+00 0.3242E-01 0.2800E+00 -0.2010E-01

0.5105E+00 0.3246E-01 0.2912E+00 -0.2012E-01

0.5218E+00 0.3248E-01 0.3038E+00 -0.2015E-01

0.5315E+00 0.3251E-01 0.3168E+00 -0.2017E-01

0.5399E+00 0.3256E-01 0.3299E+00 -0.2019E-01

0.5533E+00 0.3263E-01 0.3396E+00 -0.2021E-01

0.5686E+00 0.3273E-01 0.3535E+00 -0.2018E-01

0.5857E+00 0.3281E-01 0.3642E+00 -0.2017E-01

0.5993E+00 0.3276E-01 0.3754E+00 -0.2018E-01

0.6178E+00 0.3271E-01 0.3878E+00 -0.2017E-01

0.6310E+00 0.3265E-01 0.3993E+00 -0.2016E-01

0.6337E+O0 0.3263E-01 0.4107E+00 -0.2016E-01

0.6401E+00 0.3259E-01 0.4215E+00 -0.2015E-01

0.6490E+00 0.3249E-01 0.4272E+00 -0.2015E-01

0.6559E+00 0.3236E-01 0.4396E+00 -0.2014E-01

0.6659E+00 0.3212E-01 0.4545E+00 -0.2013E-01

0.6768E+00 0.3183E-01 0.4666E+00 -0.2010E-01

0.6884E+00 0.3152E-01 0.4793E+00 -0.2003E-01

0.7012E+00 0.3121E-01 0.4866E+00 -0.1998E-01

0.7140E+00 0.3084E-01 0.4918E+00 -0.1994E-01

0.7227E+00 0.3056E-01 0.5099E+00 -0.1974E-01

0.7350E+00 0.3013E-01 0.5220E+00 -0.1957E-01

0.7487E+00 0.2958E-01 0.5352E+00 -0.1935E-01

0.7574E+00 0.2920E-01 0.5489E+00 -0.191 IE-01

0.7673E+00 0.2873E-01 0.5673E+00 -0.1877E-01

0.7759E+00 0.2828E-01 0.5859E+00 -0.1834E-01

0.7838E+00 0.2783E-01 0.6018E+00 -0.1793E-01

0.7908E+00 0.2743E-01 0.6160E+O0 -0.1759E-01

0.7968E+00 0.2707E-01 0.6279E+00 -0.1721E-01

0.8014E+00 0.2676E-01 0.6334E+00 -0.1706E-01

0.8090E+00 0.2628E-01 0.6485E+00 -0.1670E-01

0.8178E+00 0.2567E-01 0.6603E+00 -0.1613E-01

0.8247E+00 0.2517E-01 0.6730E+00 -0.1537E-01

0.8309E+00 0.2470E-01 0.6881E+00 -0.1466E-01

0.8364E+00 0.2427E-01 0.7003E+00 -0.1363E-01

26
TableA-1.Continued.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.8414E+00 0.2386E-01 0.7127E+00 -0.1282E-01

0.8464E+00 0.2343E-01 0.7231E+O0 -0.1219E-01

0.8521E+00 0.2293E-01 0.7354E+00 -0.1134E-01

0.8576E+00 0.2242E-01 0.7485E+00 -0.1051E-01

0.8628E+00 0.2191E-01 0.7596E+00 -0.9766E-02

0.8686E+00 0.2133E-01 0.7703E+00 -0.9128E-02

0.8741E+00 0.2071E-01 0.7789E+00 -0.8438E-02

0.8800E+00 0.2008E-01 0.7890E+00 -0.7682E-02

0.8864E+00 0.1933E-01 0.8009E+00 -0.6807E-02

0.8924E+00 0.1860E-01 0.8 I06E+O0 -0.6114E-02

0.8986E+00 0.1780E-01 0.8217E+00 -0.5299E-02

0.9030E+00 0.1721E-01 0.8335E+00 -0.4442E-02

0.9084E+00 0.1649E-01 0.8404E+00 -0.4024E-02

0.9134E+00 0.1579E-01 0.8451E+00 -0.3781E-02

0.9184E+00 0.1510E-01 0.8487E+00 -0.3499E-02

0.9246E+00 0.1419E-01 0.8544E+00 -0.2679E-02

0.9301E+00 0.1334E-01 0.8595E+00 -0.2248E-02

0.9348E+00 0.1262E-01 0.8659E+00 -0.2038E-02

0.9408E+00 0.1168E-01 0.8734E+00 -0.1916E-02

0.9450E+00 0.1103E-01 0.8808E+00 -0.1843E-02

0.9490E+00 0.1040E-01 0.8867E+00 -0. i 822E-02

0.9535E+00 0.9675E-02 0.8936E+00 -0.1868E-02

0.9574E+00 0.9051E-02 0.8986E+00 -0.2000E-02

0.9613E+00 0.8411E-02 0.9034E+00 -0.1785E-02

0.9664E+00 0.7586E-02 0.9108E+00 -0.1702E-02

0.9714E+00 0.6739E-02 0.9182E+00 -0.1518E-02

0.9753E+00 0.6108E-02 0.9235E+00 -0.1426E-02

0.9790E+00 0.5493E-02 0.9300E+00 -0.1335E-02

0.9821E+00 0.4987E-02 0.9361E+00 -0.1275E-02

0.9852E+00 0.4487E-02 0.9414E+00 -0.1259E-02

0.9894E+00 0.3810E-02 0.9471E+O0 -0.1284E-02

0.9921E+00 0.3395E-02 0.9535E+00 -0.1373E-02

0.9948E+00 0.2998E-02 0.9586E+00 -0.1421E-02

0.9961E+00 0.2821E-02 0.9637E+00 -0.1524E-02

0.9975 E+00 0.2610E-02 0.9674E+00 -0.1625E-02

0.1000E+01 0.1227E-02 0.9718E+O0 -0.1748E-02

27
TableA-1.Concluded.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.9759E+00 -0.1888E-02

0.9808E+00 -0.2078E-02

0.9855E+00 -0.2270E-02

0.9896E+00 -0.2444E-02

0.9922E+00 -0.2604E-02

0.9942E+00 -0.2689E-02

0.9961E+00 -0.2803E-02

0.9974E+00 -0.2846E-02

0.9992E+00 -0.1514E-02

0.9995E+00 -0.3630E-03

0.9997E+00 0.2763E-03

0.1000E+O1 0.1 lOOE-02

28
TableA-2.Full-scalewing-splashcoordinates (_LE/TE = O/2,

1"1= 0.76, c = 9.9413 ft).

U.S. U.S. L.S. L.S.

x/c #c x/c z/c

0.O000E+O0 0.0000E+O0 0.0000E+O0 O.O000E+00

0.2019E-02 0.2853E-02 0.2019E-02 -0.2977E-02

0.4039E-02 0.5361E-02 0.4039E-02 -0.5368E-02

0.6071E-02 0.6884E-02 0.6058E-02 -0.6643E-02

0.8078E-02 0.8065E-02 0.8092E-02 -0.7512E-02

0.1012E-01 0.9086E-02 0.1010E-01 -0.8187E-02

0.1515E-01 0.1108E-01 0.1515E-01 -0.9588E-02

0.2021E-01 0.1264E-01 0.2018E-01 -0.1068E-01

0.3031E-01 0.1501E-01 0.3035E-01 -0.1223E-01

0.4041E-01 0.1696E-01 0.4041E-01 -0.1290E-01

0.6062E-01 0.2007E-01 0.6062E-01 -0.1495E-01

0.8083E-01 0.2238E-01 0.8082E-01 -0.1679E-01

0.1010E+00 0.2432E-01 0.1010E+O0 -0.1849E-01

0.1212E+00 0.2600E-01 0.1212E+00 -0.2012E-01

0.1414E+00 0.2752E-01 0.1414E+00 -0.2159E-01

0.1616E+00 0.2891E-01 0.1616E+00 -0.2285E-01

0.1818E+00 0.3015E-01 0.1818E+00 -0.2392E-01

0.2020E+00 0.3128E-01 0.2020E+00 -0.2456E-01

0.2222E+00 0.3223E-01 0.2222E+00 -0.2520E-01

0.2424E+00 0.3287E-01 0.2424E+00 -0.2584E-01

0.2626E+00 0.3348E-01 0.2626E+00 -0.2641E-01

0.2829E+00 0.3402E-01 0.2828E+00 -0.267 IE-O1

0.3031E+00 0.3447E-01 0.3030E+00 -0.2697E-01

0.3232E+00 0.3484E-01 0.3232E+00 -0.2718E-01

0.3434E+00 0.3513E-01 0.3434E+00 -0.2715E-O 1

0.3636E+00 0.3532E-01 0.3636E+00 -0.2707E-01

0.3839E+00 0.3552E-01 0.3839E+00 -0.2701E-01

0.4041E+00 0.3569E-01 0.4040E+00 -0.2693E-01

0.4242E+00 0.3582E-01 0.4242E+00 -0.2675E-01

0.4444E+00 0.3588E-01 0.4444E+00 -0.2651E-01

0.4646E+00 0.3594E-01 0.4646E+00 -0.2624E-01

0.4849E+00 0.3594E-01 0.4849E+00 -0.2586E-01

0.5253E+00 0.3491E-01 0.5253E+00 -0.2450E-01

0.5446E+00 0.3485E-01 0.5455E+00 -0.2370E-01

0.5455E+00 0.3485E-01 0.5656E+00 -0.2288E-01

29
TableA-2.Concluded.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.5657E+00 0.3474E-01 0.5859E+00 -0.2187E-01

0.6061E+00 0.3444E-01 0.6061E+00 -0.2063E-01

0.6263E+00 0.3416E-01 0.6263E+00 -0.1907E-01

0.6465E+00 0.3397E-01 0.6465E+00 -0.1708E-01

0.6667E+00 0.3370E-01 0.6667E+00 -0.1504E-01

0.6877E+00 0.3298E-01 0.6877E+00 -0.1284E-01

0.7071E+00 0.3223E-01 0.7071E+00 -0.1072E-01

0.7273E+00 0.3145E-01 0.7273E+00 -0.8346E-02

0.7475E+00 0.3054E-01 0.7475E+00 -0.6090E-02

0.7677E+00 0.2947E-01 0.7677E+00 -0.4011E-02

0.7879E+00 0.2820E-01 0.7879E+00 -0.2174E-02

0.8081E+00 0.2671E-01 0.8081E+00 -0.6614E-03

0.8283E+00 0.2510E-01 0.8283E+00 0.5901E-03

0.8485E+00 0.2337E-01 0.8485E+00 0.1547E-02

0.8687E+00 0.2141E-01 0.8687E+00 0.2518E-02

0.8889E+00 O. 1918E-01 0.8889E+00 0.2568E-02

0.9091E+00 0.1662E-01 0.9091E+00 0.2623E-02

0.9192E+00 0.1524E-01 0.9192E+00 0.1733E-02

0.9293E+00 0.1389E-01 0.9293E+00 0.1387E-02

0.9394E+00 0.1242E-01 0.9394E+00 0.1100E-02

0.9495E+00 0.1083E-01 0.9495E+00 0.8022E-03

0.9596E+00 0.9002E-02 0.9596E+00 0.2892E-03

0.9697E+00 0.7450E-02 0.9697E+00 -0.3160E-03

0.9798E+00 0.5842E-02 0.9798E+00 -0.9087E-03

0.9899E+00 0.4231E-02 0.9899E+00 -0.1443E-02

0.1000E+01 0.2643E-02 0.1000E+01 -0.1974E-02

3O
TableA-3.Full-scalewing-splashcoordinates (_)LE/TE = 0/2,

1] = 0.59, c = 10.8549 ft).

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.0000E+00 0.6326E-03 0.0000E-O0 0.4606E-05

0.1919E-04 0.8736E-03 0.1459E-04 -0.5765E-03

0.9136E-04 0.1513E-02 0.6372E-04 -0.1217E-02

0.1750E-03 0.2027E-02 0.1382E-03 -0.1821E-02

0.2948E-03 0.2566E-02 0.2656E-03 -0.2521E-02

0.5405E-03 0.3341E-02 0.4468E-03 -0.3174E-02

0.8759E-03 0.4163E-02 0.7071E-03 -0.3841E-02

0.1330E-02 0.4984E-02 0.9397E-03 -0.4324E-02

0.1692E-02 0.5553E-02 0.1375E-02 -0.5073E-02

0.2208E-02 0.6254E-02 O.1730E-02 -0.5605E-02

0.3359E-02 0.7494E-02 0.2554E-02 -0.6666E-02

0.3878E-02 0.7942E-02 0.2831E-02 -0.6952E-02

0.4324E-02 0.8301E-02 0.3232E-02 -0.7325E-02

0.5 i 60E-02 0.8940E-02 0.3593E-02 -0.7603E-02

0.5850E-02 0.9423E-02 0.4028E-02 -0.7875E-02

0.6926E-02 0.1016E-01 0.4645E-02 -0.8339E-02

0.7881E-02 0.1076E-01 0.5741E-02 -0.9067E-02

0.8618E-02 0.1119E-01 0.6639E-02 -0.9609E-02

0.9441E-02 0.1161E-01 0.7690E-02 -0.1016E-01

0.1051E-OI 0.1212E-01 0.8935E-02 °0.1074E-01

0.1148E-01 0.1256E-01 0.1025E-01 -0.1131E-01

0.1258E-01 0.1304E-01 0.1168E-01 -0.1 !85E-01

0.1379E-01 0.1356E-01 0.1307E-01 -0.1231E-01

0.1511E-01 0.1406E-01 0.1461E-01 -0.1277E-01

0.1665E-01 0.1460E-01 0.1695E-01 -0.1342E-01

0.1843E-01 0.1521E-01 0.1930E-01 -0.1399E-01

0.2053E-01 0.1589E-01 0.2192E-01 -0.1453E-01

0.2212E-01 0.1637E-01 0.2565E-01 °0.1519E-01

0.2394E-01 0.1691E-01 0.2888E-01 -0.1530E-01

0.2641E-01 0.1759E-01 0.3218E-01 -0.1574E-01

0.2834E-01 0.1811E-01 0.3604E-01 -0.1622E-01

0.3036E-01 0.1862E-01 0.4030E-01 -0.1691E-01

0.3295E-01 0.1924E-01 0.4350E-01 -0.1742E-01

0.3570E-01 0.1985E-01 0.4890E-01 -0.1813E-01

0.3839E-01 0.2042E-01 0.5347E-01 -0.1870E-01

0.4128E-01 0.2099E-01 0.5907E-01 -0.1941E-01

0.4389E-01 0.2147E-01 0.6754E-01 -0.2051E-01

0.4728E-01 0.2205E-01 0.7552E-01 -0.2153E-01

31
TableA-3.Continued.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.5185E-01 0.2279E-01 0.8327E-01 -0.2245E-01

0.5555E-01 0.2335E-01 0.8996E-01 -0.2315E-01

0.5920E-01 0.2386E-01 0.9900E-01 -0.2403E-01

0.6309E-01 0.2439E-01 O.1074E+00 -0.2492E-01

0.6683E-01 0.2487E-01 0.1144E+00 -0.2570E-01

0.7191E-01 0.2549E-01 0.1209E+00 -0.2638E-01

0.7621E-01 0.2598E-01 0.1287E+00 -0.2717E-01

0.8102E-01 0.2654E-01 0.1375E+00 -0.2805E-01

0.8468E-01 0.2694E-01 0.1469E+00 -0.2871E-01

0.8853E-01 0.2735E-01 0.1563E+00 -0.2926E-01

0.9224E-01 0.2774E-01 0.1631E+00 -0.2957E-01

0.9628E-01 0.2816E-01 0.1719E+00 -0.2980E-01

0.1042E+00 0.2897E-01 0.1797E+00 -0.2980E-01

O. 1087E+00 0.2941E-01 0.1895E+00 -0.3039E-01

0.1154E+00 0.3005E-01 0.1987E+00 -0.3085E-01

0.1213E+00 0.3062E-01 0.2084E+00 -0.3135E-01

0.1284E+00 0.3130E-01 0.2190E+00 -0.3179E-01

O. 1364E+00 0.3207E-01 0.2285E+00 -0.3210E-01

0.1444E+00 0.3275E-01 0.2406E+00 -0.3250E-01

0.1521E+O0 0.3336E-01 0.2510E+O0 -0.3282E-01

0.1603E+00 0.3402E-01 0.2602E+00 -0.3301E-01

O. 1690E+00 0.3468E-01 0.2643E+00 -0.3309E-01

0.1780E+00 0.3531E-01 0.2721E+00 -0.3322E-01

O. 1880E+00 0.3594E-01 0.2797E+00 -0.3335E-01

0.1983E+00 0.3659E-01 0.2901E+00 -0.3352E-01

0.2080E+00 0.3706E-01 0.3022E+00 -0.3369E-01

0.2193E+00 0.3760E-01 0.3116E+00 -0.3382E-01

0.2282E+00 0.3803E-01 0.3211E+00 -0.3392E-01

0.2403E+00 0.3853E-01 0.3305E+00 -0.3399E-01

0.2488E+00 0.3879E-01 0.3419E+00 -0.3404E-01

0.2563E+00 0.3900E-01 0.3520E+00 -0.3403E-01

0.2675E+00 0.3930E-01 0.3641E+00 -0.3397E-01

0.2821E+00 0.3968E-01 0.3763E+00 -0.3388E-01

0.2939E+00 0.3998E-01 0.3910E+00 -0.3377E-01

0.3061E+00 0.4023E-01 0.4046E+00 -0.3364E-01

0.3176E+00 0.4044E-01 0.4171E+00 -0.3350E-01

0.3292E+00 0.4056E-01 0.4299E+00 -0.3331E-01

0.3384E+00 0.4073E-01 0.4430E+00 -0.3309E-01

32
TableA-3.Continued.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.3481E+00 0.4084E-01 0.4551E+00 -0.3291E-01

0.3575E+00 0.4094E-01 0.4682E+00 -0.3265E-01

0.3678E+00 0.4106E-01 0.4800E+00 -0.3232E-01

0.3780E+00 0.4117E-01 0.4864E+00 -0.3214E-01

0.3900E+00 0.4121E-01 0.4910E+00 -0.3201E-01

0.4038E+00 0.4124E-01 0.5066E+00 -0.3151E-01

0.4165E+00 0.4124E-01 0.5161E+00 -0.3119E-01

0.4290E+00 0.4121E-01 0.5253E+00 -0.3085E-01

0.4417E+00 0.4119E-01 0.5345E+00 -0.3047E-01

0.4521E+00 0.4117E-01 0.5379E+00 -0.3031E-01

0.4598E+00 0.4112E-01 0.5384E+00 -0.3029E-01

0.4699E+00 0.4108E-01 0.5485E+00 -0.2988E-01

0.4816E+O0 0.4096E-01 0.5616E+O0 -0.2932E-01

0.4917E+00 0.4086E-01 0.5769E+00 -0.2855E-01

0.5059E+00 0.4069E-01 0.5921E+00 -0.2757E-01

0.5164E+00 0.4056E-01 0.6149E+00 -0.2560E-01

0.5272E+00 0.4040E-01 0.6262E+00 -0.2450E-01

0.5370E+00 0.4029E-01 0.6372E+00 -0.2342E-01

0.5372E+00 0.4029E-01 0.6463E+00 -0.2256E-01

0.5409E+00 0.4025E-01 0.6569E+00 -0.2124E-01

0.5499E+00 0.4012E-01 0.6678E+00 -0.1996E-01

0.5618E+00 0.3994E-01 0.6789E+00 -0.1828E-01

0.5724E+00 0.3979E-01 0.6898E+00 -0.1659E-01

0.5833E+00 0.3963E-01 0.7030E+00 -0.1432E-01

0.5942E+00 0.3947E-01 0.7131E+00 -0.1264E-01

0.6089E+00 0.3936E-01 0.7235E+00 -0.1084E-01

0.6246E+00 0.3914E-01 0.7327E+00 -0.9399E-02

0.6350E+00 0.3896E-01 0.7426E+00 -0.7831E-02

0.6454E+00 0.3877E-01 0.7546E+00 -0.5836E-02

0.6573E+00 0.3861E-01 0.7674E+00 -0.3945E-02

0.6706E+00 0.3818E-01 0.7788E+00 -0.2470E-02

0.6848E+00 0.3755E-01 0.7902E+00 -0.1047E-02

0.6980E+00 0.3684E-01 0.7989E+00 -0.8291E-04

0.7116E+00 0.3610E-01 0.8069E+00 0.7155E-03

0.7225E+00 0.3557E-01 0.8184E+00 0.1694E-02

0.7341E+00 0.3497E-01 0.8290E+00 0.2474E-02

0.7441E+00 0.3442E-01 0.8377E+00 0.2950E-02

0.7554E+00 0.3370E-01 0.8473E+00 0.3357E-02

33
TableA-3.Concluded.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.7672E+00 0.3289E-01 0.8538E+00 0.3548E-02

0.7796E+00 0.3195E-01 0.8631E+00 0.4168E-02

0.7923E+00 0.3089E-01 0.8719E+00 0.4047E-02

0.8020E+00 0.3001E-O1 0.8810E+00 0.3772E-02

0.8140E+00 0.2887E-01 0.8910E+00 0.3337E-02

0.8235E+00 0.2795E-01 0.9009E+00 0.2952E-02

0.8349E+00 0.2678E-01 0.9053E+00 0.2882E-02

0.8443E+00 0.2575E-01 0.9126E+00 0.2528E-02

0.8534E+00 0.2470E-01 0.9208E+00 0.2106E-02

0.8612E+00 0.2373E-01 0.9282E+00 O. 1735E-02

0.8696E+00 0.2265E-01 0.9362E+00 0.1274E-02

0.8789E+00 0.2138E-01 0.9427E+00 0.8752E-03

0.8872E+00 0.2020E-01 0.9531E+00 O. 1835E-03

0.8939E+00 0.1920E-01 0.9606E+00 -0.3900E-03

0.9021E+00 0.1794E-01 0.9693E+00 -0. 1084E-02

0.9092E+00 O. 1684E-01 0.9777E+00 -0.1563E-02

0.9179E+00 0.1549E-01 0.9844E+00 -0.1925E-02

0.9238E+00 0.1457E-01 0.9900E+00 -0.2226E-02

0.9310E+O0 0.1335E-01 0.9931E+O0 -0.2384E-02

0.9373E+00 0.1223E-01 0.9957E+00 -0.2533E-02

0.9434E+00 0.1117E-01 0.9973E+00 -0.2640E-02

0.9494E+00 0.1013E-01 0.9980E+00 -0.2655E-02

0.9556E+00 0.9066E-02 0.9996E+00 -0.1731E-02

0.9619E+00 0.8071E-02 0.9998E+00 -0.1157E-02

0.9667E+00 0.7321E-02 0.9999E+00 -0.2917E-03

0.9727E+00 0.6391E-02 0.1000E+01 0.3393E-03

0.9785E+00 0.5461E-02

0.9831E+O0 0.4677E-02

0.9873E+00 0.3883E-02

0.9916E+00 0.3085E-02

0.9949E+00 0.2499E-02

0.9974E+00 0.2125E-02

0.9987E+00 0.1910E-02

0.1000E+01 0.9842E-03

34
TableA-4.Full-scalewing-splashcoordinates (_)LE/TE = 5/10,

rl = 0.76, c = 9.8570 ft).

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.O000E-00 0.6746E-03 O.0000E-00 -0.4227E-05

0.1293E-03 0.1403E-02 0.2114E-04 -0.5631E-03

0.3213E-03 0.2130E-02 0.1936E-03 -0.1441E-02

0.5470E-03 0.2666E-02 0.3804E-03 -0.2054E-02

0.9587E-03 0.3604E-02 0.6594E-03 -0.2787E-02

0.1370E-02 0.4377E-02 0.9891E-03 -0.3421E-02

0.1721E-02 0.4922E-02 0.1245E-02 -0.3861E-02

0.2743E-02 0.6193E-02 0.1517E-02 -0.4275E-02

0.3673E-02 0.7080E-02 0.1885E-02 -0.4715E-02

0.4046E-02 0.74 !9E-02 0.3068E-02 -0.5816E-02

0.4581E-02 0.7877E-02 0.3694E-02 -0.6232E-02

0.5524E-02 0.8665E-02 0.4414E-02 -0.6621E-02

0.6815E-02 0.9647E-02 0.5505E-02 -0.7114E-02

0.7735E-02 0.1032E-01 0.6970E-02 -0.7639E-02

0.8626E-02 0.1093E-01 0.8511E-02 -0.8008E-02

O.lO18E-01 0.1190E-01 0.1004E-01 -0.8258E-02

0.1170E-01 0.1277E-01 0.1233E-01 -0.8592E-02

0.1303E-01 0.1349E-01 0.1453E-01 -0.8830E-02

0.1508E-01 0.1456E-01 0.1694E-01 -0.9009E-02

0.1733E-01 0.1566E-01 0.1975E-01 -0.9132E-02

0.1904E-01 0.1647E-01 0.2300E-01 -0.9175E-02

0.2051E-01 0.1713E-01 0.2559E-01 -0.9152E-02

0.2236E-01 0.1793E-01 0.2818E-01 -0.9120E-02

0.2480E-01 0.1892E-01 0.3027E-01 -0.9062E-02

0.2693E-01 0.1979E-01 0.3264E-01 -0.8862E-02

0.2953E-01 0.2084E-01 0.3384E-01 -0.8558E-02

0.3230E-01 0.2192E-01 0.3498E-01 -0.8354E-02

0.3427E-01 0.2266E-01 0.3616E-01 -0.8203E-02

0.3614E-01 0.2335E-01 0.3751E-01 -0.8093E-02

0.3892E-01 0.2436E-01 0.3864E-01 -0.8001E-02

0.4164E-01 0.2533E-01 0.3976E-01 -0.7983E-02

0.4564E-01 0.2670E-01 0.4105E-01 -0.8036E-02

0.4800E-01 0.2747E-01 0.4273E-01 -0.8057E-02

0.5136E-01 0.2854E-01 0.4407E-01 -0.8054E-02

0.5503E-01 0.2966E-01 0.4504E-01 -0.8051E-02

35
TableA-4.Continued.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.5922E-01 0.3090E-01 0.4611E-01 -0.8044E-02

0.6302E-01 0.3197E-01 0.4741E-01 -0.8049E-02

0.6658E-01 0.3294E-01 0.4914E-01 -0.8052E-02

0.7136E-01 0.3422E-01 0.5086E-01 -0.8070E-02

0.7514E-01 0.3520E-01 0.5353E-01 -0.8075E-02

0.7960E-01 0.3630E-01 0.5545E-01 -0.8083E-02

0.8587E-01 0.3777E-01 0.5751E-01 -0.8104E-02

0.9081E-01 0.3891E-01 0.5977E-01 -0.8125E-02

0.9658E-01 0.4019E-01 0.6259E-01 -0.8119E-02

0.1008E+O0 0.4111E-01 0.6415E-01 -0.8108E-02

0.1051E+00 0.4200E-01 0.6792E-01 -0.8082E-02

0.1118E+00 0.4335E-01 0.7184E-01 -0.8048E-02

0.1167E+00 0.4431E-01 0.7714E-01 -0.7961E-02

0.1226E+00 0.4539E-01 0.8357E-01 -0.7828E-02

0.1288E+00 0.4648E-01 0.8811E-01 -0.7730E-02

0.1352E+00 0.4753E-01 0.9508E-01 -0.7562E-02

0.1431E+00 0.4874E-01 0.1022E+00 -0.7392E-02

0. 1499E+00 0.4966E-01 0.1100E+O0 -0.7228E-02

O. 1579E+00 0.5060E-01 0.1187E+00 -0.7058E-02

O. 1650E+00 0.5134E-01 0.1267E+00 -0.6905E-02

0.1739E+00 0.5224E-01 0.1329E+00 -0.6761E-02

O.1830E+00 0.5310E-01 0.1412E+00 -0.6564E-02

0.1914E+00 0.5381E-01 0.1512E+00 -0.6247E-02

0.2002E+00 0.5457E-01 0.1589E+00 -0.6003E-02

0.2100E+00 0.5537E-01 0.1684E+00 -0.5672E-02

0.2200E+00 0.5606E-01 0.1768E+00 -0.5383E-02

0.2307E+00 0.5677E-01 0.1854E+00 -0.5040E-02

0.2401E+00 0.5740E-01 0.1961E+00 -0.4533E-02

0.2502E+00 0.5805E-01 0.2019E+00 -0.3984E-02

0.2615E+00 0.5874E-01 0.2120E+00 -0.3940E-02

0.2751E+00 0.5958E-01 0.2215E+00 -0.3986E-02

0.2863E+00 0.6021E-01 0.2326E+00 -0.3990E-02

0.2980E+00 0.6086E-01 0.2442E+00 -0.3943E-02

0.3075E+00 0.6138E-01 0.2566E+00 -0.3923E-02

0.3176E+00 0.6187E-01 0.2691E+00 -0.3756E-02

0.3292E+00 0.6241E-01 0.2854E+00 -0.3439E-02

36
TableA-4.Continued.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.3414E+00 0.6297E-01 0.3006E+00 -0.3171E-02

0.3526E+00 0.6345E-01 0.3141E+00 -0.2921E-02

0.3635E+00 0.6393E-01 0.3277E+00 -0.2508E-02

0.3756E+00 0.6444E-01 0.3421E+00 -0.2004E-02

0.3877E+00 0.6494E-01 0.3567E+00 -0.1474E-02

0.3966E+00 0.6530E-01 0.3715E+00 -0.9494E-03

0.4064E+00 0.6569E-01 0.3862E+00 -0.4472E-03

0.4209E+00 0.6626E-01 0.4019E+00 0.1336E-03

0.4347E+00 0.6673E-01 0.4175E+00 0.7626E-03

0.4482E+00 0.6720E-01 0.4333E+00 0.1453E-02

0.4635E+00 0.6771E-01 0.4482E+00 0.2122E-02

0.4766E+00 0.6817E-01 0.4576E+00 0.2551E-02

0.4862E+00 0.6845E-01 0.4709E+00 0.3191E-02

0.4930E+00 0.6865E-01 0.4825E+00 0.3800E-02

0.5091E+00 0.6917E-01 0.4891E+00 0.4160E-02

0.5126E+00 0.6922E-01 0.4932E+00 0.4389E-02

0.5222E+00 0.6949E-01 0.5078E+00 0.5268E-02

0.5294E+00 0.6967E-01 0.5209E+00 0.6151E-02

0.5403E+00 0.6994E-01 0.5329E+00 0.7003E-02

0.5516E+00 0.7022E-01 0.5439E+00 0.7770E-02

0.5656E+00 0.7052E-01 0.5543E+00 0.8487E-02

0.5799E+00 0.7082E-01 0.5645E+00 0.9221E-02

0.5841E+O0 0.7090E-01 0.5719E+00 0.9787E-02

0.5881E+00 0.7099E-01 0.5843E+00 0.1078E-01

0.5881E+00 0.7099E-01 0.5902E+00 0.1129E-01

0.5909E+00 0.7105E-01 0.5903E+00 0.1129E-01

0.5911E+O0 0.7105E-01 0.5925E+00 0.1149E-01

0.5953E+00 0.7113E-01 0.6025E+00 0.1241E-01

0.6009E+00 0.7124E-01 0.6140E+00 0.1355E-01

0.6073E+00 0.7137E-01 0.6245E+00 0.1469E-01

0.6122E+00 0.7142E-01 0.6325E+00 0.1570E-01

0.6158E+00 0.7147E-01 0.6422E+00 0.1696E-01

0.6235E+00 0.7158E-01 0.6536E+00 0.1857E-01

0.6334E+00 0.7173E-01 0.6585E+00 0.1928E-01

0.6415E+00 0.7187E-01 0.6634E+00 O.1997E-01

0.6503E+00 0.7208E-01 0.6667E+00 0.2042E-01

37
TableA-4.Continued.

U.S. U.S. L.S. L.S.

x/c z/c x/c z/c

0.6584E+00 0.7222E-01 0.6718E+00 0.2098E-01

0.6655E+00 0.7228E-01 0.6775E+00 0.2156E-01

0.6721E+00 0.7228E-01 0.6833E+00 0.2217E-01

0.6767E+00 0.7226E-01 0.6888E+00 0.2266E-01

0.6825E+00 0.7221E-01 0.6942E+00 0.2302E-01

0.6872E+00 0.7216E-01 0.6965E+00 0.2313E-01

0.6931E+00 0.7210E-01 0.6986E+00 0.2317E-01

0.6987E+00 0.7204E-01 0.7004E+00 0.2322E-01

0.7048E+00 0.7195E-01 0.7028E+00 0.2332E-01

0.7109E+00 0.7192E-01 0.7043E+00 0.2341E-01

0.7160E+00 0.7186E-01 0.7057E+00 0.2356E-01

0.7203E+00 0.7177E-01 0.7075E+00 0.2395E-01

0.7263E+00 0.7167E-01 0.7115E+00 0.2477E-01

0.7339E+00 0.7144E-01 0.7149E+00 0.2502E-01

0.7407E+00 0.7115E-01 0.7235E+00 0.2552E-01

0.7497E+00 0.7067E-01 0.7281E+00 0.2579E-01

0.7571E+00 0.7017E-01 0.7326E+00 0.2604E-01

0.7647E+00 0.6954E-01 0.7369E+00 0.2628E-01

0.7710E+00 0.6894E-01 0.7421E+O0 0.2661E-01

0.7786E+00 0.6812E-01 0.7473E+00 0.2688E-01

0.7878E+00 0.6698E-01 0.7513E+O0 0.2709E-01

0.7929E+00 0.6628E-01 0.7573E+00 0.2740E-01

0.7972E+00 0.6566E-01 0.7624E+00 0.2765E-01

0.8017E+00 0.6498E-01 0.7685E+00 0.2795E-01

0.8055E+00 0.6437E-01 0.7731E+00 0.2813E-01

0.8100E+00 0.6361E-01 0.7794E+00 0.2840E-01

0.8135E+00 0.6298E-01 0.7839E+00 0.2854E-01

0.8174E+00 0.6229E-01 0.7890E+00 0.2869E-01

0.8205E+00 0.6175E-01 0.7946E+00 0.2882E-01

0.8230E+00 0.6131E-01 0.7983E+00 0.2891E-01

0.8261E+00 0.6071E-01 0.8028E+00 0.2898E-01

0.8290E+00 0.6016E-01 0.8072E+00 0.2905E-01

0.8313E+O0 0.5971E-01 0.8117E+00 0.2910E-01

0.8344E+00 0.5909E-01 0.8162E+00 0.2914E-01

0.8376E+00 0.5842E-01 0.8215E+00 0.2917E-01

0.8438E+00 0.5707E-01 0.8261E+00 0.2919E-01

38
TableA-4.Continued.

U.S. U.S. L.S. L.S.

x/c Jc x/c z/c

0.8478E+00 0.5616E-01 0.8303E+00 0.2918E-01

0.8513E+00 0.5536E-01 0.8357E+00 0.2915E-01

0.8547E+00 0.5453E-01 0.8396E+00 0.2912E-01

0.8580E+00 0.5370E-01 0.8437E+00 0.2907E-01

0.8615E+00 0.5280E-01 0.8477E+00 0.2898E-01

0.8650E+00 0.5188E-01 0.8512E+00 0.2888E-01

0.8681E+00 0.5103E-01 0.8529E+00 0.2884E-01

0.8709E+00 0.5025E-01 0.8545E+00 0.2885E-01

0.8753E+00 0.4898E-01 0.8566E+00 0.2882E-01

0.8790E+00 0.4789E-01 0.8584E+00 0.2881E-01

0.8822E+00 0.4691E-01 0.8592E+00 0.2882E-01

0.8864E+00 0.4557E-01 0.8606E+00 0.2884E-01

0.8896E+00 0.4455E-01 0.8614E+00 0.2884E-01

0.8928E+00 0.4347E-01 0.8621E+00 0.2884E-01

0.8972E+00 0.4195E-01 0.8646E+00 0.2871E-01

0.9009E+00 0.4064E-01 0.8660E+00 0.2850E-01

0.9049E+00 0.3918E-01 0.8680E+00 0.2816E-01

0.9081E+00 0.3801E-01 0.8702E+00 0.2779E-01

0.9111E+00 0.3688E-01 0.8720E+00 0.2754E-01

0.9139E+00 0.3583E-01 0.8745E+00 0.2723E-01

0.9162E+00 0.3495E-01 0.8769E+00 0.2683E-01

0.9186E+00 0.3401E-01 0.8793E+00 0.2645E-01

0.9218E+00 0.3282E-01 0.8826E+00 0.2593E-01

0.9237E+00 0.3207E-01 0.8859E+00 0.2537E-01

0.9259E+00 0.3126E-01 0.8886E+00 0.2490E-01

0.9284E+00 0.3030E-01 0.8917E+00 0.2436E-01

0.9309E+00 0.2933E-01 0.8945E+00 0.2384E-01

0.9339E+00 0.2813E-01 0.8971E+00 0.2336E-01

0.9365E+00 0.2709E-01 0.8998E+00 0.2292E-01

0.9396E+00 0.2587E-01 0.9006E+00 0.2286E-01

0.9425E+00 0.2466E-01 0.9015E+00 0.2279E-01

0.9449E+00 0.2372E-01 0.9030E+00 0.2268E-01

0.9477E+00 0.2255E-01 0.9048E+00 0.2251E-01

0.9502E+00 0.2155E-01 0.9073E+00 0.2188E-01

0.9534E+00 0.2026E-01 0.9102E+00 0.2112E-01

0.9565E+00 0.1890E-01 0.9141E+00 0.2012E-01

39
TableA-4.Concluded.

U.S. U.S. L.S. L.S.

x/c #c x/c z/c

0.9588E+00 0.1780E-01 0.9177E+00 0.1916E-01

0.9616E+00 0.1655E-01 0.9213E+00 0.1823E-01

0.9641E+00 0.1568E-01 0.9247E+00 0.1727E-01

0.9666E+00 0.1483E-01 0.9298E+00 0.1593E-01

0.9690E+00 0.1393E-01 0.9348E+00 0.1465E-01

0.9714E+00 0.1296E-01 0.9401E+00 0.1322E-01

0.9733E+00 0.1218E-01 0.9451E+O0 0.1185E-01

0.9753E+00 0.1140E-OI 0.9496E+00 0.1060E-01

0.9776E+00 0.1047E-01 0.9544E+00 0.9302E-02

0.9793E+00 0.9770E-02 0.9583E+00 0.8425E-02

0.9821E+00 0.8625E-02 0.9626E+00 0.7276E-02

0.9841E+00 0.7824E-02 0.9669E+00 0.5937E-02

0.9868E+00 0.6734E-02 0.9714E+O0 0.4613E-02

0.9888E+00 0.5948E-02 0.9751E+00 0.3554E-02

0.9907E+00 0.5160E-02 0.9795E+00 0.2332E-02

0.9927E+00 0.4395E-02 0.9834E+00 0.1233E-02

0.9942E+00 0.3781E-02 0.9873E+00 0.1818E-03

0.9960E+00 0.3109E-02 0.9905E+00 -0.7245E-03

0.9981E+00 0.2327E-02 0.9931E+00 -0.1465E-02

0.9943E+00 -0.1829E-02

0.9960E+00 -0.2324E-02

0.9971E+00 -0.2627E-02

0.9993E+00 -0.7347E-03

0.9997E+00 0.1099E-04

0.1000E+01 0.9038E-03

40
TableA-5.Designcoordinates (SLF_./T E = 0/2, 1] = 0.93, c = 9.1426 ft).

U.S. L.S. U.S. L.S.

x/c "Jc z/c x/c z/c z/c

0.0000 -0.0215 -0.0215 0.2175 0.0297 -0.0167

0.0001 -0.0209 -0.0221 0.2417 0.0335 -0.0147

0.0002 -0.0202 -0.0228 0.2827 0.0396 -0.0108

0.0003 -0.0199 -0.0230 0.3199 0.0447 -0.0068

0.0005 -0.0197 -0.0232 0.3665 0.0509 -0.0014

0.0007 -0.0193 -0.0236 0.4131 0.0568 0.0043

0.0009 -0.0189 -0.0239 0.4596 0.0625 0.0103

0.0012 -0.0185 -0.0242 0.5062 0.0681 0.0167

0.0016 -0.0181 -0.0245 0.5527 0.0735 0.0234

0.0023 -0.0174 -0.0249 0.5993 0.0787 0.0309

0.0034 -0.0165 -0.0256 0.6365 0.0828 0.0370

0.0046 -0.0156 -0.0261 0.6971 0.0889 0.0470

0.0057 -0.0149 -0.0266 0.6971 0.0889 0.0470

0.0069 -0.0142 -0.0269 0.7375 0.0925 0.0541

0.0092 -0.0130 -0.0274 0.7779 0.0955 0.0616

0.0115 -0.0120 -0.0278 0.8183 0.0977 0.0692

0.0137 -0.0111 -0.0281 0.8384 0.0985 0.0730

0.0183 -0.0095 -0.0284 0.8587 0.0990 0.0765

0.0229 -0.0081 -0.0285 0.8788 0.0992 0.0797

0.0298 -0.0062 -0.0285 0.8990 0.0991 0.0826

0.0298 -0.0062 -0.0285 0.9293 0.0985 0.0861

0.0366 -0.0044 -0.0284 0.9495 0.0978 0.0879

0.0458 -0.0022 -0.0280 0.9697 0.0968 0.0892

0.0572 0.0005 -0.0276 0.9798 0.0962 0.0897

0.0687 0.0029 -0.0270 0.9899 0.0956 0.0902

0.0801 0.0053 -0.0264 1.0000 0.0949 0.0906

0.0916 0.0076 -0.0257

0.1145 0.0119 -0.0242

0.1374 0.0161 -0.0227

0.1603 0.0201 -0.0210

0.1832 0.0240 -0.0193

41
TableA-6.Designcoordinates (_LF__/I'E = 0/2, 11= 0.76, c = 9.9827 ft).

U.S. L.S. U.S. L.S.

x/c z/c z/c x/c z/c z/c

0.0000 -0.0135 -0.0135 0.2214 0.0395 -0.0197

0.0001 -0.0124 -0.0146 0.2679 0.0457 -0.0167

0.0002 -0.0119 -0.0151 0.3072 0.0504 -0.0136

0.0004 -0.0112 -0.0157 0.3563 0.0559 -0.0091

0.0006 -0.0107 -0.0161 0.3563 0.0559 -0.0091

0.0008 -0.0103 -0.0165 0.4054 0.0610 -0.0042

0.0011 -0.0098 -0.0169 0.4545 0.0658 0.0011

0.0015 -0.0093 -0.0173 0.5036 0.0704 0.0069

0.0021 -0.0085 -0.0179 0.5527 0.0747 0.0133

0.0031 -0.0074 -0.0187 0.6018 0.0787 0.0205

0.0042 -0.0065 -0.0195 0.6322 0.0811 0.0259

0.0052 -0.0056 -0.0201 0.6710 0.0839 0.0335

0.0052 -0.0056 -0.0201 0.7009 0.0858 0.0400

0.0063 -0.0049 -0.0206 0.7408 0.0879 0.0486

0.0084 -0.0037 -0.0214 0.7807 0.0892 0.0563

0.0105 -0.0026 -0.0220 0.8205 0.0899 0.0632

0.0126 -0.0017 -0.0225 0.8405 0.0898 0.0662

0.0168 0.0000 -0.0231 0.8604 0.0896 0.0689

0.0210 0.0014 -0.0236 0.8804 0.0891 0.0713

0.0273 0.0033 -0.0240 0.9003 0.0883 0.0732

0.0336 0.005 i -0.0243 0.9302 0.0867 0.0753

0.04 19 0.0073 -0.0245 0.9502 0.0853 0.0761

0.0524 0.0098 -0.0247 0.9701 0.0837 0.0765

0.0629 0.0122 -0.0247 0.9801 0.0828 0.0766

0.0734 0.0145 -0.0247 0.9900 0.0819 0.0767

0.0839 0.0166 -0.0246 1.0000 0.0809 0.0769

0.1049 0.0206 -0.0242

0.1258 0.0244 -0.0237

0.1468 0.0279 -0.0230

0.1678 0.0314 -0.0222

0.1992 0.0363 -0.0209

42
TableA-7.Designcoordinates (_)LE/TE = 0/2, 1"1= 0.59, c = 10.8227 ft).

U.S. L.S. U.S. L.S.

x/c z/c z/c x/c z/c z/c

0.0000 -0.0072 -0.0072 0.2145 0.0463 -0.0231

0.0001 -0.0059 -0.0085 0.2555 0.0512 -0.0214

0.0001 -0.0059 -0.0085 0.2965 0.0555 -0.0191

0.0002 -0.0053 -0.0091 0.3477 0.0604 -0.0154

0.0004 -0.0046 -0.0098 0.3989 0.0648 -0.0112

0.0008 -0.0035 -0.0108 0.4502 0.0688 -0.0065

0.0010 -0.0029 -0.0114 0.5014 0.0724 -0.0012

0.0013 -0.0023 -0.0119 0.5527 0.0758 0.0048

0.0019 -0.0014 -0.0127 0.6039 0.0788 0.0118

0.0029 -0.0002 -0.0137 0.6367 0.0805 0.0175

0.0039 0.0009 -0.0146 0.6745 0.0822 0.0250

0.0048 0.0017 -0.0152 0.7041 0.0832 0.0320

0.0058 0.0025 -0.0158 0.7435 0.0840 0.0417

0.0077 0.0039 -0.0168 0.7830 0.0841 0.0506

0.0097 0.0050 -0.0175 0.8224 0.0834 0.0578

0.0116 0.0060 -0.0181 0.8619 0.0818 0.0628

0.0155 0.0078 -0.0191 0.8816 0.0807 0.0644

0.0193 0.0093 -0.0198 0.8816 0.0807 0.0644

0.0251 0.0113 -0.0206 0.9014 0.0794 0.0655

0.0309 0.0131 -0.0211 0.9310 0.0769 0.0662

0.0387 0.0153 -0.0217 0.9507 0.0751 0.0663

0.0484 0.0178 -0.0223 0.9704 0.0730 0.0662

0.0580 0.0201 -0.0228 0.9803 0.0719 0.0661

0.0677 0.0222 -0.0231 0.9901 0.0708 0.0660

0.0774 0.0242 -0.0235 1.0000 0.0696 0.0658

0.0774 0.0242 -0.0235

0.0967 0.0279 -0.0239

0.1160 0.0314 -0.0242

0.1354 0.0346 -0.0243

0.1547 0.0377 -0.0242

0.1837 0.0421 -0.0239

43
TableA-8.Designcoordinates (_LF_./TE = 0/2, "q = 0.40, c = 11.8004 ft).

U.S. L.S. U.S. L.S.

x/c z/c z/c x/c z/c z/c

0.0000 -0.0014 -0.0014 0.2005 0.0521 -0.0265

0.0001 0.0001 -0.0028 0.2219 0.0545 -0.0262

0.0002 0.0007 -0.0034 0.2432 0.0567 -0.0257

0.0004 0.0016 -0.0042 0.2859 0.0607 -0.0242

0.0007 0.0029 -0.0054 0.3392 0.0650 -0.0214

0.0012 0.0043 -0.0067 0.3926 0.0687 -0.0179

0.0018 0.0053 -0.0076 0.4459 0.0719 -0.0140

0.0027 0.0067 -0.0088 0.4993 0.0745 -0.0092

0.0036 0.0079 -0.0097 0.5526 0.0769 -0.0036

0.0044 0.0088 -0.0106 0.6060 0.0788 0.0032

0.0053 0.0096 -0.0113 0.6412 0.0798 0.0091

0.0071 0.0109 -0.0126 0.6412 0.0798 0.0091

0.0089 0.0121 -0.0136 0.6779 0.0807 0.0162

0.0106 0.0131 -0.0144 0.7072 0.0811 0.0227

0.0142 0.0148 -0.0157 0.7463 0.0812 0.0317

0.0177 0.0163 -0.0167 0.7658 0.0810 0.0362

0.0231 0.0183 -0.0179 0.7853 0.0806 0.0404

0.0284 0.0200 -0.0189 0.8048 0.0799 0.0443

0.0284 0.0200 -0.0189 0.8243 0.0789 0.0478

0.0355 0.0221 -0.0200 0.8439 0.0777 0.0509

0.0443 0.0246 -0.0212 0.8634 0.0762 0.0534

0.0532 0.0269 -0.0222 0.8829 0.0744 0.0553

0.0621 0.0290 -0.0230 0.9024 0.0724 0.0566

0.0710 0.0309 -0.0237 0.9317 0.0688 0.0575

0.0887 0.0345 -0.0246 0.9512 0.0661 0.0573

0.1064 0.0379 -0.0253 0.9707 0.0632 0.0567

0.1242 0.04 10 -0.0257 0.9805 0.0617 0.0562

0.1419 0.0439 -0.0260 0.9902 0.0602 0.0557

0.1685 0.0479 -0.0264 1.0000 0.0587 0.0552

0.1873 0.0503 -0.0265

44
APPENDIX B

General Listing of Available Wing Pressure and Boundary-Layer Data

Table B provides nominal values for MINE ALPT and QINF. Camber is either _)LF_,/TEor _)LE/I/M/O" Appendices

indicate where to find the wing pressure coefficient data and the boundary-layer data. The boundary-layer data,

which are all in Appendix K, are in brackets, e.g., [6,7]. Refer to Nomenclature for definitions.

The following example indicates how to use this table. For example, find the wing pressure coefficient data

listing for a Camber of 5/10 at nominal conditions of MINF = 0.90, ALPT = 4° and QINF = 300 Ib/ft 2. This table

is sorted by trailing-edge camber starting at 0 ° and decreasing to 19° down. Trailing-edge up camber (-1 °) is at the

end of this table. For the given nominal conditions, the desired data is found in Appendix G. Table G-1 is a summary

of the data listed in Table G-2. From Table G-I, the data for MINF = 0.898, ALPT = 4.04 ° and QINF = 299.5 lb/ft 2

are found in Table G-2 for Flight 211 at Time 11-25-20-500.

Table B. Nominal values for MINF, ALPT and QINE with appendix letters.

Camber MINF ALPT, deg QINE Ib/ft2 Appendices

2/0 1.41 7 800 H

3/0 1.24 8 650 H

5/0 0.85 11 300 J

10/0 0.60-0.61 2,6,8,12 300-310 C

10/0 0.80-0.81 3,6,8 310 E

2/1 1.19-1.24 5,6,7 570-650 H

1/1 1.41 6 800 H

10/1 0.61 3 310 C

0/2 0.50 4,6,7,8 290-300 I

0/2 0.59-0.6 i 6,7,8,10,12,13 280-310 C,H,J

[0/2] [0.60-0.61 ] [6,7,8,9,10] [300-310] [K]

0/2 0.65 5 340 H

0/2 0.69-0.71 6,7,8,9,10,11,12,13 290-310 D

0/2 0.70 5 400 H

0/2 0.75 4 460 H

[0/2] [0.76] [3] [440-460] [K]

0/2 0.79-0.81 4,5,6,7,8,9,10,12 280-310 E

[0/2] [0.79-0.82] [3,6,7,8,9,10] [300-320] [K]

[0/2] [0.80-0.81] [4,5,6,7,8,9,10] [450-470] [K]

[0/2] [0.78-0.79] [3,4] [490-520] [K]

0/2 0.80-0.81 4,5,6,7,8,9,10 590-620 J

0/2 0.80 4 530 H

[0/2] [0.78-0.79] [4,6,9] [570-590] [K]

45
TableB.Continued.

Camber MINF ALPT, deg QINF, lb/ft2 Appendices

[0/2] [0.79-0.82] [3,4,5,6,7,8,9] [600-640] [K]

[0/2] [0.83-0.84] [8,9] [340-350] [K]

0/2 0.84-0.86 5,6,7,8,9,10,11,12 250-310 F,J

[0/2] [0.84-0.86] [5,6,7,8,9] [290-310] [K]

0/2 0.85-0.86 4,5,6,7,8,9,10 600-610 H,J

0/2 0.88-0.91 5,6,7,8,9,10,12 290-340 G,H

[0/2] [0.89-0.90] [6,7,8] [300] [K]

0/2 0.88-0.91 4,5,7,8 600-670 H,J

0/2 0.92-0.93 6,8,9 330-340 G,H

[0/2] [0.90] [7] [320] [K]

0/2 0.94-0.96 6,7,8,9,10 300-340 H

[0/2] [0.95] [6,7] [300] [K]

0/2 0.94 5 380 H

0/2 0.97-0.99 8 340-350 H

0/2 1.00-1.05 7,8,9 350-410 H

0/2 1.I 0-1.20 6,7,9 460-590 H

0/2 1.21 - 1.30 3,4,5,6,7,8,9,11 570-660 H

0/2 1.39-1.41 2,4,5,8,9 790-840 H

1/2 1.22-1.24 4,6 610-650 H

1/2 1.40 4 790 H

2/2 0.60 7 280 C

3/2 0.61 7 280 C

3/2 0.81 9 310 J

4/2 0.61 7 280 C

5/2 0.59-0.61 6,7,8,10,12 280 C

[5/2] [0.60-0.61 ] [7,8,9,10] [300-320] [K]

5/2 0.70-0.72 6,7,8,9,10,11,12 290-310 D

5/2 0.79-0.81 5,6,7,8,10 290-310 E

[5/2] [0.80-0.82] [6,7,8,9,10] [290-310] [K]

[5/2] [0.80-0.81] [4,5,6,7,8,9,10] [450-480] [K]

5/2 0.85-0.86 4,5,6,7,8,9,10,11,12 280-310 F,J

[5/2] [0.84-0.85] [6,7,8,9] [300] [K]

5/2 0.90-0.91 6,7,8,9,10,12 300-310 G

[5/2] [0.90] [6,7] [300] [K]

5/2 0.95 6,7 300 n

6/2 0.61 7 290 C

7/2 0.61 7 290 C

8/2 0.61 7 290 C

9/2 0.61 7 280 C

46
TableB.Continued.

Camber MINF ALPT,deg QINElb/ft2 Appendices

10/2 0.50-0.51 3,6,8 300 I

10/2 0.61 7,8 280-310 C

10/2 0.79-0.81 4,5,6,7,8,10,12 290-310 E

[10/2] [0.79-0.81] [6,7,8] [300-320] [K]

10/2 0.79-0.81 4,5,6,8,9 580-610 J

10/2 0.84-0.86 5,6,7,8,9,11,12 290-300 F

10/2 0.84-0.86 4,5,6,7,8,9,10 580-600 J

10/2 0.89-0.91 6,7,8,9,10,11,12 290-310 G

10/2 0.89-0.91 4,6,7,8,9 590-630 J

11/2 0.61 7 280 C

12/2 0.61 7 280 C

13/2 0.61 7 280 C

14/2 0.60 7 280 C

15/2 0.60 7 280 C

16/2 0.60 7 280 C

17/2 0.60 7 280 C

18/2 0.60 7 270 C

19/2 0.59-0.60 8 270 C

0/3 0.71 4 320 J

[0/3] [0.72-0.73] [3] [430-440] [K]

[0/3/2/2] [0.75] [3] [450] [K]

[0/3/4/4] [0.79] [4] [520] [K]

[0/3] [0.78-0.82] [4] [510-570] [K]

[0/3] [0.80-0.82] [4,5,6] [600-640] [K]

0/3 0.90 4 600 J

0/3 1.22 3 620 H

0/3 1.41 2,4,5 790-800 H

1/3 0.70 3 300 J

[1/3] [0.75-0.76] [4] [450-470] [K]

1/3 1.24 4,5 640-650 H

5/3 0.86 10 310 J

10/3 0.60-0.61 2,8,12 300 C

l/4 0.70-0.72 5,6 300-330 J

[1/4] [0.73] [5] [440-450] [K]

[1/4/3/3] [0.77] [5] [480] [K]

[1/4/5/5] [0.751 [5] [450] [K]

1/4 0.80 5 300 J

47
TableB.Continued.

Camber MINF ALl:q',deg QINElb/ft2 Appendices

[1/4] [0.80-0.81] [5] [300-310] [K]

[1/4] [0.78-0.81] [6,7] [500-560] [K]

[1/4] [0.80-0.82] [5,6,7] [610-640] [K]

[2/4] [0.49-0.50] [5] [150-160] [K]

[2/4/4/5] [0.50] [5] [160] [K]

2/4 0.70 5 290-300 J

5/4 0.86 9 310 J

10/4 0.60 3 300 C

10/4 0.80-0.81 3,6,8 300-310 E

1/5 0.81 6 300 j

[1/5] [0.81] [6] [310] [K]

[1/5/4/4] [0.80] [6] [550] [K]

[2/5] [0.48] [6] [150] [K]

2/5 0.73 7 330 J

[2/5] [0.77-0.79] [7] [490-520] [K]

[2/5] [0.77-0.80] [5,7] [560-600] [K]

[2/5/4/5] [0.78-0.79] [7] [500-520] [K]

[2/5/5/-1] [0.79] [7] [520] [K]

2/5 0.81 7 300 j

3/5 0.61 7 300 j

[3/5] [0.58] [6] [240-250] [K]

[3/5/5/6] [0.60] [6] [250] [K]

[2/6] [0.80-0.84] [7,8] [310-350] [K]

3/6 0.79-0.81 6,7,8 310-350 j

[3/6] [0.81-0.84] [8,9] [320-350] [K]

[3/6] [0.78] [8] [500-510] [K]

5/6 0.59-0.60 5,8,10 280-310 C

5/6 0.69-0.72 5,7,8,9,11 300-330 D

5/6 0.80-0.81 5,6,7,8,9,10 280-310 E

[5/6] [0.79-0.80] [5,6,7,8] [290-300] [K]

5/6 0.80 7 610 J

[5/6] [0.80-0.81] [4] [600-610] [K]

5/6 0.84-0.86 4,5,7,8,11,12 280-310 F

5/6 0.89-0.91 5,6,7,8,9,12 270-300 G

10/6 0.59-0.61 2,8,12 290-310 C

10/6 0.80 3,6 300 E

48
TableB.Continued.

Camber MINF ALl'T, deg QINF,lb/ft2 Appendices

3/7 0.81 8 310 J

4/7 0.63 8 330 J

4/7 0.73 9 330 J

[4/7] [0.73-0.77] [9] [440-490] [K]

[4/7] [0.80-0.81] [9] [310-320] [K]

5/7 0.62 7 310 J

5/7 0.86 9 310 J

10/7 0.60 3 300 C

10/7 0.81 8 310 E

5/8 0.78-0.79 9,11 310-320 J

5/9 0.86 8 310 J

6/9 0.64 10 340 J

6/9 0.70 11 310 J

10/9 0.59-0.61 2,8,12 290-310 C

10/9 0.80-0.81 3,8 300-310 E

15/9 0.50 4 260 I

0/10 0.51 12 130 I

0/10 0.81 6,8 300 E

0/10 0.89-0.91 5,6,7,8,9,10 280-300 G

5/10 0.51 11 120 I

5/10 0.60-0.61 3,8,10 300-330 C

5/10 0.69-0.70 4,6,7,8,9,10,I1 280-320 D

5/10 0.70-0.71 7,8 580-600 J

5/10 0.79-0.80 3,4,5,7,8,9,10 280-300 E

5/10 0.79-0.81 3,4,5,6,7,8 580-620 J

5/10 0.81 5,6 790-810 J

5/10 0.85-0.86 4,5,6,7,8,10 290-310 F,J

5/10 0.85-0.86 3,7,8 580-610 J

5/10 0.89-0.91 4,5,6,7,8,9,10 290-330 G

5/10 0.89-0.90 3,7,8 580-650 J

7/10 0.67 12 280 J

10/10 0.50-0.51 3,4,8 300-310 I

10/10 0.61 3,8,10,12 290-310 C

10/10 0.69-0.70 7,8,11 280-290 D

10/10 0.79-0.81 4,6,7,8,9,10 280-320 E

10/10 0.85 4 300 F

49
TableB.Continued.

Camber MINF ALPT,deg QINF,lb/ft2 Appendices

10/10 0.90 5,6,8,10 300-320 G

10/10 0.90 4 390 G

15/10 0.48-0.52 4,5 250-280 I

15/10 0.59 3 310 I

0/11 0.79-0.82 4,5,7 290-310 E

0/11 0.91 4 300 G

5/11 0.60 4,5,7 300 C

5/11 0.70-0.71 2,4,6 600-610 J

5/11 0.80 8 300 E

5/11 0.80 3 790 J

5tl 1 0.85 5 290 F

5/11 0.86 4,5 600 J

5/11 0.89-0.90 5,10 300-310 G

5/11 0.90 4 600 J

6/11 0.78 13 310 J

I0/11 0.50 4 300 I

10/11 0.60 4 300 C

10/11 0.79-0.80 5,6,8 300 E

8/12 0.60-0.61 11 290-300 j

8/12 0.64 I 1 330 J

10/12 0.59-0.61 2,8,12 290-300 C

10/12 0.80 3,10 300 E

8/13 0.60 11 290 J

9/13 0.58 11 270 J

10/13 0.60 3 300 C

10/13 0.80-0.81 3,6,8 300-310 E

5/14 0.80 12 260 E

9/14 0.61 12 300 j

5/15 0.69-0.71 3,4,5,8,9,10 280-310 D,J

5/15 0.78-0.80 4,5,6,7,8,9 220-270 E

10/15 0.59-0.61 2,8,12 290-310 C

10/15 0.79 3 300 E

10/15 0.85 4 260 F

10/15 0.90 4 300 G

50
TableB.Concluded.

Camber MINF ALPT,deg QINElb/ft2 Appendices

5/16 0.69-0.71 4,5,6,7,11,12 280-300 D

10/16 0.50 10 120 I

10/16 0.60-0.61 3,8 300-310 C

10/17 0.61 13 300 J

20/17 0.27-0.29 8,9,10 100-110 I

20/17 0.34-0.37 5,6 140-160 I

10/18 0.60 2,8,12,13 290-300 C

10/18 0.80 12 300 E

20/18 0.28-0.32 7,8,9,10,12 80-120 I

20/18 0.41 4 190 I

20/18 0.60 3 300 C

10/19 0.61 3,6 300-310 C

10/19 0.81 3,8 310 E

3/-1 1.40 9 790 H

4/-1 0.81 10 310 J

4/-1 1.20 8 570 H

5/-1 0.70-0.71 2,6,7,8 580-610 J

5/-1 0.80 11 310 J

5/-1 0.79 8 570-580 J

5/-1 0.85 12,13 310 J

5/-1 1.24 9 660 H

5/-1 1.37-1.39 9,10 750-780 H

6/-1 0.80 13 310 J

7/-1 0.63 11 390 J

7/-1 0.79 13 320 J

7/-1 1.23 10 650 H

9/-1 1.23 10 650 H

12/-1 1.22 11 640 H

51
APPENDIX C

Wing Pressure Coefficients for Nominal Dynamic Pressure

of 300 lb/ft 2 and Mach Number of 0.60.

Leading-edge wing sweep is 26% Table C-1 contains a summary of the data listing in table C-2. The asterisks (*)

in table C-2 indicate invalid values. Camber is 8LE/TE. Refer to Nomenclature for definitions.

Table C-1. Summary data.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

213 8-33-17-000 0.603 0/2 6.01 0.31 296.9 3.0E+06 0.2618

213 8-33-44-500 0.598 0/2 9.99 0.80 288.1 3.0E+06 0.2881

200 8-32-28-000 0.593 5/2 6.06 -0.24 293.0 3.0E+06 0.2680

200 8-32-37-500 0.597 5/2 6.96 -0.33 295.9 3.0E+06 0.2998

200 8-32-48-000 0.605 5/2 8.02 -0.10 304.3 3.1E+06 0.3360

200 8-33-10-500 0.610 512 12.02 0.45 319.0 3.2E+06 0.4931

216 8-49-8-000 0.600 5/2 6.34 0.80 302.6 3.1E+06 0.2473

216 8-49-55-500 0.601 5/2 7.05 -0.10 302.8 3.1E+06 0.2768

216 8-50-12-000 0.600 5/2 7.98 0.37 300.2 3. IE+06 0.3120

216 8-50-29-500 0.606 5/2 10.08 0.43 309.1 3.1E+06 0.3242

213 8-19-36-500 0.598 5/10 3.48 0.14 298.8 3.1E+06 0.3733

213 8-20-2-500 0.608 5/10 8.27 -0.04 307.1 3.1E+06 0.4979

213 8-20-18-500 0.611 5/10 10.02 0.11 329.1 3.3E+06 0.4791

213 8-19-48-500 0.598 5/11 3.90 -0.65 298.3 3.1E+06 0.3951

213 8-19-52-000 0.601 5/11 5.02 -0.59 300.7 3.1E+06 0.3888

213 8-19-57-000 0.603 5/i I 7.07 -0.36 302.6 3.1E+06 0.4444

213 8-26-19-500 0.613 10/2 8.00 -0.15 308.5 3.1E+06 0.3682

213 8-28-35-500 0.598 I0/11 3.99 -0.53 297.3 3.1E+06 0.4172

213 8-29-21-000 0.607 I0/10 7.99 -0.10 289.4 2.9E+06 0.5101

213 8-29-59-500 0.605 10/10 10.22 0.05 310.3 3.2E+06 0.6331

222 9-37-53-000 0.608 10/10 12.14 -0.24 307.4 3.1E+06 0.5239

216 8-52-13-500 0.602 5/6 5.01 0.51 304.2 3.1E+06 0.2997

216 8-52-45-500 0.588 5/6 8.00 0.37 281.1 2.9E+06 0.3856

216 8-54-28-000 0.596 5/6 10.05 0.19 296.6 3. IE+06 0.3976

2 ! 6 8-56-43-500 0.599 20/18 3.04 0.86 299.5 3.1E+06 0.2664

216 9-29-0-000 0.604 10/18 2.07 -0.04 304.8 3.1E+06 0.3364

216 9-29-6-500 0.607 10/19 3.01 -0.36 306.2 3.1E+06 0.3786

216 9-29-12-000 0.606 10/19 6.05 -0.21 303.4 3.1E+06 0.4802

216 9-29-15-000 0.603 10/18 7.91 -0.24 299.7 3.1E+06 0.5327

216 9-29-18-500 0.600 10/18 11.70 -0.12 295.4 3.0E+06 0.7044

52
TableC-1.Continued.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

216 9-30-24-500 0.605 10/15 2.06 -0.01 305.2 3.1E+06 0.3346

216 9-30-42-000 0.608 10/16 8.12 -0.30 305.8 3.1E+06 0.5323

216 9-30-47-500 0.591 10/15 12.30 -0.07 288.2 3.0E+06 0.7297

216 9-31-32-000 0.603 10/12 2.09 0.69 303.3 3.1E+06 0.2984

216 9-31-43-000 0.607 10/12 8.09 -0.41 304.8 3.1E+06 0.5067

216 9-31-47-500 0.594 10/12 12.00 -0.27 290.5 3.0E+06 0.7488

216 9-32-35-000 0.606 10/9 1.99 0.25 306.3 3.1E+06 0.3043

216 9-32-47-000 0.603 10/9 7.92 -0.41 300.2 3.1E+06 0.4942

216 9-32-51-500 0.590 10/9 11.92 -0.27 286.9 3.0E+06 0.7017

216 9-33-28-000 0.599 10/6 2.03 0.02 299.5 3.1E+06 0.3061

216 9-33-39-500 0.610 10/6 8.24 -0.10 309.6 3.1E+06 0.4955

216 9-34-22-000 0.605 10/3 2.08 -0.27 304.8 3.1E+06 0.3029

216 9-34-33-000 0.601 10/3 8.18 0.19 300.9 3.1E+06 0.4915

216 9-34-37-000 0.604 10/3 12.05 0.02 304.6 3.1E+06 0.7376

216 9-35-21-000 0.596 10/0 2.00 0.17 295.2 3.0E+06 0.2870

216 9-35-37-500 0.606 10/0 8.16 0.22 305.5 3.1E+06 0.4777

216 9-35-42-500 0.601 10/0 11.92 -0.04 300.9 3.1E+06 0.7079

198 13-6-58-500 0.600 0/2 7.01 0.60 276.3 2.8E+06 0.2999

198 13-7-40-000 0.604 2/2 6.99 0.63 279.9 2.9E+06 0.3048

198 13-7-42-000 0.605 3/2 7.05 0.60 280.6 2.9E+06 0.3033

198 13-7-45-500 0.605 4/2 6.99 0.55 280.6 2.9E+06 0.3034

198 13-7-48-500 0.606 5/2 7.03 0.60 282.0 2.9E+06 0.3168

198 13-7-52-500 0.610 6/2 6.93 0.52 285.2 2.9E+06 0.3034

198 13-7-55-500 0.611 7/2 7.00 0.52 286.6 2.9E+06 0.3070

198 13-7-59-000 0.610 8/2 6.99 0.63 285.5 2.9E+06 0.3136

198 13-8-i-000 0.609 9/2 7.03 0.60 284.8 2.9E+06 0.3253

198 13-8-4-000 0.608 10/2 7.11 0.63 284.1 2.9E+06 0.3151

198 13-8-8-000 0.608 11/2 7.19 0.71 283.9 2.9E+06 0.3258

198 13-8-11-500 0.607 12/2 7.23 0.63 283.6 2.9E+06 0.3378

198 13-8-14-500 0.606 13/2 7.27 0.60 282.3 2.9E+06 0.3375

!98 13-8-17-500 0.604 14/2 7.34 0.71 280.9 2.9E+06 0.3362

198 13-8-21-000 0.602 15/2 7.35 0.63 278.6 2.8E+06 0.3416

198 13-8-24-000 0.600 16/2 7.35 0.57 276.7 2.8E+06 0.3363

198 13-8-27-000 0.598 17/2 7.48 0.50 275.4 2.8E+06 0.3505

198 13-8-30-500 0.597 18/2 7.48 0.50 274.2 2.8E+06 0.3529

198 13-8-33-000 0.595 19/2 7.55 0.57 272.9 2.8E+06 0.3394

198 13-8-36-500 0.593 19/2 7.55 0.55 271.3 2.8E+06 0.3568

53
TableC-1.Concluded.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

216 8-52-1-000 0.604 5/6 4.99 0.37 306.2 3.1E+06 0.2850

216 8-52-52-000 0.601 5/6 7.92 0.17 292.7 3.0E+06 0.3783

216 8-54-30-000 0.600 5/6 9.99 -0.10 300.2 3.1E+06 0.4014

216 8-56-49-500 0.601 20/18 2.98 0.89 302.0 3.1E+06 0.2761

216 8-56-59-500 0.598 20/18 3.04 0.74 299.1 3.1E+06 0.2625

216 9-29-19-500 0.596 10/18 13.33 -0.41 291.8 3.0E+06 0.7196

216 9-30-29-500 0.603 10/15 2.04 0.14 303.3 3.1E+06 0.3392

216 9-30-33-500 0.604 10/16 2.93 -0.15 304.0 3.1E+06 0.3619

216 9-30-42-500 0.607 10/15 8.23 -0.50 304.3 3.1E+06 0.5364

216 9-31-36-000 0.603 10/13 2.92 -0.36 302.3 3.1E+06 0.3297

216 9-32-40-000 0.607 10/10 3.26 -0.30 307.4 3.1E+06 0.3315

216 9-33-31-000 0.600 10/7 3.01 -0.56 300.2 3.1E+06 0.3222

216 9-33-47-000 0.587 10/6 12.01 0.19 286.4 3.0E+06 0.7221

216 9-34-25-500 0.602 10/4 3.05 -0.67 301.9 3.1E+06 0.3308

216 9-35-22-500 0.599 10/0 2.03 0.22 298.2 3.1E+06 0.2836

216 9-35-30-000 0.609 10/I 3.11 -0.01 309.6 3.IE+06 0.3061

216 9-35-34-000 0.610 10/0 6.06 -0.67 310.6 3.1E+06 0.4158

198 13-8-42-000 0.590 19/2 7.63 0.60 268.4 2.8E+06 0.3751

54
Table C-2. Listing of data.

Flight 213, Wing sweep = 26 °, Time = 8-33-17-000, MINF = 0.603, Camber = 0/2, ALPT = 6.01, BETA = 0.31, QINF = 296.9,

RNPU = Y0E+06. CNWP = 0.2618

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.498 0.000 0.656 0.000 0.341 ** 0.010 - 1.796

0.060 -0.349 0.020 -0.982 0.020 - 1.141 0.020 - 1.099

0.110 -0.300 0.040 -0.560 0.060 -O217"* 0.060 -0.841

0.200 -0.252 0.060 -0.599 0.090 -0.566 0. I 10 -0.660

0.230 -0.291 0.090 -0.443 0.110 -0.542 0.140 -0.608

0.400 -0.220 0.130 -0.437 0.130 -3.929* * 0.190 -3.929* *

0.490 -0,191 0.150 -0.424 0.150 -0.490 0.250 -0.455

0.590 -0.231 0.200 -0.393 0.210 -0.499 0.400 -0.389

0.630 -0.227 0.250 -0.373 0.250 -0,427 0.490 -0.325

0.700 -0.223 0.260 -0.352 0.340 -0.401 0.580 -0.315

0.750 -0.235 0.280 -0.358 0.370 -0.381 0.650 -0.366

0.810 -0.217 0.290 -0.350 0.400 -0.337 0.700 -0.329

0.840 -0.228 0.310 -0.332 0.410 -2.675** 0.750 -0.332

0.900 -0.146 0.320 -0.339 0.430 -0,365 0.800 -0.323

0.960 -0.055 0.340 -0.320 0.440 -0.345 0.830 -0.291

0.350 -0.174"* 0.460 -0.346 0.900 -0.203

0.370 -0.309 0.490 -0.335 0.960 -0.036

0.380 -0.337 0.500 -0.342

0.400 -0.259 0.520 -0.338

0.410 -0.314 0.540 -0.324

0.430 -0.291 0.550 -0.309

0.440 -0.273 0.580 -0.320

0.460 -0.284 0.600 -0.314

0.470 -0.310 0.610 -0.318

0.490 -0293 0.650 -0.514

0.500 -0.296 0.700 -0.343

0.520 -0.284 0.750 -0346

0.530 -0.281 0,820 -0.304

0.550 -0.306 0.890 -0.152

0.560 -0.301 0900 -0.134

0.580 -0,275 0.960 0.000

0.590 -0.306

0.600 -0.294

0.640 -0.315

0.700 -0.306

0,750 -0.04.4"*

0.820 -0.263

0.870 -0.231

0.930 -0.113

0.960 -0.061

Lower Surface

0.020 -0.034 0.020 0.138 0.020 0.257 0.020 0.562

0.110 -0.107 0.060 0.090 0.060 0.157 0.060 -0.032

0.230 -0.014 0.090 0.037 0,090 0.098 0.110 0.112

0.400 -0.062 0.120 -0.028 0.120 -0.110 0.250 -0.120

0.490 -0.046 0.200 -0.031 0.200 -0.032 0.400 -0.125

0.630 2,492** 0,260 -0,093 0.250 -0.088 0.490 -0.148

0.750 -0.007 0.400 -0.085 0.400 -0.105 0.580 -0.169

0.850 0.041 0.490 -0.1 04 0.490 -0.060 0.650 -0.091

0.900 0.131 0.580 -0.121 0.580 -0.142 0.750 0.112

0.960 0.109 0.640 0.017 0.650 -0.056 0.830 0.230

0.750 0.131 0,750 0.149 0.900 0.266

0.870 0.192 0.890 0.246 0.960 0.215

0.930 0.174 0.930 0.194

0.960 0.130 0.960 0.258

CN = 0.203 0.333 0.36t 0.397

55
Table C-2. Continued.

Flight 213, Wing sweep = 26". Time = 8-33-44-500, MINF = 0.598, Camber = 0/2, ALl:q" = 9.99. BETA = 0.80. QINF = 288.1,

RNPU = 3.0E+06. CNWP = 0.2881

11 = 0.93 0.76 0.59 0.40

Upper Surface

xA: CP x/c CP x/c CP x/c CP

0020 -2.175 0.000 -0,207 0.000 -0.169"* 0.010 -2.941

0,060 -0,702 0,020 -2.787 0.020 -2.815 0.020 -2.935

0. 110 -0578 0.040 -0.934 0.060 -0.911 ** 0.060 - 1.566

0.200 -0.430 0.060 - 1.194 0.090 - 1.150 0.110 -0.885

0.230 -0.434 0.090 -0.734 0.110 -0.925 0.140 -0.718

0.400 -0.316 O. 130 -0.710 O. 130 -3.999** O. 190 -3.999**

0.490 -0.266 0.150 -0.658 0.150 -0.713 0,250 -0.565

0.590 -0.291 0.200 -0.610 0.210 -0,688 0.400 -0.469

0.630 -0.291 0.250 -0.543 0.250 -0.580 0.490 -0.398

0.700 -0.270 0.260 -0.493 0.340 -0.519 0.580 -0.338

0.750 -0.276 0.280 -0.504 0.370 -0.471 0.650 -0.337

0.810 -0,260 0.290 -0,486 0.400 -0.382 0.700 -0.319

0.840 -0.278 0.310 -0.456 0.410 -2.707** 0.750 -0.308

0.900 -0,209 0,320 -0.459 0.430 -0.435 0.800 -0.299

0.960 -0,104 0.340 -0,453 0.440 -0.401 0.830 -0.224

0.350 -0.215"* 0.460 -0.406 0.900 -0.162

0.370 -0,429 0,490 -0.365 0.960 -0.110

0.380 -0.438 0.500 -0.382

0.400 -0.373 0.520 -0.399

0.410 -0.398 0.540 -0.364

0.430 -0.377 0.550 -0.350

0.440 -0.346 0.580 -0.347

0.460 -0.360 0.600 -0.336

0.470 -0.360 0.610 -0,323

0,490 -0.353 0.650 -0.515

0.500 -0.354 0.700 -0.311

0.520 -0.338 0.750 -0.322

0.530 -0.329 0,820 -0.224

0.550 -0.362 0.890 -0.095

0.560 -0.336 0.900 -0.091

0.580 -0.312 0.960 0.008

0,590 -0.342

0,600 -0,325

0,640 -0.309

0.700 -0.307

0.750 -0.026**

0.820 -0.233

0.870 -0.181

0.930 -0.089

0.960 -0.055

Lower Surface

0.020 0.401 0.020 0,588 0.020 0.657 0.020 0,783

0. I 10 0.088 0.060 0.405 0.060 0.455 0.060 -0.013

0.230 0,111 0.090 0.312 0.090 0.367 0.1 t0 0.408

0.400 -0.013 0.120 0.226 0.120 0.138 0,250 0.073

0.490 0.003 0.200 0,161 0.200 0.176 0.400 0.019

0.630 2.617"* 0.260 0,074 0.250 0.096 0.490 -0.025

0,750 0.001 0.400 0.026 0.400 0.024 0.580 -0,071

0.850 0.030 0.490 -0.027 0.490 -0.050 0.650 -0.020

0.900 0.121 0.580 -0.050 0.580 -0.058 0.750 0.160

0.960 0.084 0.640 0.068 0,650 -0.050 0.830 0,248

0.750 0.154 0.750 0.181 0.900 0.254

0,870 0.198 0.890 0.251 0.960 0,174

0.930 0.172 0.930 0.196

0.960 0.126 0.960 0.165

CN = 0.370 0,565 0,549 0.633

56
Table C-2. Continued,

Flight 200, Wing sweep = 26 °, Time = 8-32-28-000, MINF = 0593, Camber = 5/2, ALPT = 6.06, BETA = -0.24. QINF = 293,0,

RNPU = 3.0E+06, CNWP = 0.2680

_q = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP ._c CP x./c CP x/c CP

0.020 0.069 0.000 0.778 0.000 0_967"* 0.010 -0.765

0.060 -0.144 0.020 -0.328 0.020 -0.313 0.020 -0.521 **

0.110 -0.289 0.040 -0.227 0.060 0.653** 0.060 -0.718"*

0.200 -0.286 0.060 -0.452 0.090 -0.546 0. I 10 -0.802

0.230 -0.277 0.090 -0.457 0.110 -0.717 0.140 -0.734

0.400 -0.172 O.130 -0.536 O. 130 -0.676 O. 190 .-4.056"*

0.490 -0.151 O. 150 -0.609 O. 150 -0.633 0.250 -0.433

0.590 -0.183 0,200 -0.463 0.210 -0.535 0.400 -0.352

0.630 -0.191 0.250 -0.389 0.250 -0.360 0.490 -0.311

0.700 -0.160 0.260 -0,315 0.340 -0.333 0.580 -0.281

0.750 -0.207 0.280 -0.345 0.370 -0.350 0.650 -0.302

0.810 -0.185 0.290 -0.336 0.400 -0.329 0.700 -0.295

0.840 -0.173 0.310 -0.319 0.410 -0.308 0_750 -0.309

0.900 -0. I 13 0.320 -0.307 0.430 -0.311 0.800 -0.307

0.960 -0.021 0.340 -0.283 0.440 -0.291 0.830 -0.273

0.350 -0.192** 0.460 -0.311 0.900 -0.169

0,370 -0.278 0.490 -0.243 0.960 -0.009"*

0.380 -0.314 0.500 -0.291

0.400 -0.235 0.520 -0.246

0.410 -0.297 0.540 -0,280

0.430 -0.256 0.550 -0.273

0.440 -0.215 0.580 -0.261

0.460 -0.299 0,600 -0.285

0.470 -0.273 0.610 -0.254

0.490 -0.270 0.650 0,021 **

0.500 -0.261 0.700 -0.301

0.520 -0.268 0.750 -0.345

0.530 -0.242 0.820 -0.092

0.550 -0.236 0.890 -0.147

0.560 -0.258 0.900 -0.092

0.580 -0.237 0.960 0.027

0.590 -0.283

0.600 -0.291

0.640 -0.264

0,700 -0.260

0.750 0009**

0.820 -0.193

0.870 -0.195

0.930 -0.090

0.960 -0.031

Lower Surface

0.020 -0.358 0.020 -0.212 0.020 -0.1 I0 0.020 O. 174

O. 110 -0.108 0.060 0,003 0.060 O. 105 0.060 0.018

0.230 0.001 0.090 -0.031 0.090 0.036 0.110 -0.025

0.400 -0.005 O. 120 0.006** O. 120 -0.232 0.250 -0.074

OA90 -0.004 0.200 0.018 0.200 -0.046 0.400 -0.084

0.630 O. 170 ** 0.260 -0.059 0.250 -0.017 0.490 -0.130

0.750 0.040 0.400 -0.062 0.400 -0.069 0.580 -0.154

0.850 0.097 0.490 -0.082 0.490 -0.018 0.650 -0.065

0.900 O. 188 0.580 -0.088 0.580 -0.094 0.750 O. 136

0.960 O. 146 0,640 0.04 1 0.650 0.003 0.830 0.278

0.750 O. 185 0.750 -0.019"* 0.900 0.328

0.870 O. 194 0.890 0.277 0.960 0.258

0.930 0.207 0.930 0.224

0.960 O. 163 0.960 0299

CN = 0.195 0.314 0.346 0.374

57
Table C-2. Continued.

Flight 200, Wing sweep = 26", Time = 8-32-37-500, MINF = 0.597, Camber = 5/2, ALPT = 6.96, BETA = -0.33, QINF = 295.9,

RNPU = 3.0E+06, CNWP = 0.2998

q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.1 t0 0.000 0.842 0.000 0.907** 0.010 -1.021

0.060 -0.265 0.020 -0.545 0.020 -0.528 0.020 -0.746**

0.110 -0.400 0.040 -0.396 0.060 0.528** 0.060 -0.910"*

0.200 -0.343 0.060 -0.613 0.090 -0.676 0.110 -0.922

0.230 -O 330 0.090 -0.584 0.110 -0.856 0.140 -0.775

0.400 -0.202 0.130 -0.658 0.130 -0.798 0.190 -4.012"*

0.490 -0.181 0.150 -0.710 0.150 -0.746 0.250 -0.480

0.590 -0.225 0.200 -0.534 0.210 -0.614 0.400 -0.386

0.630 -0.209 0.250 -0.459 0.250 -0.425 0.490 -0.345

0.700 -0.179 0.260 -0.369 0.340 -0.384 0.580 -0.308

0.750 -0.225 0.280 -0.403 0.370 -0.411 0.650 -0.314

0.810 -0.203 0.290 -0.385 0.400 -0.365 0.700 -0.311

0.840 -0.188 0.310 -0.370 0.410 -0.345 0.750 -0.315

0.900 -0.133 0.320 -0.349 0.430 -0.355 0.800 -0.313

0.960 -0.026 0.340 -0.330 0.440 -0.328 0.830 -0.264

0.350 -0.188"* 0,460 -0.351 0.900 -0.158

0.370 -0.307 0.490 -0.272 0.960 -0.009**

0.380 -0.357 0.500 -0.325

0.400 -0.275 0.520 -0.286

0.410 -0.321 0.540 -0.300

0.430 -0.297 0.550 -0.290

0.440 -0.234 0.580 -0.285

0.460 -0.312 0.600 -0.315

0470 -0.292 0.610 -0.301

0.490 -0.300 0.650 0.012"*

0.500 -0.290 0.700 -0.329

0.520 -0.306 0.750 -0.369

0.530 -0.270 0.820 -0.102

0.550 -0.298 0.890 -0.154

0.560 -0.296 0.900 -0. 100

0.580 -0.264 0.960 0.022

0.590 -0.311

0.600 -O.322

0.640 -0.287

0.700 -0.281

0.750 0.000"*

0.820 -0.215

0.870 -0.210

0.930 -0.102

0.960 -0.036

Lower Surface

0.020 -0.256 0.020 -0.070 0.020 0.070 0.020 0.344

0.110 -0.066 0.060 0.086 0.060 0.176 0.060 0.090

0.230 0.031 0.090 0.041 0.090 0.102 0.110 0.049

0.400 0.002 0.120 0.034" * 0.120 -0.178 0.250 -0.035

0.490 -0.005 0.200 0.053 0.200 -0.020 0.400 -0.055

0.630 0.174"* 0.260 -0.024 0.250 0.019 0.490 -0.108

0.750 0.031 0.400 -0.048 0.400 -0.042 0.580 -0.141

0.850 0.094 0.490 -0.070 0.490 -0.012 0.650 -0.046

0.900 0.169 0.580 -0.076 0.580 -0.087 0.750 0.146

0.960 0.132 0.640 0.043 0.650 0.002 0.830 0.276

0,750 O. 183 0.750 -0.027** 0.900 0.322

0.870 0.197 0.890 0.280 0.960 0.246

0.930 0.215 0.930 0.221

0.960 0.156 0.960 0.767

CN = 0.24t 0.384 0.407 0.430

58
Table C-2 Continued.

Flight 200, Wing sweep = 26 °. Time = 8-32-48-000, MINF = 0.605, Camber = 5/2, ALPT = 8.02, BETA = -0.10, QINF = 304.3,

RNPU = 3.1E+06, CNWP = 0.3360

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,363 0.000 0.825 0.000 0.850** 0,010 - 1.690

0.060 -0.394 0.020 -0.937 0.020 -0.880 0.020 - 1.031 **

0,110 -0.454 0.040 -0.625 0.060 0.247"* 0.060 -1.109"*

0.200 -0.392 0.060 -0.807 0.090 -0.850 0.110 - 1,087

0,230 -0.299 0.090 -0.752 0.110 -1.015 0.140 -0.906

0.400 -0.230 0.130 -0.811 0.130 -0.959 0.190 -3.898"*

0.490 -0.209 0.150 -0.844 0.150 -0,847 0.250 -0.533

0.590 -0.247 0.200 -0.659 0.210 -0.713 0.400 -0.414

0.630 -0.231 0.250 -0.530 0.250 -0.496 0.490 -0.356

0.700 -0.193 0.260 -0.437 0.340 -0.430 0.580 -0.317

0.750 -0.243 0.280 -0.466 0.370 -0,443 0.650 -0.326

0.810 -0.216 0.290 -0.445 0.400 -0.410 0.700 -0.310

0.840 -0.209 0.310 -0.419 0.410 -(3.386 0.750 -0.303

0.900 -0.151 0.320 -0.406 0.430 -0.394 0.800 -0.287

0.960 -0.054 0.340 -0.378 0.440 -0.357 0.830 -0.245

0.350 -0.191"* 0.460 -0.376 0.900 -0.115

0.370 -0,364 0.490 -0.291 0.960 -0.006"*

0.380 -0.398 0.500 -0.355

0.400 -0.308 0.520 -0.309

0.410 -0,374 0.540 -0.329

0.430 -0,332 0.550 -0.317

0.440 -0.282 0.580 -0.326

0.460 -0.350 0.600 -0,339

0.470 -0.332 0.610 -0.316

0.490 -0.328 0.650 0.015"*

0,500 -0.311 0.700 -0,372

0,520 -0.325 0.750 -0.374

0.530 -0.295 0.820 -0.102

0.550 -0.322 0.890 -0.151

0.560 -0.309 0.900 -0.097

0.580 -0.286 0.960 0.021

0.590 -0.321

0.600 -0.334

0.64O -0.306

0.700 -0.299

0.750 0.003"*

0,820 -0.221

0.870 -0.215

0,930 -0.111

0.960 -0.039

Lower Surface

0.020 -0.111 0.020 0.132 0.020 0.234 0.020 0,532

0.110 -0.009 0.060 0.194 0.060 0.284 0.060 0.153

0.230 0.067 0.090 0.123 0.090 0.194 0.110 0.130

0.400 0,045 0.120 0.123 ** 0.120 -0.094 0.250 0,027

0.490 0.035 0.200 0.077 0.200 0.017 0.400 -0.022

0.630 0.172"* 0.260 0.023 0,250 0.072 0.490 -0.069

0.750 0.030 0.400 -0.014 0,400 -0.013 0.580 -0.104

0.850 0.077 0.490 -0.043 0,490 -0.002 0.650 -0.031

0.900 0.168 0.580 -0.056 0.580 -0.060 0.750 0.163

0.960 0.127 0.640 0.056 0.650 0.005 0.830 0.287

0.750 0.189 0.750 -0,023** 0.900 0.334

0.870 0.208 0.890 0.290 0.960 0.248

0.930 0.212 0.930 0.232

0.960 0.162 0.960 0.729

CN = 0.292 0.473 0.480 0.495

59
Table C-2. Continued.

Flight 200, Wing sweep = 26 °, Time = 8-33-10-500, MINF = 0.610, Camber = 5/2, ALPT = 12.02, BETA = 0.45, QINF = 319.0,

RNPU = 3_2E+06, CNWP = 0.4931

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0020 -2.155 0.000 0.088 0.000 0.313"* 0.010 -2.677

0.060 -0.932 0.020 -2.630 0.020 -2.403 0.020 -2.629**

0.110 -0.857 0.040 - 1.764 0,060 -0,738 ** 0.060 -2.405 **

0.200 -0.637 0,060 -2.071 0.090 -2.202 0,110 -1.120

0.230 -0.572 0.090 - 1.113 0.110 - 1.501 0.140 -0,988

0.400 -0.359 0.130 - 1.199 0,130 - I. 117 0.190 -3.842" *

0.490 -0.301 O. 150 - 1.183 O. 150 -1.004 0.250 -0.617

0.590 -0.338 0,200 -0.923 0.210 -0,880 0.400 -0,445

0,630 -0.341 0,250 -0.700 0.250 -0,628 0.490 -0,370

0,700 -0.292 0.260 -0,600 0.340 -0,527 0.580 -0.333

0.750 -0.321 0.280 -0.616 0,370 -0,495 0.650 -0.292

0.810 -0.318 0,290 -0.583 0.400 -0.458 0,700 -0.306

0.840 -0.316 0.310 -0.550 0.410 -0.438 0,750 -0.301

0.900 -0.248 0.320 -0.550 0.430 -0.437 0,800 -0.389

0.960 -0.149 0,340 -0,499 0.440 -0.389 0.830 -0.203

0.350 -0.193"* 0,460 -0.412 0,900 -0,219

0.370 -0.468 0.490 -0,347 0.960 -0.225**

0.380 -0.509 0,500 -0.377

0.400 -0.418 0,520 -0.331

0.410 -0.460 0.540 -0.330

0.430 -0.416 0,550 -0.328

0,440 -0.367 0.580 -0.318

0.460 -0.431 0,600 -0.326

0.470 -0.436 0.610 -0.305

0.490 -0,397 0.650 0.019"*

0,500 -0.380 0.700 -0.307

0.520 -0,388 0.750 -0.337

0.530 -0.353 0.820 -0.061

0.550 -0.367 0.890 -0.086

0.560 -0.362 0.900 -0.046

0,580 -0.333 0.960 0.032

0.590 -0.381

0.600 -0.369

0,640 -0,326

0.700 -0.314

0.750 0.009"*

0.820 -0.223

0.870 -0.203

0.930 -0.093

0,960 -0.031

Lower Surface

0,020 0.344 0.020 0.628 0.020 0,649 0,020 0,790

0.110 0.172 0,060 0.476 0.060 0,553 0.060 0.352

0.230 0.186 0.090 0,375 0.090 0,439 0.110 0.362

0,400 0.084 0.120 0,326** 0.120 0.152 0.250 0.198

0.490 0.049 0.200 0.185 0.200 0.126 0.400 0. I 18

0,630 1.816"* 0.260 0.180 0.250 0.236 0.490 0.038

0.750 0,030 0.400 0.095 0.400 0.108 0.580 -0.015

0,850 0.060 0.490 0.047 0.490 0.021 0,650 0.022

0,900 0.141 0.580 0.010 0.580 0.007 0,750 0.192

0,960 0.091 0,640 0.109 0.650 0,020 0.830 0,278

0.750 0.213 0.750 -0.006** 0,900 0.311

0.870 0.208 0,890 0.282 0.960 0.171

0.930 0.208 0.930 0.217

0.960 0.160 0.960 0.629

CN = 0.506 0.741 0.712 0.623

60
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 8-49-8-000, MINF = 0.600, Camber = 5/2, ALPT = 6.34, BETA = 0.80, QINF = 302.6,

RNPU = 3. IE+06, CNWP = 0.2473

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.016 0.000 0.802 0.000 0.676"* 0.010 - 1.015

0.060 -0.255 0.020 -0.228 0.020 -0.457 0.020 -0,715

0, 110 -0.409 0.040 -0.282 0.060 -0.376** 0.060 -0.865

0.200 -0.356 0.060 -0.519 0.090 -0.678 0.110 -0.897

0.230 -0.336 0.099 -0.541 0.110 -0.734 0.140 -0.750

0.400 -0.230 0.130 -0.652 0.130 -3.974* * 0.190 -3.974* *

0.490 -0.202 0.150 -0,638 0.150 -0.633 0.250 -0,507

0.590 -0.224 0.200 -0.537 0.210 -0.587 0.400 -0.415

0.630 -0.227 0.250 -0.406 0.250 -0.483 0.490 -0.333

0.700 -0.249 0.260 -0.411 0.340 -0.431 0.580 -0.307

0.750 -0.228 0.280 -0.398 0.370 -0.413 0.650 -0.372

0.810 -0.187 0.290 -0.381 0,400 -0.345 0.700 -0.331

0.840 -0.224 0.310 -0.363 0.410 0.487" * 0.750 -0.333

0.900 -0.153 0.320 -0.381 0.430 -0.380 0.8130 -0.281

0.960 -0.032 0.340 -0.359 0.440 -0.368 0.830 -0.281

0.350 -0.132"* 0.460 -0,355 0.900 -0.186

0,370 -0.346 0.490 -0.3 zl'4 0.960 -0.021

0.380 -0.354 0.500 -0.346

0.400 -0.330 0.520 -0.359

0.410 -0.321 0.540 -0.343

0.430 -0,298 0.550 -0.318

0.4.40 -0.298 0.580 -0.309

0.460 -0.292 0.600 -0.328

0.470 -0.320 0.610 -0.330

0.490 -0.313 0.650 -0.420

0.500 -0.306 0.700 -0.340

0.520 -0.295 0.750 -0.309

0.530 -0.2% 0.820 -0.301

0.550 -0.323 0.890 -0.150

0.560 -0.322 0.900 -0. ! 25

0,580 -0.274 0.960 0,001

0.590 -0.317

0.600 -0.291

0.640 -0.323

0.700 -0.303

0.750 -0.056"*

0.820 -0.270

0.870 -0.230

0.930 -0.114

0.960 -0.052

Lower Surface

0.020 -0.322 0.020 -0.137 0.020 0012 0.020 0.253

O. 110 -0.103 0.060 0.036 0.060 0.098 0.060 -0.009

0.230 0.005 0.090 0.018 0.090 0,063 0.110 0.112

0.400 -0.038 0.120 -0.005 0.120 0.000 0.250 -0,089

0.490 -0.030 0.200 0.002 0.200 0,038 0.400 -0.107

0.630 1.900"* 0.260 -0.012 0.250 -0.057 0.490 -0.116

0.750 0.001 0.400 -0.053 0.400 -0.081 0.580 -0.163

0.850 0.029 0.490 -0.080 0.490 -0.058 0.650 -0.070

0.900 0.122 0.580 -0. 108 0.580 -0.138 0.750 0.133

0.960 0.108 0.640 0.028 0.650 -0.050 0.830 0.232

0.750 0.134 0.750 -0.015 0.900 0.278

0.870 0.201 0.890 0.264 0.960 0.222

0,930 0.175 0.930 0.209

0.960 0.128 0.960 0.216

CN = 0.224 0.360 0.374 0.428

61
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 8-49-55-500, MINF = 0.601, Camber = 5/2, ALPT = 7.05, BETA = -0.10, QINF = 302.8,

RNPU = 3. IE+06, CNWP = 0.2768

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0,020 -0.152 0.000 0.813 0.000 0.687"* 0.010 - 1.306

0.060 -0.303 0.020 -0.455 0.020 -0.656 0.020 -0.871

0.1 I 0 -0.459 0.040 -0.417 0,060 -0.455"* 0,060 -0.991

0.200 -0.395 0.060 -0.643 0.090 -0.782 O. 110 -0.966

0.230 -0.375 0.090 -0.628 O.110 -0.825 O. 140 -0.813

0.400 -0.239 0.130 -0.718 0.130 -3.960"* 0.190 -3.960"*

0.490 -0.203 0.150 -0.716 0.150 -0.693 0.250 -0.536

0.590 -0.237 0.200 -0.601 0.210 -0,644 0.400 -0.437

0,630 -0.240 0.250 -0.446 0.250 -0.521 0.490 -0,344

0.700 -0.262 0.260 -0.447 0.340 -0,447 0,580 -0.319

0.750 -0.249 0.280 -0.417 0.370 -0.446 0.650 -0.373

0.810 -0.203 0.290 -0.409 0.400 -0.383 0.700 -0.333

0.840 -0.240 0.310 -0.393 0.410 0.500** 0.750 -0.327

0.900 -0.165 0.320 -0.413 0.430 -0.397 0.800 -0.275

0.960 -0.048 0.340 -0,388 0,440 -0.390 0.830 -0.274

0.350 -0.134"* 0.460 -0.373 0.900 -0.170

0.370 -0.373 0.490 -0.353 0,960 -0.015

0.380 -0.383 0.500 -0.352

0.400 -0.342 0.520 -0,378

0.410 -0.345 0.540 -0.344

0.430 -0.311 0.550 -0.346

0.440 -0.303 0.580 -0.328

0.460 -0.317 0.600 -0.347

0.470 -0.347 0.610 -0.345

0,490 -0.330 0.650 -0.463

0.500 -0,329 0.700 -0.374

0.520 -0.304 0.750 -0.322

0.530 -0.311 0.820 -0.316

0.550 -0.333 0.890 -0.152

0.560 -0.324 0.900 -0.127

0.580 -0.295 0.960 0.000

0.590 -0.337

0.600 -0.307

0.640 -0.338

0.700 -0.319

0.750 -0.047"*

0.820 -0.279

0.870 -0.239

0,930 -0.115

0.960 -0.054

Lower Surface

0.020 -0.199 0.020 -0.010 0.020 0.119 0.020 0.367

O. 110 -0.065 0.060 0.101 0.060 0.161 0.060 -0.011

0.230 0.025 0.090 0,068 0.090 0.118 0.110 0.140

0.400 -0.025 0.120 0.036 0.120 0.057 0.250 -0.052

0.490 -0.010 0.200 0.030 0.200 0.063 0.400 -0,073

0.630 1.911 ** 0.260 0.008 0.250 -0.022 0,490 -0.088

0,750 -0.001 0.400 -0.029 0.400 -0.063 0.580 -0.135

0.850 0.027 0.490 -0.059 0.490 -0.057 0.650 -0.046

0.900 0.120 0.580 -0.091 0.580 -0.118 0.750 0.145

0.960 0.098 0.640 0.037 0.650 -0.052 0.830 0.238

0.750 0.140 0.750 -0.017 0.900 0.282

0,870 0.209 0.890 0.276 0.960 0.223

0.930 0.176 0.930 0.218

0.960 0.133 0.960 0.222

CN = 0.257 0.413 0.423 0.473

62
Table C-2, Continued.

Flight 216, Wing sweep = 26 °, Time = 8-50-12-000, MINF = 0.600, Camber = 5/2, ALPT = 7,98, BETA = 0.37, QINF = 300.2,

RNPU = 3.1E+06, CNWP = 0,3120

r I = 0.93 0.76 0.59 0.40

Upper Surface

xA" CP x/c CP x/c CP x/c CP

0.020 -0.380 0.000 0.749 0.000 0.528" * 0.010 - 1.947

0.060 -0.460 0.020 -0.770 0,020 -1.016 0,020 - 1.091

0.110 -0.557 0.040 -0.642 0.060 -0.650 ** 0.060 - 1.212

0.200 -0.459 0.060 -0.823 0.090 -0.949 0,110 - 1.106

0,230 -0.400 0.090 -0.784 0.1 | 0 -0.983 0.140 -0.922

0.4130 -0.283 0.130 -0.865 0,130 -3.969* * 0,190 -3,969* *

0.490 -0.242 0.150 -0.835 0.150 -0.812 0.250 -0.600

0.590 -0,270 0.200 -0.695 0.210 -0,727 0.400 -0,459

0.630 -0,269 0.250 -0.517 0.250 -0.594 0.490 -0.370

0,700 -0.269 0.260 -0.523 0.340 -0,500 0.580 -0,337

0.750 -0.266 0.280 -0.495 0.370 -0.493 0,650 -0,376

0.810 -0.223 0,290 -0.460 0.400 -0,442 0.700 -0.339

0.840 -0.269 0.310 -0.446 0.410 0.528"* 0.750 -0.334

0.900 -0.193 0.320 -0.469 0.430 -0.449 0.800 -0.268

0.960 -0,080 0.340 -0.436 0.440 -0A28 0.830 -0.248

0,350 -0.145 ** 0.460 -0.408 0.900 -0.157

0,370 -0.421 0.490 -0.405 0.960 -0,027

0,380 -0.412 0.500 -0.387

0.400 -0.393 0.520 -0.402

0.410 -0.387 0.540 -0,378

0.430 -0.347 0,550 -0.363

0.440 -0.352 0.580 -0,353

0.460 -0.359 0_600 -0.358

0.470 -0.361 0,610 -0.35 l

0.490 -0.365 0.650 -0.471

0.500 -0.358 0.700 -0,378

0.520 -0.334 0.750 -0.340

0.530 -0,343 0.820 -0.322

0.550 -0.353 0.890 -0.161

0.560 -0.353 0,900 -0.132

0.580 -0.322 0.960 0.006

0.590 -0.361

0.600 -0.328

0.640 -0.361

0.700 -0.344

0.750 -0.056**

0.820 -0.296

0.870 -0.252

0,930 -0.132

0.960 -0.070

Lower Surface

0.020 -0.037 0.020 0,150 0.020 0.285 0.020 0.490

0.110 -0.023 0.060 0.188 0,060 0.250 0.060 -0.015

0.230 0.055 0.090 0,154 0,090 0,183 0.110 0.208

0.400 -0,022 0.120 0.098 0.120 0.119 0.250 -0.017

0.490 -0,029 0.200 0.051 0.200 0.079 0.400 -0.049

0.630 1.952'* 0.260 0.061 0,250 0.017 0.490 -0.063

0.750 -0.013 0.400 -0.011 0.400 -0.038 0.580 -0.106

0,850 0,012 0.490 -0.044 0.490 -0.057 0,650 -0,051

0.900 0,100 0.580 -0.084 0.580 -0.102 0.750 O. 142

0,960 0.087 0.640 0.037 0.650 -0.028 0,830 0,250

0.750 0.138 0.750 -0,007 0,900 0,274

0.870 0.197 0,890 0.282 0.960 0.206

0,930 0,167 0.930 0.223

0.960 0.116 0.960 0,192

CN = 0.302 0.491 0.492 0.533

63
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 8-50-29-500, MINF = 0.606, Camber = 5/2, ALPT = 10.08, BETA = 0.43, QINF = 309.1,

RNPU = 3, IE+06, CNWP = 0,3242

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.857 0.000 0.423 0,000 0,298** 0.010 -2.275

0.060 -0.725 0.020 - 1.750 0.020 -2.201 0,020 -2.331

0. 110 -0.697 0.040 -0,323 0,060 -0,995** 0.060 -1,378

0.200 -0.577 0.060 - 1.227 0.090 - 1,233 0.110 - 1,223

0.230 -0.524 0.090 - 1.074 0. I I0 - 1.258 0.140 -0,995

0,400 -0.333 0.130 - 1,128 0.130 -3,888 * * 0.190 -3.888 **

0.490 -0.284 0.150 - 1,032 0.150 -0.962 0.250 -0.574

0,590 -0.303 0.200 -0.845 0.210 -0,855 0.400 -0.485

0.630 -0.310 0.250 -0.615 0.250 -0,675 0.490 -0.374

0.700 -0.319 0.260 -0.604 0,340 -0.565 0,580 -0.305

0,750 -0.301 0.280 -0.576 0.370 -0.533 0,650 -0.343

0.810 -0.264 0.290 -0,551 0.400 -0.450 0.700 -0.307

0.840 -0.311 0,310 -0.516 0.410 0.480** 0.750 -0,302

0.900 -0.235 0.320 -0,541 0.430 -0.486 0.800 -0,258

0.960 -0.111 0.340 -0.500 0.440 -0,463 0.830 -0.215

0,350 -0.149"* 0,460 -0.439 0.900 -0.148

0,370 -0.472 0.490 -0.415 0.960 -0.098

0.380 -0.486 0,500 -0.399

0.400 -0,445 0.520 -0.417

0.410 -0.432 0.540 -0.412

0.430 -0.399 0,550 -0.372

0.440 -0.395 0,580 -0.354

0.460 -0.396 0.600 -0.386

0.470 -0.410 0.610 -0,372

0.490 -0.397 0.650 -0488

0,500 -0.389 0.700 -0.376

0.520 -0.362 0.750 -0.333

0.530 -0.373 0.820 -0.295

0.550 -0.396 0,890 -0.141

0.560 -0,389 0.900 -0.111

0,580 -0,342 0.960 0.008

0.590 -0.380

0.600 -0.330

0.640 -0.377

0.700 -0.355

0.750 -0.035"*

0.820 -0.302

0870 -0.247

0.930 -0.127

0.960 -0.060

Lower Surface

0,020 0.212 0,020 0,436 0.020 0.483 0.020 0.683

0, I 10 0,074 0,060 0.343 0.060 0.393 0.060 0.008

0.230 0.124 0.090 0.277 0,090 0,322 0.110 0,323

0.400 0,012 O. 120 O. 195 O. 120 0.232 0.250 0.082

0.490 0.023 0.200 O. 121 0.200 O.151 0.400 0.024

0.630 1.862"* 0.260 0.131 0.250 0.110 0.490 -0.003

0.750 -0.001 0.400 0.048 0.400 0.029 0.580 -0.065

0.850 0.008 0.490 0.009 0.490 -0.034 0.650 -0.013

0.900 O. 104 0.580 -0.045 0.580 -0.069 0.750 O.169

0.960 0.074 0.640 0.073 0.650 -0.047 0.830 0.238

0.750 O. 164 0.750 -0.012 0.900 0.277

0.870 0.214 0.890 0.275 0.960 O. 182

0.930 0.191 0.930 0.218

0.960 O. 135 0.960 O. 193

CN = 0413 0,624 0.586 0.630

64
Table C-2. Continued.

Flight 213. Wing sweep = 26", Time = 8-19-36-500, MINF = 0,598, Camber = 5/10, ALPT = 3.48, BETA = 0.14. QINF = 298.8,

RNPU = 3. I E+06, CNWP = 0,3733

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x,/c CP x/c CP

0,020 0.248 0.000 0.534 0.000 0.554** 0.010 -0.297

0.060 -0.062 0.020 O.110 0.020 0.026 0.020 -0.278

O, I I0 -0.235 0.040 0.024 0.060 -0.090** 0.060 -0.523

0.200 -0.293 0.060 -0.244 0.090 -0.429 O. 110 -0.635

0.230 -0.305 0.090 -0.331 0.110 -0.508 0.140 -0.600

0.400 -0.257 0.130 -0.453 0.130 -3.993 * * 0.190 -3.993 * *

0.490 -0,257 0.150 -0,503 0.150 -0.515 0.250 -0.412

0.590 -0.356 0.200 -0.436 0.210 -0.475 0.400 -0.389

0,630 -0.390 0.250 -0.369 0.250 -0.406 0.490 -0.349

0,700 -0.504 0.260 -0.358 0.340 -0.404 0.580 -0.399

0.750 -0.693 0.280 -0.369 0.370 -0.417 0.650 -0.517

0.810 -0.640 0.290 -0.360 0.400 -0.384 0.700 -0.505

0.840 -0,672 0.310 -0.348 0.410 -2.747"* 0.750 -0.641

0,900 -0.276 0.320 -0.355 0.430 -0.413 0.800 -0.728

0.960 -0,093 0.340 -0.353 0,440 -0.396 0.830 -0.705

0.350 -0.170"* 0.460 -0.404 0.900 -0.198

0.370 -0.345 0.490 -0.377 0.960 -0. 117

0.380 -0.373 0.500 -0.422

0.400 -0.317 0.520 -0.431

0,410 -0.363 0.540 -0.425

0.430 -0.354 0.550 -0.415

0440 -0.340 0.580 -0.419

0,460 -0.350 0.600 -0.448

0.470 -0.378 0.610 -0.479

0.490 -0.375 0.650 -0.698

0.500 -0.386 0.700 -0.592

0.520 -0.375 0.750 -0.647

0.530 -0.389 0.820 -0.717

0.550 -0.419 0.890 -0,187

0.560 -0.421 0.900 -0.173

0.580 -0.400 0.960 -0.091

0.590 -0.451

0.600 -0.455

0.640 -0.585

0.700 -0.642

0.750 -0.040"*

0.820 -0.550

0.870 -0.439

0.930 -0,294

0960 -0.212

Lower Surface

0.020 -0.508 0.020 -0,444 0.020 -0.345 0,020 -0.149

0. I 10 -0.153 0.060 -0.105 0.060 -0.055 0,060 0.008

0.230 -0.031 0,090 -0.087 0,090 -0.050 0.110 -0.082

0400 0.008 O. 120 -0.054 O. 120 -0,155 0.250 -0.139

0.490 0.054 0.200 -0.024 0.200 -0.025 0.400 -0.099

0.630 1.362"* 0.260 -0.027 0.250 -0.069 0.490 -0.078

0.750 O. 168 0.400 -0.003 0.400 -0.035 0.580 -0.037

0.850 0.212 0.490 0.017 0,490 -0,049 0.650 0.103

0.900 0.303 0.580 0,054 0.580 0.023 0.750 0.318

0.960 0.194 0.640 0.257 0.650 -0.055 0.830 0.396

0.750 0.31 I 0.750 0.344 0.900 0.452

0.870 0.388 0.890 0.440 0.960 0.307

0.930 0.322 0.930 0.359

0.960 0.220 0.960 0.336

CN = 0.380 0.504 0.501 0.498

65
Table C-2. Continued.

Flight 213, Wing sweep = 26 °, Time = 8-20-2-500, MINF = 0.608, Camber = 5/10, ALPT = 8.27, BETA = -0.04, QINF = 307.1,

RNPU = 3. IE+06, CNWP = 0.4979

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.592 0.000 0.609 0.000 0.317 * * 0.010 -2.050

0.060 -0.584 0.020 - 1.162 0.020 - 1.447 0.020 - 1.966

0.110 -0.657 0.040 -0.007 0.060 -0.682" * 0.060 - 1.526

0.200 -0.559 0.060 - 1.054 0.090 - 1.135 0.110 - 1.244

0.230 -0.541 0.090 -0.977 0.110 -I.186 0.140 -1.043

0.400 -0.385 0.130 - 1.033 0.130 -3.868"* 0.190 -3.868"*

0.490 -0.363 0.150 - 1.014 0.150 -0.956 0.250 -0.670

0.590 -0.459 0.200 -0.839 0.210 -0.870 0.400 -0.531

0.630 -0.500 0.250 -0.661 0.250 -0.698 0.490 -0.474

0.700 -0.618 0.260 -0.630 0.340 -0.628 0.580 -0.476

0.750 -0.831 0.280 -0.620 0.370 -0.598 0.650 -0.592

0.810 -0.784 0.290 -0.586 0.400 -0.538 0.700 -0.562

0.840 -0.826 0.310 -0.565 0.410 -2.656"* 0.750 -0.632

0.900 -0.371 0.320 -0.573 0.430 -0.591 0.800 -0.582

0.960 -0.191 0.340 -0.555 0.440 -0.566 0.830 -0.579

0.350 -0.193"* 0.460 -0.553 0.900 -0.218

0.370 -0.530 0.490 -0.506 0.960 -0.117

0.380 -0.560 0.500 -0.549

0.400 -0.499 0.520 -0.547

0.410 -0.525 0.540 -0.542

0.430 -0.503 0.550 -0.541

0.440 -0.484 0.580 -0.534

0.460 -0.493 0.600 -0.555

0.470 -0.526 0.610 -0.566

0.490 -0.502 0.650 -0.822

0.500 -0.517 0.700 -0,667

0.520 -0.479 0.750 -0.704

0.530 -0.500 0.820 -0.682

0.550 -0.514 0.890 -0.173

0.560 -0.540 0.900 -0.165

0.580 -0.508 0.960 -0.112

0.590 -0.554

0.600 -0.551

0.640 -0.672

0.700 -0.719

0.750 -0.019"*

0.820 -0.604

0.870 -0.453

0.930 -0.242

0.960 -0.187

Lower Surface

0.020 0.099 0.020 0.340 0.020 0.408 0.020 0.590

0. 110 0.058 0.060 0.288 0.060 0.351 0.060 0.039

0.230 O. 140 0.090 0.238 0.090 0.292 O. 110 0.271

0.400 0.071 O.120 O.192 O.120 O.149 0.250 0.077

0.490 0.094 0.200 O.139 0.200 O. 155 0.400 0.04 1

0.630 1.342"* 0.260 O. 128 0.250 O. 134 0.490 0.049

0.750 0.156 0.400 0.108 0.400 0.098 0.580 0.043

0.850 0.176 0.490 0.106 0.490 -0.003 0.650 0.178

0.900 0.263 0.580 0.113 0.580 0.110 0.750 0.368

0.960 0.136 0.640 0.295 0.650 -0.044 0.830 0.447

0.750 0.323 0.750 0.366 0.900 0.499

0.870 0.404 0.890 0.470 0.960 0.338

0.930 0.319 0.930 0.376

0.960 0.220 0.960 0.333

CN = 0.618 0.815 0.804 0.834

66
Table C-2 Continued.

Flight 213, Wing sweep = 26 °, Time = 8-20-18-500, MINF = 0.61 I, Camber = 5/10, ALPT = 10.02, BETA = 0.11, QINF = 329.1,

RNPU = 3.3E+06. CNWP = 0,4791

"0 = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x./c CP

0.020 -0.977 0.000 0.261 0.000 0.110** 0,010 -2.344

0.060 -0.836 0.020 -2.137 0.020 -2.255 0.020 -2.396

O. 110 -0.826 0.040 - 1.103 0.060 - 1.181 ** 0.060 -2.207

0.200 -0,671 0.060 - 1.390 0.090 - 1,251 0.110 - 1.268

0.230 -0.672 0.090 - 1.247 0.110 - 1,323 0.140 - 1.102

0,400 -0,451 0.130 -1.303 0.130 -3,827** 0.190 -3.827**

0.490 -0.398 0,150 - 1.187 0.150 - 1.074 0.250 -0,685

0.590 -0.512 0.200 -0.967 0.210 -0,980 0.400 -0,561

0.630 -0.561 0.250 -0,749 0.250 -0.769 0,490 -0.506

0.700 -0.678 0.260 -0.712 0,340 -0.664 0,580 -0.502

0,750 -0,885 0.280 -0.704 0.370 -0,648 0.650 -0.540

0.810 -0.848 0.290 -0.656 0.400 -0.592 0.700 -0.521

0.840 -0.920 0.310 -0,638 0.410 -2.696"* 0.750 -0.562

0.900 -0.408 0.320 -0.638 0.430 -0.617 0.800 -0.532

0.960 -0.248 0,340 -0.621 0.440 -0.592 0.830 -0.448

0,350 -0.206** 0.460 -0,579 0.900 -0.260

0.370 -0.580 0,490 -0.544 0,960 -0,209

0.380 -0.614 0,500 -0.572

0.400 -0.551 0,520 -0.562

0.410 -0.570 0.540 -0.562

0.430 -0.547 0.550 -O541

0.440 -0.526 0.580 -0.544

0.460 -0.540 0.600 -0.579

0.470 -0.544 0.610 -0.572

0.490 -0.541 0,650 -0.841

0.500 -0.544 0,700 -0.658

0.520 -0.535 0.750 -0.687

0.530 -0.536 0.820 -0.622

0.550 -0.569 0.890 -0.176

0.560 -0,571 0.900 -0.165

0.580 -0.535 0.960 -0.116

0.590 -0,581

0.600 -0.568

0,640 -0.687

0.700 -0.736

0.750 -0.010"*

0,820 -0.588

0.870 -0.425

0.930 -0.211

0.960 -0.190

Lower Surface

0.020 0.287 0.020 0.581 0.020 0.548 0,020 0.707

0.1 I 0 0.120 0.060 0.399 0.060 0.44 1 0.060 0.015

0,230 0.190 0.090 0.333 0,090 0,375 0.110 0.400

0.400 0.084 0. | 20 0,257 0.120 0,239 0.250 0.140

0.490 O. 102 0.200 O. 187 0.200 O. 190 0.400 O. 102

0.630 1.036"* 0.260 O. 193 0.250 O. 190 0.490 0.084

0.750 0.146 0,400 0,143 0.400 0,132 0.580 0.089

0.850 0.161 0.490 0.127 0,490 -0.050 0.650 0,194

0,900 0.246 0.580 0,130 0.580 0.127 0,750 0.383

0.960 0.107 0,640 0,300 0.650 -0.030 0.830 0.450

0.750 0.327 0.750 0.386 0.900 0.495

0.870 0.403 0.890 0,469 0.960 0,311

0.930 0.306 0.930 0.372

0.960 0.206 0.960 0.299

CN = 0.716 0.945 0.859 0.922

67
Table C-2. Continued.

Flight 213, Wing sweep = 26 °. Time = 8-19-48-500, MINF = 0.598, Camber = 5/11, ALPT = 3.90, BETA = -0.65, QINF = 298.3,

RNPU = 3.1E+06, CNWP = 0.3951

rl = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.200 0.000 0.575 0.000 0,567** 0.010 -0.433

0.060 -0.085 0.020 0.058 0,020 -0.049 0.020 -0.351

0.110 -0,280 0.040 -0.036 0.060 -0.084"* 0.060 -0,596

0.200 -0.313 0.060 -0.286 0,090 -0.466 0.110 -0.671

0.230 -0.315 0.090 -0.384 0.110 -0.555 0.140 -0.646

0.400 -0.264 0,130 -0.496 0.130 -3.994"* 0.190 -3.994"*

0.490 -0.281 0.150 -0,542 0.150 -0.541 0,250 -0,457

0,590 -0.370 0.200 -0.45,4 0.210 -0.498 0.400 -0.413

0.630 -0.393 0,250 -0.404 0.250 -0.424 0.490 -0,377

0.700 -0.514 0.260 -0.388 0.340 -0.415 0.580 -0.409

0.750 -0,731 0.280 -0.382 0.370 -0.435 0.650 -0.523

0.810 -0,679 0.290 -0.387 0,400 -0.394 0,700 -0.500

0.840 -0,712 0.310 -0.376 0.410 -2,747'* 0,750 -0.644

0.900 -0.286 0.320 -0.387 0.430 -0,424 0.800 -0.717

0.960 -0.110 0,340 -0.362 0.440 -0.422 0.830 -0,725

0.350 -0,185"* 0.460 -0.410 0.900 -0.207

0.370 -0.373 0.490 -0.386 0.960 -0.127

0.380 -0.401 0.500 -0.442

0.400 -0.334 0.520 -0.458

0.410 -0.382 0.540 -0.434

0.430 -0.361 0.550 -0.423

0.440 -0.359 0.580 -0.432

0,460 -0.371 0,600 -0_469

0.470 -0.407 0.610 -0.489

0.490 -0.401 0.650 -0.721

0,500 -0.406 0.700 -0.620

0.520 -0.416 0.750 -0.680

0,530 -0.406 0.820 -0,749

0.550 -0,456 0.890 -0.201

0.560 -0.435 0,900 -0.173

0,580 -0,424 0.960 -0.128

0.590 -0.470

0.600 -0.460

0.640 -0,594

0.700 -0,667

0.750 -0.045"*

0.820 -0.545

0.870 -0.496

0,930 -0.308

0.960 -0.214

Lower Surface

0.020 -0.481 0.020 -0.391 0.020 -0.262 0.020 -0,075

0.110 -0.143 0.060 -0.088 0,060 -0.024 0.060 0.014

0.230 -0.025 0,090 -0.073 0.090 -0,029 0.110 -0.061

0.400 0.010 0.120 -0.04 1 0.120 -0.147 0,250 -0.125

0.490 0.056 0,200 -0.012 0,200 -0.014 0.400 -0.094

0.630 1.370"* 0.260 -0.011 0.250 -0.050 0.490 -0,072

0.750 0.167 0.400 0.014 0,400 -0.019 0.580 -0.022

0.850 0.218 0.490 0.030 0.490 -0,044 0,650 0.098

0.900 0.295 0,580 0.053 0,580 0.021 0,750 0.324

0,960 0,177 0.640 0.252 0.650 -0.065 0.830 0.392

0.750 0.302 0.750 0.343 0.900 0.447

0.870 0.379 0.890 0.443 0.960 0.313

0,930 0.302 0.930 0.354

0.960 0.226 0.960 0.347

CN = 0.400 0.531 0.529 0.529

68
Table C-2. Continued.

Flight 213, Wing sweep = 26 °, Time = 8-19-52-000, MINF = 0.601, Camber = 5/11, ALPT = 5.02, BETA = -0.59, QINF = 300.7,

RNPU = 3. IE+06, CNWP = 0.3888

q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x../c CP x,/c CP

0.020 0.050 0.000 0.755 0.000 0.574** 0.010 -0.776

0.060 -0.165 0.020 -0.184 0.020 -0.331 0.020 -0.558

0.1 I0 -0.363 0.040 -0.207 0.060 -0.275"* 0.060 -0.761

0.200 -0.382 0.060 -0.465 0.090 -0.614 0.110 -0.838

0.230 -0.368 0.090 -0.509 0.110 -0.694 0.140 -0.747

0.400 -0.288 0.130 -0.617 0.130 -3.959** 0.190 -3.959**

0.490 -0.265 0.150 -0.648 0.150 -0.628 0.250 -0.511

0.590 -0.383 0.200 -0.554 0.210 -0.601 0.400 -0.440

0.630 -0.421 0.250 -0.459 0.250 -0.496 0.490 -0.403

0.700 -0.540 0.260 -0.442 0.340 -0.482 0.580 -0.429

0.750 -0.738 0.280 -0.444 0.370 -0.460 0.650 -0.545

0.810 -0.669 0.290 -0.435 0.400 -0.424 0.700 -0.534

0.840 -0.725 0.310 -0.416 0.410 -2.721 ** 0.750 -0.664

0.900 -0.293 0.320 -0.427 0.430 -0.461 0.800 -0.721

0.960 -0.119 0.340 -0.417 0.440 -0.457 0.830 -0.701

0.350 -0.181 ** 0.460 -0.455 0.900 -0.188

0.370 -0.406 0.490 -0.418 0.960 -0.124

0.380 -0.435 0.500 -0.467

0.400 -0.382 0.520 -0.470

0.410 -0.416 0.540 -0.468

0.430 -0.400 0.550 -0.452

0.440 -0.387 0.580 -0.425

0.460 -0.409 0.600 -0.496

0.470 .-0.386 0.610 -0.507

0.490 -0.423 0.650 -0.726

0.500 -0.428 0.700 -0.626

0.520 -0.417 0.750 -0.678

0.530 -0.427 0.820 -0.725

0.550 -0.471 0.890 -0.181

0.560 -0.471 0.900 -0.174

0.580 -0.442 0.960 -0.116

0.590 -0.492

0.600 -0.487

0.640 -0.622

0.700 -0.684

0.750 -0.041 **

0.820 -0.594

0.870 -0.445

0.930 -0.272

0.960 -0.202

Lower Surface

0.020 -0.279 0.020 -0.160 0.020 -0.070 0.020 0.154

0.110 -0.090 0.060 0.025 0.060 0.099 0.060 0.017

0.230 0.016 0.090 0.012 0.090 0.061 0.110 0.038

0.400 0.029 0.120 0.021 0.120 -0.059 0.250 -0.063

0.490 0.089 0.200 0.018 0.200 0.024 0.400 -0.053

0.630 1.363** 0.260 0.022 0.250 -0.002 0.490 -0.038

0.750 0.165 0.400 0.029 0.400 0.009 0.580 -0.008

0.850 0.201 0.490 0.041 0.490 -0.043 0.650 0.123

0.900 0.289 0.580 0.071 0.580 0.047 0.750 0.335

0.960 0.177 0.640 0.265 0.650 -0.060 0.830 0.411

0.750 0.310 0.750 0.351 0.900 0.461

0.870 0.413 0.890 0.454 0.960 0.308

0.930 0.322 0.930 0.366

0.960 0.221 0.960 0.331

CN= 0.447 0.6_ 0.5_ 0.6_

69
Table C-2. Continued.

Flight 213, Wing sweep = 26", Time = 8-19-57-000, MINF = 0.603, Camber = 5/I 1, ALPT = 7.07, BETA = -0.36, QINF = 302.6,

RNPU = 3. IE+06, CNWP = 0.4444

q = 0,93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.324 0.000 0.764 0.000 0.473** 0.010 -1.727

0.060 -0.417 0.020 -0.758 0.020 -0.929 0.020 - 1.064

0.110 -0.533 0.040 -0.220 0.060 -0.513"* 0.060 -1.164

0.200 -0.497 0.060 -0.794 0.090 -0.934 0.110 - 1.102

0.230 -0.486 0.090 -0.798 0.110 -0.989 0.140 -0.932

0.400 -0.368 0.130 -0.891 0.130 -3.927** 0.190 -3.927"*

0.490 -0.372 0.150 -0.886 0.150 -0.858 0.250 -0,640

0.590 -0.438 0.200 -0.726 0.210 -0.769 0.400 -0.527

0.630 -0.465 0.250 -0.599 0.250 -0.637 0.490 -0.477

0.700 -0.604 0.260 -0.546 0.340 -0.562 0.580 -0.491

0.750 -0.811 0,280 -0.558 0.370 -0,574 0.650 -0.581

0.810 -0.764 0.290 -0.546 0.400 -0.524 0.700 -0.579

0.840 -0,794 0, 310 -0.526 0,410 -2.697 ** 0.750 -0.674

0.900 -0.351 0.320 -0.517 0.430 -0.541 0.800 -0.668

0.960 -0.181 0.340 -0.515 0.440 -0.514 0.830 -0.689

0.350 -0.185"* 0.460 -0.536 0.900 -0.233

0.370 -0.498 0.490 -0.490 0.960 -0.150

0.380 -0.515 0.500 -0.540

0.400 -0.460 0.520 -0.529

0.4 I0 -0.484 0,540 -0.511

0.430 -0.468 0.550 -0.515

0,440 -0.445 0.580 -0.519

0.460 -0.468 0.600 -0.531

0.470 -0.505 0.610 -0.577

0.490 -0.487 0.650 -0.808

0,500 -0.489 0.700 -0,670

0,520 -0,463 0.750 -0,714

0.530 -0.488 0.820 -0.725

0.550 -0.523 0.890 -0,204

0.560 -0.534 0.900 -0.19 l

0.580 -0.484 0,960 -0.129

0.590 -0.539

0.600 -0.540

0.640 -0669

0.700 -0.705

0.750 -0,034"*

0.820 -0.568

0.870 -0.468

0.930 -0.289

0.960 -0.237

Lower Surface

0.020 -0.057 0.020 0.157 0.020 0.239 0.020 0.472

0. 110 0.004 0.060 0.199 0.060 0.222 0.060 0.039

0.230 0.079 0.090 0.158 0.090 0.198 0,110 0.186

0,400 0.039 0.120 0.097 0.120 0.054 0.250 0.024

0.490 0,063 0.200 0.093 0.200 0.085 0.400 0.020

0.630 1.362 ** 0.260 0.079 0.250 0.064 0.490 0.021

0.750 0.145 0.400 0.062 0.400 0,046 0.580 0.029

0.850 0.187 0.490 0.081 0.490 -0.025 0.650 0.158

0,900 0.260 0.580 0.081 0.580 0.068 0.750 0.350

0.960 0.142 0.640 0.281 0.650 -0.059 0.830 0.424

0,750 0.307 0,750 0,356 0.900 0.472

0.870 0.395 0.890 0.462 0.960 0.314

0.930 0.306 0.930 0.356

0.960 0.198 0.960 0,325

CN = 0,552 0.733 0.725 0.760

70
Table C-2. Continued.

Flight 213, Wing sweep = 26 °, Time = 8-26-19-500, MINF = 0.613, Camber = 10/2, ALP'I" = 8.00, BETA = -0.15, QINF = 308.5,

RNPU = 3. IE+06, CNWP = 0.3682

q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 0.130 0.000 0.702 0,000 0.660"* 0.010 -0.646

0.060 -0.358 0.020 -0.184 0.020 -0.256 0,020 -0.606

0.110 -0.619 0.040 -0.261 0.060 -0.370** 0.060 -1.231

0.200 -0.548 0.060 -0.721 0.090 - 1.036 0,110 - 1,449

0.230 -0.472 0.090 -0,886 0. 110 - 1.276 0.140 - 1.081

0.400 -0.293 0.130 - 1,151 0.130 -3.803** 0.190 -3.803**

0.490 -0.243 0.150 - 1.177 0.150 -0.981 0.250 -0.608

0.590 -0.269 0.200 -0.852 0.210 -0.817 0.400 -0.444

0.630 -0.265 0.250 -0.587 0.250 -0.606 0.490 -0.361

0.700 -0.253 0.260 -0.532 0.340 -0.512 0.580 -0,338

0.750 -0.270 0.280 -0.534 0.370 -0.490 0.650 -0.366

0.810 -0.249 0.290 -0.500 0.400 -0.426 0.700 -0.331

0.840 -0.257 0.310 -0.475 0.410 -2.5%** 0.750 -0.335

0.900 -0.191 0.320 -0.480 0.430 -0.447 0.800 -0.291

0.960 -0.082 0.340 -0.454 0.440 -0.427 0.830 -0.257

0.350 -0.208* * 0.460 -0.418 0.900 -0.155

0.370 -0.423 0.490 -0.390 0.960 -0.044

0.380 -0.443 0.500 -0.406

0.400 -0.382 0.520 -0.401

0.410 -0.406 0.540 -0,379

0.430 -0.376 0.550 -0,378

0,440 -0.356 0.580 -0.371

0.460 -0.372 0.600 -0.36 I

0.470 -0.374 0.610 -0.366

0.490 -0.361 0.650 -0.521

0.500 -0.364 0.700 -0.381

0.520 -0.351 0.750 -0.370

0.530 -0.341 0.820 -0.316

0.550 -0.359 O.890 -0.148

0.560 -0.356 0.900 -0.142

0.580 -0.317 0.960 -0.00l

0.590 -0.353

0.600 -0.340

0.640 -0.355

0.700 -0.342

0.750 -0.040"*

0.820 -0.284

0.870 -0.241

0.930 -0.124

0.960 -0.060

Lower Surface

0.020 -0.257 0.020 -0.072 0.020 0.011 0.020 0.219

0, I 10 -0.014 0.060 0.136 0.060 0,195 0.060 -0.025

0.230 -0.008 0.090 0.112 0.090 0.172 0.110 0.153

0.400 0.001 0.120 0.128 0.120 0.067 0.250 0,018

0.490 -0.002 0.200 -0.017 0.200 -0.012 0.400 -0.037

0.630 2.376"* 0.260 0.074 0.250 0.060 0.490 -0.079

0.750 -0.001 0.400 0.001 0.400 -0.018 0.580 -0.118

0.850 0.034 0.490 -0.031 0.490 -0.052 0.650 -0.053

0.900 0.119 0.580 -0.070 0.580 -0.088 0.750 0.146

0.960 0.090 0,640 0.059 0.650 -0.052 0.830 0,244

0.750 0.148 0.750 0.178 0.900 0.280

0.870 0.199 0.890 0.264 0.960 0.207

0.930 0.180 0.930 0.214

0.960 0.138 0.960 0.265

CN = 0.3 t9 0.505 0.536 0.542

71
Table C-2. Continued,

Flight 213, Wing sweep = 26 °, Time = 8-28-35-500, MINT = 0,598, Camber = 10/11, ALPT = 3.99, BETA = -0.53, QINF = 297.3,

RNPU = 3. IE+06, CNWP = 0.4172

I1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0020 0,465 0,000 -0.139 0,000 0.385"* 0.010 0.135

0,060 -0.001 0,020 0,445 0,020 0,362 0,020 0,026

0.110 -0,339 0,040 0,218 0.060 0.002** 0,060 -0,556

0.200 -0.390 0,060 -0.192 0,090 -0,503 0.110 -0,905

0,230 -0.344 0,090 -0.430 0.110 -0.698 0.140 -0.738

0.400 -0.273 0.130 -0.646 0.130 -3.994"* 0.190 -3.994"*

0.490 -0.279 0.150 -0.752 0.150 -0.662 0,250 -0.480

0,590 -0.371 0.200 -0.591 0.210 -0.580 0.400 -0.421

0.630 -0,402 0.250 -0,444 0.250 -0,469 0.490 -0.388

0.700 -0.509 0.260 -0.431 0,340 -0,431 0.580 -0.400

0,750 -0.726 0.280 -0.410 0.370 -0.468 0.650 -0.540

0.810 -0,674 0,290 -0.401 0.400 -0.410 0.700 -0.502

0.840 -0.707 0.310 -0.401 0,410 -2.742** 0,750 -0.639

0.900 -0.277 0,320 -0.411 0,430 -0,447 0,800 -0.727

0.960 -0.089 0.340 -0.384 0.440 -0.414 0,830 -0.709

0.350 -0.207** 0,460 -0.437 0,900 -0,208

0.370 -0.389 0.490 -0.418 0,960 -0.121

0.380 -0.417 0.500 -0.438

0.400 -0.347 0,520 -0,477

0.410 -0,403 0.540 -0.436

0.430 -0,368 0.550 -0,439

0.440 -0.373 0.580 -0,434

0.460 -0.385 0,600 -0,457

0.470 -0.388 0.610 -0.491

0490 -0.392 0,650 -0,770

0.500 -0.419 0.700 -0.619

0.520 -0,402 0,750 -0.675

0,530 -0.419 0,820 -0,735

0.550 -0,458 0.890 -0.194

0.560 -0.457 0.900 -0.174

0.580 -0.411 0,960 -0.122

0.590 -0,485

0,600 -0,476

0.640 -0.593

0,700 -0.666

0.750 -0.053"*

0.820 -0.528

0.870 -0.531

0,930 -0.313

0.960 -0.230

Lower Surface

0,020 - 1.169 0.020 -0.650 0,020 -0.513 0.020 -0.573

0.110 -0.130 0.060 -0.126 0,060 -0.050 0.060 0.013

0.230 -0.033 0,090 -0.074 0.090 -0.017 0.110 -0.143

0,400 0.025 0.120 0.002 0.120 -0.113 0.250 -0,096

0,490 0.060 0.200 -0.041 0.200 -0.055 0,400 -0.072

0,630 2.417"* 0,260 0.010 0.250 -0.006 0.490 -0.058

0.750 0.160 0,400 0.010 0.400 -0.014 0,580 -0.023

0.850 0,203 0.490 0.041 0.490 -0.059 0.650 0. I 01

0.900 0.263 0.580 0.061 0.580 0.043 0,750 0.310

0.960 O. 156 0.640 0.271 0.650 -0.051 0.830 0.393

0.750 0.303 0.750 0.344 0,900 0.448

0.870 0.376 0,890 0.451 0.960 0.314

0.930 0,303 0,930 0,366

0,960 0.201 0.960 0,328

CN = 0.403 0.545 0,558 0.536

72
Table C-2. Continued.

Flight 213, Wing sweep = 26 °, Time = 8-29-21-000, MINF = 0.607, Camber = 10/10, ALPT = 7,99, BETA = -0.10, QINF = 289.4,

RNPU = 2.9E+06, CNWP = 0.5101

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.0l 1 0000 0.801 0.000 0607** 0.010 -0.727

0.060 -0.458 0.020 -0.304 0.020 -0.426 0.020 -0,750

O. 110 -0.734 0.040 -0.405 0.060 -0.495"* 0.060 -1.372

0.200 -0.659 0.060 -0.875 0.090 - 1,175 0.110 - 1.556

0.230 -0.587 0.090 - 1.049 0.110 - 1.447 0.140 - 1,231

0.400 -0,391 0,130 - 1.367 0.130 -3.880* * O. 190 -3.880"*

0.490 -0.360 0.150 - 1,383 0,150 - 1.089 0.250 -0.681

0.590 -0.453 0,200 -0991 0.210 -0,917 0.400 -0.534

0.630 -0.488 0.250 -0.701 0.250 -0.709 0.490 -0.472

0.700 -0.602 0.260 -0,653 0.340 -0,632 0.580 -0.496

0.750 -0.802 0.280 -0.644 0.370 -0.607 0.650 -0.573

0.810 -0.767 0.290 -0.6 [ 7 0.400 -0.545 0.700 -0.572

0.840 -0.813 0.310 -0,586 0,410 -2,594** 0.750 -0.635

0.900 -0.365 0.320 -0.589 0.430 -0.579 0.800 -0,602

0.960 -0.187 0340 -0.570 0.440 -0.556 0.830 -0.567

0.350 -0.235"* 0.460 -0.554 0,900 -0.217

0.370 -0.537 0.490 -0.503 0.960 -0.120

0,380 -0.574 0.500 -0,557

0.400 -0.497 0.520 -0.550

0.410 -0,530 0,540 -0.545

0.430 -0.511 0.550 -0.534

0.440 -0.486 0.580 -0.534

0.460 -0.511 0.600 -0.552

0.470 -0.510 0.610 -0.572

0.490 -0.504 0650 -0.842

0.500 -0.516 0.700 -0.660

0.520 -0.497 0.750 -0.707

0530 -0.504 0.820 -0.671

0.550 -0.539 0.890 -0.171

0.560 -0.541 0.900 -0.169

0.580 -0.503 0.960 -0.107

0.590 -0.555

0.600 -0.557

0.640 -0662

0.700 -0.716

0.750 -0.022"*

0.820 -0.612

0.870 -0.430

0.930 -0.227

0.960 -0.177

Lower Surface

0.020 -0.114 0.020 0.069 0.020 0.130 0.020 0,350

O. 110 0.058 0.060 0.242 0.060 0.291 0.060 0.043

0.230 0.057 0.090 0.198 0.090 0.258 0.110 0.212

0.400 0.082 0,120 0.198 0.120 0.123 0.250 0.095

0.490 0.098 0.200 0.051 0.200 0.043 0,400 0.053

0.630 2.706"* 0.260 0,167 0,250 0.152 0.490 0,032

0.750 0.153 0.400 0,117 0.400 0.101 0.580 0.058

0.850 0.182 0.490 0.107 0.490 -0.009 0.650 0.176

0.900 0.266 0.580 0.110 0.580 0.100 0.750 0.373

0.960 0.140 0.640 0.288 0.650 -0.037 0,830 0,428

0.750 0.325 0.750 0.375 0,900 0,498

0.870 0.401 0.890 0.463 0.960 0,333

0.930 0.329 0,930 0.367

0.960 0.216 0.960 0.344

CN = 0.610 0830 0.807 0.816

73
Table C-2, Continued.

Flight 213, Wing sweep = 26 °, Time = 8-29-59-500, MINF = 0.605, Camber = 10/10, ALPT = 10,22, BETA = 0.05, QINF = 310.3,

RNPU = 3.2E+06, CNWP = 0.6331

rl = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.381 0.000 0.759 0.000 0.435"* 0.010 - 1.515

0.060 -0.758 0.020 -0.856 0.020 -0,966 0.020 - 1,110

0110 -0.967 0.040 0.013 0.060 -0.829** 0.060 -1.848

0.200 -0.766 0,060 - 1.263 0.090 - 1.658 0.110 - 1.685

0,230 -0.690 0,090 - 1.339 0.110 - 1,607 0,140 - 1.422

0.400 -0,470 0.130 - 1,646 0,130 -3.906"* 0.190 -3.906"*

0.490 -0.418 0.150 - 1,958 0.150 - 1,902 0.250 -0.739

0.590 -0.505 0.200 - 1.317 0.210 - 1.142 0.400 -0.567

0.630 -0,557 0.250 -0.775 0.250 -0.783 0.490 -0.490

0,700 -0.681 0,260 -0.742 0.340 -0.688 0.580 -0.492

0.750 -0.874 0.280 -0.729 0,370 -0.656 0.650 -0.532

0.810 -0.822 0,290 -0,701 0.400 -0.591 0.700 -0.522

0.840 -0,904 0.310 -0,661 0.410 -2,707 * * 0.750 -0.567

0.900 -0.386 0.320 -0.655 0,430 -0,609 0.800 -0.584

0,960 -0,245 0,340 -0.645 0.440 -0,601 0.830 -0.440

0.350 -0,248** 0.460 -0.595 0,900 -0,288

0.370 -0.597 0.490 -0.525 0.960 -0.251

0.380 -0,642 0.500 -0.569

0,400 -0.562 0.520 -0.579

0.410 -0.581 0,540 -0,570

0.430 -0.556 0.550 -0.537

0.440 -0.525 0.580 -0.559

0.460 -0.549 0.600 -0.559

0.470 -0,563 0.610 -0.566

0.490 -0,546 0.650 -0.83 I

0.500 -0.550 0.700 -0.633

0.520 -0,529 0,750 -0,677

0.530 -0.537 0.820 -0.598

0.550 -0.568 0.890 -0.159

0,560 -0.569 0.900 -0,149

0.580 -0:534 0.960 -0.09 I

0.590 -0.576

0.600 -0.569

0,640 -0.674

0.700 -0,720

0.750 -0.002"*

0.820 -0.535

0,870 -0.440

0,930 -0.252

0,960 -0,201

Lower Surface

0.020 0.075 0,020 0.363 0.020 0.394 0.020 0.566

0.110 0.121 0.060 0.370 0,060 0.437 0,060 0,044

0.230 0,100 0,090 0.318 0.090 0.357 0.110 0,356

0.400 0.086 0.120 0.315 0.120 0,215 0.250 0.164

0,490 0.130 0,200 0.080 0.200 0,078 0,400 0.110

0.630 2.237** 0.260 0.230 0.250 0.217 0.490 0.097

0.750 0.141 0.400 0.167 0.400 0A60 0.580 0.100

0.850 0.172 0.490 0,146 0.490 0.010 0.650 0.203

0.900 0.246 0.580 0.132 0.580 0,143 0,750 0.375

0.960 0.110 0,640 0.315 0,650 -0,017 0.830 0.440

0.750 0.325 0.750 0.375 0.900 0,496

0.870 0.419 0.890 0.464 0,960 0.311

0,930 0.321 0.930 0.367

0.960 0.216 0.960 0.349

CN = 0.718 0.954 0.950 0.917

74
Table C-2. Continued.

Flight 222, Wing sweep = 26 °, Time = 9-37-53-000, MINF = 0.608, Camber = 10/10, ALPT = 12.14, BETA = -0.24, QINF = 307.4,

RNPU = 3. IE+06, CNWP = 0.5239

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP xA- CP

0.020 -0.854 0.000 0.503 0.000 5.963"* 0.010 - 1.728

0.060 - 1.045 0.020 - 1.340 0.020 - 1.406 0.020 - 1.868

0.110 -1.138 0.040 -1.154 0.060 -1.322"* 0,060 -1.908

0.200 -0.867 0.060 - 1.573 0.090 - 1.964 0.110 - 1.658

0.230 -0.696 0.090 - 1.793 0.110 -2.101 0.140 - 1.296

0.400 -0.489 0.130 - 1.572 0.130 -2.084 0.190 -3.868 * *

0.490 -0.435 0.150 - 1.958 0.150 - 1.579 0.250 -0.714

0.590 -0.554 0.200 - 1.494 0.210 - 1.442 0.400 -0.527

0.630 -0.595 0.250 -0.809 0.250 -0.891 0.490 -0.444

0.700 -0.720 0,260 -0.751 0.340 -0.691 0,580 -0.400

0.750 -0.900 0.280 -0.731 0.370 -0.635 0.650 -0.483

0.810 -0.867 0.290 -0.697 0.400 -0.563 0.700 -0.472

0.840 -0.930 0.310 -0.671 0.410 0,577"* 0.750 -0.483

0,900 -0.370 0.320 -0.673 0.430 -0.596 0.800 -0.530

0.960 -0.281 0.340 -0.659 0.440 -0.568 0.830 -0.395

0.350 -0.277** 0.460 -0.550 0.900 -0.396

0.370 -0.598 0.490 -0.495 0.960 -0.345

0.380 -0.642 0.500 -0.543

0.400 -0.463 0.520 -0.547

0.410 -0.595 0.540 -0.530

0.430 -0.568 0.550 -0.478

0.440 -0.534 0.580 -0.458

0.460 -0.561 0.600 -0.530

0.470 -0.570 0.610 -0.514

0 490 -0.542 0.650 4.626"*

0.500 -0.555 0.700 --0.567

0.520 -0.537 0.750 -0.567

0.530 -0.531 0.820 -0.485

0.550 -0.568 0.890 -0.207

0.560 -0.587 0.900 -0.182

0.580 -0.541 0.960 -0.118

0.590 -0.603

0.600 -0.565

0.640 -0.641

0.700 -0.690

0.750 -0.012"*

0.820 -0.524

0.870 -0.414

0.930 -0.195

0.960 -0.169

Lower Surface

0.020 0.313 0.020 0.501 0.020 0.569 0.020 0.688

0. 110 0211 0.060 0.469 0.060 0.530 0.060 4.357**

0.230 0.127 0.090 0.394 0.090 0.738** 0.110 0.493

0.400 0. I 17 0.120 0.395 0,120 0.386 0.250 0.236

0.490 0.151 0.200 0.128 0.200 0.137 0.400 0.186

0.630 1.479"* 0.260 0.307 0.250 0.294 0.490 0.147

0.750 0.135 0.400 0.202 0.400 0.180 0,580 0.121

0.850 0.167 0,490 0.167 0.490 0.029 0.650 0.238

0.900 0.248 0.580 0.167 0.580 0.177 0.750 0.379

0.960 0.095 0.640 0.323 0.650 -0.023 0.830 0.483

0.750 0.33 l 0.750 0.122 0.900 0.506

0.870 0.419 0.890 0.469 0.960 0.299

0.930 0.315 0.930 0.375

0.960 0.201 0.960 0.492"*

CN = 0.795 1.044 0.947 0.977

75
Table C-2. Continued.

Flight 216, Wing sweep = 26". Time = 8-52-13-500, MINF = 0.602, Camber = 5/6, ALPT = 5.01, BETA = 0.51, QINF = 304.2,

RNPU = 3. IE+06, CNWP = 0.2997

rl = 0,93 0,76 0.59 0.40

Upper Surface

x/c CP xYc CP x/c CP x/c CP

0.020 0.117 0.000 0.727 0.000 0.723** 0.010 -0.657

0.060 -0.157 0.020 -0.035 0,020 -0.220 0.020 -0.493

0.110 -0.316 0.040 -0_ 132 0.060 -0.320"* 0.060 -0.693

0.200 -0.331 0.060 -0.386 0.090 -0.564 0.110 -0.773

0.230 -0.330 0.090 -0.461 0,110 -0.636 0.140 -0.671

0.400 -0,250 0.130 -0.555 0.130 -3.944** 0.190 -3.944**

0.490 -0,228 0.150 -0.580 0.150 -0.565 0.250 -0.495

0.590 -0.290 0.200 -0,495 0.210 -0.542 0.400 -0.417

0.630 -0.313 0.250 -0.394 0.250 -0.457 0.490 -0,350

0.700 -0.396 0.260 -0.406 0.340 -0.435 0,580 -0.369

0,750 -0.474 0.280 -0.390 0.370 -0.434 0.650 -0.462

0.810 -0.396 0.290 -0,396 0.400 -0.364 0.700 -0.418

0.840 -0.442 0.310 -0,363 0A 10 0.494"* 0.750 -0.494

0.900 -0.233 0.320 -0.386 0.430 -0.414 0.800 -0.496

0.960 -0.071 0.340 -0.382 0,440 -0,393 0.830 -0,522

0.350 -0.145"* 0.460 -0.390 0.900 -0.242

0.370 -0.379 0.490 -0.386 0,960 -0.021

0.380 -0.374 0.500 -0.390

0.400 -0.348 0.520 -0.417

0.410 -0.350 0.540 -0.412

0.430 -0.319 0.550 -0.391

0.440 -0.33 t 0.580 -0,385

0.460 -0.351 0.600 -0.416

0.470 -0,365 0.610 -0.424

0490 -0358 0.650 -0.559

0.500 -0.356 0.700 -0.488

0.520 -0.339 0.750 -0.488

0.530 -0.355 0.820 -0.546

0.550 -0.396 0.890 -0,225

0.560 -0.383 0.900 -0.189

0.580 -0.354 0960 -0.010

0,590 -0.406

0.600 -0.387

0.640 -0.474

0.700 -0.499

0.750 -0.036"*

0.820 -0.501

0,870 -0.389

0.930 -0.174

0.960 -0.097

Lower Surface

0.020 -0.354 0,020 -0.258 0.020 -0.149 0.020 0.093

0.110 -0.112 0.060 0.003 0.060 0,030 0,060 0.014

0,230 0.005 0.090 -0.014 0.090 0.019 0.110 0.025

0.400 -0.004 0.120 -0.018 0.120 -0.045 0.250 -0.1 04

0.490 0.023 0,200 0.004 0.200 0.028 0.400 -0.091

0.630 1.898"* 0.260 -0.006 0.250 -0.048 0,490 -0.091

0.750 0.092 0.400 -0.008 0,400 -0,057 0.580 -0.080

0.850 0.124 0.490 -0015 0.490 -0.046 0.650 0,016

0.900 0.221 0.580 -0.027 0.580 -0.043 0.750 0.244

0,960 0.155 0.640 0.148 0.650 -0,055 0.830 0.333

0.750 0.224 0.750 -0.006 0.900 0,374

0.870 0,323 0.890 0,385 0.960 0.282

0,930 0.265 0.930 0.315

0.960 0.197 0.960 0,293

CN = 0.317 0.464 0.442 0.487

76
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 8-52-45-500, MINF = 0.588_ Camber = 5/6, ALPT = 8.00, BETA = 0.37, QINF = 281.1,

RNPU = 2.9E+06, CNWP = 0.3856

rI = 0.93 036 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c" CP

0.020 -0.472 0.000 0.685 0.000 0.497** 0.010 -2.058

0.060 -0.527 0.020 -0.935 0.020 - 1.185 0.020 -1.165

0.110 -0.538 0.040 -0.734 0.060 -0.708"* 0,060 -1.295

0,200 -0.519 0.060 -0.917 0.090 - 1.025 0. | I0 - 1.158

0.230 -0.482 0,090 -0.866 O 110 - 1,068 0.140 -0.979

0.400 -0.338 0.130 -0.949 0.130 -4,133"* 0,190 -4.133"*

0.490 -0.316 0.150 -0.908 0.150 -0.868 0,250 -0.642

0.590 -0.371 0.200 -0.764 0.210 -0.792 0.400 -0.513

0.630 -0.395 0.250 -0.589 0.250 -0.652 0.490 -0.421

0.700 -0.468 0.260 -0,572 0.340 -0.570 0.580 -0.404

0,750 -0.530 0.280 -0,567 0.370 -0.566 0,650 -0.487

0,810 -0.477 0.290 -0,539 0.400 -0.491 0.700 -0.461

0,840 -0.536 0.310 -0.510 0.410 0.670"* 0.750 -0.491

0.900 -0.330 0.320 -0.537 0.430 -0.515 0.800 -0.435

0.960 -0,163 0.340 -0.508 0.440 -0.501 0.830 -0.449

0.350 -0.161 ** 0.460 -0.486 0,900 -0.191

0.370 -0.487 0,490 -0.453 0.960 -0.062

0.380 -0.504 0.500 -0,479

0,400 -0.469 0,520 -0.493

0.410 -0.462 0.540 -0.476

0.430 -0.431 0,550 -0.461

0.440 -0.450 0.580 -0.463

0.460 -0.441 0.600 -0.482

0.470 -0.458 0.610 -0.489

0.490 -0.455 0.650 -0.628

0.500 -0.448 0.700 -0,535

0,520 -0.428 0.750 -0.531

0.530 -0.440 0.820 -0.555

0.550 -0.464 0.890 -0.209

0.560 -0.494 0,900 -0.170

0.580 -0.434 0.960 -0.017

0.590 -0.484

0.600 -0.453

0.640 -0.539

0.700 -0.554

0.750 -0.046"*

0.820 -0.541

0.870 -0.415

0.930 -0.195

0.960 -0.120

Lower Surface

0.020 0.047 0.020 0,204 0.020 0.334 0,020 0.541

0.110 0.020 0.060 0.241 0.060 0.298 0.060 0.029

0,230 0.096 0.090 0,191 0.090 0,235 0, 110 0.267

0.400 0.025 0.120 0.134 0.120 0.152 0.250 0.026

0490 0.050 0.200 0.095 0.200 0.129 0.400 0.008

0,630 2.190"* 0.260 0,103 0,250 0.071 0,490 0,009

0.750 0.072 0.400 0,049 0.400 0.030 0.580 -0.020

0.850 0.090 0.490 0,029 0,490 -0.044 0.650 0.078

0.900 0.183 0.580 0.020 0.580 0.006 0.750 0.267

0.960 0.110 0.640 0.177 0.650 -0,031 0.830 0.351

0.750 0,235 0.750 0.037 0,900 0.395

0.870 0.314 0.890 0.388 0.960 0.277

0,930 0.253 0,930 0.307

0,960 0.180 0.960 0.266

CN = 0.466 0.682 0.637 0.685

77
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 8-54-28-000, MINF = 0.596, Camber --. 5/6, ALPT = 10.05, BETA = 0.19, QINF = 296.6,

RNPU = 3. I E+06, CNWP = 0.3976

'11= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.971 0.000 0.291 0.000 0.283"* 0.010 -2.425

0.060 -0.800 0.020 -2.080 0.020 -2.364 0.020 -2.442

0.110 -0.781 0.040 -0.025 0.060 -0.939** 0.060 - 1.428

0.200 -0.640 0.060 - 1.322 0.090 - 1.319 0.1 I 0 - 1.244

0.230 -0.574 0.090 - 1.155 0.110 - 1.332 0.140 - 1.040

0.400 -0.391 0.130 -1.198 0.130 -4.015"* 0.190 -4.015"*

0.490 -0.342 0.150 - 1.107 0.150 - 1.026 0.250 -0.647

0.590 -0.413 0.200 -0.910 0.210 -0.930 0.400 -0.511

0.630 -0.443 0.250 -0,680 0.250 -0,733 0.490 -0.425

0.700 -0.514 0.260 -0.669 0.340 -0.630 0.580 -0.394

0.750 -0.589 0.280 -0.647 0.370 -0.592 0,650 -0.440

0.810 -0.543 0.290 -0.603 0.400 -0.515 0.700 -0.416

0.840 -0.608 0.310 -0.574 0.410 0.536"* 0.750 -0.426

0.900 -0.385 0.320 -0.594 0.430 -0.548 0.800 -0.395

0.960 -0,194 0.340 -0.567 0.440 -0.526 0.830 -0.320

0.350 -0.153"* 0.460 -0.502 0.900 -0.213

0.370 -0.537 0.490 -0.443 0.960 -0.150

0.380 -0.553 0.500 -0.489

0.400 -0.501 0.520 -0.503

0.410 -0.507 0.540 -0,474

0.430 -0.470 0,550 -0.469

0.440 -0.463 0.580 -0.442

0.460 -0.470 0.600 -0.473

0.470 -0.488 0.610 -0.473

0.490 -0.475 0.650 -0.657

0.500 -0.476 0.700 -0.505

0.520 -0.453 0.750 -0.505

0.530 -0.457 0.820 -0.482

0.550 -0.491 0.890 -0.126

0.560 -0A92 0,900 -0.097

0.580 -0,447 0.960 -0.005

0.590 -0.489

0.600 -0.467

0.640 -0.546

0.700 -0.563

0.750 -0.012"*

0.820 -0.527

0.870 -0.377

0.930 -0. t 79

0.960 -0.108

Lower Surface

0.020 0.293 0.020 0.487 0.020 0.545 0.020 0.710

O. 110 O. 117 0.060 0.374 0.060 0.434 0.060 0.044

0.230 0.168 0.090 0.321 0.090 0.362 0.110 0.387

0.400 0.070 O. 120 0.247 O. 120 0.266 0.250 O. 123

0.490 0.075 0.200 O. 170 0.200 O. 188 0.400 0.076

0.630 1.976"* 0.260 O. 180 0.250 O. 165 0.490 0.048

0.750 0.084 0.400 0.116 0,400 0.095 0.580 0.033

0.850 0,093 0.490 0.083 0.490 -0.021 0.650 0.113

0.900 0.183 0.580 0.058 0.580 0.052 0.750 0.280

0.960 0.107 0.640 0.210 0.650 -0.016 0.830 0.360

0,750 0.246 0,750 0,038 0.900 0.400

0.870 0,329 0.890 0.403 0.960 0.246

0.930 0.268 0.930 0.315

0.960 0.187 0.960 0.228

CN = 0,583 0.803 0.724 0.774

78
Table C-2, Continued.

Flight 216, Wing sweep = 26 °, Time = 8-56-43-500, MINF = 0.599, Camber = 20118, ALl:q" = 3.04, BETA = 0.86, QINF = 299.5,

RNPU = 3.1E+06, CNWP = 0.2664

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.758 0.000 - 1.077 0.000 -0.197"" 0.010 0.802

0.060 0.183 0.020 0.849 0.020 0.824 0.020 0.661

0. [ 10 -0.292 0.040 0.630 0.060 0.168"* 0.060 -0.166

0.200 -0518 0.060 0.082 0,090 -0.448 O. 110 - 1.125

0.230 -0,434 0.090 -0.391 0.110 -0,868 0.140 -0.830

0.400 -0.298 0.130 -01903 0.130 -3.983"* 0.190 -3.983"*

0.490 -0.282 O. 150 - 1.114 O. 150 -0.766 0.250 -0.480

0.590 -0.390 0.200 -0.730 0.210 -0.617 0.400 -0.437

0.630 -0,447 0.250 -0.469 0.250 -0.496 0.490 -0.404

0.700 -0.653 0.260 -0.473 0.340 -0.478 0.580 -0.460

0.750 -0.742 0,280 -0.464 0.370 -0.479 0.650 -0.628

0.810 -0.688 0.290 -0.446 0.400 -0.420 0.700 -0.617

0.840 -0.752 0.310 -0.427 0.410 0.524** 0.750 -0.878

0.900 -0.258 0.320 -0.451 0.430 -0.472 0.800 -0.963

0.960 -0.249 0.340 -0.434 0.440 -0.468 0.830 -0.804

0.350 -0.223** 0.460 -0.463 0.900 -0.387

0.370 -0.428 0.490 -0.451 0.960 -0.425

0.380 -0.446 0.500 -0.478

0.400 -0.404 0.520 -0.514

0.410 -0.423 0.540 -0.492

0.430 -0.399 0.550 -0.475

0.440 -0.401 0.580 -0.488

0.460 -0.420 0.600 -0.543

0.470 -0.436 0.610 -0.559

0.490 -0.445 0.650 -0.776

0.500 -0.445 0.700 -0.704

0.520 -0.451 0750 -0.77 I

0530 -0.452 0.820 -0.577

0.550 -0.491 0.890 -0.339

0.560 -0.500 0.900 -0.369

0.580 -0.466 0.960 -0.344

0.590 -0.525

0.600 -0.508

0.640 -0.682

0.700 -0.769

0.750 -0.123"*

0.820 -0.658

0.870 -0584

0.930 -0.327

0.960 -0.329

Lower Surface

0.020 -0.221 0.020 -0.370 0.020 -0.469 0.020 - 1.275

0.110 -0.173 0.060 -0.356 0.060 -0.5 l0 0.060 0.008

0.230 -0.088 0.090 -0.390 0.090 -0.605 O. 110 -0.193

0.400 -0.141 0.120 -0.360 0.120 -0.608 0.250 -0.040

0.490 -0.087 0.200 -0.082 0.200 -0.059 0400 -0.018

0.630 1.951 ** 0.260 -0.255 0.250 -0.062 0.490 0.027

0.750 -0.013 0.400 -0.059 0.400 O. I 14 0.580 0.103

0.850 0.035 0.490 0.070 0.490 -0.056 0.650 0.286

0.900 0.116 0.580 0.170 0.580 0.183 0.750 0.489

0.960 0.114 0.640 0.291 0.650 -0.126 0.830 0,514

0.750 0.326 0.750 0.002 0.900 0.562

0.870 0.396 0.890 0.566 0.960 0.383

0.930 0.365 0.930 0.458

0.960 0.253 0.960 0.327

CN = 0.318 0.538 0.516 0.664

79
Table C-2, Continued.

Flight 216, Wing sweep = 26 °, Time = 9-29-0-000, MINF = 0.604, Camber = 10/18, ALPT = 2,07, BETA = -0,04, QINF = 304,8,

RNPU = 3.1E+06, CNWP = 0,3364

rl = 0,93 0,76 0,59 0,40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.577 0.000 -0.391 0.000 0.486"* 0.010 0.392

0.060 0,073 0,020 0.615 0.020 0,539 0.020 0.224

0,110 -0.238 0.040 0.359 0.060 -0,092** 0.060 -0.303

0.200 -0.344 0.060 -0.022 0.090 -0.344 O.I I0 -0,677

0,230 -0.313 0.090 -0.270 0.110 -0.521 0.140 -0,601

0.400 -0.266 0.130 -0.504 0,130 -3.910"* 0.190 -3.910"*

0,490 -0.269 0.150 -0.600 0.150 -0.517 0.250 -0.413

0.590 -0.386 0,200 -0.479 0.210 -0.470 0,400 -0.404

0.630 -0,454 0.250 -0.357 0.250 -0.415 0.490 -0.384

0.700 -0,670 0.260 -0.373 0.340 -0,421 0.580 -0.438

0.750 -0,805 0.280 -0.357 0.370 -0.428 0,650 -0.623

0.810 -0.764 0,290 -0.361 0.400 -0.372 0,700 -0.602

0.840 -0.851 0.310 -0.349 0.410 0,519"* 0.750 -0.866

0.900 -0.311 0.320 -0.374 0.430 -0.430 0.800 -0.976

0.960 -0.307 0.340 -0.369 0.440 -0.435 0.830 -0.830

0.350 -0.168'* 0.460 -0.424 0,900 -0.394

0.370 -0.369 0.490 -0.424 0.960 -0,429

0.380 -0.384 0.500 -0,447

0.400 -0,349 0.520 -0.485

0.410 -0.367 0,540 -0.466

0.430 -0.354 0.550 -0.45 I

0.440 -0.356 0,580 -0.458

0.460 -0.362 0,600 -0.517

0.470 -0.430 0.610 -0.531

0.490 -0.406 0.650 -0.704

0.500 -0.411 0,700 -0,688

0.520 -0.386 0.750 -0.750

0.530 -0.419 0.820 -0.567

0.550 -0.451 0.890 -0.376

0.560 -0.475 0,900 -0.390

0.580 -0.434 0,960 -0,382

0.590 -0.499

0.600 -0.475

0.640 -0.663

0.700 -0.755

0.750 -0.084"*

0.820 -0.691

0.870 -0.458

0.930 -0.342

0.960 -0.341

Lower Surface

0.020 - 1.159 0,020 -0.920 0.020 -0.824 0.020 - 1.013

0. I 10 -0.165 0.060 -0.302 0,060 -0.152 0,060 0.016

0.230 -0.037 0.090 -0,130 0.090 -0.086 0,110 -0.166

0.400 0,075 0,120 -0.042 0.120 -0.055 0,250 -0.119

0.490 0.138 0.200 -0.048 0.200 -0.014 0.400 -0.057

0.630 2.301 ** 0.260 0,045 0.250 -0.013 0,490 0.016

0,750 0,234 0.400 0,079 0.400 0.019 0.580 0.086

0.850 0.243 0.490 0.122 0.490 -0.058 0.650 0.289

0.900 0.315 0.580 0,186 0,580 0.156 0.750 0.471

0.960 0.174 0.640 0,349 0.650 -0.092 0.830 0.509

0.750 0.382 0,750 0,006 0.900 0.575

0.870 0,430 0.890 0,553 0,960 0.415

0.930 0.370 0.930 0,465

0.960 0.242 0.960 0,334

CN = 0464 0.572 0.524 0.623

80
Table C-2, Continued.

Flight 216, Wing sweep = 26 °, Time = 9-29-6-500, MINF = 0.607, Camber = 10/19, ALPT = 3.01, BETA = -0.36, QINF = 306.2,

RNPU = 3.1E+06, CNWP = 0.3786

r I = 093 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.538 0.000 -0.195 0.000 0.583"* 0,010 0,298

0.060 0.037 0.020 0.530 0,020 0.446 0,020 0,121

0.110 -0.305 0.040 0.279 0.060 -0.233** 0.060 -0.414

0.200 -0.381 0.060 -0.117 0.090 -0.449 0.110 -0.797

0.230 -0.337 0090 -0,359 0.110 -0.641 0.140 -0,675

0.400 -0.284 0.130 -0.594 0.130 -3,882"* 0,190 -3,882**

0.490 -0.294 0.150 -0.690 0.150 -0.578 0.250 -0.455

0.590 -0.404 0.200 -0.549 0.210 -0,539 0.400 -0.433

0.630 -0.467 0.250 -0.407 0.250 -0.467 0.490 -0.399

0.700 -0.690 0.260 -0.415 0.340 -0.453 0.580 -0,446

0.750 -0.825 0.280 -0.413 0,370 -0.468 0.650 -0.629

0.810 -0.736 0,290 -0.405 0.400 -0.410 0.700 -0.614

0.840 -0.829 0.310 -0.387 0,410 0,528"* 0,750 -0,873

0.900 -0.326 0.320 -0.414 0.430 -0.462 0.800 -0.958

0.960 -0,336 0.340 -0.403 0.440 -0.463 0.830 -0.834

0.350 -0.172"* 0.460 -0.455 0.900 -0.399

0,370 -0,400 0.490 -0,449 0.960 -0.441

0.380 -0.417 0,500 -0.471

0.400 -0.337 0,520 -0,505

0.410 -0.399 0.540 -0.493

0.430 -0.387 0.550 -0.468

0.440 -0.386 0.580 -0.480

0.460 -0.3% 0.600 -0.540

0.470 -0.437 0.610 -0.558

0.490 -0.429 0.650 -0.703

0.500 -0,447 0.700 -0.706

0.520 -0,404 0.750 -0.772

0.530 -0.442 0,820 -0,595

0,550 -0.483 0.890 -0.407

0.560 -0.499 0.900 -0.398

0.580 -0.461 0.960 -0.401

0.590 -0.525

0600 -0.506

0.640 -0.695

0.700 -0.791

0.750 -0.070"*

0.820 -0.732

0.870 -0.424

0,930 -0.352

0.960 -0,351

Lower Surface

0.020 - 1,192 0.020 -0.690 0.020 -0.566 0.020 -0.714

0.110 -0.096 0.060 -0.135 0.060 -0.057 0.060 0.027

0,230 -0.019 0.090 -0.042 0.090 -0.016 0.110 -0.115

0.400 0.089 O. 120 0.026 0.120 -0.010 0.250 -0.075

0.490 0.155 0.200 -0.026 0.200 0.010 0.400 -0.017

0.630 2,301 ** 0.260 0.077 0.250 0,015 0.490 0.034

0.750 0.258 0.400 0.101 0.400 0.049 0.580 0.106

0,850 0,260 0.490 0,136 0.490 -0.037 0.650 0.302

0.900 0.338 0.580 0.200 0.580 0.180 0,750 0.484

0.960 0.167 0.640 0.388 0,650 -0.081 0.830 0.534

0.750 0.415 0.750 0.021 0.900 0.589

0.870 0.483 0.890 0.576 0.960 0.424

0.930 0_401 0.930 0.489

0.960 0.262 0.960 0.335

CN = 0.508 0.650 0.586 0.679

81
Table C-2. Continued.

Flight 216, Wing sweep = 26 °. Time = 9-29-12-000, MINF = 0.606, Camber = 10/19, ALPT = 6.05, BETA = -0.21, QINF = 303.4,

RNPU = 3.1E+06, CNWP = 0.4802

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 0.244 0.000 0.573 0.000 0.811"* 0.010 -0.373

0.060 -0.270 0.020 0.094 0.020 -0.061 0.020 -0.395

0.110 -0.585 0.040 -0.137 0.060 -0.651 ** 0.060 -0.988

0.200 -0.549 0.060 -0.569 0.090 -0.904 0.110 - 1.300

0.230 -0.515 0.090 -0.781 0.110 -1.126 0.140 -1.007

0.400 -0.383 0.130 - 1.042 0.130 -3.895 ** 0.190 -3.895 **

0.490 -0.368 0.150 - 1.096 0.150 -0.924 0.250 -0.638

0.590 -0.479 0.200 -0.838 0.210 -0.811 0.400 -0.546

0.630 -0.547 0.250 -0.603 0.250 -0.643 0.490 -0.488

0.700 -0.766 0.260 -0.599 0.340 -0.584 0.580 -0.524

0.750 -0.848 0.280 -0.581 0.370 -0.597 0.650 -0.677

0.810 -0.833 0.290 -0.564 0.400 -0.493 0.700 -0.658

0.840 -0.931 0.310 -0.540 0.410 0.555"* 0.750 -0.872

0.900 -0.425 0.320 -0.563 0.430 -0.562 0.800 -0.776

0.960 -0.440 0.340 -0.547 0.440 -0.557 0.830 -0.6 l 8

0.350 -0.218"* 0.460 -0.560 0.900 -0.403

0.370 -0.533 0.490 -0.541 0.960 -0.453

0.380 -0.553 0.500 -0.569

0.400 -0.321 0.520 -0.601

0.410 -0.512 0.540 -0.577

0.430 -0.491 0.550 -0.555

0.440 -0.494 0.580 -0.562

0.460 -0.509 0.600 -0.620

0.470 -0.528 0.610 -0.621

0.490 -0.522 0.650 -0.763

0.500 -0.529 0.700 -0.766

0.520 -0.507 0.750 -0.808

0.530 -0.522 0.820 -0.584

0.550 -0.551 0.890 -0.419

0.560 -0.562 0.900 -0.451

0.580 -0.536 0.960 -0.438

0.590 -0.596

0.600 -0.570

0.640 -0.748

0.700 -0.829

0.750 -0.027**

0.820 -0.742

0.870 -0.438

0.930 -0.373

0.960 -0.382

Lower Surface

0.020 -0.281 0.020 -0.148 0.020 -0.070 0.020 0.012

0.110 0.023 0.060 0.150 0.060 0.177 0.060 0.046

0.230 0.034 0.090 0.133 0.090 0.167 0.110 0.126

0.400 0.098 0.120 0.157 0.120 0.141 0.250 0.036

0.490 0.143 0.200 0.025 0.200 0.051 0.400 0.048

0.630 2.345"* 0.260 0.1 64 0.250 0.114 0.490 0.087

0.750 0.265 0.400 0.143 0.400 0. I 16 0.580 0.145

0.850 0.270 0.490 0.168 0.490 -0.007 0.650 0.312

0.900 0.352 0.580 0.210 0.580 0.211 0.750 0.506

0.960 0.140 0.640 0.411 0.650 -0.052 0.830 0.547

0.750 0.427 0.750 0.025 0.900 0.602

0.870 0.519 0.890 0.611 0.960 0.427

0.930 0.420 0.930 0.487

0.960 0.269 0.960 0.319

CN = 0.651 0.847 0.776 0.864

82
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-29-15-000, MINF = 0,603, Camber = 10/18, ALPT = 7.91, BETA = -0.24, QINF = 299.7,

RNPU = 3,1E+06, CNWP = 0.5327

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.056 0.000 0.803 0.000 0.845** 0.010 -0.785

0.060 -0.505 0.020 -0.347 0.020 -0.517 0.020 -0.785

0. I 10 -0,756 0.040 -0.093 0.060 -0.932** 0.060 - 1.408

0.200 -0.690 0,060 -0.917 0.090 - 1,227 0.110 - 1.560

0.230 -0.600 0.090 - 1.095 0.110 - 1.472 0.140 - 1.238

0.400 -0,424 0.130 - 1.409 0.130 -3.926** 0,190 -3.926 * *

0.490 -0.415 0.150 - 1.403 0.150 - 1.122 0.250 -0,706

0.590 -0.542 0.200 - 1.026 0.210 -0.947 0.400 -0.598

0.630 -0.599 0.250 -0.732 0.250 -0.764 0.490 -0.538

0.700 -0.815 0.260 -0.711 0.340 -0.679 0.580 -0.573

0.750 -0.881 0,280 -0.688 0,370 -0,667 0.650 -0.7 | 5

0.810 -0.877 0.290 -0,661 0.400 -0.608 0.700 -0.696

0.840 -0.992 0.310 -0.627 0.410 0.579"* 0.750 -0.852

0.900 -0.461 0.320 -0.649 0.430 -0.642 0.800 -0.755

0.960 -0.485 0.340 -0.624 0.440 -0.629 0.830 -0.666

0,350 -0.216"* 0.460 -0.6 t 3 0,900 -0,368

0.370 -0.603 0.490 -0.592 0.960 -0.362

0,380 -0.620 0.500 -0.610

0.400 -0.294 0,520 -0.611

0.410 -0.574 0.540 -0.628

0.430 -0.547 0.550 -0.604

0.440 -0.536 0.580 -0,59 I

0.460 -0.555 0.600 -0.650

0.470 -0.581 0.610 -0.665

0.490 -0.568 0.650 -0.817

0.500 -0.575 0.700 -0.781

0.520 -0.552 0.750 -0.820

0.530 -0,567 0.820 -0.577

0.550 -0.599 0.890 -0.429

0.560 -0.619 0.900 -0.420

0.580 -0.571 0.960 -0.430

0.590 -0.630

0.600 -0.600

0.640 -0.772

0.700 -0.852

0.750 -0.028"*

0.820 -0,659

0.870 -0.346

0.930 -0.342

0.960 -0.344

Lower Surface

0.020 0,001 0,020 0.162 0.020 0.209 0.020 0.378

0.110 0.095 0.060 0.293 0.060 0.316 0.060 0.063

0.230 0.084 0.090 0.259 0.090 0.294 0.110 0,266

0.400 0. I 19 0.120 0.220 0,120 0.243 0.250 0.120

0.490 0. | 68 0,200 0.078 0,200 0.110 0.400 0.117

0.630 2,391 ** 0,260 0.226 0.250 0.198 0.490 0.146

0.750 0.261 0.400 0.195 0.400 0.169 0.580 0.188

0,850 0.259 0.490 0.201 0.490 0.013 0,650 0.348

0.900 0.339 0,580 0,232 0,580 0,231 0.750 0.520

0.960 0.123 0.640 0.425 0.650 -0.043 0,830 0,568

0.750 0.439 0,750 0.057 0.900 0.629

0.870 0.515 0,890 0.606 0.960 0.438

0.930 0.423 0.930 0.494

0.960 0.278 0.960 0.314

CN = 0.746 0.959 0894 0.994

83
Table C-2, Continued.

Flight 216, Wing sweep = 26 °, Time = 9-29-18-500, MINF = 0.600, Camber = 10/18, ALPT = 11.70, BETA = -0.12, QINF = 295.4,

RNPU = 3.0E+06, CNWP = 0.7044

1"1= 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.900 0.000 0.368 0.000 0.485"* 0,010 -2.016

0.060 - 1.136 0.020 - 1.491 0.020 -2.016 0.020 -2,055

0,110 - I, 158 0,040 0.026 0.060 - 1.415"* 0.060 -2.055

0.200 -0.929 0.060 - 1.647 0,090 -2.091 0.1 l0 - 1,748

0.230 -0,818 0.090 - 1.907 0.110 -2.175 0,140 - 1.401

0.400 -0.582 0.130 -1,614 0.130 -3,974** 0,190 -3.974**

0.490 -0.538 0.150 -2.001 0.150 - 1.648 0.250 -0.806

0.590 -0.652 0.200 - 1.627 0.210 - 1.567 0.400 -0,645

0.630 -0.730 0.250 -0.895 0.250 - 1.044 0.490 -0,520

0.700 -0.924 0.260 -0,840 0.340 -0.773 0.580 -0.548

0.750 -0.963 0.280 -0,812 0.370 -0,719 0.650 -0.558

0.810 -0,938 0.290 -0.773 0.400 -0.639 0.700 -0.548

0.840 - 1,064 0.310 -0.719 0,410 0.597"* 0.750 -0,575

0.900 -0608 0,320 -0.749 0.430 -0.659 0.800 -0.588

0.960 -0,618 0.340 -0.725 0.440 -0,658 0,830 -0.493

0.350 -0,240"* 0.460 -0.636 0.900 -0.438

0.370 -0.692 0,490 -0.624 0.960 -0.437

0.380 -0.719 0.500 -0,623

0.400 -0,289 0.520 -0,652

0.410 -0.670 0,540 -0.624

0.430 -0.624 0.550 -0.622

0.440 -0.645 0.580 -0.634

0.460 -0.657 0.600 -0.661

0.470 -0.655 0.610 -0.635

0.490 -0.647 0.650 -0.826

0.500 -0.640 0.700 -0739

0.520 -0.640 0.750 -0.778

0.530 -0.637 0.820 -0.671

0.550 -0.665 0.890 -0.414

0,560 -0.681 0,900 -0.399

0.580 -0.641 0,960 -0,332

0.590 -0698

0.600 -0.665

0.640 -0.809

0.700 -0.892

0.750 0.003"*

0.820 -0.638

0.870 -0.327

0.930 -0.294

0.960 -0.299

Lower Surface

0.020 0.342 0.020 0.566 0.020 0.614 0.020 0.689

0.110 0.234 0,060 0.492 0.060 0.535 0.060 0,118

0.230 0.155 0.090 0.447 0.090 0.484 0.110 0.468

0.400 0.167 0.120 0.388 0.120 0.422 0.250 0.269

0.490 0.191 0.200 0.155 0.200 0.179 0.400 0.228

0.630 2.436"* 0,260 0.349 0,250 0.329 0.490 0.243

0.750 0,252 0.400 0.279 0.400 0.251 0.580 0.265

0.850 0.238 0.490 0.269 0.490 0.067 0,650 0,392

0.900 0.306 0.580 0.285 0,580 0,288 0.750 0,577

0,960 0.094 0.640 0.446 0.650 -0.019 0,830 0.596

0,750 0.449 0.750 0.068 0.900 0.649

0.870 0,520 0,890 0,632 0,960 0,438

0,930 0.424 0.930 0.525

0,960 0.288 0.960 0,324

CN = 0.960 1.190 1.128 1,141

84
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-30-24-500, MINF = 0,605, Camber = 10/15, ALI'T = 2.06, BETA = -0.01, QINF = 305.2,

RNPU = 3. IE+06, CNWP = 0.3346

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.589 0.000 -0.404 0.000 0.517"* 0.010 0.382

0.060 0. I 01 0.020 0.587 0.020 0.530 0.020 0.214

0.110 -0.190 0,040 0.354 0.060 -0.169* * 0.060 -0. 297

0.200 -0.353 0.060 -0.016 0.090 -0.362 0.110 -0.684

0.230 -0.321 0.090 -0.287 0.110 -0.514 0.140 -0.595

0.400 -0.268 0.130 -0.512 0.130 -3.899"* 0.190 -3.899"=

0.490 -0.274 0.150 -0.608 0.150 -0.500 0.250 -0.421

0.590 -0.383 0.200 -0.481 0.210 -0.478 0.400 -0.413

0.630 -0.439 0.250 -0.353 0.250 -0.424 0.490 -0.383

0.700 -0,630 0.260 -0.368 0.340 -0.430 0.580 -0.446

0.750 -0.843 0.280 -0.374 0.370 -0.428 0.650 -0.607

0.810 -0.778 0.290 -0.374 0.400 -0.387 0.700 -0.610

0.840 -0.844 0.310 -0.357 0,410 0.524"* 0.750 -0.873

0.900 -0.255 0.320 -0.378 0.430 -0.424 0.800 -0.984

0.960 -0.221 0.340 -0.374 0,440 -0.443 0.830 -0.838

0.350 -0.176"* 0.460 -0.432 0.900 -0.402

0,370 -0.374 0.490 -0.425 0.960 -0.430

0.380 -0.392 0.500 -0.455

0,400 -0.325 0.520 -0.476

0.410 -0.375 0.540 -0.467

0.430 -0.362 0.550 -0.459

0.440 -0.368 0.580 -0.466

0.460 -0370 0.600 -0.525

0.470 -0.392 0.610 -0.539

0.490 -0,410 0.650 -0.716

0.500 -0.414 0.700 -0.695

0.520 -0.402 0.750 -0,758

0.530 -0.427 0.820 -0.587

0.550 -0.459 0.890 -0.353

0.560 -0.477 0.900 -0.372

0.580 -0.422 0.960 -0.342

0.590 -0.507

0.600 -0.488

0.640 -0.677

0.700 -0.769

0.750 -0.107"*

0.820 -0598

0.870 -0.351

0.930 -0.333

0.960 -0.357

Lower Surface

0.020 - 1.182 0.020 -0.935 0.020 -0.847 0.020 - 1.021

0.110 -0.184 0.060 -0.317 0,060 -0.159 0.060 0.004

0.230 -0.057 0.090 -0.1 44 0.090 -0.095 0.110 -0.180

0.400 0.048 0.120 -0.050 0.120 -0.080 0.250 -0.121

0.490 0.089 0.200 -0.057 0.200 -0.036 0.400 -0.044

0.630 2.303** 0.260 0.029 0.250 -0.008 0.490 0.008

0.750 0.198 0.400 0.063 0.400 0.015 0.580 0,087

0.850 0.196 0.490 0.102 0.490 -0.074 0.650 0.297

0.900 0.282 0.580 0.162 0.580 0.147 0.750 0.462

0.960 0.157 0.640 0.325 0.650 -0.100 0.830 0.508

0.750 0.308 0.750 -0.002 0.900 0.559

0.870 0.339 0.890 0.547 0.960 0.412

0.930 0.261 0.930 0.463

0.960 0.143 0.960 0.313

CN = 0.421 0.527 0.519 0.623

85
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-30-42-000. MINF = 0.608, Camber = 10/16, ALPT = 8.12, BETA = -0.30, QINF = 305.8,

RNPU = 3.1E+06, CNWP = 0.5323

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0.074 0.000 0.803 0.000 0.852** 0.010 -0.835

0.060 -0.517 0.020 -0.382 0.020 -0.550 0.020 -0.815

0.110 -0.779 0.040 -0.130 0,060 -0.887** 0.060 - 1.507

0.200 -0,693 0.060 -0.918 0.090 - 1.248 0.110 - 1.571

0.230 -0.620 0.090 - 1.120 0.110 - 1.473 0.140 - 1.322

0.400 -0.434 0.130 - 1.423 0.130 -3.866 * * 0.190 -3.866* *

0.490 -0.414 0.150 - 1.704 0.150 - t ,211 0.250 -0.710

0.590 -0.524 0.200 - 1.032 0.210 -0.942 0.400 -0.590

0.630 -0.587 0.250 -0.727 0.250 -0.767 0.490 -0.531

0.700 -0.784 0.260 -0.701 0.340 -0.684 0.580 -0.575

0,750 - 1.001 0.280 -0.686 0.370 -0.673 0.650 -0.715

0.810 -0.961 0.290 -0.661 0.400 -0.600 0.700 -0.697

0.840 - 1.066 0.310 -0.625 0.410 0.549 ** 0.750 -0.860

0.900 -0.434 0.320 -0.649 0.430 -0.648 0.800 -0.743

0.960 -0.452 0.340 -0.629 0.440 -0.641 0.830 -0,666

0.350 -0.226** 0.460 -0.616 0.900 -0.373

0.370 -0.595 0.490 -0.599 0.960 -0.359

0.380 -0.616 0.500 -0.611

0,400 -0.303 0.520 -0.636

0.410 -0.570 0.540 -0.619

0.430 -0.546 0.550 -0.596

0,440 -0.541 0.580 -0.600

0,460 -0.554 0.600 -0.647

0.470 -0.574 0.610 -0.656

0.490 -0.557 0.650 -0.817

0.500 -0.567 0.700 -0.769

0.520 -0.529 0.750 -0.818

0.530 -0.564 0.820 -0.524

0.550 -0.591 0.890 -0.444

0.560 -0.598 0.900 -0.437

0.580 -0.564 0.960 -0.428

0.590 -0.622

0.600 -0.587

0,640 -0.757

0.700 -0.828

0.750 -0.035"*

0.820 -0.536

0.870 -0.311

0.930 -0.343

0.960 -0.359

Lower Surface

0.020 0.006 0.020 0.175 0.020 0.216 0.020 0.398

0.110 0.092 0.060 0.294 0.060 0,331 0.060 0.058

0.230 0.082 0.090 0.261 0.090 0.302 0.110 0.267

0.400 0.102 0.120 0.248 0.120 0.251 0.250 0.127

0.490 0.132 0.200 0.076 0.200 0.104 0.400 0.121

0.630 2.325"* 0.260 0.228 0.250 0.197 0.490 0.150

0.750 0.218 0.400 0.195 0.400 0.176 0.580 0.190

0.850 0.219 0.490 0.197 0.490 0.016 0.650 0.351

0.900 0.296 0.580 0.227 0,580 0.236 0.750 0.534

0.960 0.100 0.640 0.408 0.650 -0.046 0.830 0.578

0.750 0.378 0.750 0.052 0.900 0.630

0.870 0.419 0.890 0.618 0.960 0.436

0.930 0.322 0.930 0.509

0.960 0.179 0.960 0.347

CN = 0.734 0.932 0,901 1.009

86
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-30-47-500, MINF = 0.591, Camber = 10/15, ALPT = 12.30, BETA = -0.07, Q1NF = 288.2,

RNPU = 3.0E+06, CNWP = 0.7297

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,968 0.000 0.272 0.000 0.442"* 0.010 -2.158

0.060 - 1.203 0.020 - 1.533 0,020 -2.179 0.020 -2.213

O. 110 - 1.288 0.040 0.026 0.060 - 1.390"* 0060 -2.125

0.200 -0.959 0060 - 1.708 0.090 -2.174 0.110 - 1.684

0.230 -0.814 0.090 - 1.977 0.110 -2.276 0.140 - 1.326

0.400 -0.577 0.130 - 1.658 0.130 -4.092** 0.190 -4.092**

0.490 -0.537 0.150 -2.055 0.150 - 1,685 0.250 -0.801

0.590 -0.656 0.200 - 1.613 0,210 - 1.553 0.400 -0.630

0.630 -0.716 0.250 -0.895 0.250 - 1.007 0,490 -0,548

0.700 -0.894 0.260 -0.837 0.340 -0.750 0,580 -0.549

0.750 - 1.072 0.280 -0.824 0.370 -0.716 0.650 -0.555

0.810 - 1.047 0.290 -0.764 0.400 -0.643 0.700 -0.534

0.840 - I. 179 0.310 -0.746 0.410 0.593** 0.750 -0.594

0.900 -0,531 0.320 -0.749 0.430 -0.649 0.800 -0.582

0.960 -0.546 0.340 -0.726 0.440 -0.647 0.830 -0.463

0.350 -0.234** 0.460 -0.622 0.900 -0.463

0.370 -0.687 0.490 -0.597 0.960 -0.435

0.380 -0,718 0.500 -0.628

0.400 -0.312 0.520 -0.637

0.410 -0.661 0.540 -0.623

0.430 -0.647 0.550 -0.618

0.440 -0.615 0.580 -0.582

0.460 -0.653 0.600 -0.632

0.470 -0,648 0.610 -0.634

0.490 -0.650 0.650 -0.803

0.500 -0.627 0.700 -0.712

0.520 -0.604 0.750 -0.760

0.530 -0.620 0.820 -0.632

0,550 -0.657 0.890 -0.397

0.560 -0.676 0.900 -0.370

0.580 -0.641 0.960 -0,327

0.590 -0.683

0.600 -0.645

0.640 -0.783

0.700 -0862

0.750 -0.016"*

0.820 -0.525

0.870 -0.267

0.930 -0,263

0.960 -0.231

Lower Surface

0.020 0.364 0.020 0.575 0,020 0.610 0.020 0.693

0. I 10 0.231 0.060 0.523 0.060 0.557 0.060 0. I 16

0.230 0.139 0.090 0.466 0.090 0.506 0.110 0.481

0.400 0.159 0,120 0A01 0.120 0.422 0.250 0.270

0.490 0.183 0.200 0.140 0.200 0.179 0.400 0.233

0.630 2.477** 0.260 0.357 0.250 0,340 0.490 0.238

0.750 0.210 0.400 0.285 0.400 0.273 0.580 0.262

0.850 0.200 0.490 0.272 0.490 0.057 0.650 0.405

0,900 0.273 0.580 0.265 0.580 0.298 0,750 0.587

0.960 0.056 0.640 0.433 0.650 -0.027 0.830 0.591

0.750 0.395 0.750 0.095 0.900 0661

0.870 0.423 0.890 0.636 0.960 0.451

0.930 0.355 0.930 0.526

0.960 0.218 0.960 0.344

CN = 0.959 1.155 1.131 1.145

87
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-31-32-000, MINF = 0.603, Camber = 10/12, ALPT = 2,09, BETA = 0.69, QINF = 303.3,

RNPU = 3.1E+06, CNWP = 0.2984

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.594 0.000 -0.407 0.000 0.444* * 0,010 0.405

0.060 0.083 0.020 0.609 0.020 0.549 0,020 0,250

O 110 -0.248 0.040 0.363 0,060 -0.070** 0.060 -0.314

0.200 -0,328 0.060 -0.017 0.090 -0,344 0,110 -0,670

0.230 -0.314 0.090 -0.272 0.110 -0.532 0.140 -0,613

0.400 -0.262 0,130 -0.495 0.130 -3.924"* 0.190 -3.924"*

0.490 -0.258 0.150 -0,605 0.150 -0.520 0,250 -0.424

0.590 -0.363 0.200 -0,479 0.210 -0,458 0.400 -0,394

0.630 -0.412 0.250 -0.356 0.250 -0.405 0.490 -0,386

0.700 -0.568 0.260 -0.378 0.340 -0.418 0.580 -0,439

0.750 -0.780 0.280 -0.368 0.370 -0.431 0,650 -0,625

0,810 -0,706 0.290 -0.368 0.400 -0,376 0,700 -0.604

0.840 -0.755 0,310 -0,353 0,410 0.527** 0.750 -0.872

0.900 -0.242 0.320 -0.362 0.430 -0.426 0.800 -0.977

0.960 -0.100 0.340 -0,366 0.440 -0.436 0,830 -0.798

0.350 -0.178"* 0.460 -0.424 0.900 -0.382

0.370 -0.355 0.490 -0,406 0,960 -0.425

0,380 -0.372 0.500 -0.449

0.400 -0.324 0.520 -0.480

0,410 -0.368 0,540 -0.450

0.430 -0.339 0.550 -0.450

0.440 -0,358 0.580 -0,452

0.460 -0.359 0.600 -0.517

0.470 -0.409 0.610 -0.530

0.490 -0.406 0.650 -0.676

0.500 -0 412 0.700 -0.678

0.520 -0.389 0.750 -0,752

0.530 -0.420 0.820 -0.608

0.550 -0.462 0.890 -0.328

0.560 -0.468 0.900 -0.343

0.580 -0.418 0,960 -0.313

0.590 -0.498

0.600 -0.477

0.640 -0.659

0.700 -0.753

0.750 -0.151 **

0.820 -0,558

0.870 -0.300

0.930 -0.313

0,960 -0.294

Lower Surface

0.020 - 1.092 0,020 -0.958 0,020 -0.891 0,020 - 1.040

0.110 -0.202 0.060 -0.342 0.060 -0.175 0,060 0.007

0.230 -0.058 0.090 -0,172 0.090 -0.096 0.110 -0,196

0.400 0.026 0.120 -0.058 0,120 -0.090 0.250 -0.122

0.490 0.078 0.200 -0,064 0.200 -0.030 0.400 -0,059

0,630 2.3 ] 7"* 0.260 0.029 0.250 -0.023 0.490 0.022

0.750 0.150 0,400 0.056 0.400 0.020 0.580 0.101

0.850 0.166 0.490 0,091 0.490 -0.082 0.650 0.285

0.900 0.243 0.580 0,1 44 0.580 0,148 0,750 0.464

0,960 0.157 0.640 0.315 0,650 -0.136 0,830 0,525

0.750 0.252 0.750 -0.003 0.900 0.583

0,870 0.231 0,890 0.547 0.960 0,408

0,930 0.194 0.930 0.466

0.960 0.089 0.960 0.338

CN --- 0.376 0.482 0,503 0.619

88
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-31-43-000, MINF = 0.607, Camber = 10/12, ALPT = 8.09, BETA = -0.41, QINF = 304.8,

RNPU = 3. IE+06, CNWP = 0.5067

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.081 0.000 0.793 0.000 0.849"* 0.010 -0,816

0.060 -0.527 0.020 -0.381 0.020 -0.566 0.020 -0.816

0,1 I 0 -0.780 0.040 -0.097 0.060 -0.942"* 0.060 - 1.490

0,200 -0.694 0.060 -0.934 0,090 - 1.240 0.110 - 1.575

0.230 -0.611 0.090 -1,122 0.110 -I.485 0,140 -1.325

0.400 -0.419 0.130 - 1.420 0.130 -3,877 * * 0.190 -3.877 * *

0.490 -0.396 0,150 - 1.684 0.150 - 1.238 0.250 -0.683

0.590 -0.490 0,200 - 1.034 0.210 -0,952 0.400 -0.584

0.630 -0.546 0.250 -0.722 0.250 -0.761 0.490 -0.531

0.700 -0.704 0.260 -0.702 0,340 -0.685 0.580 -0.565

0.750 -0.938 0.280 -0.687 0.370 -0.681 0.650 -0.705

0.810 -0.878 0,290 -0,653 0.400 -0.593 0.700 -0.687

0.840 -0,977 0,310 -0.616 0.410 0,552** 0.750 -0.840

0.900 -0.347 0,320 -0.636 0.430 -0.648 0,800 -0.745

0.960 -0.284 0.340 -0.616 0.440 -0.635 0.830 -0.658

0.350 -0.220** 0.460 -0.605 0.900 -0,364

0.370 -0.588 0.490 -0.577 0.960 -0.342

0.380 -0.603 0.500 -0.612

0.400 -0,305 0.520 -0.636

0.410 -0.564 0.540 -0.606

0,430 -0.534 0.550 -0.585

0.440 -0.530 0.580 -0.583

0.460 -0.549 0.600 -0.636

0.470 -0.568 0.610 -0,643

0.490 -0.546 0.650 -0.793

0.500 -0.557 0.700 -0,763

0,520 -0.530 0,750 -0.801

0.530 -0.546 0.820 -0.495

0.550 -0.556 0.890 -0.380

0.560 -0.598 0.900 -0,384

0,580 -0.544 0.960 -0.359

0.590 -0.605

0,600 -0.578

0.640 -0,723

0.700 -0.793

0.750 -0.094"*

0.820 -0.395

0.870 -0.274

0.930 -0.292

0.960 -0.279

Lower Surface

0.020 0.008 0.020 0.174 0.020 0.234 0.020 0.413

0.110 0.090 0.060 0.296 0.060 0.334 0.060 0.046

0.230 0.080 0.090 0,258 0.090 0.307 0.110 0.279

0.400 0,067 0,120 0.250 0.120 0,253 0,250 0.135

0.490 0.112 0.200 0.064 0.200 0.106 0.400 0.112

0,630 2.334** 0.260 0.227 0.250 0.206 0.490 0,138

0.750 0.160 0.400 0.186 0.400 0.159 0.580 0.202

0.850 0.165 0.490 0.184 0.490 -0.025 0.650 0,340

0.900 0.253 0,580 0.189 0.580 0.232 0,750 0.528

0.960 0.098 0.640 0.364 0,650 -0.101 0,830 0.567

0.750 0.303 0.750 0.040 0,900 0.634

0.870 0,332 0.890 0,601 0,960 0.439

0.930 0.220 0.930 0.491

0.960 0.098 0.960 0.334

CN = 0.670 0867 0.874 0.997

89
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-31-47-500, MINF -- 0.594, Camber = I0/12, ALPT = 12.00, BETA -- -0.27, QINF = 290.5,

RNPU = 3.0E+06, CNWP = 0.7488

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.918 0.000 0.341 0.000 0.438"* 0.010 -2.062

0,060 - 1. I 18 0,020 - 1.528 0.020 -2.103 0.020 -2.123

0.110 -1.201 0.040 0.004 0.060 -1.370"* 0.060 -2.101

0.200 -0.930 0.060 - 1.670 0.090 -2.127 0.110 - 1.688

0.230 -0.786 0.090 -1.933 0.110 -2.229 0.140 -1.326

0,400 -0.572 0.130 - 1.638 0,130 -4.052"* 0.190 -4.052"*

0.490 -0.513 0.150 -2.031 0.150 - 1.685 0.250 -0.802

0.590 -0.611 0.200 -1.566 0,210 -1.519 0.400 -0.617

0.630 -0.693 0.250 -0.871 0.250 -0.932 0.490 -0.512

0.700 -0.847 0.260 -0.803 0.340 -0.735 0.580 -0.505

0.750 - 1.039 0.280 -0.792 0.370 -0.686 0.650 -0.558

0.810 - 1.017 0.290 -0.765 0.400 -0,630 0.700 -0.537

0.840 - 1.116 0.310 -0.723 0.410 0.596** 0.750 -0.559

0.900 -0.443 0.320 -0.761 0.430 -0.651 0.800 -0.577

0.960 -0.413 0.340 -0.721 0,440 -0.627 0.830 -0.457

0,350 -0.229* * 0.460 -0.613 0.900 -0.504

0.370 -0.681 0.490 -0.607 0.960 -0.431

0.380 -0.725 0.500 -0.596

0.400 -0.294 0.520 -0,622

0.410 -0.649 0.540 -0.618

0.430 -0.623 0.550 -0.593

0.440 -0.608 0.580 -0.602

0.460 -0.628 0.600 -0.634

0.470 -0.659 0.610 -0.629

0.490 -0.629 0.650 -0.817

0.500 -0.623 0.700 -0,702

0,520 -0.574 0.750 -0.788

0.530 -0.612 0.820 -0.668

0.550 -0.646 0.890 -0.387

0.560 -0.653 0.900 -0.379

0.580 -0.608 0.960 -0.331

0.590 -0.676

0.600 -0.617

0.640 -0,770

0.700 -0.843

0,750 -0.057"*

0.820 -0.330

0.870 -0.216

0.930 -0.249

0.960 -0.297

Lower Surface

0.020 0.343 0.020 0.564 0.020 0.582 0.020 0.695

0.110 0.223 0.060 0.489 0.060 0.546 0.060 0.108

0.230 0.146 0.090 0.434 0.090 0.488 0.110 0.485

0.400 0.120 0.120 0.361 0.120 0.418 0.250 0.269

0.490 0.133 0.200 0.128 0.200 0.171 0.400 0.231

0.630 2.465** 0.260 0.329 0.250 0.330 0.490 0.243

0.750 0.158 0.400 0.264 0.400 0.258 0.580 0.268

0.850 0.143 0.490 0.247 0.490 0.034 0.650 0.387

0.900 0.227 0.580 0.251 0.580 0.289 0.750 0.575

0.960 0.054 0.640 0.403 0.650 -0.060 0.830 0.594

0.750 0.317 0.750 0.102 0.900 0.649

0. 870 0.313 0.890 0.631 0.960 0.440

0.930 0.228 0.930 0.522

0.960 0.137 0.960 0.330

CN = 0.886 1.076 1.111 1.131

90
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-32-35-000, MINF = 0.606, Camber = 10/9, ALPT = 1.99, BETA = 0.25, QINF = 306.3,

RNPU = 3.1E+06, CNWP = 0.3043

"q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 0.602 0.000 -0.425 0.000 0.480** 0.010 0.427

0.060 0.097 0020 0.628 0.020 0,565 0.020 0.260

0. 110 -0.206 0.040 0.379 0.060 -0.140"* 0.060 -0+284

0,200 -0.334 0,060 0.005 0,090 -0.325 0.110 -0.657

0.230 -0.278 0.090 -0,255 0. I 10 -0.495 0.140 -0.584

0,400 -0.239 0.130 -0,480 0.130 -3,895* * 0.190 -3.895 **

0,490 -0.246 0.150 -0.581 0.150 -0.501 0,250 -0.401

0.590 -0.331 0.200 -0.463 0.210 -0453 0.400 -0.392

0,630 -0.368 0,250 -0,346 0.250 -0,402 0.490 -0.367

0.700 -0.494 0,260 -0.355 0.340 -0.408 0.580 -0.429

0.750 -0.660 0.280 -0+350 0.370 -0.414 0.650 -0.613

0.810 -0.588 0.290 -0.350 0.400 -0.366 0.700 -0.582

0.840 -0.633 0.310 -0.335 0,410 0.514"* 0.750 -0.851

0.900 -0.281 0.320 -0.358 0.430 -0.417 0.800 -0.968

0.960 -0,083 0.340 -0,350 0.440 -0.416 0.830 -0.803

0.350 -0.165"* 0.460 -0.414 0.900 -0,395

0.370 -0.349 0.490 -0.440 0.960 -0.415

0.380 -0.368 0.500 -0.420

0.400 -0.329 0.520 -0.461

0.410 -0.353 0.540 -0.454

0.430 -0.333 0.550 -0.440

0.440 -0.340 0.580 -0.442

0.460 -0.352 0.600 -0.506

0470 -0.381 0.610 -0.519

0.490 -0.384 0.650 -0.692

0.500 -0,397 0.700 -0.677

0.520 -0.372 0.750 -0.739

0.530 -0.400 0.820 -0.568

0.550 -0.426 0.890 -0.315

0.560 -0,452 0900 -0,339

0.580 -0.416 0.960 -0,297

0.590 -0.474

0.600 -0.457

0.640 -0.638

0.700 -0.729

0.750 -0,158**

0.820 -0.576

0.870 -0.284

0.930 -0.315

0.960 -0.339

Lower Surface

0.020 - 1.001 0,020 -0.977 0.020 -0.915 0.020 - 1,097

O. 110 -0.233 0.060 -0.381 0.060 -0.199 0.060 0.009

0.230 -0.059 0.090 -0.193 0.090 -0.098 O.110 -0.208

0.400 0.031 0,120 -0.080 0.120 -0.091 0.250 -0.122

0.490 0.065 0.200 -0.058 0.200 -0.037 0.400 -0.053

0.630 2,287** 0.260 0.020 0,250 -0.024 0.490 0.006

0.750 O. 124 0.400 0.050 0,400 0.016 0,580 0.092

0.850 0.144 0.490 0.081 0.490 -0.1 04 0.650 0.295

0.900 0.223 0,580 0.137 0.580 0.152 0.750 0.470

0.960 0.158 0.640 0.282 0.650 -0.164 0.830 0.516

0.750 0,207 0.750 0.007 0.900 0.575

0.870 0.208 0.890 0.548 0.960 0.422

0.930 0.187 0.930 0.467

0.960 0.094 0.960 0.313

CN = 0.326 0.455 0.485 0.606

91
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-32-47-000, MINF = 0.603, Camber = 10/9, ALPT = 7.92, BETA = -0.41, QINF = 300.2,

RNPU = 3,1E+06. CNWP = 0.4942

1] = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.041 0.000 0,806 0.000 0.835'* 0.010 -0.772

0.060 -0.504 0.020 -0,337 0,020 -0.493 0.020 -0.730

0,110 -0.764 0.040 -0.435 0.060 -0.908** 0.060 - 1.373

0.200 -0.673 0,060 -0,893 0.090 - 1,213 0.110 - 1.546

0,230 -0.590 0,090 - 1.094 0.110 - 1.461 0.140 -1.218

0,400 -0,409 0,130 - 1,389 0.130 -3.928* * 0.190 -3.928 **

0.490 -0.382 0.150 - 1.389 0.150 - 1,104 0.250 -0.699

0.590 -0.458 0.200 - 1.016 0.210 -0,941 0,400 -0.585

0,630 -0.503 0.250 -0.714 0.250 -0.750 0.490 -0.527

0.700 -0.628 0.260 -0.698 0,340 -0.672 0.580 -0.559

0.750 -0.807 0.280 -0.669 0,370 -0,659 0.650 -0.702

0.810 -0.748 0.290 -0.643 0,400 -0,579 0,700 -0.694

0.840 -0.815 0.310 -0,606 0,410 0.569"* 0.750 -0.852

0.900 -0.442 0.320 -0,621 0,430 -0,620 0.800 -0.748

0.960 -0.231 0.340 -0,605 0.440 -0.616 0.830 -0.629

0.350 -0.219"* 0.460 -0.593 0.900 -0.367

0,370 -0.574 0.490 -0,577 0.960 -0.354

0.380 -0.596 0.500 -0.590

0.400 -0.291 0,520 -0.619

0.410 -0,553 0,540 -0,594

0.430 -0.526 0.550 -0.575

0.440 -0.516 0.580 -0.563

0,460 -0,539 0,600 -0.628

0.470 -0.563 0.610 -0.632

0.490 -0.537 0.650 -0.757

0.500 -0.544 0.700 -0.741

0,520 -0.513 0,750 -0.794

0.530 -0,533 0,820 -0.513

0.550 -0.561 0,890 -0.352

0.560 -0,577 0,900 -0.354

0.580 -0.532 0,960 -0.339

0.590 -0.585

0.600 -0.564

0.640 -0.707

0.700 -0,779

0.750 -0.109"*

0,820 -0.389

0.870 -0,299

0.930 -0.265

0.960 -0.286

Lower Surface

0.020 -0.038 0.020 0,135 0,020 0,208 0.020 0,388

0.110 0.079 0,060 0.283 0.060 0.320 0.060 0,054

0,230 0.072 0,090 0.250 0,090 0.294 0.110 0.257

0,400 0,073 0,120 0.240 O. 120 0.234 0.250 0.128

0.490 0.093 0.200 0.069 0.200 0.095 0.400 0.122

0.630 2.378** 0.260 0.217 0.250 0.196 0.490 0.148

0.750 0.114 0.400 0.171 0.400 0.174 0.580 0.189

0.850 0.123 0.490 0,165 0.490 -0.032 0.650 0.346

0.900 0.216 0.580 0.181 0.580 0,222 0.750 0.534

0,960 0.102 0,640 0.351 0,650 -0.108 0.830 0.575

0,750 0.248 0.750 0.048 0.900 0.631

0.870 0.271 0.890 0.604 0.960 0.440

0.930 0.232 0.930 0.492

0.960 0,130 0.960 0.325

CN = 0.616 0.833 0,853 0,983

92
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-32-5t-500, MINF = 0.590, Camber = 10/9, ALPT = l 1.92, BETA = -0.27, Q1NF = 286.9,

RNPU = 3.0E+06, CNWP = 0.7017

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.919 0.000 0.345 0.000 0.445"* 0.010 -2,035

0.060 - 1.136 0.020 - 1.561 0.020 -2.076 0.020 -2.097

0.1 I 0 - 1.218 0.040 0.006 0.060 - 1.392"* 0.060 -2.118

0.200 -0.942 0.060 - 1.704 0.090 -2.134 0.110 - 1.743

0.230 -0.810 0.090 - 1,961 0.110 -2,256 0.140 - 1.356

0.400 -0.562 0.130 -1,672 0.130 -4.101"* 0.190 -4.101"*

0.490 -0.514 0.150 -2.070 0_ 150 - 1 _713 0,250 -0.840

0.590 -0.592 0.200 - 1.569 0.210 - 1.571 0.400 -0.646

0.630 -0.652 0.250 -0,867 0.250 -0.972 0.490 -0.551

0,700 -0.770 0.260 -0.826 0.340 -0.742 0.580 -0,568

0.750 -0,943 0.280 -0.807 0,370 -0.732 0.650 -0.632

0.810 -0.886 0.290 -0.770 0.400 -0.636 0.700 -0.600

0.840 -0.990 0.310 -0,736 0.410 0.604** 0.750 -0.678

0.900 -0.499 0.320 -0.759 0.430 -0.672 0.800 -0.664

0.960 -0.306 0.340 -0.729 0.440 -0.660 0.830 -0.476

0.350 -0251 ** 0.460 -0.640 0.900 -0.448

0.370 -0.696 0.490 -0.612 0.960 -0.390

0.380 -0.718 0.500 -0.627

0.400 -0.300 0.520 -0.661

0.410 -0.658 0.540 -0,640

0.430 -0.632 0.550 -0.608

0.440 -0.616 0.580 -0.605

0.460 -0.637 0.600 -0.655

0.470 -0.652 0.610 -0.637

0.490 -0.630 0.650 -0.793

0.500 -0.633 0.700 -0.728

0.520 -0.603 0,750 -0.780

0.530 -0.615 0.820 -0.603

0.550 -0.624 0.890 -0.355

0.560 -0.661 0.900 -0.354

0.580 -0.608 0.960 -0.305

0.590 -0.679

0600 -0.628

0.640 -0759

0700 -0.822

0.750 -0086**

0.820 -0,266

0.870 -0.175

0.930 -0.273

0.960 -0.230

Lower Surface

0.020 0.338 0.020 0.554 0.020 0.590 0.020 0.697

0. 110 0.2 t9 0.060 0.500 0,060 0,539 0.060 0.096

0.230 0.130 0.090 0.444 0.090 0.488 0.110 0.498

0.400 0.127 0.120 0.378 0.120 0.409 0.250 0.272

0.490 0.128 0.200 0.127 0,200 0.152 0.400 0.228

0.630 2.497** 0,260 0,334 0.250 0,328 0.490 0.240

0.750 0.106 0.400 0.254 0.400 0.258 0.580 0,263

0.850 0.104 0.490 0,232 0.490 0.013 0.650 0.389

0.900 0.183 0,580 0.228 0.580 0,286 0.750 0.573

0.960 0.063 0,640 0.379 0.650 -0,097 0.830 0.601

0.750 0,255 0.750 0.075 0.900 0.655

0.870 0.265 0.890 0.625 0.960 0.444

0.930 0.236 0,930 0.523

0.960 0.156 0.960 0.321

CN = 0.844 1.057 I. 103 1.166

93
Table C-2. Continued.

Flight 216, Wing sweep = 26°, Time = 9-33-28-000, MINF = 0.599, Camber = 10/6, ALPT -- 2.03, BETA = 0.02, QINF = 299.5,

RNPU = 3. I E+06, CNWP = 0.3061

1"1= 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.588 0.000 -0,393 0,000 0,460** 0,010 0.399

0.060 0,085 0.020 0.589 0.020 0.542 0.020 0.229

0.1 I 0 -0,229 0,040 0.356 0.060 -0.100"* 0.060 -0.307

0.200 -0.324 0,060 -0,021 0.090 -0.323 0.110 -0.668

0.230 -0.299 0,090 -0.273 0,110 -0.529 0.140 -0.602

0.400 -0,233 0.130 -0.499 0.130 -3.978"* 0.190 -3.978 **

0.490 -0.233 0.150 -0.594 0.150 -0.525 0.250 -0.405

0.590 -0.288 0.200 -0.469 0.210 -0.468 0.400 -0.397

0.630 -0.311 0.250 -0.350 0.250 -0.400 0,490 -0.385

0.700 -0.395 0,260 -0.365 0.340 -0.398 0.580 -0.424

0.750 -0.480 0.280 -0.368 0.370 -0.419 0.650 -0.612

0.810 -0,417 0.290 -0.345 0.400 -0.363 0.700 -0.591

0.840 -0457 0.310 -0,335 0.410 0.529** 0.750 -0.858

0.900 -0.255 0.320 -0.357 0.430 -0.407 0.800 -0.979

0.960 -0.080 0.340 -0.347 0.440 -0.435 0.830 -0.835

0.350 -0.173"* 0.460 -0.408 0.900 -0.381

0.370 -0.360 0.490 -0.400 0.960 -0.404

0.380 -0.362 0.500 -0.449

0.400 -0.332 0.520 -0.473

0.410 -0.350 0.540 -0.446

0.430 -0.336 0.550 -0.433

0,440 -0.337 0.580 -0.448

0.460 -0,343 0.600 -0.501

0,470 -0,378 0.610 -0.513

0.490 -0.377 0.650 -0.653

0.500 -0,385 0.700 -0.666

0.520 -0.345 0.750 -0.737

0.530 -0.390 0.820 -0.593

0.550 -0.422 0.890 -0.314

0.560 -0.439 0.900 -0.316

0.580 -0,401 0,960 -0.289

0.590 -0.467

0.600 -0.443

0.640 -0.618

0,700 -0.708

0.750 -0.172"*

0.820 -0.623

0.870 -0.261

0.930 -0.281

0.960 -0.287

Lower Surface

0.020 - 1.154 0.020 -0.953 0.020 -0.760 0.020 -0.979

0.110 -0.187 0,060 -0.302 0.060 -0,141 0.060 0,014

0.230 -0.048 0.090 -0.140 0,090 -0,077 0.110 -0,188

0.400 0.014 0.120 -0.034 0.120 -0,072 0.250 -0.107

0.490 0.045 0.200 -0.062 0.200 -0.020 0,400 -0.049

0.630 2.343"* 0.260 0.033 0.250 -0.013 0.490 0.018

0.750 0.081 0.400 0,052 0.400 0,020 0.580 0.098

0.850 0,098 0.490 0,079 0,490 -0,102 0.650 0.295

0.900 0.173 0.580 0.121 0.580 0.152 0.750 0.476

0.960 0.128 0.640 0.277 0.650 -0.167 0.830 0.519

0.750 0,166 0.750 0,011 0.900 0.580

0.870 0,143 0.890 0,557 0.960 0.424

0.930 0.166 0.930 0,460

0.960 0.089 0.960 0.353

CN = 0,275 0,450 0,495 0.620

94
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-33-39-500, MINF = 0.610, Camber = 10/6, ALP'I" = 8,24, BETA = -0,10, QINF = 309.6,

RNPU = 3.1E+06, CNWP = 0.4955

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.093 0.000 0,807 0,000 0.803** 0.010 -0.836

0.060 -0559 0.020 -0.443 0,020 -0.547 0.020 -0.816

0.110 -0.770 0.040 -0.013 0.060 -0910"* 0,060 -1.520

0,200 -0.708 0.060 -0.963 0,090 - 1,259 0. 110 - 1.592

0.230 -0.614 0.090 -1.142 0,110 -1.492 0.140 -1,386

0.400 -0.411 0.130 -1.461 0.130 -3.844** 0.190 -3,844"*

0,490 -0.381 0.150 - 1.750 0.150 - 1.305 0,250 -0.726

0,590 -0.436 0.200 - 1,042 0.210 -0.951 0.400 -0,581

0,630 -0.465 0.250 -0,736 0,250 -0.769 0.490 -0.536

0.700 -0,547 0.260 -0.710 0.340 -0.687 0.580 -0.570

0.750 -0,654 0,280 -0.689 0,370 -0,676 0.650 -0.702

0.810 -0.600 0.290 -0.664 0.400 -0.597 0.700 -0.666

0.840 -0,661 0.310 -0.623 0.410 0,517"* 0.750 -0.833

0.900 -0.435 0.320 -0.644 0,430 -0.637 0.800 -0.705

0.960 -0.244 0.340 -0.613 0.440 -0,610 0.830 -0.634

0,350 -0.234** 0.460 -0,609 0.900 -0.380

0,370 -0.592 0.490 -0.581 0.960 -0.350

0.380 -0.615 0.500 -0.606

0,400 -0.332 0.520 -0.607

0.410 -0.568 0.540 -0.596

0430 -0,539 0.550 -0.588

0,440 -0.531 0,580 -0.587

0.460 -0.528 0.600 -0.639

0.470 -0.559 0.610 -0.646

0.490 -0.546 0.650 -0.769

0.500 -0.551 0.700 -0.750

0.520 -0.527 0.750 -0.802

0.530 -0.544 0.820 -0.492

0,550 -0,578 0.890 -0.372

0.560 -0.596 0.900 -0,371

0,580 -0.536 0,960 -0,343

0.590 -0.600

0.600 -0.572

0.640 -0.715

0.700 -0,780

0.750 -0.144"*

0.820 -0.504

0.870 -0.301

0.930 -0.325

0.960 -0.316

Lower Surface

0,020 -0.005 0.020 0,182 0,020 0,233 0,020 0.406

0.110 0.070 0.060 0.286 0.060 0,329 0,060 0.049

0.230 0.070 0.090 0,253 0.090 0,301 0.110 0.262

0.400 0.053 0.120 0.237 0.120 0,241 0.250 0.127

0.490 0.054 0.200 0.064 0.200 0.085 0.400 0.119

0.630 2.271 ** 0.260 0.225 0.250 0.198 0.490 0,144

0.750 0,048 0.400 0.163 0.400 0.162 0.580 0.196

0.850 0.060 0.490 0,167 0.490 -0.045 0.650 0,343

0,900 0,147 0.580 0.165 0.580 0.222 0,750 0.534

0.960 0.064 0,640 0.334 0.650 -0.139 0,830 0.562

0.750 0.208 0.750 0.040 0.900 0.629

0,870 0.21 l 0,890 0.607 0,960 0.437

0.930 0.201 0,930 0,499

0,960 0.102 0.960 0.335

CN = 0,561 0.853 0.869 1,004

95
Table C-2. Continued.

Flight 216, Wing sweep = 26 °. Ttme= 9-34-22-000, MINF = 0.605, Camber = 10/3, ALPT = 2.08, BETA = -0.27, QINF = 304.8,

RNPU = 3.1E+06, CNWP = 0.3029

rl = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.576 0.000 -0.376 0.000 0.511 ** 0.010 0.393

0.060 0.101 0.020 0.588 0.020 0.531 0.020 0.215

0.110 -0.247 0.040 0.347 0.060 -0.139"* 0.060 -0.332

0.200 -0.328 0.060 -0.046 0.090 -0.363 0.110 -0.705

0.230 -0.285 0.090 -0.279 0.110 -0,538 0.140 -0.610

0,400 -0.224 0.130 -0.513 0.130 -3.905 * * 0.190 -3.905 * *

0.490 -0.210 0.150 -0.601 0.150 -0.526 0.250 -0.415

0.590 -0.251 0.200 -0.482 0.210 -0.479 0.400 -0.399

0.630 -0,259 0.250 -0.354 0.250 -0.417 0.490 -0.374

0.700 -0.291 0.260 -0.362 0.340 -0.415 0.580 -0.437

0.750 -0.309 0.280 -0.357 0.370 -0.429 0.650 -0.612

0.810 -0.265 0.290 -0.357 0.400 -0.381 0.700 -0.591

0.840 -0.298 0.310 -0.339 0.410 0.525"* 0.750 -0.868

0.900 -0.201 0.320 -0.357 0.430 -0.424 0,800 -0.985

0.960 -0.068 0.340 -0.351 0.440 -0,434 0.830 -0.857

0.350 -0.171 "* 0.460 -0.417 0.900 -0.394

0.370 -0.350 0.490 -0.411 0.960 -0.430

0.380 -0.366 0.500 -0.437

0.400 -0.337 0.520 -0.461

0.410 -0.351 0.540 -0.455

0.430 -0.340 0.550 -0.448

0.440 -0.335 0.580 -0.415

0.460 -0.347 0.600 -0.503

0.470 -0.382 0.610 -0.514

0.490 -0.376 0.650 -0.693

0.500 -0.383 0.700 -0.671

0,520 -0.364 0.750 -0.745

0.530 -0.390 0.820 -0.597

0.550 -0.415 0.890 -0.326

0.560 -0.441 0.900 -0.341

0.580 -0.397 0.960 -0.315

0.590 -0.456

0.600 -0.417

0.640 -0.604

0.700 -0.692

0.750 -0,214"*

0.820 -0.607

0.870 -0.435

0.930 -0.286

0.960 -0.281

Lower Surface

0,020 - 1.257 0,020 -0.926 0.020 -0.756 0.020 -0.965

0.110 -0.207 0.060 -0,329 0.060 -0.148 0,060 0.004

0.230 -0,057 0.090 -0.136 0.090 -0.090 0,110 -0.195

0,400 -0,022 0.120 -0,029 0.120 -0.080 0.250 -0.118

0.490 0.005 0.200 -0.057 0.200 -0.029 0.400 -0.059

0.630 2.307"" 0.260 0.015 0.250 -0.022 0.490 0,000

0.750 0.013 0.400 0.030 0.400 0.010 0.580 0.087

0.850 0.033 0,490 0,057 0.490 -0.131 0.650 0.283

0.900 0.106 0.580 0.098 0.580 0.140 0,750 0.467

0,960 0.091 0.640 0.248 0.650 -0.206 0.830 0.5 ]7

0.750 0.109 0.750 -0.002 0.900 0.566

0.870 0.113 0.890 0.545 0,960 0.415

0.930 0.139 0.930 0.468

0.960 0.060 0.960 0.313

CN = 0.194 0.434 0.492 0.620

96
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-34-33-000, MINF = 0.601, Camber = 10/3, ALPT = 8.18, BETA = 0.19, QINF = 300.9,

RNPU = 3.1E+06, CNWP = 0.4915

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0081 0.000 0.819 0.000 0.832** 0.010 -0.854

0.060 -0.532 0.020 -0.413 0.020 -0.581 0.020 -0.834

0. 110 -0.786 0.040 -0.004 0.060 -0.962** 0.060 - 1.496

0.200 -0.672 0.060 -0.954 0.090 - 1.253 0. 110 - 1.603

0.230 -0.589 0.090 - 1.127 0.110 - 1.512 0.140 - 1.305

0.400 -0.379 0.130 - 1.439 0.130 -3.949"* 0.190 -3.949"*

0.490 -0.342 0.150 - 1.589 0.150 - 1.178 0.250 -0.713

0.590 -0.378 0.200 - 1.038 0.210 -0.954 0.400 -0.578

0.630 -0.385 0.250 -0.713 0.250 -0.764 0.490 -0.522

0.700 -0.407 0.260 -0.698 0.340 -0.671 0.580 -0.559

0.750 -0.427 0.280 -0.677 0.370 -0.666 0,650 -0.681

0.810 -0.383 0.290 -0.643 0.400 -0.579 0.700 -0.662

0.840 -0.423 0310 -0.609 0.4 l0 0.538"* 0750 -0.793

0.900 -0.329 0.320 -0.630 0.430 -0.635 0.800 -0.67 I

0.960 -0.189 0.340 -0.605 0.440 -0.616 0.830 -0.583

0.350 -0.225** 0.460 -0.593 0.900 -0.345

0.370 -0.574 0.490 -0.562 0.960 -0.338

0.380 -0.591 0.500 -0.590

0.400 -0,324 0.520 -0.618

0.410 -0.550 0,540 -0.609

0.430 -0.526 0.550 -0.589

0.440 -0.526 0.580 -0.581

0.460 -0.528 0.600 -0.627

0.470 -0.544 0.610 -0.632

0 490 -0.529 0.650 -0.761

0.500 -0.534 0.700 -0.747

0.520 -0.513 0.750 -0.793

0.530 -0,522 0.820 -0.501

0.550 -0,543 0.890 -0.345

0.560 -0.570 0,900 -0.370

0.580 -0.512 0.960 -0,336

0.590 -0.571

0.600 -0.549

0.640 -0.687

0.700 -0.757

0.750 -0.178"*

0.820 -0.584

0.870 -0.285

0,930 -0.299

0.960 -0.298

Lower Surface

0.020 0.001 0.020 0.196 0.020 0.245 0.020 0,424

0,1 I 0 0.078 0.060 0.296 0.060 0.344 0.060 0.057

0.230 0.070 0.090 0.260 0.090 0.311 O. 110 0.276

0.400 0,046 0.120 0.246 0.120 0.249 0.250 0.136

0.490 0.039 0,200 0.068 0.200 0.093 0.400 0.128

0,630 2.343"* 0.260 0.216 0,250 0,209 0.490 0.150

0.750 -0,003 0,400 0.162 0.400 0.168 0.580 0,183

0,850 0.007 0.490 0,134 0.490 -0.076 0.650 0.351

0.900 0.079 0,580 0.156 0.580 0.227 0.750 0,541

0.960 0.042 0.640 0,315 0.650 -0.180 0.830 0.581

0,750 0,156 0,750 0.033 0.900 0.635

0.870 0.173 0.890 0.594 0.960 0.444

0.930 0.172 0.930 0.501

0.960 0.081 0.960 0.331

CN = 0.469 0.824 0.854 0,992

97
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-34-37-000, MINF = 0.604, Camber = 10/3, ALPT = 12.05, BETA = 0.02, QINF = 304.6,

RNPU = 3.1E+06, CNWP = 0.7376

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.937 0.000 0.340 0.000 0.417 * * 0.010 -2.036

0.060 - 1.190 0.020 - 1.479 0.020 -2.067 0.020 -2.129

0.110 -1.224 0.040 0.010 0.060 - 1.374"* 0.060 -1.991

0.200 -0.934 0.060 - 1.660 0.090 -2.123 0.110 - 1.844

0.230 -0.808 0.090 -1.950 0.110 -2.202 0.140 -1.603

0.400 -0.538 0.130 - 1.598 0.130 -3.915"* 0.190 -3.915"*

0.490 -0.468 0.150 - 1.973 0.150 - 1.557 0.250 -0.786

0.590 -0.507 0.200 - 1.633 0.210 - 1.535 0.400 -0.645

0.630 -0.529 0.250 - 1.076 0.250 - 1.208 0.490 -0.556

0.700 -0.525 0.260 -0.961 0.340 -0.879 0.580 -0.555

0.750 -0.542 0.280 -0.889 0.370 -0.807 0.650 -0.604

0.810 -0.498 0.290 -0.795 0.400 -0.718 0.700 -0.595

0.840 -0.557 0.310 -0.737 0.410 0.518" * 0.750 -0.662

0.900 -0.433 0.320 -0.755 0.430 -0.716 0.800 -0.669

0.960 -0.287 0.340 -0.723 0.440 -0.702 0.830 -0.494

0.350 -0.247 =* 0.460 -0.672 0.900 -0.485

0.370 -0.672 0.490 -0.624 0.960 -0.449

0.380 -0.699 0.500 -0.646

0.400 -0.335 0.520 -0.682

0.410 -0.648 0.540 -0.639

0.430 -0.602 0.550 -0.610

0.440 -0.605 0.580 -0.631

0.460 -0.607 0.600 -0.650

0.470 -0.622 0.610 -0.635

0.490 -0.596 0.650 -0.768

0.500 -0.606 0.700 -0.702

0.520 -0.585 0.750 -0.751

0.530 -0.584 0.820 -0.668

0.550 -0.615 0.890 -0.371

0.560 -0.618 0.900 -0.342

0.580 -0.589 0.960 -0.300

0.590 -0.636

0.600 -0.59 I

0.640 -0.702

0.700 -0.765

0.750 -0.122"*

0.820 -0.533

0.870 -0.235

0.930 -0.216

0.960 -0.215

Lower Surface

0.020 0.344 0.020 0.585 0.020 0.607 0.020 0.697

0.110 0.221 0.060 0.513 0.060 0.551 0.060 0.081

0.230 0.117 0.090 0.455 0.090 0.501 0.110 0.480

0.400 0.085 0.120 0.394 0.120 0.410 0.250 0.270

0.490 0.097 0.200 0.128 0.200 0.141 0.400 0.231

0.630 2.301 ** 0.260 0.341 0.250 0.326 0.490 0.246

0.750 -0.004 0.400 0.241 0.400 0.258 0.580 0.263

0.850 -0.017 0.490 0.227 0.490 0.010 0.650 0.383

0.900 0.046 0.580 0.202 0.580 0.275 0.750 0.573

0.960 -0.003 0.640 0.340 0.650 -0.121 0.830 0.613

0.750 0.181 0.750 0.075 0.900 0.664

0.870 0.241 0.890 0.616 0.960 0.452

0.930 0.199 0.930 0.506

0.960 0.105 0.960 0.324

CN : 0.696 1.054 1.123 1.177

98
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-35-21-000, MINF = 0.596, Camber = 10/0. ALPT = 2.00, BETA = 0.17, QINF = 295.2,

RNPU = 3.0E+06, CNWP = 0.2870

11 = 0.93 0.76 0.59 0,40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 0597 0.000 -0.452 0.000 0.430"* 0.010 0.432

0.060 0.090 0.020 0.621 0.020 0.559 0.020 0.269

0. 110 -0.213 0040 0.372 0.060 -0.157"* 0.060 -0.263

0.200 -0.306 0.060 -0.021 0.090 -0.348 0.110 -0.633

0.230 -0,262 0.090 -0.249 0.110 -0.506 0.140 -0.581

0.400 -0,198 0.130 -0,476 0.130 -4,023 * * 0.190 -4.023 * *

0,490 -0.177 0.150 -0.573 0,150 -0.505 0.250 -0.398

0.590 -0,202 0.200 -0.451 0,210 -0.453 0.400 -0.389

0.630 -0.190 0.250 -0.332 0.250 -0.399 0.490 -0.363

0.700 -0.179 0.260 -0,344 0.340 -0.404 0.580 -0.424

0.750 -0.155 0.280 -0.330 0.370 -0.392 0,650 -0.606

0.810 -0.112 0.290 -0.330 0.400 -0.353 0,700 -0.584

0.840 -0.138 0.310 -0.319 0.410 0.551"* 0.750 -0.864

0.900 -0.129 0.320 -0.342 0.430 -0.413 0.800 -0.987

0.960 -0,032 0.340 -0.333 0.440 -0.411 0.830 -0.835

0.350 -0.161 ** 0.460 -0.407 0.900 -0.384

0.370 -0.329 0.490 -0.399 0.960 -0.425

0.380 -0.346 0,500 -0.428

0.400 -0.330 0,520 -0.455

0.410 -0.334 0.540 -0.440

0.430 -0.321 0.550 -0.430

0.440 -0.332 0.580 -0434

0A60 -0.328 0.600 -0.500

0.470 -0.360 0.610 -0.508

0.490 -0.353 0.650 -0.661

0.500 -0.362 0.700 -0,661

0.520 -0.334 0.750 -0.744

0.530 -0.368 0.820 -0.617

0,550 -0.397 0.890 -0,330

0,560 -0.411 0.900 -0.341

0.580 -0.381 0.960 -0.320

0.590 -0.426

0.600 -0.410

0.640 -0582

0.700 -0.671

0.750 -0.263**

0.820 -0.662

0.870 -0.606

0.930 -0.338

0.960 -0.337

Lower Surface

0.020 - 1.067 0.020 - 1.007 0.020 -0.865 0.020 - 1.087

0,110 -0.252 0.060 -0.375 0.060 -0,198 0.060 -0.002

O 230 -0.068 0.090 -0.205 0.090 -0.108 0,110 -0.206

0.400 -0.036 0.120 -0.079 0.120 -0.106 0.250 -0.124

0.490 -0.008 0.200 -0.068 0,200 -0.042 0.400 -0.058

0.630 2.391 ** 0.260 0.003 0,250 -0.028 0.490 0,003

0.750 -0.031 0.400 0.018 0.400 0.000 0.580 0.084

0.850 -0.013 0,490 0.038 0.490 -0,163 0.650 0.287

0.900 0.044 0.580 0,072 0.580 0.139 0.750 0.467

0,960 0.072 0.640 0.220 0.650 -0,246 0,830 0.511

0.750 0.036 0.750 -0.004 0.900 0,567

0.870 0.055 0.890 0.542 0.960 0.415

0,930 0.090 0.930 0.459

0.960 0.023 0.960 0.322

CN = 0.113 0.401 0.469 0.599

99
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-35-37-500, MINF = 0.606, Camber = 10/0, ALPT = 8.16, BETA = 0.22, QINF -- 305.5,

RNPU = 3.1E+06, CNWP = 0,4777

i"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.069 0.000 0.807 0.000 0.786** 0.010 -0.821

0.060 -0.526 0.020 -0.390 0.020 -0.545 0.020 -0.787

0. 110 -0.772 0.040 -0.492 0.060 -0.883** 0.060 -1.494

0.200 -0.656 0.060 -0.960 0,090 - 1.255 0.110 - 1.599

0.230 -0.583 0.090 - 1.122 0.110 - 1.501 0.140 - 1.332

0.400 -0.372 0.130 - 1.419 0.130 -3.896"* 0.190 -3.896"*

0.490 -0.318 0.150 - 1.669 0.150 - 1.205 0.250 -0.723

0.590 -0.3 ] 0 0.200 - 1.017 0.210 -0.937 0.400 -0.576

0.630 -0,313 0.250 -0.723 0.250 -0.762 0.490 -0.530

0.700 -0.274 0.260 -0.701 0.340 -0.667 0.580 -0.561

0,750 -0,254 0.280 -0.679 0.370 -0.669 0.650 -0.682

0.810 -0.215 0.290 -0.645 0.400 -0.584 0.700 -0.673

0.840 -0.261 0,310 -0.608 0.410 0.523"* 0.750 -0.809

0.900 -0.237 0,320 -0.628 0.430 -0.617 0.800 -0.688

0.960 -0.144 0.340 -0.588 0.440 -0.617 0, 830 -0.622

0.350 -0.217** 0.460 -0.585 0.900 -0.356

0.370 -0.575 0.490 -0.574 0,960 -0.353

0.380 -0.593 0.500 -0.601

0.400 -0.329 0.520 -0.613

0.410 -0.546 0.540 -0.592

0.430 -0.501 0.550 -0.575

0.440 -0.505 0.580 -0.575

0.460 -0.517 0.600 -0.612

0.470 -0.531 0.610 -0.643

0.490 -0,508 0.650 -0.774

0.500 -0.525 0.700 -0.753

0.520 -0.481 0.750 -0.809

0.530 -0.510 0.820 -0.514

0.550 -0.547 0.890 -0.388

0.560 -0.564 0.900 -0.375

0.580 -0.491 0.960 -0.365

0.590 -0.557

0.600 -0.537

0.640 -0.681

0.700 -0.759

0.750 -0.242"*

0.820 -0.633

0.870 -0,434

0.930 -0.333

0,960 -0.339

Lower Surface

0.020 -0.029 0.020 0.170 0.020 0.235 0,020 0.397

0.110 0.056 0.060 0.268 0.060 0.325 0.060 0.032

0.230 0,053 0.090 0.241 0.090 0.295 0.110 0.271

0.400 0.021 0.120 0.225 0.120 0.229 0.250 0.120

0.490 0.004 0.200 0.057 0.200 0,079 0.400 0.113

0.630 2.301 ** 0.260 0.199 0.250 0.185 0.490 0.138

0.750 -0.072 0.400 O. 143 0.400 O. 155 0.580 O. 198

0.850 -0.060 0.490 0.1 40 0.490 -0.096 0.650 0.340

0.900 -0.004 0.580 0.126 0.580 0.225 0.750 0.532

0.960 0.013 0.640 0.297 0.650 -0.212 0.830 0.583

0.750 0.076 0.750 0.029 0.900 0.628

0.870 0.105 0.890 0.600 0.960 0.434

0.930 0.114 0.930 0.491

0.960 0.031 0.960 0.341

CN = 0.375 0.815 0.847 0.991

100
Table C-2. Continued.

Flight 216, Wing sweep = 26 °. Time = 9-35-42-500, MINF = 0.601, Camber = 1010, ALPT = 11.92, BETA = -0.04, QINF = 3009.

RNPU = 3.1E+06, CNWP = 0.7079

rl = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x./c CP x./c CP

0.020 -0.888 0.000 0.386 0.000 0,432"* 0.010 - 1.992

0.060 - 1.113 0.020 - 1.433 0.020 -2.000 0.020 -2.04 t

0,110 -I.193 0.040 -0.011 0060 -1.332"* 0.060 -2.040

0.200 -0.894 0.060 - 1.661 0,090 -2,087 0.110 - 1.760

0.230 -0,737 0.090 - 1,908 0.1 I0 -2,180 0.140 - 1.420

0,400 -0,496 0,130 - 1.614 0.130 - 3.959" * 0.190 -3.959"*

0.490 -0.419 0.150 -2.008 0.150 -1,654 0.250 -0.835

0,590 -0.432 0.200 - 1.601 0.210 - 1.573 0,400 -0.622

0.630 -0.428 0.250 -0,898 0.250 - 1.040 0.490 -0,518

0.700 -0.392 0,260 -0,815 0.340 -0,743 0.580 -0.520

0,750 -0.347 0.280 -0.789 0.370 -0.719 0,650 -0.572

0.810 -0.308 0.290 -0.737 0.400 -0.598 0.700 -0,552

0.840 -0.360 0,310 -0.699 0.410 0,527" * 0.750 -0.613

0.900 -0.329 0.320 -0.713 0.430 -0.647 0.800 -0.591

0.960 -0.220 0,340 -0.688 0.440 -0.639 0,830 -0.438

0.350 -0,259"* 0.460 -0.619 0,900 -0.421

0.370 -0.655 0.490 -0.589 0.960 -0.401

0.380 -0.682 0,500 -0.609

0.400 -0.350 0.520 -0.634

0,410 -0.622 0.540 -0.617

0.430 -0.600 0.550 -0,594

0.440 -0.581 0.580 -0.580

0,460 -0.592 0.600 -0.633

0.470 -0.616 0,610 -0.627

0.490 -0.593 0.650 -0.793

0.500 -0,591 0.700 -0,726

0,520 -0.557 0,750 -0.783

0,530 -0.571 0,820 -0.674

0.550 -0.598 0.890 -0.367

0,560 -0,608 0.900 -0.358

0.580 -0.567 0,960 -0.311

0.590 -0.615

0.600 -0.585

0.640 -0.711

0.700 -0.782

0.750 -0,218"*

0,820 -0.555

0.870 -0.347

0.930 -0,300

0,960 -0.313

Lower Surface

0.020 0.322 0,020 0.556 0.020 0.597 0.020 0,695

0.110 0.201 0.060 0.498 0.060 0.546 0.060 0.07 I

0,230 0.107 0,090 0.440 0,090 0.486 0.110 0,495

0.400 0.075 0.120 0,373 0.120 0.395 0,250 0,272

0.490 0.057 0.200 0.100 0.200 0,125 0.400 0,233

0,630 2.332** 0,260 0.323 0,250 0.329 0.490 0.238

0.750 -0,057 0.400 0,236 0.400 0.245 0.580 0.255

0.850 -0.078 0.490 0.204 0.490 -0.044 0,650 0,392

0,900 -0.016 0,580 0.186 0.580 0.281 0.750 0.578

0.960 -0.022 0.640 0.322 0,650 -0.190 0,830 0,599

0.750 0.108 0.750 0.036 0.900 0.652

0,870 0.149 0,890 0.626 0.960 0.444

0,930 0.147 0.930 0.515

0.960 0.063 0.960 0.353

CN = 0.585 1,021 1.082 1.138

101
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-6-58-500, MINF = 0.600, Camber = 0/2, ALPT = 7,01, BETA = 0.60, QINF = 276.3,

RNPU = 2.8E+06. CNWP = 0,2999

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.575 0.000 0,601 0.000 -7.991 * * 0.010 -2.228 * *

0.060 -0.376 0,020 - 1.110"* 0.020 - 1.242'* 0.020 -1,383"*

0.110 -0,287 0.040 -0,721 0.060 - 1,762"* 0.060 -0.954

0.200 -0.284 0.060 -0.618 0.090 -0.616 0.110 -0.679

0,230 -0.282 0.099 -0.486 0.110 -0.574 0.140 2.071 **

0.400 -0.190 0.130 -0.510 0.130 -0.605 0.190 -7.847"*

0.490 -0.178 0.150 -0.4.44 0.150 -0.462 0,250 -0.478

0.590 -0.202 0,200 -0,404 0,210 -0.554 0.400 -0.362

0.630 -0.212 0.250 -0.368 0.250 -0.452 0.490 -0.322

0,700 -0.229 0.260 -0.364 0.340 -0,393 0.580 -0,309

0.750 -0.186 0.280 -0.359 0,370 -0.395 0.650 -0.370

0.810 -0.191 0.290 -0.359 0.400 -0.353 0,700 -0.324

0.840 -0.197 0.310 -0.326 0,410 -0.325 0.750 -0.318

0.900 -0. I 12 0.320 -0.331 0.430 -0.357 0.800 -0.247

0.960 -0.021 0.340 -0.3.34 0.440 -0.354 0.830 -0,274

0.350 -0.103"* 0.460 -0.330 0.900 -0.143

0.370 -0.315 0.490 -0.276 0.960 0.012

0.380 -0.289 0,500 -0.312

0.400 -0.256 0.520 -0.330

0.410 -0.284 0.540 -0.302

0.430 -0.274 0.550 -0.282

0.440 -0,270 0,580 -0,265

0.460 -0.278 0.600 -0.313

0.470 -0.322 0.610 -0.238

0.490 -0.268 0.650 -4,889 *°

0,500 -0.261 0.700 -0.315

0.520 -0.259 0.750 -0.260

0.530 -0,249 0.820 -0.284

0.550 -0.249 0.890 -0.121

0.560 -0.260 0,900 -0.103

0.580 -0.227 0.960 -0.026

0.59(} -0.263

0.600 -0.255

0,640 ...4.714"*

0.700 -0.267

0.750 -0.241

0.820 -4.902**

0.870 -0.183

0,930 -0.076

0.960 -0.021

Lower Surface

0.020 0. l I 1 0.020 0.271 0,020 0.374 0.020 0.666

0.110 -0.031 0.060 0.211 0.060 0.263 0.060 1.589"*

0,230 0.035 0.090 0.144 0.090 0.184 0.110 0.125

0.400 -0.031 0.120 0.053 0.120 0.039 0.250 -0.037

0.490 -0,047 0.200 0.070 0.200 0.091 0.400 -0.058

0.630 1.636"* 0.260 -0.012 0,250 -0.023 0.490 -0,097

0.750 0.018 0.400 -4,921 * * 0.400 -0.047 0,580 -0.135

0.850 0.082 0.490 -0,055 0.490 0,002 0.650 -0.027

0,900 0.126 0.580 -0.025 0.580 -0.111 0.750 0.173

0.960 0.124 0.640 0.289 0.650 0.013 0,830 0.271

0.750 0.125 0.750 0.242 0.900 0.335

0,870 0,216 0.890 ******** 0.960 0.258

0.930 0,183 0.930 0.228

0.960 0.118 0,960 -4,920**

CN = 0.215 0.377 0.394 0.404

102
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-7-40-000, MINF = 0.604, Camber = 2/2, ALPT = 6.99, BETA = 0.63, QINF = 279.9,

RNPU = 2.9E+06. CNWP = 0.3048

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.396 0.000 0.789 0.000 -7.884'* 0.0t0 - 1.948"*

0.060 -0,329 0.020 -0.734"* 0.020 -0.985"* 0.020 - 1.001 **

0.1 I 0 -0.379 0.040 -0.585 0.060 - 1.697" * 0.060 -0.984

0.200 -0.319 0,060 -0.591 0.090 -0.662 0,110 -0.784

0.230 -0.356 0.090 -0.524 0.110 -0.662 0.140 2.060**

0.400 -0.205 O. 130 -0.578 O. 130 -0.711 O. 190 -7.742" *

0.490 -0.189 O. 150 -0.542 O. 150 -0.534 0.250 -0.454

0.590 -0.201 0.200 -0.461 0.210 -0.595 0.400 -0.370

0.630 -0.207 0.250 -0.374 0.250 -0.467 0.490 -0.341

0.700 -0.227 0.260 -0.386 0.340 -0.410 0.580 -0.303

0.750 -0.189 0.280 -0.381 0.370 -0.396 0.650 -0.371

0.810 -0.203 0.290 -0.371 0.400 -0.370 0.700 -0.306

0.840 -0.192 0.310 -0.351 0,410 -0.335 0.750 -0.311

0.900 -0.113 0.320 -0.338 0.430 -0.366 0.800 -0.257

0.960 -0.019 0.340 -0.357 0.440 -0.358 0.830 -0.278

0,350 -0.100"* 0.460 -0.335 0.900 -0.149

0.370 -0.324 0.490 -0.334 0.960 -0.001

0.380 -0.297 0.500 -0.315

0.400 -0.251 0.520 -0.324

0.410 -0.296 0.540 -0.310

0.430 -0.268 0.550 -0.290

0.440 -0.274 0.580 -0.259

0.460 -0.298 0.600 -0.319

0.470 -0.301 0.610 -0.233

0.490 -0.270 0.650 -4.823**

0500 -0.255 0.700 -0.320

0.520 -0.253 0250 -0.266

0.530 -0.251 0.820 -0.278

0.550 -0.263 0.890 -0.122

0,560 -0.274 0.900 -0.105

0.580 -0.229 0.960 -0.027

0.590 -0.252

0.600 -0.276

0.640 -4.650**

0.700 -0,269

0.750 -0.239

0.820 -4.836**

0.870 -0.178

0,930 -0.080

0.960 -0.018

Lower Surface

0.020 0.019 0.020 O.135 0.020 0.263 0.020 0.544

O. 110 -0.058 0.060 O.175 0.060 0.234 0.060 1,570"*

0.230 -0,028 0.090 0.116 0.090 0.157 0.110 0.104

0.400 -0,032 O. 120 0.054 0.120 0.023 0.250 -0.034

0.49t3 -0.036 0.200 0.010 0.200 0,070 0.400 -0.051

0.630 1,617" * 0.260 0.006 0.250 -0.013 0.490 -0.093

0.750 0.024 0.400 -4.855** 0.400 -0.044 0.580 -0.120

0.850 0.084 0.490 -0.052 0.490 -0,011 0.650 -0.047

0,900 0.130 0.580 -0,022 0.580 -0.107 0.750 O.179

0.960 O. 120 0,640 0.288 0.650 0.015 0.830 0.274

0.750 0.126 0.750 0.233 0.900 0,337

0.870 0.215 0.890 ******** 0.960 0.257

0.930 0.195 0.930 0.236

0.960 O. 115 0.960 -4.853**

CN = 0,221 0.384 0407 0.417

103
Table C-2, Continued.

Flight 198, Wing sweep = 26 °, Time = 13-7-42-000, MINF = 0.605, Camber = 3/2, ALPT = 7.05, BETA = 0.60, QINF = 280,6,

RNPU = 2.9E+06. CNWP = 0.3033

rl = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0.311 0.000 0.827 0.000 -7.864"* 0.010 - 1.875"*

0.060 -0.328 0.020 -0.652** 0.020 -0.869** 0.020 -0.931 **

O. 110 -0.341 0.040 -0.534 0.060 - 1.632** 0.060 -0.982

0.200 -0,346 0.060 -0,589 0.090 -0,671 0.110 -0.814

0,230 -0.315 0.090 -0.531 0.110 -0.689 0,140 2.042**

0.400 -0.205 0.130 -0,607 0.130 -0.764 0.190 -7.723 **

0.490 -0.200 0.150 -0,566 0.150 -0,551 0.250 -0.498

0.590 -0.204 0.200 -0.483 0.210 -0.604 0.400 -0,369

0.630 -0.210 0,250 -0.380 0,250 -0.474 0.490 -0.325

0.700 -0.227 0,260 -0,385 0.340 -0,417 0,580 -0.313

0.750 -0.188 0,280 -0,379 0.370 -0,395 0,650 -0.386

0.8 t 0 -0,194 0.290 -0.380 0.400 -0.369 0.700 -0.327

0,840 -0,191 0.310 -0.354 0,410 -0.343 0.750 -0.318

0.900 -0.110 0,320 -0.347 0.430 -0.365 0.800 -0.256

0.960 -0,018 0.340 -0.349 0,440 -0.357 0.830 -0.277

0,350 -0.094** 0.460 -0,334 0.900 -0.158

0.370 -0.323 0.490 -0.333 0.960 0,006

0.380 -0301 0.500 -0.325

0,400 -0.250 0,520 -0.323

0.410 -0,295 0,540 -0,309

0.430 -0,280 0.550 -0.289

0.440 -0.276 0.580 -0.22 I

0.460 -0.297 0,600 -0.334

0.470 -0,300 0.610 -0,232

0.490 -0.274 0.650 -4.811 **

0.500 -0.260 0.700 -0.308

0.520 -0.260 0,750 -0.269

0.530 -0,254 0.820 -0.277

0.550 -0.253 0.890 -0.125

0.560 -0.280 0.900 -0.1 04

0.580 -0,228 0,960 -0,023

0.590 -0.270

Q600 -0,280

0.640 ...4.638**

0.700 -0.268

0,750 -0.238

0.820 -4.824**

0.870 -0.185

0,930 -0,080

0,960 -0,018

Lower Surface

0,020 -0.022 0,020 0,086 0.020 0.205 0,020 0.498

O.I I 0 -0.049 0.060 O. 139 0.060 0.219 0.060 1.566**

0.230 0.013 0.090 0.097 0.090 0.146 0.110 0.104

0.400 -0.024 O. 120 0.038 O. 120 0.023 0.250 -0.034

0,490 -0,044 0,200 0.002 0.200 0.034 0.400 -0.051

0.630 1.613"* 0.260 0.007 0,250 -0,005 0,490 -0,093

0,750 0.020 0.400 -4,842** 0,400 -0.044 0,580 -0,130

0,850 0.084 0.490 -0.051 0,490 -0.010 0,650 -0.047

0.900 0.126 0.580 -0,026 0.580 -0.107 0,750 0.178

0.960 0.125 0,640 0,284 0.650 0.015 0.830 0.269

0.750 0.126 0.750 0,233 0.900 0,336

0.870 0.200 0,890 ******** 0.960 0.259

0.930 0.210 0.930 0.235

0.960 0.119 0.960 -4.841"*

CN = 0.220 0.380 0.408 0,429

104
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-7-45-500, MINF = 0,605. Camber = 4/2, ALPT = 6.99, BETA = 0.55, QINF = 280.6.

RNPU = 2.9E+06, CNWP = 0.3034

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.158 0000 0.863 0.000 -7,863"* 0,010 - 1.422"*

0,060 -0.287 0.020 -0.467"* 0,020 -0,687"* 0.020 -0,850"*

0. 110 -0,352 0.040 -0,461 0.060 -1.657** 0,060 -0,980

0.200 -0,358 0.060 -0.538 0,090 -0,692 0.110 -0,865

0.230 -0,333 0.090 -0,539 0.110 -0,726 0,140 2.037**

0.400 -0.211 0.130 -0.630 0.130 -0.811 0.190 -7.721 **

0,490 -0.191 0.150 -0.619 0.150 -0.584 0.250 -0.511

0,590 -0.207 0.200 -0.511 0.210 -0.612 0,400 -0.367

0,630 -0.209 0.250 -0.399 0.250 -0,480 0,490 -0.323

0,700 -0,225 0.260 -0,397 0,340 -0.415 0.580 -0.300

0,750 -0.187 0,280 -0,387 0.370 -0.401 0,650 -0,369

0.810 -0.192 0.290 -0,359 0.400 -0,367 0.700 -0.326

0,840 -0.190 0.310 -0.347 0,410 -0,333 0.750 -0.316

0.900 -0.109 0.320 -0.345 0,430 -0,364 0,800 -0.254

0,960 -0,017 0.340 -0,354 0.440 -0,367 0.830 -0.275

0.350 -0.092"* 0.460 -0.332 0.900 -0.157

0,370 -0,326 0.490 -0.323 0.960 0,007

0.380 -0,300 0.500 -0,323

0,400 -0.260 0.520 -0.321

0.410 -0.296 0.540 -0.322

0.430 -0,278 0.550 -0,287

0.440 -0.281 0.580 -0.275

0.460 -0.295 0,600 -0.317

0,470 -0,299 0.610 -0,245

0,490 -0.272 0,650 -4,809**

0.500 -0,264 0,700 -0.314

0.520 -0.267 0,750 -0.263

0.530 -0,256 0,820 -0,275

0,550 -0,260 0,890 -0.124

0,560 -0.258 0.900 -0.103

0.580 -0,233 0.960 -0.02 I

0.590 -0,268

0,600 -0,273

0,640 -4.637**

0,700 -0.271

0,750 -0.240

0,820 -4,822**

0,870 -O176

0,930 -0.078

0.960 -0.016

Lower Surface

0.020 -0.101 0.020 0.010 0.020 0.138 0.020 0.421

0.110 -0,055 0,060 0.121 0.060 0.193 0.060 1.568 **

0,230 0,055 0,090 0,086 0,090 0.132 0.110 0,073

0,400 -0,030 0.120 0,040 0.120 0,006 0,250 -0.029

0490 -0,042 0.200 0.058 0.200 0,046 0,400 -0,057

0.630 1.614"* 0.260 0,016 0.250 -0.003 0,490 -0,095

0,750 0.018 0.400 -4.841 ** 0,400 -0.053 0.580 -0.128

0.850 0.085 0.490 -0.050 0.490 0,007 0,650 -0,030

0.900 0.131 0,580 -0.020 0,580 -0.113 0.750 0.170

0.960 0,122 0.640 0,286 0,650 0.017 0.830 0.271

0,750 0,127 0.750 0,234 0,900 0.338

0,870 0.227 0.890 ******** 0.960 0,258

0,930 0.192 0,930 0.233

0,960 0.120 0,960 -4,840**

CN = 0,227 0.385 0.412 0,431

105
Table C-2. Continued.

Flight 198, Wing sweep = 26 °. Time = 13-7-48-500, MINF = 0.606, Camber = 5/2, ALPT = 7.03, BETA = 0.60, QINF = 282.0,

RNPU = 2.9E+06, CNWP = 0.3168

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0,065 0.000 0.868 0,000 -7.824 * * 0.010 -0,967 * *

0,060 -0,236 0.020 -0,342"* 0,020 -0,559"* 0.020 -0.812"*

0 110 -0.386 0,040 -0.409 0,060 - 1.622** 0.060 -0.997

0.200 -0,384 0,060 -0.551 0,090 -0,733 0.110 -0.955

0,230 -0.331 0.090 -0.564 0.110 -0,790 0.140 2.027"*

0.400 -0.210 0.130 -0,689 0.130 -0,884 0.190 -7,683 **

0.490 -0.197 0.150 -0.679 0.150 -0.634 0.250 -0.523

0.590 -0.201 0,200 -0,555 0.210 -0.649 0.400 -0.372

0.630 -0.211 0.250 -0.411 0.250 -0.493 0.490 -0.322

0.700 -0.228 0.260 -0.410 0,340 -0.430 0.580 -0.309

0.750 -0.190 0.280 -0.404 0,370 -0.416 0.650 -0.376

0.810 -0.191 0.290 -0.386 0,400 -0,388 0.700 -0,324

0.840 -0.197 0.310 -0.355 0.410 -0.347 0.750 -0.315

0,900 -0.113 0.320 -0.361 0,430 -0.378 0.800 -0.253

0,960 -0.016 0,340 -0.360 0.440 -0.365 0.830 -0.274

0,350 -0.091 ** 0,460 -0.342 0.900 -0.156

0.370 -0.335 0,490 -0,337 0,960 0.008

0.380 -0.312 0,500 -0.331

0.400 -0.270 0.520 -0.337

0.410 -0.305 0.540 -0.321

0.430 -0302 0.550 -0.299

0,440 -0.289 0.580 -0,255

0,460 -0.306 0,600 -0.315

0.470 -0.304 0.610 -0.244

0.490 -0.279 0,650 -4,785**

0,500 -0.285 0,700 -0.319

0,520 -0.241 0,750 -0.269

0.530 -0.258 0.820 -0.278

0,550 -0.268 0,890 -0.123

0.560 -0,277 0.900 -0.102

0.580 -0,232 0,960 -0.025

0,590 -0.257

0.600 -0,282

0,640 -4.614"*

0700 -0.273

0.750 -0.231

0,820 -4.799**

0.870 -0.186

0.930 -0.078

0,960 -0,016

Lower Surface

0,020 -0.161 0.020 -0,034 0.020 0.105 0.020 0.413

0.110 -0.054 0.060 0.125 0.060 0.192 0.060 1.561 **

0,230 0.051 0.090 0.080 0.090 0.131 0.110 0.062

0.400 -0.022 0.120 0,056 0.120 0.015 0.250 -0.025

0.490 -0.038 0.200 0.061 0.200 0.050 0.400 -0.049

0.630 1,607"* 0.260 0.024 0,250 0,005 0.490 -0.090

0,750 0,010 0.400 -4.817"* 0.400 -0,041 0.580 -0.128

0.850 0.085 0.490 -0.045 0,490 0,007 0.650 -0.030

0,900 0.134 0.580 -0.020 0.580 -0.108 0.750 0.169

0.960 0.126 0.640 0,295 0.650 0.017 0,830 0.279

0,750 0.127 0.750 0.241 0.900 0,336

0,870 0.226 0,890 ******** 0.960 0.257

0.930 0.192 0.930 0,236

0.960 0.120 0,960 -4.816"*

CN = 0.228 0.401 0.431 0,448

106
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-7-52-500, MINF = 0.610, Camber = 6/2, ALPT = 6.93, BETA = 0.52. QINF = 285.2,

RNPU = 2.9E+06, CNWP = 0.3034

r I = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c C P x/c C P x/c CP

0.020 0.099 0.000 0.810 0.000 -7.737** 0,010 -0.846"*

0.060 -0.225 0.020 -0.136"* 0.020 -0.355'* 0.020 -0.605"*

0 110 -0.383 0.040 -0.286 0.060 - 1.585"* 0.060 -0.921

0.200 -0.408 0.060 -0.498 0.090 -0.715 0,110 - 1,007

0.230 -0.348 0,090 -0.559 0.110 -0.801 0.140 2.003**

0.400 -0.209 0.130 -0.710 0.130 -0.939 0.190 -7.597 * *

0.490 -0.193 0. [ 50 -0.723 0.150 -0.646 0.250 -0.504

0.590 -0.208 0.200 -0.573 0.210 -0.643 0.400 -0.369

0.630 -0.206 0.250 -0.421 0.250 -0.489 0.490 -0.329

0.700 -0.222 0.260 -0.414 0.340 -0.426 0.580 -0.307

0.750 -0.185 0.280 -0.401 0.370 -0A04 0.650 -0.373

0.810 -0.190 0.290 -0.392 0.400 -0.370 0.700 -0.321

0.840 -0.196 0.310 -0.355 0,410 -0.345 0.750 -0.320

0.900 -0A 10 0.320 -0.358 0.430 -0.375 0.800 -0.259

0.960 -0.017 0.340 -0357 0.440 -0,362 0.830 -0.282

0.350 -0.102"* 0,460 -0.340 0.900 -0.165

0.370 -0,337 0.490 -0.303 0.960 0.006

0.380 -0.310 0.500 -0.319

0.400 -0.257 0.520 -0.335

0.410 -0.303 0.540 -0.318

0.430 -0.287 0.550 -0.296

0.440 -0.277 0.580 -0.262

0.460 -0.304 0.600 -0.326

0.470 -0.295 0.610 -0.242

0,490 -0.277 0,650 -4732"*

0,500 -0.238 0.700 -0,325

0.520 -0.264 0.750 -0,267

0,530 -0,256 0.820 -0.267

0.550 -0,267 0.890 -0.127

0.560 -0.268 0.900 -0.105

0.580 -0.237 0.960 -0.022

0.590 -0.273

0.600 -0.280

0.640 -4.563**

0.700 -0.267

0.750 -0.241

0.820 -4.745"*

0.870 -0.185

0.930 -0.070

0.960 -0.021

Lower Surface

0.020 -0.209 0.020 -0.144 0.020 -0.013 0.020 0.226

O. 110 -0.065 0.060 0.083 0.060 O. 147 0.060 1,542"*

0.230 0.029 0.090 0,056 0.090 O. 102 O. 110 0.081

0.400 -0.016 O, 120 0.078 O, 120 -0.004 0,250 -0.026

0.490 -0.039 0,200 0.041 0.200 0.034 0,400 -0,057

0.630 1.587"* 0.260 0.030 0,250 0.004 0.490 -0.098

0.750 0.017 0.400 -4.763 * * 0.400 -0.042 0.580 -0.138

0.850 0.083 0.490 -0.050 0.490 0.005 0.650 -0.038

0.900 O. 131 0.580 -0.021 0.580 -0.112 0.750 0,176

0.960 0.128 0.640 0.283 0.650 0.016 0.830 0.274

0.750 0.129 0.750 0.241 0 900 0.337

0.870 0.222 0.890 ******** 0.960 0.259

0.930 0.196 0.930 0.232

0.960 O. I 17 0,960 -4.762"*

CN = 0.226 0.392 0.423 0.453

107
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-7-55-500, MINF = 0,611, Camber = 7/2, ALPT = 7.00, BETA = 0.52, QINF = 286.6,

RNPU = 2.9E+06, CNWP = 0.3070

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 O. 165 0.000 0.767 0.000 -7.699** 0.010 -0.709**

0,060 -0.223 0.020 -0.033"* 0,020 -0.270** 0.020 -0.513**

0.110 -0,405 0.040 -0.244 0.060 -1.544"* 0,060 -0,982

0,200 -0.432 0.060 -0.479 0,090 -0.733 0.110 - 1.085

0,230 -0.346 0.090 -0.592 0.110 -0,873 0.140 1.993"*

0.400 -0,208 0.130 -0.774 0.130 - 1.023 0.190 -7.560"*

0,490 -0.195 0.150 -0,790 0.150 -0.660 0.250 -0.515

0.590 -0,207 0.200 -0.610 0,210 -0,674 0.400 -0.375

0.630 -0.205 0,250 -0.433 0.250 -0.494 0,490 -0.327

0.700 -0.229 0.260 -0.418 0,340 -0.424 0,580 -0.305

0,750 -0.188 0,280 -0,417 0.370 -0.419 0.650 -0.371

0.810 -0.197 0,290 -0,404 0,400 -0.398 0,700 -0,320

0.840 -0.187 0.310 -0.367 0.410 -0.351 0.750 -0.318

0.900 -0.112 0.320 -0,370 0,430 -0.373 0,800 -0.257

0.960 -0,017 0.340 -0.370 0,440 -0.371 0,830 -0.280

0.350 -0.113"* 0,460 -0,350 0,900 -0.154

0.370 -0.342 0490 -0.340 0.960 0.011

0,380 -0.318 0.500 -0.327

0.400 -0,278 0,520 -0,333

0.410 -0.311 0.540 -0.316

0,430 -0.298 0.550 -0,295

0,440 -0,288 0.580 -0.270

0.460 -0.308 0.600 -0,324

0,470 -0,300 0.610 -0.241

0,490 -0.279 0,650 -4,709**

0.500 -0.276 0,700 -0.323

0.520 -0,270 0,750 -0,273

0,530 -0,262 0,820 -0.283

0.550 -0,265 0,890 -0,126

0.560 -0.260 0.900 -0.107

0.580 -0.236 0.960 -0.021

0,590 -0,276

0,600 -0.278

0.640 -4.540"*

0.700 -0.277

0.750 -0.244

0820 -4.722**

0,870 -0.188

0.930 -0.081

0.960 -0.020

Lower Surface

0,020 -0,247 0020 -0.179 0.020 -0.045 0,020 0,171

0.110 -0.054 0.060 0.091 0.060 0.132 0,060 1,534"*

0.230 0.022 0,090 0.065 0.090 0.107 0. I I 0 0.113

0.400 -0,015 0.120 0,070 0.120 0.014 0.250 -0.019

0.490 -0.034 0,200 0.033 0.200 0,027 0.400 -0,056

0,630 1.580* * 0,260 0.045 0.250 0.012 0.490 -0.090

0,750 0.021 0,400 -4,740"* 0.400 -0,042 0.580 -0.137

0.850 0.083 0.490 -0,042 0.490 0.006 0.650 -0,030

0,900 0.130 0,580 -0.021 0,580 -0.103 0.750 0.176

0,960 0.123 0.640 0.286 0.650 0.016 0.830 0,273

0,750 0.133 0,750 0,240 0,900 0,336

0.870 0.240 0,890 ******** 0.960 0.258

0.930 0.195 0,930 0.239

0,960 0.121 0.960 -4.739**

CN = 0.231 0.408 0,437 0,472

108
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-7-59-000, MINF = 0.610, Camber = 8/2, ALPT = 6.99, BETA = 0.63, QINF = 285.5,

RNPU = 2.9E+06, CNWP = 0.3136

-q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.265 0.000 0.650 0.000 -7.730"* 0.010 -0.513'*

0.060 -0.195 0.020 O.109"* 0.020 -0. 119"* 0.020 -0.449'*

0. 110 -0.418 0.040 -0.170 0.060 - 1.570"* 0.060 -0.964

0.200 -0.441 0.060 -0.449 0.090 -0.747 0.110 - h 131

0,230 -0.407 0.090 -0.595 0. 110 -0.905 0.140 2.001 **

0.400 -0.217 0.130 -0.812 0.130 - 1.090 0.190 -7.591 **

0.490 -0.1% 0.150 -0.835 0.150 -0.715 0.250 -0.518

0.590 -0.208 0,200 -0.636 0.210 -0.682 0.400 -0.376

0.630 -0.206 0.250 -0.435 0,250 -0.503 0.490 -0.329

0.700 -0.226 0.260 -0,420 0.340 -0.426 0.580 -0,307

0.750 -0.184 0.280 -0,419 0.370 -0.412 0.650 -0,372

0.810 -0.166 0.290 -0.411 0400 -0.377 0.700 -0.321

0.840 -0.191 0.310 -0.368 0.410 -0.353 0.750 -0.320

0.900 -0.108 0.320 -0.372 0.430 -0.375 0.800 -0.251

0.960 -0,010 0.340 -0.371 0.440 -0.373 0.830 -0.281

0,350 -0.102"* 0,460 -0.345 0.900 -0.155

0.370 -0.344 0.490 -0.334 0.960 0.015

0.380 -0.319 0.500 -0.329

0.400 -0.268 0.520 -0.335

0.410 -0.309 0.540 -0,318

0.430 -0.299 0.550 -0.2%

0.440 -0.306 0.580 -0.281

0.460 -0.304 0,600 -0.312

0.470 -0.301 0.610 -0.242

0.490 -0,281 0.650 -4.728"*

0.500 -0272 0.700 -0.321

0.520 -0.271 0.750 -0.27 I

0,530 -0.260 0.820 -0.285

0.550 -0,266 0.890 -0.123

0,560 -0.281 0.900 -0 102

0.580 -0.237 0.960 -0.033

0.590 -0.278

0.600 -0.290

0.640 -4.559"*

0.700 -0.275

0.750 -0.241

0.820 -4.741 **

0.870 -0.185

0.930 -0.078

0.960 -0.017

Lower Surface

0,020 -0.278 0.020 -0.244 0,020 -0.112 0,020 0.071

0.110 -0.048 0.060 0.087 0.060 0.133 0.060 1.541 **

0.230 0018 0.090 0.059 0.090 0.102 0.110 0.081

0.400 -0.008 0.120 0,070 0.120 0.019 0.250 -0.012

0.490 -0.035 0.200 0.025 0.200 0.013 0.400 -0.049

0.630 1.586"* 0.260 0.053 0.250 0.019 0.490 -0.090

0.750 0.020 0.400 -4.759** 0.400 -0.042 0,580 -0.138

0.850 0.087 0.490 -0.042 0.490 0,005 0.650 -0D31

0.900 0,131 0.580 -0.017 0,580 -0.104 0.750 0.176

0.960 0.128 0.640 0.287 0.650 0.023 0.830 0.274

0.750 0.133 0.750 0.237 0900 0.337

0.870 0,222 0.890 ******** 0.960 0.259

0.930 0.1% 0.930 0.240

0.960 0.121 0.960 -4.758**

CN = 0.238 0.408 0.443 0.476

109
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-8-1-000, MINF = 0.609, Camber = 9/2, ALPT = 7.03, BETA = 0.60, QINF = 284.8,

RNPU = 2.9E+06, CNWP = 0.3253

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x,/c CP x/c CP

0.020 0.305 0.000 0,589 0,000 -7,750** 0.010 -0.427**

0.060 -0,188 0.020 0.128"* 0.020 -0.044"* 0.020 -0.385"*

0.110 -0.433 0.040 -0.142 0.060 -1.516"* 0.060 -0968

0.200 -0.464 0.060 -0.419 0.090 -0.773 0.110 -1.198

0.230 -0.370 0.090 -0.616 0.110 -0.956 0.140 2,023"*

0.400 -0.215 0.130 -0,850 0,130 -1.158 0.190 -7.611"*

0.490 -0.202 0.150 -0.885 0.150 -0,745 0.250 -0.521

0.590 -0.210 0,200 -0.668 0.210 -0.705 0,400 -0.379

0.630 -0.216 0.250 -0,437 0.250 -0.514 0.490 -0.331

0.700 -0.229 0,260 -0.438 0.340 -0.437 0,580 -0.309

0.750 -0.191 0.280 -0.432 0.370 -0.423 0.650 -0.375

0.810 -0.192 0.290 -0.423 0.400 -0.388 0,700 -0.324

0.84(} -0.198 0.310 -0.378 0.410 -0.355 0,750 -0.322

0.900 -0.112 0,320 -0,379 0.430 -0.394 0.800 -0.261

0,960 -0.019 0.340 -0.381 0.440 -0.375 0.830 -0.274

0.350 -0.126** 0.460 -0,351 0.900 -0.148

0.370 -0.350 0.490 -0.360 0.960 0.013

0,380 -0.326 0.500 -0.331

0.400 -0.270 0.520 -0,337

0.410 -0.315 0.540 -0.335

0.430 -0.302 0.550 -0,299

0.440 -0.295 0.580 -0.292

0.460 -0,306 0.600 -0.328

0.470 -0.270 0.610 -0.245

0.490 -0.287 0.650 -4.741 **

0.500 -0.280 0.700 -0.331

0.520 -0,282 0.750 -0,277

0.530 -0.266 0.820 -0.287

0.550 -0.269 0.890 -0.129

0.560 -0,290 0.900 -0.1 04

0,580 -0,246 0.960 -0.039

0.590 -0.280

0.600 -0.282

0.640 -4.571"*

0.700 -0.277

0.750 -0.247

0.820 -4.754"*

0.870 -0.191

0.930 -0.080

0,960 -0.019

Lower Surface

0,020 -0.368 0.020 -0.265 0.020 -0.147 0.020 0.029

0.110 -0.043 0.060 0.085 0.060 0.131 0,060 1,542 **

0.230 0.012 0.090 0.057 0.090 0.106 0. I 10 0.079

0.400 -0.006 0.120 0.099 0.120 0.021 0,250 -0.007

0.490 -0.033 0.200 0.020 0.200 0.011 0.400 -0.043

0,630 1.588"* 0.260 0,059 0,250 0.025 0.490 -0.092

0.750 0.023 0.400 -4.773** 0.400 -0.033 0,580 -0.129

0.850 0.085 0.490 -0.036 0.490 0.004 0.650 -0.032

0.900 0.129 0.580 -0.015 0.580 -0.106 0.750 0.175

0.960 0.126 0.640 0.289 0.650 0.018 0.830 0.273

0.750 0.131 0.750 0.240 0,900 0,336

0,870 0.220 0,890 ******** 0.960 0,258

0.930 0.194 0.930 0,238

0.960 0.116 0.960 -4.771"*

CN = 0.240 0.416 0.457 0.488

110
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-84-000, MINF = 0.608, Camber = 10/2, ALPT = 7.11, BETA = 0.63, QINF = 284.1,

RNPU = 2.9E+06, CNWP = 0.3151

rl = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 0.370 0.000 0.481 0.000 -7.771 ** 0.010 -0.296**

0.060 -0.17 l 0.020 0.209** 0.020 0.048"* 0.020 -0.299**

0.110 -0.448 0.040 -0.087 0,060 -1.521 ** 0.060 -0.973

0.200 -0.481 0.060 -0.422 0,090 -0.771 0.110 - 1.223

0.230 -0.393 0.090 -0.638 0.110 - 1.008 0.140 2.001 **

0.400 -0.221 0.130 -0.902 0.130 - 1.240 0.190 -7.631 **

0.490 -0.201 0.150 -0.939 0.150 -0.758 0.250 -0.539

0.590 -0.213 0.200 -0.695 0.210 -0.719 0.400 -0.389

0.630 -0.219 0,250 -0.468 0.250 -0,525 0.490 -0.334

0.700 -0.231 0.260 -0.448 0.340 -0.448 0.580 -0.3 l 2

0.750 -0,193 0.280 -0.435 0.370 -0.426 0.650 -0.369

0.810 -0.203 0.290 -0.426 0.400 -0.390 0.700 -0.315

0.840 -0.208 0.310 -0.384 0.410 -0.358 0.750 -0.317

0.900 -0.114 0.320 -0.386 0.430 -0.396 0.800 -0.256

0.960 -0.021 0.340 -0.384 0.440 -0.378 0.830 -0.277

0.350 -0.145** 0.460 -0.357 0.900 -0.150

0,370 -0.357 0.490 -0.347 0.960 0.007

0.380 -0.334 0.500 -0.344

0.400 -0.284 0.520 -0.340

0.410 -0.321 0.540 -0.338

0.430 -0.304 0.550 -0.30 l

0.440 -0.301 0.580 -0.276

0.460 -0.321 0.600 -0.331

0.470 -0.334 0.610 -0.247

0.490 -0.290 0.650 -4.755**

0.500 -0.282 0.700 -0.333

0.520 -0.293 0.750 -0.280

0.530 -0.272 0.820 -0.285

0.550 -0.271 0.890 -0.13 I

0560 -0.266 0.900 -0.106

0.580 -0.242 0.960 -0.025

0.590 -0.283

0.600 -0.290

0.640 -4.584**

0.700 -0.280

0.750 -0.250

0.820 -4.768**

0.870 -0.190

0.930 -0.086

0.960 -0.028

Lower Surface

0.020 -0.332 0.020 -0.300 0.020 -0.182 0.020 -0.047

0.110 -0.030 0.060 0.080 0.060 0.123 0.060 1.544**

0.230 0,010 0.090 0.062 0.090 0.110 0.110 0.099

0.400 -0.008 0.120 0.102 0. 120 0.033 0.250 -0.005

0.490 -0.031 0.200 0.014 0.200 0,002 0.400 -0.045

0.630 1.590** 0.260 0.072 0.250 0.031 0.490 °0.095

0.750 0.021 0.400 -4.786** 0.400 -0.035 0.580 -0.132

0.850 0.084 0.490 -0.038 0.490 0.002 0,650 -0.034

0.900 O. 128 0.580 -0.013 0.580 -0. I O0 0.750 0.173

0.960 0.120 0.640 0.288 0,650 0.020 0.830 0.272

0.750 0.130 0.750 0.235 0.900 0.335

0.870 0.248 0.890 ******** 0.960 0.250

0.930 0.193 0.930 0.237

0.960 0.118 0.960 -4.785**

CN = 0.246 0.429 0.463 0.497

111
Table C-2. Continued.

Flight 198, Wing sweep = 26 '_. Time = 13-8-8-000, MINF = 0,608, Camber = 11/2, ALPT = 7.19. BETA = 0.71, QINF = 283.9,

RNPU = 2.9E+06, CNWP = 0.3258

1"I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.452 0,000 0.289 0.000 -7.779 * * 0.010 -0.131 * *

0.060 -0,153 0.020 0.310"* 0.020 0.166"* 0.020 -0.212"*

0.110 -0.474 0.040 -0.021 0.060 - 1.471 * * 0.060 -0.953

0.200 -0.511 0.060 -0.408 0,090 -0.835 0.110 - 1.289

0.230 -0.415 0.090 -0.659 0,110 -1.077 0.140 2.013"*

0.400 -0.231 0.130 -0.967 0.130 - 1.344 0.190 -7,639"*

0.490 -0.211 0.150 - 1,017 0.150 -0.822 0.250 -0.541

0.590 -0.215 0.200 -0.732 0.210 -0.741 0.400 -0.391

0.630 -0.225 0.250 -0.484 0.250 -0,535 0.490 -0.336

0.700 -0.237 0,260 -0.457 0.340 -0,450 0.580 -0.325

0.750 -0.195 0.280 -0.446 0.370 -0,437 0.650 -0.371

0.810 -0.212 0.290 -0.438 0.400 -0.400 0.700 -0.317

0.840 -0,202 0.310 -0.393 0.410 -0,368 0.750 -0.319

0.900 -0.116 0.320 -0.393 0.430 -0.398 0.800 -0.258

0.960 -0.023 0.340 -0.394 0.440 -0.386 0.830 -0,279

0.350 -0.147"* 0.460 -0.359 0.900 -0.147

0.370 -0.363 0.490 -0.349 0.960 0.005

0.380 -0.341 0.500 -0.336

0.400 -0.298 0.520 -0.342

0.410 -0.327 0.540 -0.333

0,430 -0.307 0.550 -0,303

0.440 -0.306 0,580 -0.260

0.460 -0.323 0.600 -0.333

0.470 -0.288 0.610 -0.249

0.490 -0.296 0.650 -4 760"*

0.500 -0.290 0.700 -0.343

0.520 -0278 0.750 -0.278

0.530 -0.274 0.820 -0.287

0,550 -0.283 0,890 -0.129

0.560 -0.295 0.900 -0.102

0.580 -0,244 0.960 -0.019

0.590 -0.289

0.600 -0.287

0,640 -4.590"*

0.700 -0.282

0.750 -0.248

0.820 -4.773**

0.870 -0.192

0.930 -0.084

0.960 -0.022

Lower Surface

0.020 -0.402 0.020 -0.331 0.020 -0.217 0.020 -0.143

O. I I0 -0.011 0.060 0.070 0.060 0.114 0.060 1.544"*

0.230 0.000 0.090 0.072 0.090 0. I 13 0.110 0.098

0.400 -0.002 0.120 0.120 0.120 0,054 0.250 0.004

0.490 -0.025 0.200 0,005 0.200 -0.007 0.400 -0,047

0.630 1,589"* 0.260 0,086 0.250 0.045 0.490 -0.088

0.750 0.019 0.400 -4.791 * * 0.400 -0.027 0.580 -0.123

0.850 0.082 0.490 -0.036 0.499 0.000 0.650 -0.028

0.900 0,123 0.580 -0.011 0.580 -0.102 0.750 0.182

0.960 0.123 0.640 0.286 0.650 0.018 0.830 0,279

0.750 0,128 0.750 0.241 0.900 0.334

0.870 0.217 0.890 ******** 0.960 0.248

0.930 0,191 0.930 0,236

0.960 0.116 0.960 -4.790"*

CN = 0.257 0,434 0.477 0.512

112
Table C-2. Continued,

Flight 198, Wing sweep = 26 °, Time = 13-8-11-500, MINF = 0,607, Camber = 12/2, ALPT = 7,23, BETA = 0.63, QINF = 283.6,

RNPU = 2.9E+06, CNWP = 0.3378

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP xA" CP

0.020 0.492 0.000 O. 107 0.000 -7.787** 0.010 0.034**

0.060 -0.145 0.020 0.432"* 0.020 0.250"* 0.020 -0.102"*

0.110 -0.488 0.040 0.038 0.060 -1.500"* 0.060 -0.911

0,200 -0.513 0.060 -0.378 0,090 -0,826 0.110 - 1,291

0.230 -0,338 0.090 -0.670 0.110 -1.117 0.140 2.000**

0.400 -0.229 0.130 - 1.018 0.130 - 1.469 0.190 -7.647"*

0.490 -0.209 0.150 - 1.092 0.150 -0.851 0.250 -0.543

0.590 -0.225 0,200 -0.752 0.210 -0.764 0.400 -0.386

0,630 -0.223 0,250 -0.500 0.250 -0.545 0.490 -0.348

0.700 -0.231 0.260 -0.474 0.340 -0.452 0.580 -0.327

0.750 -0.201 0.280 -0.458 0.370 -0,439 0.650 -0,373

0.810 -0.198 0,290 -0.450 0.400 -0.402 0.700 -0,330

0.840 -0.204 0.310 -0.401 0.410 -0.370 0.750 -0.321

0900 -0.110 0.320 -0.400 0.430 -0.401 0.800 -0.260

0.960 -0.032 0.340 -0,403 0.440 -0.399 0.830 -0.281

0.350 -0.143 ** 0.460 -0,361 0,900 -0.144

0,370 -0,372 0,490 -0.351 0.960 0.008

0.380 -0.352 0.500 -0.348

0.400 -0.300 0.520 -0.344

0.410 -0.336 0.540 -0.342

0.430 -0.321 0.550 -0.305

0.440 -0,308 0.580 -0.271

0.460 -0.325 0.600 -0.335

0.470 -0.338 0,610 -0.266

0,490 -0.298 0.650 --4.766**

0.500 -0.298 0.700 -0.334

0.520 -0.289 0.750 -0.284

0.530 -0.280 0.820 -0.285

0.550 -0.285 0.890 -0.135

0.560 -0,290 0.900 -0,110

0,580 -0.253 0960 -0.029

0,590 -0.291

0.600 -0.299

0.640 -4.595"*

0.700 -0.288

0.750 -0.254

0.820 -4.779**

0.870 -0.194

0.930 -0.090

0.960 -0.024

Lower Surface

0.020 -0,886 0,020 -0.354 0,020 -0.252 0.020 -0.233

0.1 I 0 -0.020 0.060 0,068 0.060 0.126 0.060 1.543"*

0.230 -0.006 0.090 0.077 0.090 0.122 0.110 0.117

0.400 0.001 0.120 0.142 0,120 0.071 0.250 0.009

0.490 -0.038 0.200 0.003 0,200 -0.009 0.400 -0.04 1

0.630 1,589"* 0,260 0_092 0.250 0.051 0.490 -0,082

0.750 0.017 0.400 -4.797"* 0.400 -0.028 0.580 -0.125

0.850 0.076 0.490 -0.034 0.490 0.013 0.650 -0.030

0,900 0, 110 0,580 -0.013 0.580 -0.097 0,750 0.175

0.960 0.117 0.640 0.284 0.650 0.020 0.830 0.269

0.750 0.126 0.750 0.239 0,900 0.332

0.870 0.216 0.890 ******** 0,960 0.247

0.930 0.190 0.930 0.234

0.960 0A 11 0.960 -4.796**

CN = 0.245 0.443 0.488 0.517

113
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-8-14-500, MINF = 0.606, Camber = 13/2, ALFr = 7.27, BETA = 0.60, QINF = 282.3,

RNPU = 2.9E+06, CNWP = 0.3375

q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.534 0.000 -0.037 0.000 -7.827"* 0.010 0. 122"*

0.060 -0.118 0.020 0.474** 0.020 0.335"* 0.020 -0.022**

0.110 -0.505 0.040 0.086 0.060 - 1.442 ** 0.060 -0.940

0.200 -0.545 0.060 -0.349 0.090 -0.832 0.110 - 1.300

0.230 -0.421 0.090 -0.676 0.110 - 1.153 0.140 2.008"*

0.400 -0.236 0.130 - 1.060 0.130 - 1.561 0.190 -7.686 **

0.490 -0.212 0.150 - 1.134 0.150 -0.866 0.250 -0,548

0.590 -0.220 0,200 -0.775 0.210 -0.759 0.400 -0.390

0.630 -0.222 0.250 -0.504 0.250 -0.550 0.490 -0.342

0.700 -0.238 0.260 -0.471 0.340 -0.456 0.580 -0.320

0.750 -0.196 0.280 -0.462 0.370 -0.443 0.650 -0.377

0.810 -0,201 0.290 -0.454 0.400 -0.368 0.700 -0,323

0.840 -0.207 0.310 -0,405 0.410 -0.374 0.750 -0,325

0.900 -0.118 0.320 -0.408 0.430 -0.405 0.800 -0.263

0.960 -0.027 0.340 -0.407 0.440 -0.381 0.830 -0.274

0.350 -0.151 * * 0.460 -0.365 0.900 -0.147

0.370 -0,372 0.490 -0.363 0,960 0.001

0.380 -0.346 0.500 -0.342

0.400 -0.292 0.520 -0.348

0.410 -0,336 0,540 -0.331

0.430 -0.325 0.550 -0.309

0.440 -0.318 0,580 -0.284

0.460 -0.329 0.600 -0,338

0.470 -0.328 0.610 -0.239

0.490 -0.301 0.650 ..4.791 **

0.500 -0.290 0.700 -0.337

0.520 -0.292 0.750 -0.287

0,530 -0.283 0.820 -0.288

0.550 -0.288 0,890 -0.133

0,560 -0,294 0.900 -0.112

0.580 -0.256 0.960 -0.035

0.590 -0.290

0.600 -0.297

0.640 -4.620**

0.700 -0.291

0.750 -0.253

0.820 -4,804"*

0.870 -0.197

0,930 -0.080

0,960 -0.026

Lower Surface

0.020 - 1.066 0.020 -0.416 0.020 -0.289 0,020 -0.317

0.110 -0.050 0.060 0.059 0.060 0.111 0.060 1,549"*

0.230 -0.012 0.090 0.075 0.090 0.126 0.110 0.138

0.400 0.006 0.120 0.152 0.120 0.078 0.250 0.007

0.490 -0.029 0,200 -0.003 0.200 -0.011 0.400 -0.044

0.630 1.595"* 0,260 0.090 0.250 0.050 0.490 -0,085

0.750 0.011 0.400 -4.823 ** 0.400 -0.030 0,580 -0.127

0.850 0.078 0.490 -0.028 0.490 -0,004 0.650 -0.032

0.900 0.117 0.580 -0.011 0.580 -0.099 0.750 0.179

0.960 0.111 0.640 0.291 0.650 0.018 0,830 0.268

0.750 0.143 0.750 0,238 0.900 0.332

0.870 0.215 0.890 ******** 0.960 0.252

0.930 O. 189 0.930 0.233

0.960 O. 113 0.960 -4.821 **

CN = 0.251 0.449 0.488 0.521

114
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-8-17-500, MINF = 0.604, Camber = 14/2, ALPT = 7.34, BETA = 0.71, QINF = 280.9,

RNPU = 2.9E+06, CNWP = 0.3362

rl = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 0.578 0.000 -0.154 0.000 -7.866 * * 0.010 0.190* *

0.060 -0.109 0.020 0.559"* 0.020 0.423"* 0.020 0.041 **

0.110 -0.507 0.040 0.129 0.060 - 1.409 ** 0.060 -0.899

0.200 -0.561 0.060 -0.334 0.090 -0.847 0.110 - 1.306

0.230 -0.443 0.090 -0.688 0.110 -I.188 0.140 2.018"*

0.400 -0.238 0.130 -1.115 0.130 -1.711 0,190 -7.724**

0.490 -0.217 0.150 - 1.208 0.150 -0.888 0.250 -0.551

0.590 -0.221 0.200 -0.803 0.210 -0.778 0.400 -0.392

0.630 -0,227 0.250 -0.493 0.250 -0.553 0.490 -0.344

0.700 -0.239 0.260 -0.488 0.340 -0.459 0.580 -0.333

0.750 -0.201 0.280 -0,474 0.370 -0.454 0.650 -0.388

0.810 --0.195 0.290 -0.466 0.400 -0.408 0,700 -0.325

0.840 -0.208 0.310 -0.411 0.410 -0.376 0.750 -0.319

0.900 -0.122 0.320 -0.415 0.430 -0.407 0.800 -0.257

0.960 -0,035 0.340 -0417 0.440 -0.394 0.830 -0.276

0,350 -0.164"* 0.460 -0.367 0.900 -0.148

0.370 -0.382 0,490 -0.365 0.960 -0.003

0.380 -0.353 0,500 -0.374

0.400 -0.293 0.520 -0.359

0.410 -0.34 [ 0.540 -0.333

0.430 -0.326 0.550 -0.311

0440 -0.298 0.580 -0.267

0.460 -0.331 0.600 -0.340

0.470 -0.344 0.610 -0256

0.490 -0.307 0.650 -4.815"*

0.500 -0.297 0.700 -0.328

0.520 -0.294 0.750 -0.285

0.530 -0.281 0.820 -0.286

0.550 -0.290 0.890 -0.130

0.560 -0.309 0,900 -0.107

0.580 -0.258 0.960 -0.020

0,590 -0,296

0.600 -0.294

0.640 -4.643**

0.700 -0.285

0.750 -0.255

0.820 -4.828"*

0.870 -0,194

0.930 -0.089

0.960 -0.027

Lower Surface

0.020 - I. I 01 0.020 -0.418 0.020 -0.290 0.020 -0.384

0.110 -0.051 0.060 0.007 0.060 0.132 0.060 1.556"*

0.230 -0.012 0.090 1.298 0.090 0.137 0.110 0.138

0.400 0.006 0.120 0.141 0.120 0.097 0.250 0.021

0.490 -0.014 0.200 -0.007 0.200 -0.019 0.400 -0.036

0.630 1.602"* 0.260 0.106 0.250 0.065 0.490 -0.085

0.750 0.027 0.400 -4.847"* 0.400 -0.025 0.580 -0.128

0,850 0.075 0.490 -0.024 0.490 -0.004 0.650 -0.017

0.900 0.106 0.580 -0.004 0.580 -0. 100 0.750 O. 175

0.960 0.103 0.640 0,292 0.650 0.022 0.830 0.269

0.750 0.126 0,750 0.239 0.900 0.333

0.870 0.216 0.890 ******** 0.960 0.253

0.930 0.189 0.930 0.234

0.960 0.114 0.960 -4.845" *

CN = 0.261 0.475 0.496 0.528

115
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-8-21-000, MINF = 0.602, Camber = 15/2, ALPT = 7.35, BETA = 0.63, QINF = 278.6,

RNPU = 2.8E+06, CNWP = 0.3416

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP xA" CP x/c CP

0.020 0.616 0.000 -0.317 0.000 -7.931 ** 0.010 0.320* *

0.060 -0.070 0.020 0.584"* 0.020 0.512"" 0.020 0.120"*

0.110 -0.524 0.040 0.203 0.060 - 1.414"* 0.060 -0.839

0.200 -0.580 0.060 -0.287 0.090 -0.828 0.110 -1.317

0.230 -0.487 0.090 -0.694 0.110 -1.211 0,140 2.014"*

0.400 -0.240 O. 130 - 1.161 O. 130 - 1.762 O.190 -7.788 **

0.490 -0.211 0.150 - 1.275 0.150 -0,904 0.250 -0.555

0.590 -0.231 0,200 -0.821 0.210 -0,785 0.400 -0.388

0.630 -0.225 0.250 -0.511 0,250 -0.557 0.490 -0.347

0.700 -0.242 0.260 -0.492 0.340 -0.463 0.580 -0.313

0.750 -0.203 0.280 -0,478 0.370 -0.449 0.650 -0.382

0.810 -0,213 0.290 -0.445 0.400 -0.436 0,700 -0.328

0.840 -0.195 0.310 -0.415 0.410 -0.380 0.750 -0.322

0.900 -0.118 0.320 -0.419 0.430 -0.410 0,800 -0.259

0.960 -0.012 0.340 -0.413 0.440 -0.388 0.830 -0.278

0.350 -0.1 44** 0.460 -0.370 0.900 -0.139

0,370 -0.382 0.490 -0.345 0.960 0.005

0.380 -0.352 0.500 -0.357

0,400 -0.308 0.520 -0.353

0.410 -0325 0.540 -0.336

0.430 -0.329 0.550 -0.313

0.440 -0.320 0.580 -0.288

0.460 -0.319 0.600 -0.343

0.470 -0,347 0.610 -0.273

0.490 -0,306 0.650 -4.855**

0.500 -0.294 0.700 -0.323

0.520 -0.296 0.750 -0.272

0.530 -0.284 0.820 -0.288

0.550 -0.302 0.890 -0.131

0.560 -0.283 0.900 -0.109

0.580 -0.238 0.960 -0.032

0.590 -0.295

0.600 -0.297

0.640 -4.681 **

0.700 -0.272

0.750 -0.253

0.820 -4.868"*

0.870 -0.196

0.930 -0,094

0.960 -0.027

Lower Surface

0.020 - 1.229 0.020 -0.510 0.020 -0.293 0.020 -0.473

0.110 -0.081 0.060 -0.069 0.060 0.140 0.060 1.569 **

0.230 -0.005 0.090 0.066 0.090 0.149 0.110 0.161

0.400 0.022 0.120 0.130 0.120 0.131 0.250 0.024

0.490 0.014 0.200 -0,011 0.200 -0.019 0,400 -0.037

0,630 1.615"* 0.260 0.115 0.250 0.074 0.490 -0.079

0,750 0,027 0.400 -4.887 ** 0.400 -0.005 0.580 -0.109

0.850 0,086 0.490 -0.017 0.490 -0.004 0.650 -0.029

0.900 0.107 0.580 0.004 0.580 -0.093 0.750 0.176

0.960 0.103 0.640 0.301 0.650 0.022 0.830 0.271

0.750 0.126 0,750 0.252 0.900 0.351

0.870 0.207 0.890 ******** 0.960 0.249

0.930 0.187 0.930 0.243

0.960 0. I 18 0,960 -4.886**

CN = 0.269 0.448 0.510 0.534

116
Table C-2. Continued.

Flight 198, Wing sweep = 26 °. Time = 13-8-24-000, MINF = 0.600, Camber = 16/2, ALPT = 7.35, BETA = 0.57, QINF = 276.7.

RNPU = 2.8E+06. CNWP = 0.3363

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP xA" CP x/c CP x/c CP

0.020 0.654 0.000 -0.425 0.000 -7.984** 0,010 0.375**

0.060 -0.051 0.020 0.651 ** 0.020 0.559** 0.020 0.166"*

0.1 I 0 -0.528 0.040 0.236 0.060 - 1.396" * 0.060 -0.845

0.200 -0,584 0.060 -0.273 0.090 -0.827 0,110 - 1,305

0.230 -0.450 0.090 -0.699 0. I I 0 - 1,245 0.140 2.028"*

0.400 -0.242 0.130 - 1,197 0.130 - 1.829 0.190 -7.840"*

0,490 -0,217 0,150 - 1.332 0.150 -0.929 0,250 -0.559

0,590 -0.225 0,200 -0.839 0.210 -0,780 0.400 -0.399

0.630 -0.223 0,250 -0.515 0.250 -0.561 0,490 -0.339

0,700 -0.240 0.260 -0.496 0.340 -0.466 0,580 -0.321

0.750 -0.201 0,280 -0.472 0.370 -0.4.44 0,650 -0.385

0.810 -0,206 0.290 -0.464 0.400 -0.399 0.700 -0.330

0.840 -0.220 0,310 -0,418 0.410 -0383 0,750 -0.316

0,900 -0.12 [ 0.320 -0,422 0.430 -0.413 0,800 -0.254

0.960 -0,036 0,340 -0,416 0.440 -0.395 0,830 -0.270

0,350 -0.167"* 0.460 -0.370 0.900 -0.140

0.370 -0,385 0.490 -0.363 0,960 0.005

0,380 -0.354 0.500 -0.349

0.400 -0.310 0.520 -0.340

0,410 -0.343 0.540 -0.338

0.430 -0.332 0.550 -0.316

0.440 -0.306 0.580 -0.290

0.460 -0.321 0.600 -0333

0.470 -0.335 0.610 -0,245

0490 -0.308 0650 -4.887**

0.500 -0,297 0.700 -0.337

0.520 -0.299 0.750 -0.286

0.530 -0.286 0.820 -0.286

0.550 -0.285 0.890 -0.113

0,560 -0,307 0.900 -0.110

0,580 -0,262 0,960 -0.029

0.590 -0.297

0.600 -0.309

0.640 -4.713"*

0.700 -0.290

0.750 -0.255

0.820 -4.901 **

0.870 -0.194

0.930 -0.087

0.960 -0.024

Lower Surface

0.020 - 1.049 0.020 -0.557 0.020 -0.329 0.020 -0.574

0.110 -0.169 0,060 -0.106 0.060 0.141 0.060 1.579"*

0.230 -0.025 0.090 0.006 0.090 0.155 0.110 0.162

0.400 0.046 0.120 0.106 0.120 0.131 0.250 0,028

0.490 0.001 0.200 -0.019 0,200 -0.027 0.400 -0,037

0.630 1.626"* 0.260 0,107 0.250 0,074 0.490 -0.079

0750 0.023 0.400 -4.920** 0.400 -0.021 0,580 -0.120

0.850 0.071 0.490 -0.013 0.490 -0,005 0.650 -0.030

0.900 0.101 0.580 0.007 0,580 -0.094 0.750 0.177

0.960 0.099 0.640 0.306 0.650 0,022 0.830 0.273

0.750 0.127 0.750 0.234 0.900 0.346

0.870 0.193 0.890 ******** 0.960 0.244

0.930 O. 184 0.930 0.229

0.960 O, 111 0.960 -4.918"*

CN = 0.251 0448 0.505 0.533

117
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-8-27-000, MINF -- 0.598, Camber = 17/2, ALPT = 7.48, BETA = 0.50, QINF = 275.4,

RNPU = 2.8E+06, CNWP = 0.3505

TI= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.692 0.000 -0.506 0.000 -8.024"* 0.010 0.423"*

0.060 -0.031 0.020 0.696** 0.020 0.605** 0.020 0.213**

0.110 -0.531 0.040 0.269 0.060 - 1.403"* 0.060 -0.826

0.200 -0.602 0.060 -0.258 0.090 -0.842 0.110 - 1.312

0.230 -0.514 0.090 -0.703 0.110 -1.270 0.140 2.044**

0.400 -0.243 0.130 - 1.254 0.130 - 1.904 0.190 -7.879 **

0.490 -0.222 0.150 - 1.401 0.150 -0.943 0.250 -0.562

0.590 -0.226 0.200 -0.867 0.210 -0.810 0.400 -0.401

0.630 -0.224 0.250 -0.518 0.250 -0.572 0.490 -0.341

0.700 -0.241 0.260 -0.506 0.340 -0.469 0.580 -0.317

0.750 -0.202 0.280 -0.484 0.370 -0.464 0.650 -0.378

0.810 -0.207 0.290 -0.476 0.400 -0.417 0.700 -0.332

0.840 -0.213 0.310 -0.423 0.410 -0.393 0,750 -0.318

0.900 -0.128 0.320 -0.424 0.430 -0.416 0.800 -0.255

0.960 -0.036 0.340 -0.410 0.440 -0.408 0.830 -0.272

0.350 -0.168"* 0.460 -0.375 0.900 -0.141

0.370 -0.391 0.490 -0.357 0.960 -0.004

0.380 -0.361 0.500 -0.351

0.400 -0.312 0.520 -0.357

0.410 -0.349 0,540 -0.340

0.430 -0334 0.550 -0,318

0.440 -0.328 0.580 -0.273

0.460 -0.351 0.600 -0.334

0.470 -0.288 0.610 -0.262

0.490 -0.310 0.650 -4.912**

0.500 -0.304 0.700 -0.327

0.520 -0.317 0.750 -0.284

0.530 -0.288 0.820 -0.283

0.550 -0.277 0.890 -0.129

0.560 -0.302 0.900 -0.105

0.580 -0.256 0.960 -0.033

0.590 -0.289

0.600 -0.301

0.640 -4.736**

0.700 -0.287

0.750 -0.249

0.820 -4.925**

0.870 -0.195

0.930 -0.084

0.960 -0.024

Lower Surface

0.020 - 1.044 0.020 -0.619 0.020 -0,399 0.020 -0.647

O. 110 -0.192 0.060 -0.139 0.060 O. 113 0.060 1.586**

0.230 -0.034 0.090 -0.007 0.090 O. 166 O. 110 O. 195

0.400 0.062 O. 120 0.062 O. 120 O. 136 0.250 0.035

0.490 0.001 0.200 -0.024 0.200 -0.035 0.400 -0.030

0.630 1.633"* 0.260 0.108 0.250 0.082 0.490 -0.080

0.750 0.027 0.400 -4.944"* 0.400 -0.021 0,580 -0.120

0.850 0.079 0.490 -0.001 0.490 -0.005 0.650 -0.026

0.900 0.095 0.580 0.015 0.580 -0.087 0.750 0.172

0.960 0.095 0.640 0.311 0.650 0.022 0.830 0.274

0.750 0.127 0.750 0.235 0.900 0.332

0.870 0.199 0.890 ******** 0.960 0.245

0.930 0.180 0.930 0.230

0.960 0.107 0.960 -4.943"*

CN = 0.257 0.450 0.511 0.540

118
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-8-30-500, MINF = 0,597, Camber = 18/2, ALPT = 7.48, BETA = 0.50, QINF = 274.2,

RNPU = 2.8E+06, CNWP = 0.3529

rl = 0.93 0.76 0,59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.710 0.000 -0.678 0,000 -8.059** 0.010 0.492**

0.060 -0.003 0.020 0.740** 0.020 0.657** 0.020 0.304**

O. 1 l 0 -0.547 0.040 0.300 0.060 - 1.327* * 0.060 -0.785

0.200 -0.627 0,060 -0.210 0.090 -0.825 O. 110 - 1.319

0.230 -0.477 0.090 -0.702 0.110 - 1.297 0.140 2.044* *

0.400 -0.254 0,130 - 1,305 0.130 - 1.967 0.190 -7.914"*

0490 -0.213 0.150 - 1.498 0.150 -0.967 0.250 -0.567

0.590 -0.225 0.200 -0,885 0.210 -0.805 0.400 -0.404

0.630 -0.227 0.250 -0.536 0.250 -0.577 0,490 -0.344

0.700 -0.244 0.260 -0,517 0.340 -0,472 0.580 -0.321

0.750 -0.209 0.280 -0.498 0.370 -0.467 0.650 -0.382

0.810 -0.219 0.290 -0.480 0.400 -0.413 0.700 -0.324

0.840 -0.224 0.310 -0.434 0,410 -0388 0,750 -0.313

0.900 -0.130 0.320 -0.433 0.430 -0.419 0,800 -0.254

0.960 -0.038 0.340 -0.430 0.440 -0.401 0.830 -0.265

0,350 -0.176"* 0.460 -0,372 0.900 -0.134

0.370 -0.394 0,490 -0.320 0.960 -0.002

0.380 -0.369 0.500 -0.355

0.400 -0.315 0,520 -0.361

0.410 -0,352 0.540 -0.344

0.430 -0.337 0.550 -0.321

0.440 -0.327 0.580 -0.295

0.460 -0.335 0.600 -0.338

0.470 -0.348 0.610 -0.265

0_490 -0.313 0.650 -4.934"*

0.500 -0.307 0.700 -0.338

0.520 -0.303 0.750 -0.287

0.530 -0.294 0.820 -0.295

0.550 -0.290 0,890 -0.127

0.560 -0.312 0.900 -0.107

0.580 -0.259 0.960 -0.031

0,590 -0,297

0.600 -0.283

0.640 -4.758**

0.700 -0.290

0.750 -0.256

0.820 -4,948"*

0.870 -0,198

0.930 -0,090

0.960 -0.026

Lower Surface

0.020 -0.931 0.020 -0.642 0.020 -0.540 0.020 -0.757

0.110 -0.231 0.060 -0.153 0.060 0.053 0.060 1.591 **

0.230 -0.052 0.090 -0.048 0.090 0.165 0.1 I 0 0.205

0.400 0.048 0.120 0.028 0.120 0.153 0.250 0.040

0.490 0.007 0.200 -0.034 0.200 -0.044 0.400 -0.024

0.630 1.638"* 0.260 0,086 0.250 0.092 0.490 -0,074

0.750 0.025 0.400 -4.967 * * 0,400 -0.001 0.580 -0.123

0.850 0.069 0.490 0.005 0.490 -0.007 0.650 -0.028

0.900 0.088 0,580 0.021 0.580 -0.089 0.750 0.171

0.960 0.089 0.640 0.307 0,650 0.028 0,830 0.264

0.750 0.126 0.750 0.234 0.900 0.328

0.870 0.208 0,890 ******** 0.960 0.244

0.930 O. 175 0.930 0.220

0.960 O, 106 0.960 -4.965 * *

CN = 0.248 0.452 0.515 0.543

119
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-8-33-000, MINF = 0.595, Camber = 19/2, ALPT = 7.55, BETA = 0.57, QINF = 272.9,

RNPU = 2.8E+06, CNWP = 0.3394

"O= 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.722 0.000 -0.690 0.000 -8.100"* 0.010 0.540**

0.060 0.007 0.020 0.828** 0.020 0,678** 0.020 0.329**

0.110 -0.550 0.040 0.337 0.060 - 1.327" * 0.060 -0.790

0.200 -0.638 0.060 -0.196 0.090 -0.841 0.110 -1.326

0.230 -0.459 0.090 -0.721 0,110 - 1.323 0.140 2.061 **

0.400 -0.248 0.130 - 1.334 0.130 -2.017 0.190 -7.954 **

0.490 -0.222 0.150 - 1.538 0.150 - 1.008 0.250 -0.570

0.590 -0.239 0.200 -0,914 0.210 -0,815 0.400 -0.407

0.630 -0.233 0.250 -0,553 0.250 -0.580 0.490 -0.346

0.700 -0.241 0.260 -0.520 0.340 -0,475 0.580 -0.322

0.750 -0.210 0.280 -0.485 0.370 -0.461 0.650 -0.384

0.810 -0.203 0.290 -0,492 0.400 -0.423 0.700 -0.325

0.840 -0.217 0.310 -0.440 0.410 -0.390 0.750 -0.315

0.900 -0.120 0.320 -0.440 0,430 -0,422 0.800 -0.252

0,960 -0.039 0.340 -0.436 0.440 -0,403 0.830 -0,266

0.350 -0.161 ** 0.460 -0.380 0.900 -0,124

0.370 -0,396 0.490 -0.362 0.960 -0.006

0,380 -0.362 0.500 -0.336

0.400 -0.329 0.520 -0.363

0.410 -0.358 0.540 -0.345

0.430 -0.339 0.550 -0.323

0.440 -0.343 0.580 -0.278

0.460 -0.344 0.600 -0.340

0.470 -0.357 0.610 -0.266

0.490 -0.315 0.650 -4,959"*

0.500 -0.315 0.700 -0.340

0,520 -0,305 0.750 -0.288

0.530 -0.292 0.820 -0.288

0.550 -0.292 0. 890 -0,128

0.560 -0.300 0.900 -0.102

0.580 -0,261 0.960 -0,027

0.590 -0.303

0.600 -0.311

0.640 -4.782"*

0.700 -0.292

0.750 -0.257

0.820 -4.973**

0.870 -0.195

0.930 -0.082

0.960 -0.030

Lower Surface

0.020 -0.926 0.020 -0.460 0.020 -0.577 0.020 -0.739

0.110 -0.276 0,060 -0.227 0,060 0.010 0.060 1.599 **

0.230 -0.049 0,090 -0.133 0.090 0.160 0.110 0.229

0.400 0.056 0.120 -0.022 0.120 0.154 0.250 0.048

0.490 0.023 0.200 -0.038 0.200 -0.052 0.400 -0,024

0.630 1.646** 0.260 0,090 0.250 0.105 0.490 -0.075

0.750 0.034 0.400 -4.992** 0.400 -0.012 0.580 -0.112

0.850 0.074 0.490 0,005 0.490 -0.007 0.650 -0.033

0.900 0.094 0.580 0.029 0.580 -0.090 0.750 0.171

0.960 0.094 0.640 0.315 0.650 0.028 0.830 0.274

0.750 0.126 0.750 0.235 0.900 0.342

0,870 0.199 0.890 ******** 0.960 0.238

0.930 0,180 0.930 0.230

0.960 0.102 0.960 -4.990**

CN = 0.247 0.450 0.517 0.551

120
Table C-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-8-36-500, MINF = 0.593, Camber = 19/2, ALPT = 7.55, BETA = 0.55, QINF = 271.3,

RNPU = 2.8E+06, CNWP = 0.3568

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.726 0.000 -0.686 0.000 -8.147"* 0.010 0.543**

0.060 0.007 0.020 0.769** 0.020 0.682** 0.020 0.330**

0.110 -0.566 0.040 0.335 0.060 - 1.342 * * 0.060 -0.771

0.200 -0.642 0.060 -0_213 0.090 -0.823 0.110 - 1.334

0.230 -0.493 0090 -0.726 0.110 - 1.331 0.140 2.059"*

0.400 -0.241 0.130 - 1.357 0.130 -2.042 0.190 -8,001 **

0.490 -0.216 0.150 - 1.538 0.150 - 1.005 0.250 -0.558

0.590 -0,232 0.200 -0.919 0.210 -0.825 0.400 -0.401

0.630 -0.230 0.250 -0.542 0.250 -0.583 0.490 -0.349

0.700 -0.247 0.260 -0.516 0.340 -0.478 0.580 -0.324

0.750 -0.207 0.280 -0.514 0.370 -0.464 0.650 -0.377

0.810 -0.213 0.290 -0.486 0.400 -0.418 0.700 -0.328

0.840 -0.210 0,310 -0.443 0.410 -0.384 0.750 -0.317

0.900 -0,132 0.320 -0.443 0.430 -0.407 0.800 -0.254

0.960 -0,039 0.340 -0.435 0,440 -0.405 0.830 -0.258

0.350 -0.178"* 0.460 -0.380 0.900 -0.125

0.370 -0.399 0.490 -0.340 0.960 -0,007

0.380 -0.374 0.500 -0.359

0,400 -0.319 0.520 -0.365

0.410 -0.356 0.540 -0.348

0.430 -0.341 0.550 -0.325

0.440 -0.332 0.580 -0.289

0.460 -0.333 0.600 -0.326

0.470 -0.359 0.610 -0.260

0.490 -0.317 0.650 -4.988**

0.500 -0.311 0.700 -0.335

0.520 -0.307 0.750 -0.286

0.530 -0.294 0.820 -0.269

0.550 -0.294 0.890 -0,124

0.560 -0.309 0.900 -0.103

0.580 -0.270 0.960 -0032

0.590 -0.301

0.600 -0.297

0.640 -4.810"*

0.700 -0.294

0350 -0.259

0.820 -5.002"*

0,870 -0 196

0.930 -0.087

0.960 -0.031

Lower Surface

0.020 -0.912 0,020 -0.429 0.020 -0.529 0.020 -0,723

0.110 -0,256 0.060 -0.237 0.060 0.010 0.060 1.608"*

0.230 -0.053 0.090 -0.147 0.090 0.150 0,110 0.252

0.400 0.060 0,120 -0.014 0.120 0.135 0,250 0.048

0.490 0.015 0.200 -0.038 0.200 -0.052 0.400 -0.016

0.630 1.656"* 0.260 0.091 0.250 0.105 0.490 -0.075

0.750 0.033 0.400 -5.021 ** 0.400 -0.002 0.580 -0,113

0,850 0.082 0.490 0.009 0.490 -0.007 0.650 -0.029

0.900 0.101 0.580 0.033 0.580 -0.082 0.750 0.172

0.960 0.094 0.640 0.317 0.650 0.031 0.830 0.266

0.750 0.117 0.750 0,252 0.900 0.328

0.870 0.190 0.890 ******** 0.960 0.246

0.930 0.177 0.930 0.222

0,960 0.102 0960 -5.020**

CN = 0.251 0.450 0,519 0.553

121
Table C-2. Continued.

Flight 216. Wing sweep = 26 °, Time = 8-52-1-000, MINF = 0.604, Camber = 5/6, ALPT = 4.99. BETA = 0.37, QINF = 306.2,

RNPU = 3. IE+06, CNWP = 0.2850

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,"c CP x/c CP x/c CP

0.020 0.126 0.000 0.709 0.000 0.753"* 0.010 -0.646

0.060 -0.160 0.020 -0.049 0.020 -0.202 0.020 -0.483

0.110 -0.350 0.040 -0.138 0.060 -0.332** 0.060 -0.689

0.200 -0.328 0.060 -0.397 0.090 -0.574 0.110 -0.762

0.230 -0.341 0.090 -0.449 0.110 -0.623 0.140 -0.666

0.400 -0.241 0.130 -0.565 0.130 -3.919"* 0.190 -3.919"*

0.490 -0.241 0.150 -0.572 0.150 -0.562 0.250 -0.477

0.590 -0.306 0.200 -0.505 0.210 -0.530 0.400 -0.414

0.630 -0.328 0.250 -0.378 0.250 -0.468 0.490 -0.357

0.700 -0.393 0.260 -0.396 0.340 -0.446 0.580 -0.352

0.750 -0.457 0.280 -0.402 0.370 -0.424 0.650 -0.473

0.810 -0.414 0.290 -0.393 0.400 -0.382 0.700 -0.429

0.840 -0.460 0.310 -0.361 0.410 0.491 ** 0.750 -0.491

0.900 -0.248 0.320 -0.393 0.430 -0.404 0.800 -0.507

0.960 -0.085 0.340 -0.365 0.440 -0.390 0.830 -0.518

0.350 -0.144"* 0.460 -0.399 0.900 -0.240

0.370 -0.358 0.490 -0.376 0.960 -0.043

0.380 -0.371 0.500 -0.387

0.400 -0.349 0.520 -0.420

0.410 -0.347 0.540 -0.409

0.430 -0.330 0.550 -0.375

0.440 -0.337 0.580 -0.368

0.460 -0.349 0.600 -0.407

0.470 -0.383 0.610 -0.408

0.490 -0.374 0.650 -0.576

0.500 -0.363 0.700 -0.499

0.520 -0.337 0.750 -0.484

0.530 -0.367 0.820 -0.542

0.550 -0.385 0.890 -0.237

0.560 -0.406 0.900 -0.173

0.580 -0.352 0.960 -0.027

0.590 -0.418

0.600 -0.389

0.640 -0.488

0.700 -0.509

0.750 -0.036**

0.820 -0.515

0.870 -0.393

0.930 -0.190

0.960 -0.107

Lower Surface

0.020 -0.361 0.020 -0.276 0.020 -0.161 0.020 0.074

0.110 -0.131 0.060 -0.029 0.060 0.016 0.060 0.000

0.230 -0.008 0.090 -0.022 0.090 0.000 0.110 0.021

0.400 -0.021 0.120 -0.039 0.120 -0.058 0.250 -0.117

0.490 0.009 0.200 0.001 0.200 0.028 0.400 -0.108

0.630 1.887"* 0.260 -0.009 0.250 -0.068 0.490 -0.091

0.750 0.078 0.400 -0.015 0.400 -0.070 0.580 -0.089

0.850 0.127 0.490 -0.032 0.490 -0.056 0.650 0.030

0.900 0.223 0.580 -0.012 0.580 -0.063 0.750 0.229

0.960 0.145 0.640 0.147 0.650 -0.055 0.830 0.321

0.750 0.223 0.750 0.009 0.900 0.372

0.870 0.326 0.890 0.390 0.960 0.269

0.930 0.246 0.930 0.299

0.960 O. 193 0.960 0.289

CN = 0.313 0.464 0.437 0.477

122
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 8-52-52-000, MINF = 0.601, Camber = 5/6, ALPT = 7.92, BETA = 0.17, QINF = 292.7,

RNPU = 3.0E+06, CNWP = 0.3783

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.439 0.000 0.727 0.000 0.539"* 0.010 - 1.957

0.060 -0.509 0.020 -0.86 | 0.020 - I. 116 0.020 - 1.100

0.110 -0.602 0.040 -0.700 0.060 -0,738"* 0.060 - 1.267

0.200 -0,514 0.060 -0.915 0.090 -1.019 0.110 -1,155

0,230 -0.493 0.090 -0.861 0.110 - 1.065 0.1 40 -0,961

0.400 -0.342 0.130 -0.941 0.130 -3.957 * * 0.190 -3.957 **

0.490 -0.314 0.150 -0.912 0,150 -0.862 0.250 -0,633

0.590 -0.371 0.200 -0,759 0.210 -0.791 0.400 -0.516

0.630 -0.397 0.250 -0.581 0,250 -0.651 0.490 -0.426

0.700 -0.471 0.260 -0.573 0,340 -0.565 0,580 -0.417

0.750 -0,544 0.280 -0.556 0.370 -0,562 0.650 -0.501

0.810 -0.490 0.290 -0.529 0.400 -0.489 0.700 -0.467

0.840 -0,540 0.310 -0.512 0.410 0.656"* 0.750 -0.51 I

0.900 -0,330 0.320 -0.532 0,430 -0.513 0.800 -0.449

0.960 -0.151 0,340 -0.504 0.440 -0,494 0.830 -0.457

0.350 -0.168"* 0.460 -0.492 0.900 -0.190

0.370 -0.485 0,490 -0.468 0.960 -0,062

0.380 -0.505 0.500 -0,482

0.400 -0.453 0.520 -0.493

0,410 -0.459 0.540 -0.473

0,430 -0,440 0,550 -0.457

0,440 -0.428 0.580 -0.447

0.460 -0.438 0.600 -0.490

0.470 -0.436 0.610 -0.486

0.490 -0.451 0.650 -0.653

0.500 -0.444 0.700 -0.546

0.520 -0.430 0.750 -0,542

0.530 -0.439 0.820 -0.566

0.550 -0.467 0.890 -0.211

0,560 -0.476 0.900 -0.166

0.580 -0,426 0.960 -0.015

0.590 -0.485

0.600 -0.458

0.640 -0.544

0,700 -0,564

0.750 -0,043**

0.820 -0.549

0,870 -0.401

0,930 -0.189

0.960 -0.117

Lower Surface

0,020 0,023 0,020 0.198 0.020 0.302 0,020 0.517

0.110 0.010 0.060 0.229 0.060 0,270 0,060 0.025

0.230 0,089 0.090 0.178 0.090 0.223 0.110 0.254

0.400 0.040 0.120 0.122 0.120 0.130 0,250 0.020

0.490 0.041 0.200 0.089 0.200 0.108 0.400 -0,002

0.630 2.116* * 0.260 0,089 0,250 0,065 0.490 -0.001

0.750 0.070 0.400 0.048 0,400 0,022 0.580 -0.022

0.850 0.091 0.490 0,026 0.490 -0.04 1 0.650 0.072

0,900 0.188 0,580 0.021 0.580 0,003 0,750 0,273

0.960 0.112 0.640 0.179 0.650 -0.047 0,830 0,352

0,750 0.241 0.750 0.019 0.900 0.395

0,870 0,323 0,890 0.388 0.960 0.276

0.930 0.263 0,930 0.307

0.960 0.181 0,960 0.258

CN = 0.470 0.677 0.630 0.679

123
Table C-2. Continued.

Flight 216, Wing sweep = 26 °. Time = 8-54-30-000, MINF = 0.600, Camber = 5/6, ALPT = 9.99, BETA = -0.10, QINF = 300.2,

RNPU = 3.1E+06, CNWP = 0.4014

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.929 0.000 0.336 0.000 0.306 * * 0.010 -2.366

0.060 -0.764 0.020 -1.999 0.020 -2.305 0.020 °2.393

0.110 -0.761 0.040 -0.030 0.060 - 1.038' * 0.060 - 1.391

0.200 -0.607 0.060 - 1.292 0.090 - 1.315 0.110 - 1.230

0,230 -0.550 0.090 - 1.143 0.110 - 1.326 0,140 -1.046

0.400 -0.388 0.130 - 1.185 0.130 -3.969"* 0.190 -3.969"*

0,490 -0.354 0.150 - 1.099 0.150 - 1.001 0.250 -0.655

0.590 -0.417 0.200 -0.901 0.210 -0,906 0.400 -0.527

0.630 -0.439 0.250 -0.673 0.250 -0,726 0.490 -0.421

0.700 -0.517 0.260 -0.655 0.340 -0.623 0.580 -0.401

0.750 -0.599 0.280 -0.640 0.370 -0.594 0.650 -0.446

0.810 -0.545 0.290 -0.606 0,400 -0.503 0.700 -0.433

0.840 -0.606 0,310 -0.572 0.410 0.528"* 0.750 -0.444

0.900 -0.387 0.320 -0,592 0.430 -0.557 0.800 -0.398

0.960 -0.197 0.340 -0.561 0.440 -0.531 0.830 -0.345

0,350 -0.158"* 0.460 -0.508 0.900 -0.212

0.370 -0,532 0.490 -0.484 0.960 -0.141

0.380 -0.548 0.500 -0.475

0.400 -0.497 0.520 -0.498

0.410 -0.502 0.540 -0.483

0.430 -0.466 0.550 -0.463

0.440 -0.462 0.580 -0.456

0.460 -0.466 0,600 -0.481

0.470 -0.496 0.610 -0.469

0.490 -0.475 0.650 -0.667

0.500 -0.477 0.700 -0.522

0.520 -0.463 0.750 -0.511

0.530 -0.460 0.820 -0,486

0.550 -0.486 0.890 -0.122

0.560 -0.494 0.900 -0.103

0.580 -0.450 0.960 -0.010

0.590 -0.511

0.600 -0.473

0.640 -0.554

0.700 -0.573

0.750 -0.013"*

0.820 -0.544

0.870 -0.385

0,930 -0.182

0.960 -0.108

Lower Surface

0.020 0.267 0.020 0.470 0.020 0.529 0.020 0.694

0.110 0.105 0.060 0.379 0.060 0,427 0.060 0.057

0.230 0.165 0.090 0.296 0.090 0,354 0.110 0,361

0.400 0.057 0.120 0,235 0.120 0,253 0.250 0.117

0.490 0.080 0.200 0.166 0.200 0.191 0.400 0.074

0.630 1.952" * 0.260 0.176 0.250 0.162 0.490 0.061

0,750 0.086 0.400 0.110 0.4(30 0.093 0,580 0.031

0.850 0.095 0.490 0.080 0.490 -0.008 0.650 0.114

0.900 0.185 0.580 0.060 0.580 0.050 0.750 0.289

0.960 0.1 04 0.640 0.214 0.650 -0.014 0.830 0.358

0.750 0.259 0.750 0.036 0.900 0.399

0.870 0.333 0.890 0.404 0.960 0.254

0.930 0.271 0.930 0.317

0.960 0.191 0.960 0.224

CN = 0.574 0.803 0.722 0.776

124
Table C-2, Continued.

Flight 216, Wing sweep = 26 °, Time = 8-56-49-500, MINF = 0.601, Camber = 20/18, ALPT = 2.98, BETA = 0.89, QINF = 302.0,

RNPU = 3.1E+06, CNWP = 0.2761

rl = 0.93 0.76 0.50 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.755 0.000 - 1.098 0,000 -0.166"* 0.010 0.801

0.060 O, 186 0.020 0.837 0.020 0.812 0.020 0.651

O. 1 I 0 -0.364 0.040 0.624 0.060 0.208" * 0.060 -0.170

0.200 -0.519 0.060 0,077 0.090 -0.450 O. 110 - 1.140

0.230 -0.435 0.090 -0.401 0,110 -0.875 0.140 -0,828

0.400 -0.301 O. 130 -0.907 O, 130 -3.956 * * O. 190 -3.956 * *

0.490 -0.2% O, 150 - 1.122 0_150 -0,773 0.250 -0.482

0.590 -0.399 0.200 -0.735 0.210 -0.627 0.400 -0.438

0.630 -0.452 0.250 -0.483 0.250 -0.501 0.490 -0.406

0.700 -0.656 0.260 -0.481 0.340 -0.479 0.580 -0.462

0,750 -0.683 0.280 -0.456 0.370 -0,480 0.650 -0.638

0.810 -0.666 0.290 -0.448 0,400 -0.429 0.700 -0.617

0.840 -0.743 0.3 l0 -0.43 l 0.410 0.515** 0.750 -0.883

0.900 -0.243 0,320 -0.457 0.430 -0.473 0.800 -0,960

0.960 -0.252 0.340 -0.436 0.440 -0.469 0.830 -0.820

0.350 -0.226** 0,460 -0.470 0.900 -0.398

0,370 -0.433 0,490 -0.460 0.960 -0.427

0.380 -0.452 0.500 -0.479

0.400 -0.416 0,520 -0.515

0.410 -0.425 0,540 -0.500

0.430 -0.401 0.550 -0.489

0.440 -0.406 0.580 -0,506

0.460 -0.422 0.600 -0.543

0.470 -0.450 0.610 -0.559

0.490 -0.447 0,650 -0.812

0.500 -0.457 0.700 -0.729

0.520 -0.430 0.750 -0.777

0.530 -0.457 0.820 -0.586

0.550 -0,492 0.890 -0.369

0.560 -0.507 0.900 -0.376

0.580 -0.467 0960 -0.367

0.590 -0.531

0.600 -0.513

0.640 -0.688

0.700 -0.775

0.750 -0.123"*

0.820 -0.673

0.870 -0.515

0.930 -0,326

0.960 -0.324

Lower Surface

0.020 -0.234 0.020 -0.3% 0.020 -0.470 0,020 - 1.334

O. 110 -0, | 76 0.060 -0.381 0.060 -0.524 0.060 0,003

0.230 -0.088 0.090 -0,398 0,090 -0.591 0,110 -0,197

0.400 -0.134 0.120 -0.383 0,120 -0.608 0.250 -0.044

0.490 -0.062 0.200 -0.090 0,200 -0.070 0.400 -0.016

0.630 1,930"* 0.260 -0.297 0.250 -0.102 0,490 0.022

0,750 -0.006 0.400 -0.030 0.400 0,123 0.580 0.102

0,850 0.022 0.490 0.083 0.490 -0.061 0.650 0.278

0.900 0.088 0.580 0.175 0.580 0.184 0.750 0.480

0.960 0,075 0.640 0.328 0.650 -0.127 0.830 0,513

0.750 0.343 0.750 -0.003 0.900 0.553

0.870 0.443 0.890 0,549 0.960 0.381

0,930 0,401 0.930 0.446

0.960 0,275 0.960 0.347

CN = 0.321 0.55 l 0.520 0.664

125
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 8-56-59-500, MINF = 0.598, Camber = 20/18, ALPT = 3.04, BETA = 0.74, QINF = 299.1,

RNPU = 3.1E+06, CNWP = 0.2625

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.752 0.000 -1.090 0.000 -0.212"* 0.010 0.800

0.060 0.195 0.020 0.824 0.020 0.818 0.020 0.649

O. 110 -0.381 0.040 0.616 0.060 0.200"* 0.060 -0.173

0.200 -0.526 0.060 0.075 0.090 -0.446 0.110 -1.153

0.230 -0,460 0.090 -0,407 0.110 -0.886 0.140 -0.838

0.400 -0.306 0.130 -0.924 0.130 -3.996"* 0.190 -3.996"*

0.490 -0,305 0.150 - 1.127 0.150 -0.799 0.250 -0.488

0,590 -0.397 0.200 -0.749 0.210 -0.630 0.400 -0.445

0.630 -0.454 0.250 -0.490 0.250 -0.493 0.490 -0.417

0.700 -0.668 0.260 -0.481 0.340 -0.486 0.580 -0.468

0.750 -0.758 0.280 -0.472 0.370 -0.472 0.650 -0.646

0.810 -0.675 0.290 -0.458 0.400 -0.435 0.700 -0.611

0.840 -0.753 0.310 -0.434 0.4 l0 0.518"* 0.750 -0.890

0.900 -0.265 0.320 -0.459 0.430 -0.480 0.800 -0.965

0.960 -0.264 0.340 -0.442 0.440 -0.475 0.830 -0.812

0.350 -0.230** 0.460 -0,457 0.900 -0.403

0.370 -0.436 0.490 -0.459 0.960 -0.417

0.380 -0.458 0.500 -0.495

0.400 -0.408 0.520 -0.505

0.410 -0.428 0.540 -0.486

0.430 -0.407 0.550 -0.483

0.440 -0.412 0.580 -0.478

0.460 -0.416 0.600 -0.536

0.470 -0.456 0.610 -0.553

0.490 -0.453 0.650 -0.780

0.500 -0.452 0.700 -0.705

0.520 -0.436 0.750 -0.776

0.530 -0.460 0.820 -0.589

0.550 -0.498 0.890 -0.347

0.560 -0.502 0.900 -0.361

0.580 -0.467 0.960 -0.352

0.590 -0.533

0.600 -0.515

0.640 -0.687

0700 -0.777

0.750 -0.123"*

0.820 -0.689

0870 -0.416

0.930 -0.323

0.960 -0.330

Lower Surface

0.020 -0.219 0.020 -0.370 0.020 -0.492 0.020 - 1.388

0.110 -0.187 0.060 -0.349 0.060 -0.518 0.060 0.001

0.230 -0.091 0.090 -0.407 0.090 -0.594 0. I 10 -0.180

0.400 -0.141 0.120 -0.382 0.120 -0.582 0.250 -0.040

0.490 -0.087 0.200 -0.090 0.200 -0.066 0.400 -0.004

0.630 1.946"* 0.260 -0,298 0.250 -0.076 0.490 0.028

0.750 0.011 0.400 -0.017 0.400 0.117 0.580 0.110

0.850 0.047 0.490 0,105 0.490 -0.063 0.650 0.279

0.900 0.120 0.580 0.182 0.580 0.177 0.750 0.483

0.960 0.086 0.640 0.303 0.650 -0.134 0.830 0.522

0.750 0.336 0.750 -0.001 0.900 0.570

0.870 0.435 0.890 0.545 0.960 0.388

0.930 0.377 0.930 0.433

0.960 0.250 0.960 0.341

CN = 0,333 0.551 0.519 0.676

126
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-29-19-500, MINF = 0.596, Camber = 10/18, ALPT = 13.33, BETA = -0.41, QINF = 291.8,

RNPU = 3.0E+06, CNWP = 0.7196

rI = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.193 0.000 0.048 0.000 0.297 ** 0.010 -2.402

0.060 - 1.356 0.020 -2.317 0.020 -2.429 0.020 -2.408

0.110 - 1.295 0.040 0.017 0.060 - 1.404"* 0.060 -2.115

0.200 - 1.021 0.060 - 1.759 0.090 -2,231 0.110 - 1.515

0.230 -0.841 0.090 -2,091 0.110 -2.292 0,140 -1.300

0,400 -0.626 0.130 - 1.632 0.130 -4.021 ** 0.190 -4.021 * *

0.490 -0.588 0,150 - 1.756 0.150 - 1,515 0.250 -0.742

0.590 -0.704 0,200 - 1.640 0,210 - 1,490 0.400 -0.595

0.630 -0.771 0,250 -1.182 0.250 - 1.225 0.490 -0.472

0,700 -0.960 0.260 - 1.073 0.340 -0.872 0.580 -0.493

0.750 -0.899 0.280 -1.002 0.370 -0.796 0.650 -0.505

0.810 -0.881 0,290 -0.904 0,400 -0.659 0.700 -0.519

0.840 - 1,007 0.310 -0,822 0.410 0.606"* 0,750 -0,596

0,900 -0.605 0,320 -0.832 0.430 -0,695 0.800 -0.591

0,960 -0.647 0,340 -0.782 0.440 -0.673 0.830 -0.574

0.350 -0.282** 0.460 -0,635 0.900 -0.513

0.370 -0.729 0.490 -0.590 0.960 -0.495

0.380 -0,752 0.500 -0.591

0.400 -0,295 0.520 -0,619

0.410 -0.686 0.540 -0.590

0.430 -0.660 0.550 -0.567

0.440 -0.641 0.580 -0.580

0.460 -0.654 0.600 -0.5%

0.470 -0.671 0.610 -0.588

0.490 -0.663 0.650 -0.735

0.500 -0,654 0.700 -0.659

0.520 -0.621 0.750 -0.679

0.530 -0.644 0,820 -0.648

0.550 -0,673 0.890 -0.463

0.560 -0.698 0.900 -0.465

0,580 -0,64 1 0.960 -0.419

0.590 -0.703

0.600 -0.666

0.640 -0.773

0.700 -0.845

0.750 -0,040"*

0.820 -0.593

0.870 -0.355

0.930 -0.337

0.960 -0.323

Lower Surface

0.020 0,425 0.020 0,602 0.020 0,649 0.020 0.721

0. I 10 0.260 0.060 0.543 0.060 0.596 0,060 0.091

0.230 0.140 0,090 0,493 0.090 0,519 0.1 l0 0,522

0.400 0_ 164 0.120 0.433 0.120 0.466 0.250 0.306

0.490 O. 195 0,200 0.159 0,200 0.189 0.400 0.258

0.630 2.467"* 0.260 0.377 0.250 0.346 0.490 0.263

0.750 0.250 0.400 0.285 0.400 0.285 0,580 0.255

0.850 0.232 0.490 0,268 0.490 0.047 0.650 0.380

0,900 0.285 0.580 0.291 0.580 0.286 0.750 0.580

0.960 0,076 0.640 0.450 0.650 -0.047 0,830 0.598

0.750 0.449 0,750 0.070 0.900 0.629

0.870 0,523 0.890 0.626 0.960 0.412

0.930 0,416 0.930 0,518

0.960 0.289 0,960 0.283

CN = 1.003 1.241 1.146 1.136

127
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-30-29-500, MINF = 0.603, Camber = 10/15, ALPT = 2.00, BETA = 0.14, QINF = 303.3,

RNPU = 3.1E+06, CNWP = 0.3392

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.591 0.000 -0.382 0.000 0.457"* 0.010 0.407

0.060 0.095 0.020 0.603 0.020 0.545 0.020 0.249

0.110 -0.224 0.040 0.368 0.060 -0.111 ** 0.060 -0.301

0.200 -0.330 0.060 -0.018 0.090 -0.342 0.110 -0.638

0.230 -0.325 0.090 -0.268 0.110 -0.520 0.140 -0.597

0.400 -0.264 0.130 -0,497 0.130 -3.926* * 0.190 -3.926**

0.490 -0.267 0.150 -0.596 0.150 -0.516 0.250 -0.419

0.590 -0.384 0.200 -0,486 0.210 -0.460 0.400 -0.396

0.630 -0.430 0.250 -0.356 0.250 -0.407 0.490 -0.373

0.700 -0.622 0.260 -0.365 0.340 -0.405 0.580 -0.441

0.750 -0.840 0.280 -0.360 0.370 -0.403 0.650 -0.627

0.810 -0.771 0.290 -0.356 0.400 -0.377 0.700 -0.592

0.840 -0.851 0.310 -0.344 0.410 0.525** 0.750 -0.860

0.900 -0.252 0.320 -0.368 0.430 -0.421 0.800 -0.97 I

0.960 -0.221 0.340 -0.354 0.440 -0.424 0.830 -0.822

0,350 -0.160"* 0.460 -0.417 0.900 -0.383

0.370 -0.361 0.490 -0.423 0.960 -0.412

0.380 -0.378 0.500 -0.436

0.400 -0.326 0.520 -0.450

0.410 -0.359 0.540 -0.465

0.430 -0.367 0.550 -0.438

0.440 -0.346 0.580 -0.457

0.460 -0.360 0.600 -0.505

0.470 -0.397 0.610 -0.53 t

0.490 -0.397 0.650 -0.671

0.500 -0.400 0.700 -0.677

0.520 -0.362 0.750 -0.757

0.530 -0.411 0.820 -0.583

0.550 -0.44 1 0.890 -0.349

0.560 -0.450 0.900 -0.367

0.580 -0.426 0.960 -0.346

0.590 -0.489

0.600 -0.455

0.640 -0.657

0.700 -0.748

0.750 -0.092"*

0.820 -0.594

0.870 -0.342

0.930 -0.340

0.960 -0.347

Lower Surface

0.020 - 1.153 0.020 -0.949 0.020 -0.809 0.020 - 1.002

0.110 -0.163 0,060 -0.307 0.060 -0.149 0.060 0.016

0.230 -0.045 0.090 -0.136 0.090 -0.079 0.110 -0.183

0.400 0.064 0.120 -0.046 0.120 -0.060 0.250 -0.110

0.490 0.112 0.200 -0,005 0.200 -0.032 0.400 -0.047

0.630 2.316"* 0.260 0.002 0.250 -0.024 0,490 0.020

0.750 0.215 0.400 0.061 0,400 0.013 0.580 0.099

0.850 0.220 0.490 0.114 0.490 -0.055 0.650 0.297

0.900 0.299 0.580 0.175 0.580 0.146 0.750 0.472

0.960 0.174 0,640 0.332 0.650 -0.096 0.830 0.523

0.750 0.330 0.750 0.010 0,900 0.561

0.870 0,344 0.890 0.545 0.960 0.421

0.930 0.278 0.930 0.478

0.960 0.156 0.960 0.335

CN = 0438 0.526 0.511 0.620

128
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-30-33-500, MINF = 0.604, Camber = 10/16, ALPT = 2.93, BETA = -0.15, QINF = 30.4,0,

RNPU = 3.1E+06, CNWP = 0.3619

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x,/c CP x/c CP

0.020 0534 0.000 -0.204 0.000 0.573** 0.010 0.272

0.060 0.030 0.020 0.527 0.020 0.442 0.020 0.104

0.110 -0.303 0.040 0.270 0.060 -0.258** 0.060 -0.445

0.200 -0.391 0.060 -0.125 0.090 -0.465 0,110 -0.791

0.230 -0.347 0,090 -0.369 0.110 -0.643 0.140 -0.687

0.400 -0.293 0.130 -0.605 0.130 -3.916"* 0.190 -3.916"*

0.490 -0.285 0.150 -0.694 0.150 -0.597 0.250 -0.466

0.590 -0.399 0.200 -0.549 0.210 -0,541 0.400 -0.430

0.630 -0.463 0.250 -0.405 0.250 -0.467 0.490 -0.409

0.700 -0.654 0.260 -0.418 0.340 -0.456 0.580 -0.456

0.750 -0.869 0.280 -0.415 0.370 -0.464 0.650 -0.631

0.810 -0.804 0.290 -0.406 0.400 -0.413 0,700 -0.621

0.840 -0.871 0.310 -0.391 0.410 0.524" * 0.750 -0.872

0.900 -0.291 0.320 -0.415 0,430 -0.457 0,800 -0.941

0,960 -0.280 0.340 -Q406 0.440 -0.463 0.830 -0.820

0,350 -0.175"* 0.460 -0.454 0.900 -0.391

0,370 -0.403 0.490 -0.452 0.960 -0.427

0.380 -0.422 0.500 -0.472

0.400 -0.336 0.520 -0.499

0.410 -0.403 0.540 -0.491

0.430 -0.386 0.550 -0.473

0.440 -0.387 0.580 -0.482

0.460 -0.394 0.600 -0.539

0.470 -0.434 0610 -0.556

0.490 -0.427 0.650 -0.711

0.500 -0.436 0.700 -0.71 I

0,520 -0.414 0.750 -0.771

0.530 -0.44 1 0.820 -0.590

0.550 -0.476 0.890 -0.366

0.560 -0.491 0.900 -0.387

0.580 -0,451 0.960 -0.369

0.590 -0.519

0.600 -0.497

0.640 -0.684

0.700 -0.778

0.750 -0.081 **

0.820 -0.5%

0.870 -0.308

0.930 -0,340

O.96O -0.346

Lower Surface

0.020 - 1,207 0.020 -0.695 0,020 -0.562 0,020 -0,714

0.110 -0.104 0.060 -0.151 0.060 -0.059 0.060 0.016

0.230 -0.030 0.090 -0.049 0.090 -0.023 0. 110 -0.123

0.400 0.064 O. 120 0.012 O.120 -0.018 0.250 -0.077

0.490 0.120 0.200 -0.034 0.200 -0.004 0.400 -0.032

0.630 2.310"* 0.260 0.066 0.250 0.008 0.490 0.027

0.750 0.211 0.400 0.083 0.400 0.042 0.580 0.099

O.850 0.220 0.490 O.122 0.490 -0,048 0,650 0,296

0.900 0.287 0,580 O.179 0,580 O. 167 0.750 0.480

0,960 O, 149 0.640 0.357 0.650 -0.089 0.830 0.522

0,750 0.346 0.750 0.010 0.900 0.579

0.870 0.370 0.890 0.572 0.960 0.414

0.930 0.288 0.930 0.485

0.960 0.159 0.960 0.326

CN = 0.482 0.593 0.578 0.675

129
Table C-2. Continued.

Flight 216. Wing sweep = 26 °, Time = 9-30-42-500, MINF = 0.607, Camber = 10/15, ALPT = 8.23, BETA = -0.50, QINF = 304.3,

RNPU = 3.1E+06. CNWP = 0.5364

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.081 0.000 0.805 0.000 0.802** 0.010 -0.837

0.060 -0.537 0,020 -0.401 0.020 -0.559 0.020 -0.817

0.110 -0.793 0.040 -0.180 0.060 -0.967"* 0.060 - 1.513

0.200 -0,695 0.060 -0.951 0.090 - 1.252 0.110 - 1.577

0,230 -0.612 0.090 -1.124 0.110 -1.479 0.140 -1.292

0.400 -0.434 0.130 - 1.429 0.130 -3.883 ** 0.190 -3.883"*

0.490 -0.41 I 0.150 - 1.687 0.150 - 1.199 0.250 -0,705

0.590 -0.514 0.200 - 1.036 0.210 -0.954 0.400 -0.592

0.630 -0.581 0.250 -0.723 0.250 -0.769 0.490 -0.532

0.700 -0.775 0.260 -0.716 0.340 -0.686 0.580 -0.566

0,750 -0.989 0.280 -0.697 0.370 -0,675 0.650 -0.697

0.810 -0.936 0.290 -0.662 0.400 -0.594 0,700 -0.699

0.840 - 1.044 0.310 -0.627 0.410 0.553"* 0.750 -0.841

0.900 -0.425 0.320 -0.655 0.430 -0.635 0.800 -0.732

0.960 -0,438 0.340 -0.624 0.440 -0.632 0.830 -0.668

0.350 -0.231 ** 0.460 -0.612 0.900 -0.374

0.370 -0.597 0.490 -0.601 0.960 -0.347

0,380 -0,618 0,500 -0.613

0.400 -0.281 0.520 -0,637

0.410 -0.571 0.540 -0.62 I

0.430 -0,547 0.550 -0.598

0.440 -0.539 0.580 -0.601

0.460 -0.549 0.600 -0.649

0.470 -0.581 0.610 -0.657

0.490 -0.562 0.650 -0.794

0.500 -0.563 0.700 -0,771

0.520 -0.546 0.750 -0.817

0.530 -0.561 0,820 -0,546

0.550 -0.583 0.890 -0.428

0.560 -0.606 0.900 -0.432

0,580 -0.565 0.960 -0,422

0,590 -0.623

0.600 -0.593

0.640 -0.759

0.700 -0.831

0.750 -0.04 1 **

0.820 -0.515

0.870 -0.322

0.930 -0.343

0.960 -0.349

Lower Surface

0.020 0.018 0,020 0.177 0,020 0.250 0.020 0.407

0,110 0.091 0.060 0.293 0.060 0.321 0.060 0.060

0.230 0.084 0.090 0.264 0.090 0.301 0.110 0.260

0.400 0.100 0.120 0.250 0.120 0.254 0.250 0.129

0.490 0.134 0.200 0,082 0.200 0.100 0.400 0.127

0.630 2.338** 0.260 0.228 0,250 0.200 0.490 0.152

0,750 0.202 0.400 0.190 0.400 0.173 0.580 0.192

0.850 0.211 0.490 0.192 0.490 0.010 0.650 0.351

0.900 0.293 0.580 0.219 0.580 0,232 0.750 0.533

0.960 0.094 0.640 0.397 0.650 -0.052 0.830 0.574

0.750 0,365 0.750 0.054 0,900 0.629

0,870 0,396 0.890 0.616 0.960 0.440

0.930 0.303 0.930 0.499

0.960 0.170 0.960 0.326

CN = 0.726 0.925 0.898 1.004

130
Table C-2. Continued,

Flight 216, Wing sweep = 26", Time = 9-31-36-000, MINF = 0.603, Camber = 10/13, ALPT = 2.92, BETA = -0.36, QINF = 302.3,

RNPU = 3.1E+06, CNWP = 0.3297

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.543 0.000 -0.224 0.000 0.567** 0.010 0.279

0,060 0.045 0.020 0.535 0.020 0.449 0.020 0.1 I 0

0.110 -0.323 0.040 0.287 0.060 -0,254"* 0.060 -0.463

0.200 -0.376 0.060 -0.121 0.090 -0.452 0.110 -0.790

0.230 -0.343 0.090 -0.349 0,110 -0.624 0,140 -0.686

0.400 -0.275 O. 130 -0.584 O. 130 -3.934"* O. 190 -3.934"*

0.490 -0.278 O. 150 -0.677 O. 150 -0.562 0.250 -0.449

0.590 -0.381 0,200 -0.536 0,210 -0.530 0,400 -0.427

0.630 -0.430 0.250 -0.402 0.250 -0.457 0.490 -0.406

0.700 -0.593 0.260 -0.416 0.340 -0.446 0.580 -0.454

0.750 -0.819 0.280 -0.399 0.370 -0.462 0.650 -0,629

0.810 -0,747 0.290 -0.386 0.400 -0.403 0.700 -0.609

0.840 -0.805 0.310 -0.378 0.410 0.532** 0.750 -0,872

0.900 -0.235 0.320 -0.399 0.430 -0.455 0.800 -0.948

0.960 -0.150 0.340 -0.390 0.440 -0.450 0.830 -0, 819

0.350 -0.166"* 0.460 -0.446 0.900 -0.397

0.370 -0.386 0.490 -0.434 0.960 -0.432

0.380 -0,406 0.500 -0.460

0.400 -0.322 0.520 -0.497

0.410 -0.387 0.540 -0.475

0.430 -0.360 0.550 -0.470

0.440 -0.372 0.580 -0.471

0.460 -0.380 0.600 -0.525

0.470 -0.419 0.610 -0.541

0.490 -0.409 0.650 -0.681

0.500 -0.417 0.700 -0.688

0.520 -0.404 0.750 -0.752

0.530 -0.425 0.820 -0.538

0.550 -0.455 0.890 -0.339

0.560 -0.471 0.900 -0.348

0.580 -0.436 0.960 -0.324

0.590 -0.490

0.600 -0.476

0640 -0.654

0700 -0.745

0.750 -0.105"*

0.820 -0.419

0.870 -0.280

0,930 -0.304

0.960 -0.292

Lower Surface

0.020 - 1.225 0020 -0.704 0.020 -0.560 0.020 -0.706

0.1 I 0 -0.112 0.060 -0.158 0.060 -0.080 0.060 0.021

0.230 -0,029 0.090 -0.050 0.090 -0.023 0.110 -0,119

0.400 0.040 O. 120 0.017 0.120 -0.021 0.250 -0.072

0.490 0.096 0.200 -0.029 0.200 -0.006 0.400 -0.023

0.630 2.328** 0.260 0.065 0.250 0.009 0.490 0.032

0.750 0.172 0.400 0,081 0.400 0.047 0.580 0.105

0.850 0.181 0.490 0.112 0.490 -0.057 0.650 0.303

0.900 0.262 0.580 0,166 0.580 0.173 0,750 0.488

0.960 0.155 0.640 0.342 0.650 -0.112 0,830 0.522

0.750 0.287 0.750 0.019 0.900 0.588

0.870 0.273 0.890 0.581 0.960 0.416

0,930 0.208 0,930 0.500

0.960 0.103 0.960 0.341

CN = 0.432 0.530 0.558 0.678

131
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-32-40-000, MINF = 0.607, Camber = 10/10, ALP'I" = 3.26, BETA = -0.30, QINF = 307.4,

RNPU = 3.1E+06, CNWP = 0.3315

I"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x./c CP

0.020 0.527 0.000 -0.179 0.000 0.565"* 0.010 0,248

0.060 0.038 0.020 0.501 0.020 0.428 0.020 0.102

0.110 -0,290 0.040 0.262 0.060 -0.218** 0.060 -0.461

0.200 -0.376 0.060 -0.140 0.090 -0.471 0.110 -0.822

0.230 -0.344 0.090 -0.375 0.110 -0.655 0.140 -0.681

0.400 -0.277 0.130 -0.606 0.130 -3.875 * * 0.190 -3.875 * *

0.490 -0.276 0.150 -0,700 0.150 -0.609 0.250 -0.462

0.590 -0,366 0.200 -0.556 0.210 -0.554 0.400 -0.433

0.630 -0.410 0.250 -0.402 0,250 -0.466 0.490 -0.406

0.700 -0.549 0.260 -0.415 0.340 -0.445 0.580 -0,473

0.750 -0.739 0.280 -0.411 0.370 -0.460 0.650 -0,625

0.810 -0.650 0.290 -0.403 0.400 -0.403 0.700 -0.615

0.840 -0.719 0.310 -0.388 0.410 0.517"* 0,750 -0.874

0.900 -0.311 0.320 -0.408 0.430 -0,468 0.800 -0.946

0.960 -0.112 0.340 -0.397 0.440 -0.459 0.830 -0.812

0.350 -0.185** 0.460 -0.451 0.900 -0.406

0.370 -0.393 0.490 -0.433 0.960 -0.439

0.380 -0.415 0.500 -0.468

0.400 -0.323 0.520 -0,495

0.410 -0,393 0.540 -0.487

0.430 -0.383 0.550 -0.469

0.440 -0.378 0.580 -0.469

0.460 -0.391 0.600 -0.522

0.470 -0.418 0.610 -0.538

0.490 -0.404 0.650 -0.676

0.500 -0.421 0.700 -0.687

0.520 -0.403 0,750 -0.749

0.530 -0.427 0.820 -0.474

0.550 -0.463 0.890 -0.328

0.560 -0.475 0.900 -0.351

0.580 -0.435 0,960 -0.315

0.590 -0.501

0.600 -0.479

0.640 -0.652

0.700 -0.739

0.750 -0.127"*

0.820 -0.440

0.870 -0.303

0.930 -0.319

0.960 -0.358

Lower Surface

0.020 - 1.211 0.020 -0,682 0.020 -0.542 0.020 -0.663

0.110 -0.110 0.060 -0.139 0.060 -0,047 0.060 0.018

0.230 -0.031 0.090 -0.050 0.090 -0.015 0.110 -0.103

0,400 0.025 0.120 0.018 0.120 -0.019 0.250 -0.071

0.490 0,074 0.200 -0.031 0.200 0.001 0.400 -0.026

0.630 2.284"* 0.260 0.061 0.250 0.014 0.490 0.033

0.750 0.136 0.400 0.073 0.400 0.040 0.580 0.107

0.850 0.156 0.490 0.101 0,490 -0,077 0.650 0.299

0.900 0.235 0.580 0.149 0.580 0.171 0.750 0.478

0.960 O. 150 0.640 0.323 0.650 -0.131 0.830 0.532

0.750 0.236 0.750 0.008 0.900 0.584

0.870 0.221 0.890 0.579 0.960 0.420

0.930 0.199 0.930 0.500

0.960 0.106 0.960 0.349

CN = 0.399 0.529 0,556 0.684

132
Table C-2. Continued,

Flight 216, Wing sweep = 26 °, Time = 9-33-31-000, MINF = 0.600, Camber = 10f7, ALPT = 3.01, BETA = -0.56, QINF = 300,2,

RNPU = 3.1E+06, CNWP = 0,3222

T1= 0,93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.545 0.000 -0.247 0.000 0.555** 0.010 0.313

0.060 0.045 0.020 0.529 0,020 0.459 0.020 0.143

0,110 -0.300 0.040 0.287 0.060 -0.172"* 0.060 -0.413

0.200 -0.363 0.060 -0,115 0.090 -0.433 0.110 -0.766

0.230 -0,281 0.090 -0.343 0 110 -0.620 0,140 -0.664

0.400 -0.256 0.130 -0,571 0.130 -3.970"* 0.190 -3.970" *

0,490 -0.245 0.150 -0.663 0.150 -0.584 0,250 -0.448

0.590 -0.324 0.200 -0.526 0.210 -0.515 0.400 -0.425

0.630 -0,342 0.250 -0.389 0.250 -0.451 0.490 -0.400

0.700 -0.434 0,260 -0.400 0.340 -0.443 0,580 -0.445

0.750 -0.531 0.280 -0.389 0,370 -0.451 0,650 -0.623

0.810 -0.468 0,290 -0,381 0.400 -0.400 0,700 -0.612

0.840 -0.510 0.310 -0.368 0.410 0.527** 0.750 -0.872

0.900 -0,284 0.320 -0,389 0.430 -0.452 0,800 -0.971

0.960 -0.103 0.340 -0,382 0.440 -0,452 0.830 -0.834

0.350 -0,171 ** 0.460 -0,437 0.900 -0,391

0.370 -0.376 0.490 -0.431 0.960 -0.437

0,380 -0.391 0.500 -0.454

0.400 -0,355 0.520 -0.493

0.410 -0.377 0.540 -0.474

0.430 -0.360 0.550 -0.458

0.440 -0,341 0.580 -0.466

0.460 -0.368 0.600 -0.526

0.470 -0.398 0.610 -0.540

0.490 -0.397 0.650 -0.678

0.500 -0.402 0,700 -0.691

0,520 -0.393 0.750 -0.755

0.530 -0.416 0.820 -0.539

0.550 -0.449 0.890 -0.327

0.560 -0.464 0.900 -0.338

0.580 -0.421 0.960 -0.315

0.590 -0.485

0.600 -0,464

0.640 -0.641

0.700 -0.734

0.750 -0.158"*

0.820 -0.619

0.870 -0,265

0.930 -0.293

0.960 -0.325

Lower Surface

0,020 - 1,283 0.020 -0,753 0.020 -0,573 0.020 -0.733

0.110 -0,135 0.060 -0.183 0,060 -0.064 0.060 0.012

0.230 -0.039 0.090 -0.072 0.090 -0.028 0.110 -0.108

0,400 0.012 0.120 0.001 0.120 -0.031 0.250 -0.082

0,490 0.043 0.200 -0.038 0,200 -0.015 0,400 -0.022

0.630 2.335** 0.260 0.052 0,250 0,008 0.490 0.023

0,750 0.087 0.400 0.065 0.400 0.038 0.580 0.106

O.850 O. 104 0.490 0.085 0.490 -0.096 0.650 0.296

0.900 O.181 0.580 O.127 0.580 0.165 0.750 0.473

0.960 O, 130 0.640 0,297 0.650 -0.158 0.830 0.510

0.750 0.181 0.750 0.006 0.900 0.583

0,870 0.178 0.890 0,568 0.960 0.415

0.930 0.171 0,930 0.487

0.960 0,099 0.960 0370

CN = 0.314 0.505 0.544 0.666

133
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-33-47-000, MINF = 0.587, Camber = 10/6, ALPT = 12.01, BETA = 0.19, QINF = 286.4,

RNPU = 3.0E+06, CNWP = 0.7221

rl = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.953 0.000 0.303 0.000 0.466"* 0.010 -2.165

0.060 - 1.164 0.020 - 1.600 0.020 -2.196 0.020 -2.190

O. 110 - 1.209 0.040 -0.011 0.060 - 1.403"* 0.060 -2.146

0.200 -0.934 0,060 - 1.740 0.090 -2.173 O.110 - 1.721

0.230 -0.750 0.090 -2,000 0,110 -2,279 0.140 - 1.314

0.400 -0.540 0.130 - 1.661 0.130 -4.140"* 0.190 -4.140 **

0.490 -0.497 0.150 -2.075 0.150 - 1.706 0.250 -0.843

0.590 -0,546 0,200 - 1.571 0.210 - 1.561 0.400 -0.620

0.630 -0,605 0.250 -0.872 0.250 -0.945 0.490 -0.515

0.700 -0.671 0.260 -0.830 0.340 -0.744 0.580 -0.498

0.750 -0.747 0.280 -0.815 0.370 -0.709 0,650 -0.554

0.810 -0.716 0,290 -0.764 0.400 -0.623 0.700 -0.531

0.840 -0.793 0.310 -0.737 0.410 0.574"* 0.750 -0.552

0.900 -0,537 0.320 -0.744 0.430 -0.659 0.800 -0.587

0.960 -0.331 0,340 -0.732 0.440 -0.645 0.830 -0.446

0.350 -0,247"* 0.460 -0,628 0.900 -0.494

0.370 -0.691 0.490 -0.590 0.960 -0.484

0.380 -0,702 0.500 -0.615

0.400 -0.340 0,520 -0.643

0.410 -0.658 0.540 -0.615

0.430 -0.625 0.550 -0.600

0.440 -0.599 0.580 -0.595

0.460 -0.630 0.600 -0.620

0.470 -0.649 0.610 -0.633

0.490 -0.612 0.650 -0.819

0.500 -0.628 0.700 -0.734

0,520 -0.596 0.750 -0.782

0.530 -0,599 0.820 -0.647

0.550 -0.627 0.890 -0.376

0.560 -0.653 0,900 -0.348

0.580 -0.590 0.960 -0.307

0.590 -0.660

0.600 -0.610

0.640 -0.749

0.700 -0.813

0.750 -0,122'*

0.820 -0.357

0.870 -0.264

0.930 -0.221

0.960 -0.235

Lower Surface

0.020 0.344 0.020 0.568 0.020 0.607 0.020 0.710

0. I 10 0.210 0.060 0.497 0.060 0.551 0,060 0.095

0.230 0.110 0.090 0.452 0,090 0.487 0.110 0.483

0.400 0.099 0.120 0.389 0.120 0.411 0.250 0.263

0.490 0.104 0.200 0.111 0.200 0.136 0.400 0.227

0.630 2.470"* 0.260 0.341 0.250 0,320 0.490 0.232

0.750 0.057 0.400 0.249 0,400 0.267 0.580 0.252

0.850 0.043 0.490 0.216 0.490 0,012 0.650 0.381

0,900 0.118 0,580 0.208 0.580 0.270 0,750 0.563

0.960 0,038 0.640 0.359 0.650 -0.121 0.830 0,590

0.750 0.205 0.750 0.088 0.900 0.640

0.870 0.249 0,890 0.618 0,960 0.422

0.930 0.224 0.930 0.507

0,960 0.124 0.960 0.330

CN = 0.770 1.053 1.105 1.135

134
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-34-25-500, MINF = 0.602, Camber = 10/4, ALPT = 3.05, BETA = -0.67, QINF = 301.9,

RNPU = 3.1E+06, CNWP = 0.3308

r[ = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.527 0.000 -0.185 0.000 0.615** 0.010 0.257

0.060 0.043 0.020 0.496 0.020 0.433 0.020 0.094

0.110 -0.291 0.040 0,271 0.060 -0.140 ** 0.060 -0.445

0.200 -0.368 0.060 -0.138 0.090 -0.475 0.110 -0.793

0.230 -0.328 0.090 -0.360 0.110 -0.650 0.140 -0.680

0.400 -0.247 0.130 -0.587 0.130 -3.941"* 0.190 -3.941"*

0.490 -0.218 0.150 -0.676 0.150 -0.598 0.250 -0.452

0.590 -0.261 0.200 -0.547 0.210 -0.533 0.400 -0.437

0.630 -0.276 0.250 -0.406 0.250 -0.463 0.490 -0.390

0.700 -0.330 0.260 -0.398 0.340 -0.434 0.580 -0.446

0.750 -0.343 0.280 -0.403 0.370 -0.464 0.650 -0.622

0.810 -0.295 0.290 -0.394 0.400 -0.384 0.700 -0.60|

0.840 -0.344 0.310 -0.379 0.410 0.531 ** 0,750 -0.882

0.900 -0.215 0.320 -0.398 0.430 -0.457 0.800 -0.966

0.960 -0.074 0.340 -0.387 0.440 -0.443 0.830 -0.837

0.350 -0.152** 0.460 -0.447 0.900 -0.373

0.370 -0.370 0.490 -0.436 0.960 -0.449

0.380 -0.400 0.500 -0.468

0.400 -0.324 0.520 -0.497

0.410 -0.370 0.540 -0.464

0.430 -0.351 0.550 -0.463

0.440 -0.350 0.580 -0.470

0.460 -0.373 0.600 -0.504

0.470 -0.389 0.610 -0.544

0.490 -0.398 0.650 -0.696

0,500 -0.387 0.700 -0.684

0.520 -0,352 0.750 -0.765

0.530 -0.399 0.820 -0.537

0.550 -0.445 0.890 -0, 314

0.560 -0.442 0.900 -0.354

0.580 -0.405 0.960 -0.323

0.590 -0.449

0.600 -0.439

0.640 -0.614

O.700 -0.701

0.750 -0.182"*

0.82O -0.597

0.870 -0.340

0.930 -0.291

0.960 -0.301

Lower Surface

0.020 - 1.237 0.020 -0.655 0.020 -0.50 ! 0.020 -0.671

0,110 -0.121 0.060 -0.122 0.060 -0.070 0.060 0.019

0.230 -0.042 0.090 -0.067 0.090 -0.011 0.110 -0.121

0.400 -0.010 0.120 0.005 0.120 -0.037 0.250 -0.082

0.490 0.028 0.200 -0.027 0.200 0.013 0.400 -0.029

0.630 2.330** 0.260 0.059 0.250 0.008 0.490 0.038

0.750 0.025 0.400 0.050 0.400 0.031 0.580 0.099

0.850 0.039 0.490 0.084 0.490 -0. l 17 0.650 0.287

0.900 0.114 0.580 0.104 0.580 0.171 0.750 0.473

0.960 0.089 0.640 0.274 0.650 -0.171 0.830 0.537

0.750 0.124 0.750 -0.001 0.900 0.593

0.870 0.124 0.890 0.566 0.960 0.426

0.930 0.174 0.930 0.491

0.960 0.098 0.960 0.349

CN = 0.243 0.493 0.547 0.674

135
Table C-2. Continued,

Flight 216, Wing sweep = 26 °, Time = 9-35-22-500, MINF = 0.599, Camber = 10/0, ALPT = 2,03, BETA = 0.22, QINF = 298.2,

RNPU = 3.1E+06, CNWP = 0.2836

= 0,93 0,76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.600 0,000 -0.430 0.000 0.461 ** 0.010 0.428

0.060 0,089 0,020 0.615 0.020 0,562 0.020 0,257

0.110 -0.222 0.040 0,376 0,060 -0.060** 0,060 -0,281

0.200 -0.302 0.060 -0.020 0.090 -0.334 0.110 -0,646

0.230 -0,278 0.090 -0.255 0.110 -0.509 0,140 -0.592

0.400 -0,199 0.130 -0.483 0.130 -3.981 ** 0.190 -3.981 **

0.490 -0.182 0.150 -0.579 0,150 -0,508 0,250 -0.394

0.590 -0.207 0,200 -0.457 0.210 -0.457 0.400 -0.385

0,630 -0,192 0,250 -0.341 0,250 -0,394 0.490 -0,368

0.700 -0.180 0,260 -0.333 0,340 -0,399 0,580 -0.419

0,750 -0.153 0.280 -0.344 0.370 -0.404 0.650 -0.599

0.810 -0,117 0,290 -0.344 0.400 -0.357 0.700 -0.588

0.840 -0,144 0.310 -0,325 0.410 0.546** 0,750 -0.855

0.900 -0.122 0.320 -0,338 0.430 -0,408 0.800 -0.984

0,960 -0.031 0.340 -0,336 0.440 -0,417 0.830 -0,844

0,350 -0.164"* 0,460 -0,408 0.900 -0.389

0,370 -0.332 0,490 -0,402 0.960 -0,428

0.380 -0.351 0.500 -0.437

0,400 -0,327 0.520 -0.458

0.410 -0.334 0.540 -0.435

0.430 -0.318 0.550 -0.438

0.440 -0,319 0.580 -0.447

0.460 -0.336 0.600 -0.494

0.470 -0.362 0.610 -0.516

0.490 -0.357 0.650 -0.683

0.500 -0.363 0.700 -0,672

0,520 -0,346 0,750 -0.755

0,530 -0.367 0.820 -0.598

0.550 -0.402 0.890 -0.330

0.560 -0.412 0.900 -0.343

0.580 -0.377 0.960 -0.323

0,590 -0.421

0.600 -0.411

0,640 -0,589

0.700 -0.675

0.750 -0.260**

0.820 -0,670

0,870 -0.632

0.930 -0.334

0.960 -0.347

Lower Surface

0.020 - 1.021 0.020 -0,989 0.020 -0,856 0,020 - 1.075

0.110 -0.236 0.060 -0,367 0,060 -0,182 0,060 -0.001

0,230 -0.071 0,090 -0,202 0.090 -0.106 0. I 10 -0.204

0.400 -0,035 0.120 -0.086 0.120 -0.1 04 0.250 -0.122

0.490 -0.015 0.200 -0.066 0,200 -0,035 0.400 -0,057

0.630 2.367** 0.260 0.003 0,250 -0.028 0,490 0,003

0.750 -0.019 0.400 0.026 0.400 0.001 0.580 0.089

0.850 -0.017 0,490 0.046 0.490 -0.154 0.650 0.285

0,900 0,041 0.580 0.076 0.580 0.138 0,750 0.472

0.960 0,063 0.640 0.226 0,650 -0,243 0.830 0.515

0,750 0.045 0.750 -0,007 0.900 0,580

0.870 0.055 0.890 0.545 0,960 0,417

0.930 0,086 0.930 0.462

0,960 0.024 0.960 0.343

CN = 0.118 0.409 0.474 0.603

136
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-35-30-000, MINF = 0.609, Camber = 10/l, ALPT = 3.11, BETA = -0.01, QINF = 309.6,

RNPU = 3.1E+06, CNWP = 0.3061

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.549 0.000 -0.223 0.000 0.548** 0.010 0.283

0.060 0.042 0.020 0.521 0.020 0,450 0,020 O. 128

O. 110 -0.279 0.040 0.278 0.060 -0.238** 0.060 -0.431

0,200 -0.350 0.060 -0.123 0.090 -0.451 0. I 10 -0.801

0.230 -0.319 0.090 -0.352 0.110 -0.638 0.140 -0.689

0.400 -0.230 0.130 -0.584 0,130 -3.847 * * 0.190 -3.847 * *

0.490 -0.209 0.150 -0.677 0.150 -0.602 0.250 -0.459

0.590 -0.235 0.200 -0.538 0.210 -0.537 0.400 -0.437

0.630 -0.235 0.250 -0.400 0.250 -0.456 0.490 -0.403

0.700 -0.227 0.260 -0.399 0.340 -0.441 0.580 -0.453

0.750 -0.209 0.280 -0.397 0,370 -0.440 0.650 -0.625

0.810 -0.174 0.290 -0.380 0.400 -0.406 0.700 -0.614

0.840 -0.195 0.310 -0.370 0.410 0.514"* 0.750 -0.871

0.900 -0.164 0.320 -0.393 0.430 -0.450 0.800 -0.939

0,960 -0.056 0.340 -0.381 0.440 -0,450 0.830 -0.811

0.350 -0.177** 0.460 -0.445 0.900 -0.399

0.370 -0.375 0.490 -0.422 0.960 -0.442

0.380 -0.390 0.500 -0.460

0,400 -0.334 0.520 -0.489

0.410 -0.373 0.540 -0.484

0.430 -0.355 0.550 -0.467

0.440 -0.353 0.580 -0.463

0.460 -0.356 0.600 -0.521

0.470 -0.391 0.610 -0.535

0.490 -0.385 0.650 -0.693

0.500 -0.395 0.700 -0.688

0.520 -0.369 0.750 -0.757

0.530 -0.400 0.820 -0.525

0.550 -0.438 0.890 -0.359

0.560 -0.437 0.900 -0.364

0.580 -0,400 0.960 -0. 340

0.590 -0.464

0.600 -0.44 1

0.640 -0.604

0.700 -0.684

0.750 -0.234**

0.820 -0,604

0.870 -0.554

0.930 -0.320

0.960 -0,319

Lower Surface

0.020 - 1.287 0.020 -0.755 0.020 -0.582 0.020 -0.647

0,110 -0.168 0.060 -0.196 0.060 -0.073 0.060 0.001

0.230 -0.048 0.090 -0,092 0.090 -0.033 0. 110 -0.126

0.400 -0.032 0.120 -0.010 0.120 -0.049 0.250 -0.084

0.490 -0.020 0.200 -0.048 0.200 -0.025 0.400 -0.032

0.630 2.268"* 0.260 0.033 0.250 0.000 0.490 0.015

0.750 -0.031 0.400 0.04 1 0.400 0.026 0.580 0.102

0.850 -0.011 0.490 0.057 0.490 -0.132 0.650 0.29 I

0.900 0,063 0.580 0.090 0.580 0.156 0.750 0.475

0.960 0.067 0.640 0.256 0.650 -0.219 0.830 0,523

0.750 0,077 0.750 -0.005 0.900 0.578

0.870 0,081 0.890 0.568 0.960 0.409

0.930 0.113 0.930 0.483

0,960 0.046 0.960 0.336

CN = 0.168 0.469 0.533 0.668

137
Table C-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-35-34-000, MINF = 0.610, Camber = 10/0, ALPT = 6.06, BETA = -0.67, QINF = 310.6,

RNPU = 3.1E+06, CNWP -- 0.4158

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.261 0.000 0.556 0.000 0.797** 0.010 -0.320

0.060 -0.243 0.020 0.094 0.020 -0.045 0.020 -0.382

0.110 -0.542 0.040 -0.125 0.060 -0.607" * 0.060 -0.961

0.200 -0.524 0.060 -0.557 0.090 -0.878 0.110 - 1.267

0.230 -0.451 0.090 -0.753 0.110 -1.108 0.140 - 1.000

0.400 -0.303 0.130 - 1.009 0.130 -3.835"* 0.190 -3.835"*

0.490 -0.262 0.150 - 1.071 0.150 -0.910 0.250 -0.619

0.590 -0,284 0.200 -0.818 0.210 -0.790 0.400 -0.529

0.630 -0.265 0.250 -0.581 0.250 -0.637 0.490 -0.474

0.700 -0.260 0.260 -0.562 0.340 -0.585 0.580 -0.508

0.750 -0.222 0.280 -0.558 0.370 -0.569 0,650 -0.658

0.810 -0.194 0.290 -0.533 0.400 -0.505 0.700 -0.639

0.840 -0.223 0.310 -0.507 0.410 0.512"* 0.750 -0.861

0.900 -0.196 0.320 -0.527 0.430 -0.536 0.800 -0.788

0.960 -0.097 0.340 -0.490 0.440 -0.544 0.830 -0.654

0.350 -0.208"* 0.460 -0.531 0.900 -0.401

0.370 -0.487 0,490 -0.516 0.960 -0.419

0.380 -0.507 0.500 -0.535

0.400 -0.316 0.520 -0.571

0.410 -0.470 0.540 -0,547

0.430 -0.446 0.550 -0.535

0.440 -0.439 0.580 -0.518

0.460 -0,456 0.600 -0.586

0.470 -0.476 0.610 -0.597

0.490 -0.469 0.650 -0.733

0.500 -0_469 0_700 -0.736

0.520 -0.444 0.750 -0.802

0.530 -0.464 0.820 -0.558

0.550 -0.502 0.890 -0.375

0.560 -0.506 0.900 -0.380

0.580 -0.462 0.960 -0.362

0.590 -0.517

0.600 -0.497

0.640 -0.651

0.700 -0.731

0.750 -0.227**

0820 -0.621

0.870 -0.532

0.930 -0.323

0.960 -0.339

Lower Surface

0.020 -0.328 0.020 -0.147 0.020 -0.070 0.020 0.005

O. I 10 -0.025 0.060 O.127 0.060 O.157 0.060 0.029

0.230 0.010 0.090 OA 11 0.090 0.161 0.110 O. 113

0.400 -0.003 O. 120 O. 131 O, 120 O. 110 0.250 0.046

0.490 -0.027 0.200 0.022 0.200 0.034 0.400 0.059

0.630 2.261"* 0.260 O. 123 0.250 0.123 0.490 0.083

0.750 -0.054 0.400 0.109 0.400 0.I 11 0.580 0.140

0.850 -0.027 0.490 0.107 0.490 -0.1 04 0.650 0.325

0.900 0.032 0.580 0.107 0.580 0.187 0.750 0.506

0.960 0.050 0.640 0.276 0.650 -0.197 0.830 0.551

0.750 0.074 0.750 0.009 0.900 0.604

0.870 0.091 0.890 0.602 0.960 0.416

0,930 0.120 0.930 0.484

0.960 0.031 0.960 0.334

CN = 0.277 0.661 0.723 0.852

138
Table C-2. Concluded.

Flight 198, Wing sweep = 26 °, Time = 13-8-42-000, MINF = 0.590, Camber = 19/2, ALPT = 7,63, BETA = 0.60, QINF = 268.4,

RNPU = 2.8E+06, CNWP = 0,3751

r I = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.738 0.000 -0.643 0,000 -8.239** 0.010 0.523"*

0.060 0.004 0,020 0.747"* 0.020 0.712"* 0.020 0.348"*

0.110 -0.546 0.040 0.344 0.060 - 1.400"* 0.060 -0.766

0,200 -0.651 0.060 -0.218 0.090 -0.842 0.110 -1.335

0.230 -0.453 0.090 -0,736 0.110 - 1.348 0.140 2,095**

0.400 -0,238 0,130 - 1.340 0.130 -2,024 0.190 -8.090"*

0.490 -0,229 0.150 - 1,532 0.150 -0.993 0,250 -0.566

0.590 -0.221 0.200 -0.904 0,210 -0.810 0.400 -0,392

0.630 -0.219 0.250 -0,549 0,250 -0.576 0.490 -0,328

0.700 -0.248 0.260 -0.515 0.340 -0.470 0,580 -0.303

0.750 -0.212 0,280 -0.496 0,370 -0.456 0.650 -0,377

0.810 -0.202 0,290 -0.477 0.400 -0,368 0.700 -0.322

0,840 -0.215 0,310 -0.430 0,410 -0.391 0.750 -0.299

0,900 -0.117 0.320 -0.445 0.430 -0.398 0.800 -0.235

0.960 -0.042 0.340 -0,426 0.440 -0.412 0.830 -0,263

0.350 -0.173** 0.460 -0.383 0.900 -0.113

0.370 -0,386 0.490 -0.379 0.960 0.016

0.380 -0.359 0,500 -0.349

0.400 -0.309 0,520 -0,356

0.410 -0.363 0.540 -0.354

0.430 -0.331 0.550 -0.301

0.440 -0.305 0,580 -0.285

0.460 -0.352 0.600 -0.348

0.470 -0.351 0.610 -0,242

0.490 -0.303 0.650 -5.045 * *

0.500 -0.289 0.700 -0.325

0.520 -0.297 0.750 -0.268

0.530 -0,284 0.820 -0.275

0.550 -0,299 0,890 -0.128

0,560 -0.299 0,900 -0.106

0.580 -0.252 0.960 -0.035

0.590 -0.306

0.600 -0.303

0.640 -4.865**

0.700 -0_280

0,750 -0,244

0.820 -5.059**

0.870 -0.18t

0.930 -0.070

0.960 -0.013

Lower Surface

0,020 -0.867 0.020 -0,382 0.020 -0.556 0.020 -0,726

0,110 -0,245 0.060 -0.222 0.060 0.053 0,060 1.623"*

0,230 -0.052 0.090 -0.135 0.090 0.182 0.110 0.269

0.400 0.070 0.120 0.000 0.120 O. 180 0.250 0.046

0.490 0.045 0.200 -0.04 1 0,200 -0.047 0.400 -0.027

0.630 1.671 ** 0.260 0.105 0.250 0.104 0.490 -0.062

0.750 0.039 0.400 -5.078 * * 0.400 -0.004 0.580 -0.117

0,850 0,084 0.490 0.023 0.490 0.015 0.650 -0,007

0,900 0.112 0.580 0.043 0.580 -0,086 0.750 0.188

0,960 0,104 0.640 0.319 0.650 0.041 0,830 0.282

0.750 0.123 0.750 0,248 0.900 0.323

0.870 0.216 0.890 ******** 0.960 0.249

0.930 0,192 0.930 0.222

0.960 0.117 0.960 -5.077 * *

CN = 0.257 0.453 0.524 0.552

139
APPENDIX D

Wing Pressure Coefficients for Nominal Dynamic Pressure

of 300 lb/ft 2 and Mach Number of 0.70.

Leading-edge wing sweep is 26 °. Table D-1 contains a summary of the data listing in table D-2. The asterisks

(*) in table D-2 indicate invalid values. Camber is _LE/TE"Refer to Nomenclature for definitions.

Table D-1. Summary of data.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

191 8-55-8-000 0.705 0/2 6.09 -0.16 304.7 2.7E+06 0.2787

191 8-55-9-500 0.704 0/2 5.96 -0.30 304.0 2.7E+06 0.2751

195 8-29-56-000 0.701 0/2 6.01 0.23 301.5 2.7E+06 0.2488

195 8-30-7-000 0.704 0/2 5.95 0.26 304.3 2.7E+06 0.2436

195 8-30-12-000 0.705 0/2 7.02 -0.30 306.0 2.8E+06 0.2474

195 8-30-20-000 0.700 0/2 7.00 0.15 300.5 2.7E+06 0.2668

195 8-30-35-500 0.687 0/2 8.10 0.18 285.2 2.6E+06 0.2909

195 8-30-47-000 0.693 0/2 9.07 0.10 292.1 2.7E+06 0.3584

195 8-30-52-000 0.704 0/2 10.14 0.26 302.0 2.7E+06 0.3427

!95 8-30-58-500 0.702 0/2 10.90 0.23 301.4 2.7E+06 0.3936

200 8-30-17-000 0.696 0/2 6.16 -0.27 296.3 2.7E+06 0.2922

200 8-30-25-000 0.696 0/2 7.02 -0.33 295.5 2.7E+06 0.3127

200 8-30-31-000 0.696 0/2 7.99 -0.18 296.0 2.7E+06 0.3561

200 8-30-32-000 0.696 0/2 8.20 -0.33 296.0 2.7E+06 0.3388

222 10-51-24-000 0.692 0/2 11.95 0.54 298.1 2.7E+06 0.2582

222 10-51-25-000 0.691 0/2 12.25 -0.44 298.2 2.7E+06 0.2470

222 10-51-27-000 0.689 0/2 12.96 0.37 298.7 2.7E+06 0.1691

191 8-57-6-500 0.703 5/2 7.17 -0.14 303.6 2.7E+06 0.3272

191 8-57-14-000 0.708 5/2 9.11 -0.06 310.1 2.8E+06 0.4156

195 8-33-5-500 0.708 5/2 6.15 0.07 304.1 2.7E+06 0.3052

195 8-33-27-500 0.705 5/2 7.22 -0.03 300.8 2.7E+06 0.3432

195 8-33-43-500 0.695 5/2 8.05 -0.08 291.9 2.7E+06 0.3907

195 8-34-2-000 0.715 5/2 9.12 0.07 312.3 2.8E+06 0.4406

195 8-34-8-500 0.715 5/2 10.07 -0.08 311.4 2.8E+06 0.3911

195 8-34-12-500 0.703 5/2 11.06 0.05 299.5 2.7E+06 0.3610

195 8-34-26-000 0.697 5/2 11.27 0.05 297.5 2.7E+06 0.3728

195 8-34-33-500 0.697 5/2 11.88 0.13 301.7 2.7E+06 0.3778

195 8-35-52-000 0.700 5/6 5.12 -0.48 297.3 2.7E+06 0.3726

195 8-35-59-000 0.701 5/6 6.97 -0.37 297.2 2.7E+06 0.4529

195 8-36-15-000 0.705 5/6 8.03 -0.11 296.8 2.7E+06 0.4727

140
TableD-1.Concluded.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

195 8-36-33-000 0.721 5/6 9.17 0.15 332.1 2.9E+06 0.4460

195 8-36-45-500 0.692 5/6 11.00 0.05 313.4 2.9E+06 0.4383

195 8-37-22-000 0.691 5/6 11.06 -0.19 312.5 2.9E+06 0.4411

195 8-39-31-500 0.696 5/10 3.95 -0.03 282.6 2.6E+06 0.3128

195 8-39-46-000 0.691 5/10 6.00 -0.32 278.5 2.5E+06 0.3859

195 8-39-57-500 0.690 5/10 7.01 -0.37 276.5 2.5E+06 0.4296

195 8-40-7-500 0.701 5/10 8.06 -0.11 286.0 2.6E+06 0.5042

195 8-41-2-000 0.686 5/10 6.99 -0.19 283.2 2.6E+06 0.4150

195 8-41 - 12-000 0.700 5/10 8.12 -0.08 299.5 2.7E+06 0.4919

195 8-41-18-500 0.703 5/10 9.29 0.10 306.0 2.8E+06 0.5275

195 8-41-26-000 0.697 5/10 10.06 -0.06 303.2 2.8E+06 0.5327

195 8-41-50-000 0.699 5/10 11.06 -0.06 313.7 2.8E+06 0.5325

195 8-41-58-500 0.700 5/10 11.02 0.28 319.4 2.9E+06 0.5307

204 8-29-13-000 0.695 10/10 7.18 0.17 281.4 2.6E+06 0.5226

204 8-29-16-000 0.691 10/10 8.13 0.25 279.8 2.6E+06 0.5499

204 8-29-23-000 0.694 10/10 11.25 0.80 290.0 2.6E+06 0.5207

223 10-6-25-000 0.702 5/15 3.12 0.25 288.0 2.6E+06 0.3044

223 10-6-40-000 0.702 5/16 4.04 -0.2 ! 288.1 2.6E+06 0.3618

223 10-6-42-000 0.704 5/16 5.16 -0.07 289.9 2.6E+06 0.3858

223 10-6-44-500 0.705 5/16 6.08 -0.27 290.5 2.6E+06 0.4093

223 10-6-48-000 0.703 5/16 7.02 -0.21 288.2 2.6E+06 0.4371

223 10-6-54-000 0.702 5/15 7.98 -0.21 286.1 2.6E+06 0.5183

223 10-6-58-500 0.706 5/15 9.99 0.19 292.3 2.6E+06 0.6355

223 10-7-4-000 0.703 5/16 11.03 -0.10 295.0 2.7E+06 0.6281

223 10-7-12-500 0.693 5/16 11.95 -0.56 296.7 2.7E+06 0.6443

204 8-30-51-000 0.692 5/15 3.04 -0.24 282.6 2.6E+06 0.3626

204 8-30-57-500 0.697 5/15 5.04 -0.12 284.6 2.6E+06 0.4324

204 8-31-0-000 0.692 5/15 4.07 -0.07 278.7 2.5E+06 0.4111

204 8-31-8-500 0.692 5/15 8.21 0.25 279.4 2.6E+06 0.6380

204 8-31-11-500 0.692 5/15 9.29 0.34 280.9 2.6E+06 0.7725

204 8-31-17-500 0.687 5/16 11.05 -0.41 283.8 2.6E+06 0.7577

141
Table D-2. Listing of Data.

Flight 191, Wing sweep = 26 °, Time = 8-55-8-000, MINF = 0.705, Camber = 0/2, ALPT = 6.09, BETA = -0.16, QINF = 304.7,

RNPU = 2.7E+06, CNWP = 0.2787

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.510 0.000 0.788 0.000 -5.753** 0.010 -1,520

0.060 -0.296 0,020 - 1.137 0.020 - 1.261 0.020 - 1.584

0.110 -0.235 0.040 -0.607 0.060 -0.514"* 0.060 -0,704

0.200 -0.232 0.060 -0.640 0.090 -0.567 0,110 -0.635

0.230 -0,279 0.090 -0.489 0.1 I 0 -0.620 0.140 -0.597

0.400 -0.188 0.130 -0.469 0.130 -0.544 0.190 -6,394"*

0.490 -0.184 0.150 -0.472 0,150 -0.496 0.250 -0.452

0.590 -0.213 0.200 -0.355 0.210 -0.554 0.400 -0.340

0.630 -0.215 0.250 -0.416** 0.250 -0.393 0.490 -0.349

0.700 -0.179 0.260 -0.295 0.340 -0.375 0.580 -0.320

0.750 -0.214 0.280 -0.362 0.370 -0.369 0.650 -0,350

0.810 -0.248 0.290 -0.362 0.400 -0.361 0.700 -0.330

0.840 -0.209 0.310 -0.330 0.410 -0.314 0.750 -0.351

0.900 -0. I 13 0.320 -0,302 0.430 -0,358 0.800 -0.355

0.960 -0,045 0.340 -0.315 0.440 -0.324 0.830 -0.308

0.350 -0.210"* 0.460 -0.346 0.900 -0.172

0.370 -0.291 0,490 -0.284 0.960 -0.004

0.380 -0.303 0.500 -0.335

0.400 -0.209 0.520 -0.284

0,410 -0.32 l 0.540 -0.306

0.430 -0.279 0.550 -0.312

0.440 -0.240 0.580 -0.31 l

0.460 -0.330 0.600 -0.297

0.470 -0.285 0.610 -0.235

0.490 -0.277 0.650 -3.704**

0,500 -0.261 0,700 -0.347

0.520 -0.291 0.750 -0.410

0.530 -0.252 0.820 -0.313

0,550 -0.275 0.890 -0.133

0.560 -0.267 0.900 -0.107

0.580 -0.244 0.960 -0.009

0.590 -0.286

0.600 -0.327

0.640 -3.545"*

0.700 -0.294

0.750 -0.241

0.820 -3.716"*

0,870 -0,206

0.930 -0.095

0.960 -0.023

Lower Surface

0.020 -0.079 0,020 0.127 0,020 0.197 0,020 0.507

0.110 -0.120 0.060 0.114 0.060 0.234 0.060 1.922"*

0.230 0.006 0.090 0.010 0.090 0.078 0.110 -0.006

0.400 -0.037 0.120 -0.019 0.120 -0.315"* 0.250 -0.118

0.490 -0.062 0.200 0.009 0.200 -0,077 0.400 -0.119

0.630 1.947"* 0.260 -0.130 0.250 -0.069 0.490 -0.202

0.750 0.023 0.400 -3.733 * * 0.400 -0.091 0.580 -0.192

0.850 0.093 0.490 -0.106 0.490 -0.006 0.650 -0.076

0.900 0.175 0.580 -0,049 0.580 -0.134 0.750 0.143

0.960 0.142 0.640 0.266 0.650 0.021 0.830 0.290

0.750 0.152 0.750 0.237 0.900 0.348

0,870 0.213 0.890 ******** 0.960 0.258

0.930 0.222 0.930 0.236

0.960 0.139 0.960 -3.477**

CN = 0.192 0,354 0.382 0.401

142
Table D-2. Continued.

Flight 191, Wing sweep = 26 °, Time = 8-55-9-500, MINF = 0.704, Camber = 0/2, ALPT = 5.96, BETA = -0.30, QINF = 3040,

RNPU = 2.7E+06, CNWP = 0.2751

i'1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP xJc CP x/c CP

0.020 -0.503 0.000 0.798 0.000 -5.766"* 0.010 - 1.523

0.060 -0.297 0.020 - 1,118 0,020 - 1.209 0.020 - 1.588

0.110 -0.224 0.040 -0.591 0.060 -0,573** 0.060 -0.699

0.200 -0.233 0.060 -0.626 0.090 -0.558 0.110 -0,637

0.230 -0.294 0.090 -0.486 0,110 -0.613 0.140 -0.592

0.400 -0.203 0.130 -0.457 0, 130 -0.545 0.190 -6.409* *

0.490 -0.185 0.150 -0.466 0,150 -0.472 0.250 -0.440

0.590 -0,210 0.200 -0.364 0.210 -0.560 0.400 -0.334

0.630 -0.208 0.250 -0.417"* 0,250 -0.386 0.490 -0.350

0.700 -0.180 0.260 -0,296 0,340 -0.376 0.580 -0,321

0.750 -0,218 0.280 -0.354 0,370 -0.363 0.650 -0.359

0.810 -0.249 0.290 -0.363 0.400 -0.362 0.700 -0.345

0.840 -0.195 0.310 -0.325 0.410 -0.315 0,750 -0.351

0.900 -0. I11 0.320 -0.299 0.430 -0.359 0.800 -0,356

0.960 -0.046 0.340 -0.309 0.440 -0.325 0.830 -0,309

0.350 -0.211 ** 0.460 -0.341 0.900 -0.181

0.370 -0.288 0,490 -0.285 0.960 -0.008

0,380 -0,300 0,500 -0.336

0.400 -0,220 0.520 -0.285

0.410 -0.316 0,540 -0.307

0.430 -0,268 0.550 -0.3 t3

0.440 -0.237 0.580 -0.294

0.460 -0.331 0.600 -0.298

0.470 -0,292 0.610 -0.236

0490 -0.274 0.650 -3.712"*

0.500 -0,240 0.700 -0.348

0.520 -0,277 0.750 -0.411

0.530 -0.256 0,820 -0.314

0.550 -0.290 0.890 -0.133

0.560 -0.262 0.900 -0.107

0.580 -0.245 0.960 -0.010

0.590 -0.283

0.600 -0.328

0.640 -3.553**

0.700 -0.29 I

0.75O -0.238

0.820 -3.724**

0.870 -0.207

0.930 -0.095

0.960 -0,016

Lower Surface

0.020 -0,098 0.020 0.099 0.020 0.182 0.020 0.495

0.1 I 0 -0.120 0.060 0.103 0.060 0.207 0.060 1.927 * *

0,230 0.005 0.090 0.004 0.090 0.059 0.110 -0006

0.400 -0.040 0.120 -0.026 0.120 -0.316** 0.250 -0.118

0.490 -0,066 0.200 0.002 0,200 -0.077 0.400 -0.119

0.630 1.951 ** 0,260 -0.134 0.250 -0.077 0.490 -0.203

0.750 0.027 0.400 -3.742* * 0.400 -0,092 0.580 -0.192

0.850 0,093 0.490 -0.106 0.490 -0.006 0,650 -0.084

0.900 0.175 0.580 -0,053 0.580 -0,134 0.750 0.143

0.960 0.146 0.640 0,266 0.650 0.021 0.830 0.282

0.750 0.160 0.750 0.237 0.900 0.345

0870 0.213 0,890 ******** 0.960 0.259

0.930 0.208 0.930 0.237

0.960 0.135 0,960 -3.485**

CN = 0.193 0.348 0.377 0.399

143
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-29-56-000, MINF = 0,701, Camber = 0/2, ALPT = 6.01, BETA = 0.23, QINF = 301.5,

RNPU = 2.7E+06. CNWP = 0.2488

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.468 0,000 0,804 0,000 -6,585** 0.010 -1.584

0.060 -0,293 0,020 -0.893 0,020 - 1.165 0.020 - 1.565

0.110 -0,245 0.040 -0.567 0.060 - 1.260* * 0,060 -0,689

0.200 -0.251 0.060 -0,570 0.090 -0,579 0.110 -0.607

0,230 -0.244 0,090 -0.449 0.110 -0.558 0,140 1.900"*

0,400 -0,197 0.130 -0.465 0.130 -0.559 0.190 -6.453 **

0,490 -0.182 0.150 -0.439 0.150 -0.444 0.250 -0,463

0.590 -0,204 0,200 -0,374 0.210 -0.545 0.400 -0.363

0,630 -0.210 0.250 -0.354 0,250 -0,433 0.490 -0.347

0.700 -0.229 0,260 -0,337 0.340 -0.395 0,580 -0.318

0.750 -0.201 0.280 -0.351 0.370 -0,397 0,650 -0.384

0.810 -0.202 0.290 -0.347 0.400 -0.350 0.700 -0.343

0.840 -0,200 0.310 -0.315 0.410 -0.349 0.750 -0.346

0,900 -0.111 0.320 -0.329 0.430 -0.377 0.800 -0,301

0,960 -0.016 0.340 -0.334 0.440 -0,349 0,830 -0.296

0.350 -0.150"* 0,460 -0,334 0.900 -0.181

0,370 -0.307 0.490 -0.323 0.960 -0,001

0.380 -0.291 0.500 -0.318

0.400 -0.261 0,520 -0.341

0.410 -0.297 0.540 -0,336

0,430 -0,267 0.550 -0.306

0,440 -0.254 0.580 -0.281

0.460 -0.306 0,600 -0,364

0,470 -0.299 0.610 -0.250

0,499 -0.281 0,650 -3.742 * *

0.500 -0,275 0,700 -0.335

0.520 -0,264 0,750 -0,289

0.530 -0.256 0,820 -0,293

0.550 -0,277 0.890 -0.131

0.560 -0.298 0.900 -0.103

0.580 -0.251 0,960 -0.03 I

0.590 -0.304

0.600 -0,291

0,640 -3.582**

0.700 -0.289

0,750 -0.257

0,820 -3,755**

0,870 -0.204

0.930 -0,085

0,960 -0.012

Lower Surface

0.020 -0.074 0.020 0.064 0,020 0.168 0,020 0.486**

0.110 -0.126 0,060 0.105 0.060 0.158 0.060 5.5 l 2 **

0.230 0.006 0,090 0,025 0,090 0.052 0.110 0.009

0,400 -0.055 0.120 -0,030 0.120 -0.106 0,250 -0.1 44

0,490 -0,076 0.200 0.013 0,200 -0,029 0.400 -0.126

0.630 3.342** 0,260 -0.101 0,250 -0.106 0.490 -0.167

0.750 0.012 0.400 -3.772 ** 0.400 -0.127 0,580 -0.199

0.850 0.071 0.490 -0.110 0.490 -0,024 0.650 -0.081

0,900 0.138 0,580 -0.071 0.580 -0.1 64 0.750 0.150

0.960 0.130 0,640 0,245 0.650 -0.014 0.830 0.261

0.750 0.111 0.750 0.188 0.900 0.330

0.870 0.203 0.890 ******** 0.960 0.256

0.930 O. 193 0.930 0.235

0960 O. 108 0.960 -3.771 **

CN = 0.178 0.335 0,350 0.386

144
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-30-7-000, MINF = 0.704, Camber = 0/2, ALPT = 5.95, BETA = 0.26, QINF = 304,3,

RNPU = 2.7E+06, CNWP = 0.2436

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.424 0.000 0.828 0.000 -6.530"* 0,010 - 1.541

0.060 -0.255 0.020 -0.822 0.020 -0.822 0.020 - 1.522

0.110 -0.223 0.040 -0.526 0.060 -1.178"* 0.060 -0.706

0.200 -0.256 0.060 -0.542 0.090 -0,556 0.110 -0.594

0,230 -0.271 0.090 -0.424 0,110 -0.527 0.140 1.890"*

0.400 -0.180 0,130 -0.440 0,130 -0.548 0.190 -6.400 **

0.490 -0.169 0,150 -0.419 0.150 -0.432 0.250 -0.457

0.590 -0,206 0.200 -0.352 0.210 -0.527 0.400 -0.352

0.630 -0,200 0.250 -0.343 0,250 -0.421 0,490 -0.336

0.700 -0.215 0,260 -0.320 0,340 -0.383 0,580 -0.297

0.750 -0.195 0,280 -0.331 0,370 -0.378 0,650 -0.395

0.810 -0.206 0,290 -0,331 0.400 -0.303 0,700 -0.332

0.840 -0.197 0.310 -0.298 0.410 -0,334 0.750 -0,335

0.900 -0.105 0,320 -0.305 0.430 -0.351 0.800 -0,305

0.960 -0.001 0,340 -0.320 0,440 -0.338 0.830 -0,300

0.350 -0.146"* 0.460 -0.318 0,900 -0.172

0.370 -0.293 0.490 -0.313 0.960 0.015

0.380 -0.281 0.500 -0.317

0.400 -0.240 0.520 -0.330

0.410 -0.283 0.540 -0.325

0.430 -0.257 0.550 -0.301

0.440 -0.244 0.580 -0.254

0.460 -0.296 0.600 -0.352

0.470 -0.301 0.610 -0.240

0.490 -0,266 0.650 -3.714 * *

0.500 -0.259 0.700 -0.325

0.520 -0.246 0.750 -0.285

0.530 -0.246 0.820 -0.291

0.550 -0.267 0.890 -0.126

0.560 -0.275 0.900 -0.095

0,580 -0.235 0.960 -0.030

0.590 -0.285

0.600 -0.286

0.640 -3.555**

0.700 -0.286

0.750 -0.250

0,820 -3.726**

0,870 -0.194

0.930 -0.072

0.960 -0.008

Lower Surface

0.020 -0.094 0.020 0.043 0.020 0,143 0,020 0.477"*

O. 110 -0.130 0,060 0.097 0.060 O,151 0.060 5.454 **

0.230 0.017 0.090 0.001 0.090 0.047 O. 110 -0.003

0.400 -0.046 0.120 -0.036 0.120 -0.114 0.250 -0.148

0.490 -0.068 0,200 0.010 0.200 -0.034 0.400 -0.125

0.630 3.304"* 0,260 -0.107 0.250 -0.112 0.490 -0,158

0.750 0.020 0,400 -3.743"* 0,400 -0.119 0.580 -0,194

0,850 0.082 0.490 -0,109 0.490 -0,017 0.650 -0,072

0.900 0.150 0,580 -0.066 0.580 -0.154 0,750 O. 142

0,960 0.141 0.640 0,237 0.650 -0.006 0.830 0.275

0.750 0.125 0.750 0.194 0.900 0.341

0.870 0,209 0.890 ******** 0.960 0.261

0,930 O. 199 0.930 0.248

0.960 O. 118 0.960 -3.742"*

CN = 0.178 0,322 0.342 0.380

145
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-30-12-000, MINF = 0.705, Camber = 0/2, ALPT = 7.02, BETA = -0.30, QINF = 306.0,

RNPU = 2.8E+06, CNWP = 0.2474

r_ = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.830 0.000 0.672 0.000 -6.500"* 0.010 - 1.683

0.060 -0.414 0.020 - 1.425 0.020 - 1.536 0.020 - 1.748

O. 110 -0.318 0.040 -0.699 0.060 - 1.637"* 0.060 - 1.609

0.200 -0.310 0.060 -0.726 0.090 -0.590 O. 110 -0.597

0.230 -0.312 0.090 -0.561 0.110 -0.602 0.140 1.867"*

0.400 -0.222 0.130 -0.559 0.130 -0.620 0.190 -6.371 **

0.490 -0.200 0.150 -0.520 0.150 -0.502 0.250 -0.489

0.590 -0.230 0.200 -0.443 0.210 -0.614 0.400 -0.391

0.630 -0.231 0.250 -0.411 0.250 -0.490 0,490 -0.359

0,700 -0.246 0.260 -0.384 0.340 -0.441 0,580 -0.323

0.750 -0.223 0.280 -0.406 0.370 -0.421 0.650 -0.393

0.810 -0.227 0.290 -0.389 0.400 -0.386 0.700 -0.357

0.840 -0.225 0.310 -0.356 0.410 -0.380 0.750 -0.340

0.900 -0.133 0.320 -0.365 0.430 -0.386 0,800 -0,282

0.960 -0.043 0.340 -0.373 0,440 -0.374 0.830 -0.286

0.350 -0.162"* 0,460 -0.356 0.900 -0.150

0.370 -0,344 0.490 -0.347 0.960 0.004

0.380 -0.325 0.500 -0.336

0.400 -0.277 0.520 -0.369

0.410 -0.329 0.540 -0.357

0.430 -0.294 0.550 -0.331

0.440 -0.285 0,580 -0.293

0.460 -0.348 0.600 -0.381

0.470 -0.293 0.610 -0.273

0.490 -0.302 0.650 -3.700"*

0.500 -0.301 0.700 -0.350

0.520 -0.304 0.750 -0.311

0.530 -0.279 0.820 -0.304

0.550 -0.281 0.890 -0.132

0.560 -0.317 0,900 -0 101

0.580 -0.272 0,960 -0.026

0.590 -0.311

0.600 -0.310

0.640 -3.542 * *

0.700 -0.308

0.750 -0.280

0.820 -3.712"*

0.870 -0.214

0.930 -0.089

0.960 -0.021

Lower Surface

0,020 0.04 1 0.020 0.235 0.020 0.304 0,020 0.605 **

0.110 -0.070 0.060 0.192 0.060 0.235 0.060 5.418"*

0.230 0,033 0.090 0.101 0.090 0.129 0.110 0.060

0.400 -0.049 0.120 0.030 0.120 -0.035 0.250 -0.088

0.490 -0.060 0.200 0.060 0.200 0.046 0.400 -0.087

0,630 3.279"* 0.260 -0,052 0.250 -0.056 0.490 -0.134

0.750 0.013 0.400 -3.729** 0.400 -0.085 0.580 -0.175

0.850 0,064 0.490 -0.085 0.490 -0.015 0.650 -0.064

0.900 0.135 0.580 -0.054 0,580 -0.138 0.750 0.159

0.960 0. I 17 0.640 0.252 0,650 0.009 0,830 0.267

0.750 0.141 0.750 0.197 0.900 0.333

0.870 0.210 0.890 ******** 0.960 0.247

0.930 0.195 0,930 0.240

0.960 0.107 0.960 -3.728**

CN = 0.231 0.415 0.405 0.463

146
Table D-2. Continued.

Flight 195, Wing sweep = 26 °. Time = 8-30-20-000, MINF = 0.700, Camber = 0/2, ALPT = 7.00, BETA = 0.15, Q1NF = 300.5,

RNPU = 2.7E+06, CNWP = 0.2668

_1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -O799 0.000 0.671 0.000 -6.605"* 0.010 -1.736

0.060 -0.423 0.020 - 1.452 0.020 - 1.566 0.020 - 1.760

0.110 -0.314 0.040 -0.713 0.060 -1.561"* 0.060 -1.618

0.200 -0.289 0.060 -0,726 0.090 -0.602 O. 110 -0.629

0.230 -0.319 0.090 -0.563 0.110 -0.614 0.140 1.906"*

0.400 -0. 228 O. 130 -0.554 O. 130 -0.633 O. 190 -6.473"*

0.490 -0.205 0.150 -0.515 O. 150 -0.504 0.250 -0.499

0.590 -0.235 0.200 -0.441 0.210 -0.608 0.400 -0.392

0.630 -0.233 0.250 -0.420 0.250 -0.489 0.490 -0.357

0.700 -0.248 0.260 -0.386 0.340 -0.428 0.580 -0.305

0.750 -0.210 0.280 -0.401 0.370 -0.422 0.650 -0.393

0.810 -0.229 0.290 -0.397 0.400 -0.394 0.700 -0.344

0.840 -0.208 0.310 -0.357 0.410 -0.381 0.750 -0.340

0.900 -0.134 0.320 -0.365 0.430 -0.409 0.800 -0.281

0.960 -0.038 0.340 -0.374 0.440 -0.368 0.830 -0.293

0.350 -0.167'* 0,460 -0.363 0.900 -0.145

0.370 -0.348 0.490 -0.354 0.960 0.007

0.380 -0.333 0.500 -0,338

0.400 -0,294 0.520 -0,359

0.410 -0.336 0.540 -0.351

0.430 -0.303 0.550 -0.326

0.440 -0.288 0.580 -0.300

0.460 -0.331 0.600 -0.377

0.470 -0,319 0.610 -0.272

0.490 -0.305 0.650 -3.754"*

0.500 -0.303 0.700 -0.340

0.520 -0.280 0.750 -0.31l

0.530 -0.278 0.820 -0.303

0.550 -0.282 0.890 -0.132

0.560 -0.311 0.900 -0.089

0.580 -0.265 0.960 -0.028

0.590 -0.318

0,600 -0.297

0.640 -3.593**

0.700 -0.308

0.750 -0.276

0.820 -3.766**

0.870 -0.215

0.930 -0.096

0.960 -0.023

Lower Surface

0.020 0.060 0.020 0.220 0.020 0.309 0.020 0.602**

0.110 -0.073 0.060 0.190 0.060 0.251 0.060 5.529" *

0.230 0.025 0.090 0.116 0.090 0.130 0. 110 0.064

0.400 -0.037 0.120 0.029 0.120 -0.023 0.250 -0.091

0.490 -0,062 0.200 0.057 0.200 0.045 0.400 -0.076

0.630 3.352** 0.260 -0.058 0.250 -0.055 0.490 -0.130

0.750 0.023 0.400 -3.784** 0,400 -0.088 0.580 -0.155

0.850 0.060 0.490 -0.074 0.490 -0.025 0.650 -0.066

0.900 O. 131 0.580 -0.056 0.580 -0.142 0.750 0.160

0.960 O. 114 0.640 0.252 0.650 0.001 0.830 0.285

0.750 0.123 0.750 0.218 0.900 0,331

0.870 0.213 0.890 ******** 0.960 0,259

0.930 O. 190 0.930 0.236

0.960 O. 108 0.960 -3.782 * *

CN = 0.231 0.416 0.408 0.470

147
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-30-35-500, MINF = 0.687, Camber = 0/2, ALPT = 8.10, BETA = 0.18, QINF = 285.2,

RNPU = 26E+06, CNWP = 0.2909

11 = 0,93 0.76 0.59 0.40

Upper Surface

.r../c CP x/c CP x/c CP x/c CP

0.020 - 1.545 0.000 0,492 0.000 -6.923 ** 0.010 - 1.977

0.060 -0.496 0.020 - 1.825 0,020 - 1.896 0.020 -2.002

0.110 -0.394 0.040 - 1,629 0.060 - 1.868"* 0.060 - 1.897

0,200 -0,353 0.060 -0.935 0.090 -1,067 0.110 -0.820

0.230 -0.387 0,090 -0.549 0.110 -0.782 0.140 2,017"*

0.400 -0.248 0.130 -0.586 0.130 -0.570 0.190 -6,784 **

0.490 -0.215 0.150 -0.560 0.150 -0.497 0,250 -0.503

0.590 -0,240 0,200 -0.480 0.210 -0,623 0.400 -0.391

0.630 -0.242 0,250 -0.448 0.250 -0.515 0.490 -0.368

0.700 -0.257 0,260 -0.420 0,340 -0.474 0,580 -0.329

0,750 -0.229 0,280 -0,429 0.370 -0.454 0.650 -0.381

0.810 -0.237 0.290 -0,420 0.400 -0,400 0,700 -0.343

0,840 -0.235 0.310 -0.385 0,410 -0.393 0,750 -0.320

0900 -0.149 0.320 -0.394 0.430 -0.423 0.800 -0.251

0,960 -0.055 0,340 -0.401 0.440 -0,395 0.830 -0.252

0.350 -0.157** 0.460 -0.375 0.900 -0,126

0.370 -0,370 0,490 -0.389 0.960 -0.019

0.380 -0.347 0.500 -0.369

0,400 -0.313 0.520 -0.371

0.410 -0.353 0,540 -0.362

0,430 -0,324 0.550 -0.335

0.440 -0.302 0.580 -0.308

0,460 -0.354 0,600 -0.389

0.470 -0.342 0.610 -0.257

0.490 -0.317 0.650 -3.918 * *

0.500 -0.311 0,700 -0.339

0,520 -0.303 0.750 -0.301

0,530 -0.289 0,820 -0.280

0.550 -0.304 0.890 -0.114

0.560 -0.314 0.900 -0,090

0,580 -0,278 0,960 -0.025

0,590 -0,322

0,600 -0.315

0,640 -3,748**

0.700 -0.305

0.750 -0,279

0,820 -3,931"*

0.870 -0.200

0,930 -0,082

0.960 -0.020

Lower Surface

0.020 0.163 0.020 0.365 0.020 0.448 0.020 0.703"*

0.110 0.002 0.060 0,294 0.060 0.342 0.060 5.865**

0.230 0,062 0.090 0.196 0.090 0.223 0,110 0.167

0,400 -0.015 0.120 0.102 0.120 0.042 0.250 -0,025

0.490 -0,034 0,200 0.117 0,200 0.109 0,400 -0,033

0,630 3.571 ** 0.260 0,000 0.250 0.012 0.490 -0.082

0.750 0.009 0.400 -3.949"* 0.400 -0,047 0.580 -0.138

0.850 0.059 0,490 -0.053 0,490 -0.010 0.650 -0,030

0.900 0.123 0.580 -0.024 0,580 -0.104 0.750 0.177

0,960 0.107 0.640 0.281 0.650 0.016 0,830 0.279

0,750 0.125 0.750 0.199 0,900 0.338

0,870 0,203 0.890 ******** 0.960 0.235

0.930 0.196 0.930 0.241

0.960 0.106 0.960 -3,948 **

CN = 0,281 0.488 0.488 0.533

148
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-30-47-000, MINF = 0,693, Camber = 0/2, ALPT = 9.07, BETA = 0.10. QINF = 292.1,

RNPU = 2.7E+06, CNWP = 0,3584

"q = 0,93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP .r../c CP

0.020 - 1,765 0,000 0.360 0.000 -6.772** 0.010 -2.102

0.060 -0.606 0.020 - 1.930 0.020 -2.042 0.020 -2.126

0.110 -0.418 0,040 -1.818 0.060 -1.905** 0.060 -2.067

0.200 -0.409 0,060 -1.781 0.090 -1.891 O. 110 - 1.306

0,230 -0,405 0.090 -1.124 0.110 -1,631 0, t40 1,958"*

0,400 -0,279 0.130 -0.892 0.130 - 1,064 0.190 -6.636" *

0,490 -0.250 0.150 -0.521 0.150 -0,663 0.250 -0.490

0,590 -0.260 0.200 -0,428 0.2 | 0 -0.529 0.400 -0416

0,630 -0,269 0,250 -0,463 0.250 -0,497 0.490 -0,387

0,700 -0.280 0,260 -0.423 0,340 -0,477 0.580 -0.352

0,750 -0.253 0.280 -0.445 0,370 -0,482 0.650 -0,379

0.810 -0.261 0.290 -0,437 0,400 -0,374 0.700 -0.333

0,840 -0.266 0.310 -0.397 0.410 -0,406 0,750 -0.310

0,900 -0.174 0.320 -0,415 0,430 -0,443 0.800 -0,265

0.960 -0.077 0,340 -0.418 0.440 -0,405 0.830 -0.249

0.350 -0. |67"* 0.460 -0.387 0,900 -0.149

0,370 -0.390 0,490 -0.370 0,960 -0,060

0.380 -0.370 0,500 -0.378

0.400 -0,326 0,520 -0,378

0.410 -0,373 0,540 -0.373

0.430 -0,339 0,550 -0,345

0,440 -0,322 0,580 -0.317

0,460 -0.381 0,600 -0,378

0.470 -0,366 0,610 -0.278

0.490 -0.336 0,650 -3,839"*

0.500 -0.335 0.700 -0,333

0.520 -0.318 0,750 -0.300

0.530 -0.302 0,820 -0,268

0.550 -0.323 0.890 -0.109

0.560 -0.330 0 900 -0.092

0.580 -0.291 0.960 -0,030

0.590 -0,348

0.600 -0,326

0.640 -3,673**

0.700 -0.311

0,750 -0.278

0.820 -3.851 **

0.870 -0.197

0,930 -0.089

0,960 -0.029

Lower Surface

0,020 0,262 0.020 0470 0,020 0,504 0.020 0,747**

0.110 0,038 0.060 0.362 0.060 0.390 0,060 5.713 **

0.230 0,085 0,090 0.248 0,090 0,279 0.110 0.196

0.400 -0.005 0.120 0.155 0. 120 0,096 0.250 0.011

0,490 -0,032 0.200 0.149 0.200 0.147 0.400 -0,008

0,630 3.473"* 0,260 0.031 0.250 0.044 0.490 -0,063

0.750 0.007 0,400 -3.869' * 0.400 -0.029 0,580 -0. ] 12

0.850 0,048 0,490 -0.039 0,490 -0,004 0.650 -0.028

0.900 0.113 0,580 -0.018 0,580 -0,092 0.750 0.184

0.960 0.093 0.640 0.279 0,650 0.021 0.830 0.279

0.750 0.123 0,750 0,204 0.900 0,338

0.870 0,209 0.890 ******** 0.960 0.225

0,930 0.193 0,930 0,244

0.960 0,109 0,960 -3.868"*

CN = 0.322 0,567 0.583 0.607

149
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-30-52-000, MINF = 0,704, Camber = 0/2, ALPT = 10,14, BETA = 0.26, QINF = 302.0,

RNPU = 2,7E+06, CNWP = 0.3427

'q = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -1.892 0,000 0,257 0.000 -6.561 ** 0.010 -2.155

0.060 - 1.764 0_020 - 1.880 0,020 -2.103 0.020 -2.174

0.110 -0.342 0.040 - 1.810 0.060 - 1.874"* 0.060 -2.128

0.200 -0.418 0.060 - 1.903 0.090 - 1.577 0,110 - 1.911

0.230 -0.435 0.090 -1.861 0.110 -1.381 0.140 1.887"*

0.400 -0,290 0.130 - 1.214 0,130 - 1.263 0.190 -6.429"*

0.490 -0.268 0.150 - 1,037 0.150 - 1.086 0.250 -0.525

0.590 -0.271 0.200 -0.827 0,210 -1.112 0.400 -0.454

0.630 -0.288 0.250 -0.391 0.250 -0.869 0.490 -0.409

0.700 -0,286 0.260 -0.357 0.340 -0.596 0.580 -0.337

0.750 -0.253 0.280 -0.394 0.370 -0.501 0.650 -0.348

0.810 -0.265 0.299 -0.396 0.400 -0.431 0.700 -0.330

0.840 -0.270 0.310 -0.380 0.410 -0.421 0.750 -0.283

0.900 -0.177 0.320 -0,379 0.430 -0.411 0.800 -0.253

0.960 -0.089 0.340 -0.415 0.440 -0.374 0.830 -0.218

0.350 -0.144"* 0.460 -0.346 0.900 -0.150

0,370 -0.377 0.490 -0.347 0.960 -0.081

0.380 -0.358 0,500 -0.319

0,400 -0.320 0.520 -0.331

0.410 -0.373 0.540 -0.337

0.430 -0,348 0.550 -0.324

0.440 -0.293 0.580 -0.268

0.460 -0.351 0.600 -0.350

0.470 -0,342 0.610 -0.216

0.490 -0.319 0.650 -3.723" *

0.500 -0,323 0.700 -0.258

0,520 -0.305 0.750 -0.243

0.530 -0.285 0.820 -0.208

0.550 -0.303 0.890 -0,080

0.560 -0.314 0.900 -0,086

0.580 -0.284 0.960 -0.026

0,590 -0.314

0.600 -0.303

0.640 -3.563**

0.700 -0.276

0,750 -0.244

0.820 -3.736**

0,870 -0.166

0.930 -0.065

0.960 -0.011

Lower Surface

0.020 0.321 0.020 0.545 0.020 0.583 0.020 0.789**

O. 110 0.074 0.060 0.405 0.060 0.461 0.060 5.515" *

0.230 0.112 0,090 0.316 0.090 0.335 0.110 0.264

0.400 0.016 0.120 0.219 0.120 0.148 0.250 0.074

0.490 -0,020 0.200 0.191 0,200 0.200 0.400 0.039

0.630 3,348** 0,260 0.084 0.250 0.083 0,490 -0.035

0.750 0.006 0,400 -3.753** 0.400 0.010 0.580 -0.080

0.850 0.060 0.490 -0,023 0,490 0.003 0.650 -0.016

0.900 0.119 0.580 -0.011 0.580 -0.078 0.750 0.182

0.960 0.100 0.640 0.276 0.650 0.028 0.830 0.282

0,750 0.145 0,750 0.222 0.900 0,345

0.870 0.211 0.890 ******** 0,960 0.211

0.930 0.198 0.930 0.239

0.960 0.102 0.960 -3.752 * *

CN = 0.417 0.646 0.643 0.706

150
Table D-2. Continued.

Flight 195, Wing sweep = 26", Time = 8-30-58-500, MINF = 0.702, Camber = 0/2, ALPT = 10.90, BETA = 0.23, QINF = 301.4,

RNPU = 2.7E+06, CNWP = 0.3936

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -2.017 0.000 O. 139 0.000 -6.584"* 0.010 -2.246

0.060 - 1.806 0.020 -2.034 0.020 -2.280 0.020 -2.263

O. 110 -0.624 0.040 - 1.825 0,060 -2,006** 0.060 -2.248

0.200 -0.518 0.060 - 1.981 0.090 -2.076 O. I 10 - 1.926

0.230 -0.525 0.090 - 1.567 O. 110 - 1.843 O. 140 1.874"*

0.400 -0.302 O. 130 - 1.349 O. 130 - 1.48 l O. 190 -6.452"*

0.490 -0.290 0.150 - 1.148 O. 150 - 1.282 0.250 -0.537

0.590 -0.272 0.200 -0.972 0.210 - 1.266 0.400 -0.451

0.630 -0.300 0.250 -0.532 0.250 -0.853 0,490 -0.402

0.700 -0.280 0.260 -0.471 0,340 -0.517 0.580 -0,313

0,750 -0.232 0,280 -0.486 0.370 -0,452 0,650 -0.352

0.810 -0.247 0.290 -0.470 0.400 -0392 0.700 -0.327

0.840 -0.259 0.310 -0.447 0.410 -0.360 0.750 -0.331

0.900 -0.162 0.320 -0.477 0.430 -0.378 0.800 -0,321

0960 -0.079 0,340 -0.454 0.440 -0.365 0.830 -0.216

0.350 -0,176"* 0.460 -0.341 0.900 -0.198

0.370 -0.410 0.490 -0.330 0.960 -0.166

0.380 -0,391 0.500 -0,326

0,400 -0.364 0,520 -0.325

0.410 -0.387 0.540 -0.320

0.430 -0.357 0.550 -0.284

0.440 -0.347 0.580 -0.283

0.460 -0,386 0.600 -0.324

0.470 -0.367 0.610 -0.207

0.490 -0.335 0.650 -3.741 * *

0.500 -0.309 0.700 -0.259

0.520 -0.317 0.750 -0.230

0.530 -0.300 0.820 -0.188

0.550 -0.306 0.890 -0.075

0.560 -0,313 0.900 -0.058

0.580 -0.275 0,960 -0.030

0.590 -0.301

0.600 -0.290

0.640 -3.581"*

0.700 -0.266

0.750 -0,227

0.820 -3.754**

0,870 -0.131

0.930 -0.065

0.960 -0.029

Lower Surface

0.020 0,375 0.020 0,610 0.020 0.635 0,020 0,819"*

0.110 0,1 04 0.060 0.449 0.060 0.490 0,060 5.514 **

0.230 0.116 0,090 0.350 0,090 0.371 0.110 0.308

0.400 0,012 0.120 0.252 0.120 0,186 0.250 0.096

0.490 -0.0 l0 0,200 0.219 0.200 0.216 0.400 0.042

0.630 3.343"* 0.260 0.095 0.250 0.115 0.490 -0.017

0.750 0.016 0.400 -3,771 * * 0.400 0.019 0.580 -0.081

0.850 0.034 0.490 -0.012 0.490 0.006 0.650 -0.005

0,900 0.090 0,580 0.010 0.580 -0.072 0.750 0.185

0.960 0.072 0.640 0,277 0,650 0,038 0.830 0,277

0.750 0.126 0.750 0.204 0.900 0.336

0.870 0.191 0.890 ******** 0,960 0,197

0.930 0.172 0.930 0.213

0.960 0.072 0.960 -3,770**

CN = 0.456 0.672 0.695 0.732

151
Table D-2. Continued.

Flight 200, Wing sweep = 26 °, Time = 8-30-17-000, MINF = 0.696, Camber = 0/2, ALPT = 6,16, BETA = -0.27, QINF = 296.3,

RNPU = 2.7E+06, CNWP = 0.2922

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x,/c CP x/c CP

0.020 -0.569 0.000 0.783 0,000 0.757** 0.010 -1.654

0.060 -0.322 0.020 - 1.119 0.020 - 1.342 0.020 - 1.610"*

0.110 -0.271 0.040 -0.620 0_060 0.415"* 0.060 -0,641"*

0.200 -0.215 0.060 -0.644 0.090 -0.538 0.110 -0.588

0.230 -0.254 0.090 -0.455 0.110 -0.617 0,140 -0,603

0.400 -0.194 0,130 -0.426 0.130 -0.510 0.190 -2.948 * *

0.490 -0.169 0.150 -0.464 0.150 -0,549 0.250 -0.437

0.590 -0.229 0.200 -0.366 0.210 -0.519 0.400 -0.378

0.630 -0.213 0.250 -0.394 0.250 -0.380 0.490 -0,335

0.700 -0.178 0.260 -0.313 0.340 -0.361 0,580 -0.308

0.750 -0.225 0.280 -0.349 0.370 -0.387 0.650 -0,348

0.810 -0.188 0.290 -0.349 0.400 -0.371 0.700 -0.321

0.840 -0.173 0.310 -0.330 0.410 -0,321 0.750 -0.336

0.900 -0.110 0.320 -0.321 0.430 -0.339 0.800 -0.319

0,960 -0.022 0.340 -0.295 0.440 -0.292 0.830 -0.282

0.350 -0,204** 0.460 -0.339 0.900 -0.152

0,370 -0.280 0,490 -0.272 0.960 0.006**

0.380 -0.333 0,500 -0.310

0.400 -0.238 0.520 -0.269

0.410 -0.316 0.540 -0.292

0.430 -0.270 0.550 -0.277

0.440 -0.219 0.580 -0.285

0.460 -0.302 0.600 -0.300

0.470 -0.285 0.610 -0.300

0.490 -0.273 0.650 0.027**

0.500 -0.264 0.700 -0,336

0.520 -0.275 0.750 -0.380

0.530 -0,259 0.820 -0.108

0.550 -0,288 0.890 -0.150

0.560 -0.277 0.900 -0.094

0.580 -0.249 0.960 0.029

0.590 -0,315

0.600 -0.311

0.640 -0.279

0.700 -0.288

0.750 -0.007 * *

0,820 -0.215

0.870 -0.198

0.930 -0.087

0.960 -0.024

Lower Surface

0.020 -0.082 0.020 0.101 0,020 0.228 0.020 0.532

0.110 -0.094 0.060 0.093 0.060 0.203 0.060 0.072

0.230 -0.011 0.090 0.029 0.090 0.088 0.110 0.018

0.400 -0.028 0.120 -0,025"* 0.120 -0.243 0.250 -0.107

0.490 -0.035 0.200 -0.006 0.200 -0.054 0.400 -0.107

0.630 1.232"* 0.260 -0.126 0.250 -0.055 0.490 -0.168

0,750 0.024 0.400 -0.101 0.400 -0.097 0.580 -0.176

0,850 0.083 0.490 -0.116 0.490 -0.012 0.650 -0,073

0.900 0.183 0.580 -0.111 0.580 -0.123 0.750 0.136

0.960 0.140 0.640 0.046 0,650 0.017 0.830 0.275

0.750 0.179 0,750 -0.012"* 0.900 0.349

0.870 0.207 0.890 0.287 0.960 0,273

0.930 0.204 0.930 0.228

0.960 0.167 0.960 0.741

CN = 0.196 0.333 0.355 0,352

152
Table D-2. Continued.

Flight 200, Wing sweep = 26 °, Time = 8-30-25-000, MINF = 0.696, Camber = 0/2, ALPT = 7.02, BETA = -0.33, QINF = 295.5,

RNPU = 2.7E+06, CNWP = 0.3127

r 1 = 0.93 0.76 0.59 0.40

Upper Surface

r/c CP x/c CP _c CP _c CP

0.020 -0.930 0.000 0.648 0.000 0.713** 0.010 - 1.718

0.060 -0.423 0.020 - 1.656 0,020 -1.608 0.020 - 1.758**

0.110 -0.326 0.040 -0.738 0.060 0.279** 0.060 - 1.597"*

0.200 -0.262 0.060 -0.783 0,090 -0,557 0. 110 -0.630

0.230 -0.288 0,090 -0.554 0.110 -0.669 0,140 -0.678

0.400 -0.198 0,130 -0.516 0.130 -0.567 0.190 -2.952"*

0.490 -0.184 0.150 -0.530 0.150 -0.589 0,250 -0,462

0,590 -0.225 0.200 -0.435 0.210 -0.558 0.400 -0,389

0.630 -0.221 0,250 -0.429 0.250 -0.413 0.490 -0.341

0.700 -0.190 0,260 -0.359 0.340 -0.396 0.580 -0.315

0.750 -0.233 0,280 -0,390 0,370 -0.408 0.650 -0.324

0.810 -0.214 0.290 -0,377 0.400 -0.361 0.700 -0.318

0.840 -0.199 0.310 -0.366 0.410 -0.357 0.750 -0.333

0.900 -0.136 0.320 -0.349 0.430 -0.359 0.800 -0.316

0.960 -0.033 0.340 -0.326 0.440 -0.335 0.830 -0.260

0,350 -0.190"* 0.460 -0.353 0.900 -0.135

0.370 -0.318 0.490 -0.284 0.960 0.003**

0.380 -0.358 0,500 -0,331

0.400 -0.271 0.520 -0.283

0.410 -0.338 0.540 -0.310

0.430 -0.290 0.550 -0.300

0.440 -0,249 0.580 -0.299

0.460 -0.323 0.600 -0,324

0.470 -0.308 0.610 -0.31 I

0.490 -0.300 0.650 0.016"*

0.500 -0.291 0.700 -0.344

0.520 -0.302 0.750 -0.388

0.530 °0.274 0.820 -0.101

0.550 -0.312 0.890 -0.138

0.560 -0.292 0.900 -0.085

0,580 -0,273 0.960 0.037

0.590 -0.316

0.600 -0.323

0.640 -0.304

0.700 -0.292

0,750 0.004**

0,820 -0.219

0.870 -0,209

0.930 -0.090

0.960 -0.024

Lower Surface

0.020 0,019 0.020 0,258 0.020 0.368 0.020 0.639

0.110 -0.05 t 0.060 0. [ 89 0.060 0.274 0.060 0.140

0.230 0.005 0.090 0,095 0.090 O. 159 O. 110 0.084

0.400 -0.013 0.120 0,054** 0.120 -0.165 0.250 -0.065

0.490 -0.016 0.200 0,032 0,200 -0.009 0,400 -0.077

0,630 1.239" * 0.260 -0,078 0,250 -0.021 0,490 -0.126

0.750 0.032 0.400 -0.070 0.400 -0.063 0.580 -0.157

0.850 0,084 0.490 -0.085 0.490 -0.001 0.650 -0.068

0.900 0.182 0.580 -0.091 0.580 -0.105 0,750 0.150

0,960 0.140 0.640 0.044 0.650 0.006 0.830 0.289

0.750 0.1% 0.750 -0.023** 0,900 0.339

0.870 0.215 0.890 0.2% 0.960 0.263

0,930 0.216 0.930 0.240

0.960 0.168 0.960 0.747

CN = 0.236 0.405 0.391 0.387

153
Table D-2. Continued.

Flight 200, Wing sweep = 26 °, Time = 8-30-31-000, MINF = 0,696, Camber = 0/2, ALPT = 7.99, BETA = -0,18, QINF = 296.0,

RNPU = 2.7E+06. CNWP = 0.3561

tl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x,"c CP x/c CP x,/c CP

0.020 - 1.569 0.000 0,496 0.000 0,623"* 0,010 - 1,888

0,060 -0.436 0.020 - 1.945 0.020 - 1.795 0,020 - 1.907"*

0.110 -0,423 0.040 - 1.608 0.060 -0.231 ** 0.060 - 1.768"*

0,200 -0.304 0,060 -1.193 0.090 -1.014 0.110 -0.902

0,230 -0.292 0.090 -0.531 0.110 -0,901 0.140 -0.627

0.400 -0.240 0.130 -0.526 0,130 -0.510 0.190 -2.951"*

0.490 -0.214 0.150 -0.558 0.150 -0,567 0.250 -0.494

0.590 -0.252 0.200 -0.479 0.210 -0.576 0.400 -0.400

0.630 -0.244 0.250 -0.484 0.250 -0,446 0.490 -0.355

0.700 -0.206 0.260 -0,404 0.340 -0.429 0,580 -0.329

0,750 -0.253 0.280 -0.429 0.370 -0.419 0.650 -0.338

0.810 -0,225 0,290 -0.420 0.400 -0.394 0.700 -0.322

0.840 -0.225 0.310 -0.398 0,410 -0,384 0.750 -0.322

0.900 -0.158 0.320 -0.384 0,430 -0.378 0.800 -0.291

0.960 -0.065 0.340 -0.357 0.440 -0.349 0.830 -0.236

0.350 -0.215"* 0,460 -0.373 0.900 -0.126

0.370 -0.351 0.490 -0.302 0.960 -0.017**

0.380 -0.384 0.500 -0.334

0.400 -0.297 0.520 -0.303

0,410 -0.365 0.540 -0.327

0.430 -0.332 0.550 -0.317

0.440 -0.287 0.580 -0,303

0.460 -0.351 0.600 -0.339

0.470 -0.325 0,610 -0.314

0.490 -0.324 0.650 0.012"*

0.500 -0.317 0,700 -0.344

0.520 -0.306 0.750 -0.388

0.530 -0.292 0.820 -0.102

0.550 -0.316 0,890 -0.125

0.560 -0.308 0.900 -0.078

0.580 -0.291 0.960 0.054

0.590 -0.333

0.600 -0.331

0.640 -0,31 I

0.700 -0.303

0.750 0.007**

0.820 -0.219

0.870 -0.202

0.930 -0.098

0.960 -0.028

Lower Surface

0,020 0.169 0.020 0.381 0.020 0.450 0.020 0.717

0.110 -0.005 0.060 0.276 0,060 0.362 0.060 0.195

0,230 0.031 0.090 0.167 0.090 0.230 0.110 0.151

0,400 0.002 O. 120 O.108 ** O,120 -0.1 O0 0.250 -0.015

0.490 -0.005 0.200 0.083 0.200 0.04 1 0.400 -0,040

0.630 1.233** 0.260 -0.031 0.250 0.027 0.490 -0.092

0.750 0,016 0,400 -0.040 0.400 -0,027 0.580 -0.130

0.850 0.076 0.490 -0.062 0.490 -0.001 0.650 -0.057

0.900 0,169 0,580 -0.076 0.580 -0.079 0.750 0.165

0.960 0.128 0.640 0,051 0,650 0.009 0.830 0.292

0.750 0.200 0.750 -0.027** 0.900 0.340

0.870 0.21 I 0.890 0.295 0.960 0.252

0.930 0,211 0.930 0.236

0.960 O. 164 0.960 0.734

CN = 0,273 0.479 0.463 0.451

154
Table D-2. Continued.

Flight 200, Wing sweep = 26 °, Time = 8-30-32-000, MINF = 0.696, Camber = 0/2, ALPT = 8.20, BETA = -0.33, QINF = 296.0,

RNPU = 2.7E+06, CNWP = 0.3388

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1,642 0.000 0.471 0.000 0.630"* 0,010 - 1.910

0.060 -0.474 0.020 - 1.945 0.020 - 1.812 0.020 - 1.907"*

0.1 l 0 -0.388 0.040 - 1.655 0.060 -0.255 ** 0.060 - 1,821 * *

0.200 -0.317 0.060 - 1.664 0.090 - 1.088 0.110 -0.981

0,230 -0.329 0.090 -0,583 0,110 -1,028 0,140 -0.645

0.400 -0.255 0,130 -0.486 0,130 -0,570 0,190 -2,951 **

0.490 -0,214 0.150 -0.550 0.150 -0.558 0.250 -0.480

0.590 -0,252 0,200 -0.473 0.210 -0.567 0.400 -0,400

0.630 -0.248 0.250 -0.484 0.250 -0.446 0.490 -0.364

0.700 -0.213 0.260 -0.411 0.340 -0.429 0.580 -0.329

0.750 -0.253 0.280 -0.438 0,370 -0,443 0,650 -0,338

0.810 -0.232 0.290 -0.420 0.400 -0.402 0,700 -0.322

0,840 -0.225 0.310 -0.405 0,410 -0.376 0.750 -0,322

0.900 -0.161 0,320 -0.384 0.430 -0.378 0.800 -0.291

0.960 -0.062 0.340 -0.364 0.440 -0.349 0.830 -0.236

0.350 -0.199"* 0,460 -0,373 0,900 -0,121

0.370 -0,355 0.490 -0.310 0.960 -0.017"*

0.380 -0,394 0.500 -0,353

0.400 -0,308 0,520 -0.303

0.410 -0.368 0.540 -0.327

0.430 -0.332 0.550 -0.329

0.440 -0,277 0.580 -0.312

0.460 -0.351 0.600 -0.339

0.470 -0.331 0.610 -0.314

0.490 -0.328 0.650 0.0t2"*

0.500 -0.317 0.700 -0.337

0.520 -0,329 0.750 -0.384

0.530 -0.296 0.820 -0.096

0.550 -0.316 0.890 -0.121

0.560 -0,315 0.900 -0.078

0.580 -0.291 0.960 0.036

0.590 -0.333

0.600 -0.336

0.640 -0.31 I

0.700 -0.306

0.750 0.015"*

O.82O -0.215

0,870 -0.206

0.930 -0.091

0.960 -0.021

Lower Surface

0.020 0.148 0.020 0.402 0.020 0.466 0,020 0.730

0.1 I0 0.005 0.060 0.287 0.060 0,376 0,060 0.202

0.230 0.031 0.090 0,182 0.090 0.244 0.110 0.151

0.4130 -0.002 0.120 0.101 ** 0.120 -0.091 0.250 -0.009

0.490 -0.001 0.200 0.090 0.200 0.055 0.400 -0.033

0.630 1.233** 0.260 -0.023 0.250 0.034 0.490 -0.092

0.750 0.028 0.400 -0.036 0.400 -0.027 0.580 -0.130

0.850 0.076 0.490 -0,059 0.490 0.002 0.650 -0.042

0.900 0.169 0.580 -0.072 0,580 -0.079 0.750 0.165

0.960 0.123 0.640 0.059 0,650 0.009 0.830 0.292

0.750 0.191 0,750 -0.027** 0.900 0.340

0.870 0,202 0.890 0.295 0.960 0246

0,930 0.211 0.930 0.236

0.960 0.167 0,960 0.730

CN = 0.285 0.496 0.471 0.463

155
Table D-2. Continued

Flight 222, Wing sweep = 26 °, Time = 10-51-24-000, MINF = 0.692, Camber = 0/2, ALPT = 11.95, BETA = 0.54, QINF = 298.1,

RNPU = 2.7E+06, CNWP = 0.2582

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x./c CP

0.020 -2.194 0.000 -0.074 0,000 2.424 ** 0.010 -2.306

0.060 - 1.398 0.020 -2.289 0.020 -2.242 0,020 -2.344

0. 110 -0.984 0.040 - 1.898 0.060 -5.086** 0.060 -2.281

0.200 -0.500 0.060 -1.694 0.090 -1.321 0.110 - 1.596

0.230 -0.421 0.090 -1.232 0.110 -1.381 0.140 - 1,475

0.400 -0.347 0.130 - 1.064 0.130 - 1.242 0.190 -2.986"*

0.490 -0.305 0.150 -0.931 0.150 - 1.207 0,250 -0.670

0.590 -0.308 0.200 -0.805 0.210 - 1.082 0.400 -0.492

0,630 -0.315 0,250 -0.746 0,250 -0.811 0.490 -0.401

0.700 -0.283 0.260 -0.665 0.340 -0.740 0.580 -0.348

0.750 -0.281 0,280 -0.682 0.370 -0.679 0.650 -0,367

0.810 -0.277 0,290 -0.638 0.400 -0.617 0.700 -0,357

0.840 -0.272 0.310 -0.628 0,410 -3,988** 0.750 -0.367

0.900 -0.208 0.320 -0.583 0,430 -0.612 0.800 -0.390

0,960 -0.125 0,340 -0,592 0.440 -0.539 0.830 -0,276

0,350 -0,325** 0.460 -0.554 0,900 -0,270

0,370 -0.514 0.490 -0.425 0.960 -0.241

0.380 -0.572 0.500 -0.512

0.400 -0.471 0.520 -0.467

0.410 -0.522 0.540 -0.43 ]

0.430 -0.468 0.550 -0.374

0.440 -0.413 0.580 -0.364

0.460 -0.466 0.600 -0.408

0.470 -0.424 0.610 -0.336

0,490 -0.388 0650 1.046"*

0.500 -0.386 0.700 -0.315

0.520 -0.408 0,750 -0.362

0.530 -0.347 0.820 -0.244

0.550 -0.379 0.890 -0,175

0.560 -0.354 0.900 -0.154

0.580 -0,353 0.960 -0.109

0.590 -0.364

0.600 -0.364

0.640 -0.254

0.700 -0,293

0,750 -0.014"*

0,820 -0,167

0.870 -0.160

0.930 -0.182

0.960 -0.1 64

Lower Surface

0.020 0.420 0.020 0.656 0.020 0.717 0.020 0.837

0.110 0.136 0.060 0.467 0.060 0,522 0.060 0.770"*

0.230 0,092 0.090 0.352 0.090 0.111 ** 0.110 0.364

0.400 0.010 0.120 0.311 0,120 0.131 0.250 0.134

0.490 0.011 0.200 0.207 0.200 0.179 0.400 0.081

0.630 0.830** 0,260 0,093 0.250 0.163 0.490 -0.005

0.750 -0,030 0.400 0.033 0.400 0,037 0,580 -0,065

0.850 0,030 0.490 -0.027 0.490 -0.023 0.650 0.000

0.900 0.103 0.580 -0.047 0.580 -0.045 0.750 0.119

0.960 0,053 0.640 0,063 0,650 -0.045 0.830 0.303

0.750 0.155 0,750 0,007 0.900 0.285

0.870 0.162 0.890 0.210 0,960 0.151

0.930 0.141 0,930 0.156

0.960 0.052 0.960 -3.216"*

CN = 0.458 0,674 0.654 0.806

156
Table D-2. Continued.

Flight 222, Wing sweep = 26 °, Time = 10-51-25-000, MINF = 0.691, Camber = 0/2, ALPT = 12.25, BETA = -0.44, QINF = 298.2,

RNPU = 2.7E+06, CNWP = 0.2470

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.473 0.000 -0.162 0.000 2.417 * * 0.010 -2.214

0.060 - 1.305 0.020 -2.182 0.020 - 1.769 0.020 - 1.917

0.110 - 1.257 0.040 - 1.846 0.060 -5.092 ** 0.060 - 1.579

0.200 -0.672 0,060 - 1.561 0.090 - 1.533 0.110 - 1.529

0.230 -0.516 0.090 - 1.293 0.110 - 1.604 0.140 - 1.073

0.400 -0.362 0.130 - 1.220 0.130 - 1.484 0.190 -2.992**

0.490 -0.312 0,150 - 1.127 0.150 - 1.309 0.250 -0,860

0.590 -0,308 0.200 - 1.014 0.210 - 1.135 0.400 -0.674

0.630 -0.280 0.250 -0.828 0,250 -0.796 0,490 -0.535

0.700 -0.253 0.260 -0.726 0.340 -0.656 0.580 -0.440

0.750 -0.242 0.280 -0.762 0.370 -0.608 0.650 -0.466

0.810 -0.237 0.290 -0.692 0.400 -0.565 0.700 -0.457

0.840 -0.234 0.310 -0.652 0.410 -3.994"* 0750 -0.396

0.900 -0.188 0.320 -0.607 0.430 -0.506 0.800 -0.432

0.960 -0.132 0.340 -0.618 0.440 -0.453 0.830 -0.338

0.350 -0.344** 0.460 -0.457 0.900 -0.295

0.370 -0,509 0.490 -0.394 0.960 -0.256

0.380 -0,569 0.500 -0.429

0.400 -0.463 0.520 -0.406

0.410 -0,511 0,540 -0.396

0.430 -0.472 0,550 -0.342

0.440 -0.467 0.580 -0.321

0.460 -0.447 0.600 -0.352

0.470 -0.423 0.610 -0.315

0.490 -0.364 0.650 1.039"*

0.500 -0.394 0.700 -0.278

0.520 -0.369 0.750 -0.281

0.530 -0.336 0.820 -0.237

0.550 -0.371 0.890 -0.212

0.560 -0.322 0.900 -0.161

0.580 -0.318 0.960 -0.130

0.590 -0.334

0.600 -0.337

0.640 -0.228

0.700 -0.252

0.750 -0.021 **

0.820 -0.152

0.870 -0.145

0.930 -0.130

0.960 -0.108

Lower Surface

0.020 0.438 0.020 0.681 0.020 0.725 0.020 0.823

0.110 0.135 0.060 0.475 0.060 0.543 0.060 0.763"*

0,230 0.104 0.090 0.360 0.090 0.1 04"* 0,110 0.493

0.400 0.014 0.120 0.325 0.120 0.156 0.250 0. [ 40

0.490 0.022 0.200 0.211 0.200 0,200 0.400 0.082

0.630 0.823** 0.260 0.115 0.250 0.171 0.490 -0.005

0.750 -0.026 0.400 0.045 0.400 0.040 0,580 -0.062

0.850 0.022 0.490 -0.019 0.490 -0.015 0.650 -0.004

0.900 0,108 0.580 -0.040 0.580 -0.038 0.750 0.142

0.960 0.044 0.640 0.066 0.650 -0.037 0.830 0.273

0.750 0.170 0.750 0.030 0.900 0.290

0.870 0.151 0.890 0.195 0.960 0.159

0.930 0,130 0.930 0.142

0.960 0,067 0.960 -3.222"*

CN = 0.484 0.691 0.663 0.838

157
Table D-2. Continued.

Flight 222, Wing sweep -- 26 °, Time -- 10-51-27-000, MINF = 0.689, Camber = 0/2, ALPT = 12.96, BETA -- 0.37, QINF = 298,7,

RNPU = 2.7E+06, CNWP = 0.1691

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 - 1.374 0.000 -0.194 0.000 2,392"* 0.010 - 1,951

0.060 - 1.285 0020 - 1.790 0.020 - 1.046 0.020 - 1.739

0. I 10 - 1.085 0.040 - 1.405 0.060 -5.105"* 0,060 - 1.506

0.200 -0.637 0.060 - 1.209 0.090 -0.874 0.110 -1.361

0.230 -0.470 0.090 - 1.101 O. 110 -0.969 0.140 -1.206

0.400 -0.353 O.130 -0.994 O,130 -0.809 O. 190 -3.009**

0.490 -0.318 O. 150 -0.983 O.150 -0.843 0.250 -0.978

0.590 -0.311 0.200 -0.874 0.210 -0.789 0.400 -0.756

0.630 -0.279 0.250 -0.729 0.250 -0.693 0.490 -0.630

0.700 -0.244 0.260 -0.669 0.340 -0.723 0.580 -0.520

0.750 -0.249 0.280 -0.683 0.370 -0.662 0.650 -0.544

0.810 -0.239 0.290 -0.639 0.400 -0.615 0.700 -0.542

0.840 -0.248 0.3 I0 -0.627 0.410 -4.009"* 0.750 -0.453

0.900 -0.202 0.320 -0.607 0.430 -0.641 0.800 -0.479

0.960 -0.159 0.340 -0.609 0.440 -0.599 0.830 -0.375

0.350 -0.341 ** 0.460 -0.604 0.900 -0.341

0.370 -0.541 0.490 -0.545 0.960 -0.280

0.380 -0.597 0.500 -0.590

0.400 -0.465 0.520 -0.566

0.410 -0.535 0.540 -0.537

0.430 -0,498 0.550 -0.481

0.440 -0.431 0.580 -0.436

0.460 -0.486 0.600 -0.464

0.470 -0.440 0.610 -0.414

0.490 -0.403 0.650 1,016"*

0.500 -0.468 0.700 -0.443

0.520 -0.407 0.750 -0.438

0.530 -0.366 0.820 -0,347

0.550 -0.399 0.890 -0.296

0.560 -0.375 0.900 -0.238

0.580 -0.343 0,960 -0.241

0.590 -0.392

0.600 -0.397

0.640 -0.239

0.700 -0.276

0.750 -0.031 **

0.820 -0.178

0.870 -0,199

0.930 -0.207

0.960 -0.203

Lower Surface

0.020 0.467 0.020 0.720 0.020 0.748 0.020 0.849

O. I 10 O. 163 0.060 0.505 0.060 0.590 0.060 0.740"*

0.230 0.123 0.090 0.388 0.090 0.083"* 0.110 0.379

0.400 0.033 0.120 0.304 0.120 0.190 0.250 0.175

0.490 0.030 0.200 0.234 0.200 0.228 0.400 O. 111

0.630 0.800"* 0.260 O. 134 0.250 O. 193 0.490 0.011

0.750 -0.026 0.400 0.060 0.400 0.058 0.580 -0.054

0.850 0.022 0.490 -0.007 0.490 -0.029 0.650 0.001

0.900 0.094 0.580 -0.039 0.580 -0.037 0.750 O. 140

0.960 0.031 0.640 0.056 0.650 -0.058 0.830 0.295

0.750 O. 153 0.750 0.030 0.900 0.282

0.870 0.223 0.890 O. 181 0.960 O. 137

0.930 0.079 0.930 O. 120

0.960 0.009 0.960 -3.239**

CN = 0.475 0.666 0.639 0.886

158
Table D-2. Continued.

Flight I91, Wing sweep = 26 °, Time = 8-57-6-500, MINF = 0.703, Camber = 5/2, ALPT = 7.17, BETA = -0.14, QINF = 303.6,

RNPU = 2.7E+06, CNWP = 0.3272

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.132 0.000 0.874 0.000 -5.781 * * 0.010 - 1.248

0.060 -0.264 0.020 -0.637 0.020 -0.513 0.020 -0.709

0. 110 -0.432 0.040 -0,429 0.060 -0.587** 0.060 - 1,173

0.200 -0.393 0.060 -0.697 0.090 -0.833 0.1 I 0 - 1.002

0.230 -0.417 0.090 -0.730 0.110 - 1.027 0.140 - 1.348

0.400 -0.235 0.130 -0.896 0.130 - 1.137 0.190 -6.425"*

0.490 -0.208 0.150 -0,903 0.150 -0,788 0.250 -0.524

0.590 -0.249 0.200 -0.641 0.210 -0.732 0.400 -0.377

0.630 -0.229 0.250 -0.541 ** 0.250 -0.482 0.490 -0.381

0.700 -0.192 0.260 -0.398 0.340 -0.432 0.580 -0.357

0.750 -0.235 0.280 -0.455 0.370 -0.419 0.650 -0.362

0.810 -0.266 0.290 -0.447 0.400 -0.414 0.700 -0.339

0.840 -0.189 0.310 -0.406 0.410 -0.363 0.750 -0.353

0.900 -0.130 0.320 -0.374 0.430 -0.399 0.800 -0.336

0.960 -0.061 0.340 -0.386 0.440 -0.361 0.830 -0.295

0.350 -0.205** 0.460 -0,380 0.900 -0.139

0.370 -0.347 0.490 -0.316 0.960 -0,008

0.380 -0.347 0.500 -0.368

0.400 -0.268 0.520 -0.297

0.410 -0.37 l 0.540 -0.329

0.430 -0.333 0.550 -0.331

0.440 -0.277 0.580 -0.306

0.460 -0.373 0.600 -0.316

0.470 -0.325 0.610 -0.272

0.499 -0,315 0.650 -3725"*

0.500 -0.304 0.700 -0.367

0.520 -0.317 0.750 -0.423

0.530 -0.288 0.820 -0.313

0.550 -0.311 0.890 -0.131

0.560 -0.299 0.900 -0.107

0.580 -0.278 0.960 -0.007

0.599 -0.3 l 1

0.600 -0.351

0.640 -3.566"*

0.700 -0.314

0.750 -0.257

0.820 -3.737**

0.870 -0.215

0.930 -0.093

0.960 -0.025

Lower Surface

0.020 -0.222 0.020 -0.028 0.020 0.064 0.020 0.344

0.110 -0.068 0.060 0.109 0.060 0.233 0.060 1.921 **

0.230 0.049 0.090 0.045 0.090 0.105 0.110 0.050

0.400 -0,009 0.120 0.053 0.120 -0.242** 0.250 -0.027

0.490 -0.045 0.200 0.068 0200 -0.038 0.400 -0.055

0.630 1.945"* 0.260 -0.028 0.250 0.024 0.490 -0.153

0.750 0.029 0.400 -3.754** 0.400 -0.036 0.580 -0.156

0.850 0.088 0.490 -0.063 0.490 0.004 0.650 -0.056

0.900 O. 168 0.580 -0.022 0.580 -0.092 0.750 O. 164

0.960 0.136 0.640 0.285 0.650 0.04 | 0.830 0.305

0.750 0.166 0.750 0.251 0.900 0.358

0.870 0.219 0.890 ******** 0.960 0.265

0.930 0.218 0.930 0.250

0.960 0.141 0.960 -3.497"*

CN = 0.263 0.454 0485 0.521

159
Table D-2, Continued.

Flight 191, Wing sweep = 26 °, Time = 8-57-14-000, MINF = 0.708, Camber = 5/2, ALPT = 9.11, BETA = -0.06, QINF = 310.1,

RNPU = 2.8E+06, CNWP = 0.4156

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.677 0,000 0.772 0.000 -5.681 * * 0.010 - 1.480

0.060 -0.622 0.020 - 1.118 0,020 - 1.234 0.020 - 1.544

0.110 -0.646 0.040 -0.788 0.060 -0.792"* 0.060 - 1.543

0.200 -0.502 0.060 -1.107 0.090 -1.325 0.110 -1.641

0.230 -0.473 0.090 - 1.212 0.110 - 1.444 0.140 - 1,667

0.400 -0.288 0.130 - 1.296 0.130 - 1.491 0.190 -6.311 **

0.490 -0.253 0.150 - 1.367 0.150 - 1.489 0.250 -0.553

0.590 -0.270 0.200 - 1.268 0.210 - 1.456 0.400 -0,396

0.630 -0.264 0.250 -0.579** 0,250 -0.536 0.490 -0.385

0.700 -0.228 0.260 -0.442 0,340 -0.460 0.580 -0.342

0.750 -0.281 0.280 -0.499 0,370 -0.472 0.650 -0.339

0.810 -0.31 l 0.290 -0.506 0.400 -0.461 0.700 -0.335

0.840 -0.272 0.310 -0.451 0.410 -0.378 0.750 -0.317

0.900 -0.174 0.320 -0.422 0.430 -0.442 0.800 -0.295

0.960 -0.108 0.340 -0.446 0.440 -0.401 0.830 -0.227

0.350 -0.202** 0.460 -0.403 0.900 -0.102

0.370 -0.406 0.490 -0.331 0.960 -0.031

0.380 -0.398 0.500 -0.390

0.400 -0.308 0.520 -0.325

0.410 -0.409 0.540 -0.369

0.430 -0.364 0.550 -0.353

0.440 -0.316 0.580 -0.326

0.460 -0.404 0.600 -0.340

0.470 -0.355 0.610 -0.272

0.490 -0.346 0,650 -3.667 * *

0.500 -0.347 0.700 -0.362

0.520 -0,340 0.750 -0.414

0.530 -0.315 0.820 -0.287

0.550 -0.349 0.890 -0.110

0.560 -0.328 0.900 -0,087

0.580 -0.297 0.960 0.014

0.590 -0.330

0.600 -0.388

0.640 -3.512"*

0.700 -0.325

0.750 -0.279

0.820 -3.680**

0.870 -0.214

0.930 -0.095

0,960 -0.024

Lower Surface

0.020 0.028 0.020 0.306 0.020 0.358 0.020 0.582

O. 110 0.032 0.060 0.305 0.060 0.395 0.060 1.860"*

0.230 0.117 0.090 0.197 0.090 0.257 0.110 0.164

0.400 0.023 O. 120 O. 182 O. 120 -0.092 ** 0.250 0.070

0.490 -0.016 0.200 O. 137 0.200 0.016 0.400 0.017

0.630 1.884"* 0.260 0.051 0.250 O. 124 0.490 -0.085

0.750 0.028 0.400 -3.696** 0.400 0.021 0.580 -0.096

0.850 0.079 0.490 -0.015 0.490 0.018 0.650 -0.033

0.900 O. 154 0.580 0.000 0.580 -0.055 0.750 O.182

0.960 O. 121 0.640 0.301 0.650 0.055 0.830 0.306

0.750 O. 178 0.750 0.253 0.900 0.363

0.870 0.222 0.890 ******** 0.960 0.238

0.930 0.221 0.930 0.238

0.960 O. 142 0.960 -3.444**

CN = 0.372 0.631 0.650 0.660

160
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-33-5-500, MINF = 0.708, Camber = 5/2, ALPT = 6,15, BETA = 0.07, QINF = 304.1,

RNPU = 27E÷06, CNWP = 0.3052

"ll = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.076 0.000 0,795 0.000 -6,501 * * 0.010 -0.823

0.060 -0.202 0.020 -0.179 0.020 -0.31 I 0.020 -0.541

0.110 -0.346 0.040 -0.249 0.060 -1.163"* 0.060 -0.837

0.200 -0.364 0.060 -0,476 0.090 -0.659 0.110 -0,915

0,230 -0.340 0.090 -0.527 0.110 -0.805 0.140 1.877**

0.400 -0.212 0.130 -0,688 0,130 -0.973 0.190 -6.370"*

0,490 -0,211 0.150 -0.712 0.150 -0.640 0.250 -0.474

0.590 -0,216 0.200 -0.538 0.210 -0,649 0.400 -0.362

0.630 -0.207 0.250 -0.416 0.250 -0.474 0.490 -0.341

0.700 -0.232 0.260 -0.390 0,340 -0.424 0.580 -0.318

0.750 -0.194 0.280 -0.388 0,370 -0.397 0.650 -0,376

0.810 -0.210 0.290 -0,381 0.400 -0.377 0.700 -0.338

0.840 -0.207 0,310 -0.338 0.410 -0.363 0.750 -0.338

0.900 -0.117 0.320 -0,358 0.430 -0.377 0,800 -0.287

0.960 -0.011 0.340 -0.350 0.440 -0.369 0,830 -0.310

0.350 -0.137"* 0,460 -0.347 0.900 -0,182

0.370 -0.335 0,490 -0.337 0.960 0.001

0.380 -0.322 0.500 -0.327

0.400 -0.268 0.520 -0.326

0.410 -0.307 0.540 -0.334

0.430 -0.288 0,550 -0.297

0.440 -0,293 0.580 -0.247

0.460 -0,315 0.600 -0.362

0.470 -0.297 0.610 -0.264

0.490 -0.278 0.650 -3.683**

0.500 -0.291 0.700 -0.349

0.520 -0.279 0.750 -0.302

0.530 -0.270 0.820 -0.305

0.550 -0.295 0.890 -0.136

0.560 -0,298 0.900 -0.105

0.580 -0.243 0.960 -0.029

0.590 -0.293

0.600 -0.300

0,640 -3,524"*

0.700 -0.299

0,750 -0,257

0.820 -3.695**

0.870 -0,204

0,930 -0,075

0.960 -0.025

Lower Surface

0.020 -0.270 0.020 -0.238 0.020 -0,137 0.020 0.165**

0,110 -0.133 0.060 0.036 0.060 0.091 0.060 5.490"*

0,230 0.015 0.090 -0.027 0.090 0,003 0,110 0.001

0.400 -0.024 0,120 -0.003 0.120 -0. [ 18 0.250 -0,098

0.490 -0.063 0.200 0.047 0,200 0,003 0.400 -0.120

0.630 3.339"* 0.260 -0,045 0.250 -0.064 0.490 -0.160

0.750 0.028 0.400 -3.712** 0.400 -0.094 0.580 -0.175

0.850 0.087 0.490 -0,079 0.490 -0,005 0.650 -0.068

0.900 0.140 0.580 -0.061 0.580 -0,136 0.750 0.161

0.960 0.141 0.640 0.250 0.650 0,0 l 3 0.830 0.279

0.750 0.138 0.750 0.199 0.900 0.345

0.870 0,208 0.890 ******** 0.960 0.266

0.930 0.192 0.930 0.253

0.960 0.126 0.960 -3.711 **

CN = 0,212 0.365 0.397 0.408

161
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-33-27-500, MINF = 0,705, Camber = 5/2, ALPT = 7.22, BETA = -0.03, QINF = 300.8,

RNPU = 2.7E+06, CNWP = 0.3432

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.133 0.000 0.866 0.000 -6.563"* 0.010 - 1.328

0.060 -0.342 0.020 -0.474 0.020 -0.549 0.020 -0.594

0. I 10 -0.442 0.040 -0.445 0.060 - 1.294 ** 0.060 - 1.168

0.200 -0.425 0.060 -0.656 0,090 -0.856 0.110 -0.955

0.230 -0.386 0.090 -0.703 0.110 -0.966 0.140 1.881 **

0.400 -0.236 0.130 -0.881 0.130 - 1.155 0.190 -6.431 **

0.490 -0.216 0.150 -0.860 0.150 -0.787 0.250 -0.533

0.590 -0,232 0.200 -0.642 0.210 -0.704 0.400 -0.399

0.630 -0.237 0.250 -0.477 0.250 -0.529 0.490 -0.373

0.700 -0.252 0.260 -0.440 0.340 -0.465 0.580 -0.323

0,750 -0.229 0.280 -0.443 0.370 -0.454 0.650 -0.394

0.810 -0.241 0.290 -0,435 0.400 -0.423 0.700 -0.358

0.840 -0.231 0.310 -0.394 0.410 -0.389 0.750 -0.340

0.900 -0.139 0,320 -0.400 0,430 -0.417 0.800 -0.274

0.960 -0.038 0.340 -0.401 0.440 -0.396 0.830 -0.286

0.350 -0.1 44** 0,460 -0,378 0.900 -0.138

0.370 -0.370 0.490 -0.354 0.960 0,014

0.380 -0.348 0.500 -0.360

0.400 -0.308 0.520 -0.369

0.410 -0.352 0.540 -0.364

0.430 -0.320 0.550 -0.343

0.440 -0.302 0.580 -0.301

0.460 -0.348 0,600 -0.382

0.470 -0.331 0,610 -0,265

0.490 -0.313 0.650 -3.715"*

0.500 -0.285 0.700 -0.361

0.520 -0.2% 0.750 -0.322

0.530 -0.292 0.820 -0.312

0.550 -0.306 0.890 -0.132

0.560 -0.317 0.900 -0.102

0.580 -0.278 0.960 -0.024

0.590 -0.323

0.600 -0.319

0.640 -3.554**

0.700 -0.319

0.750 -0.286

0,820 -3.727**

0.870 -0.215

0,930 -0.089

0,960 -0.016

Lower Surface

0,020 -0.199 0.020 -0.047 0.020 0.050 0.020 0.354**

0.110 -0.065 0.060 0.130 0.060 0.192 0.060 5.559**

0.230 0,043 0.090 0.068 0.090 0.102 0.110 0.067

0.400 -0,026 0,120 0.051 0.120 -0.047 0.250 -0.044

0.490 -0.059 0.200 0.078 0.200 0.032 0.400 -0.069

0.630 3.385** 0.260 -0.001 0.250 0.004 0.490 -0.116

0.750 0.012 0.400 -3.744* * 0.400 -0.060 0.580 -0.162

0.850 0,075 0.490 -0.059 0,490 -0,006 0.650 -0.051

0.900 0.137 0.580 -0.031 0.580 -0.113 0.750 0.167

0.960 0.125 0.640 0.275 0.650 0.022 0.830 0.277

0.750 0.151 0.750 0.218 0,900 0.344

0.870 0.219 0.890 ******** 0.960 0.251

0.930 0.204 0.930 0.250

0.960 O. 119 0.960 -3.743 * *

CN = 0.257 0.45 t 0.474 0.465

162
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-33-43-500, MINF = 0.695, Camber = 5/2, ALPT = 8.05, BETA = -008, QINF = 291,9.

RNPU = 2.7E+06, CNWP = 0.3907

rl = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,347 0.000 0.854 0.000 -6,756** 0.0 lO - 1.403

0.060 -0,448 0.020 -0.714 0.020 -0,818 0.020 - 1.421

O, 110 -0.471 0,040 -0.628 0.060 - 1.475"* 0.060 - 1.217

0.200 -0.469 0.060 -0.826 0,090 - 1.121 0,110 - 1.031

0.230 -0443 0,090 -0.832 0.110 -0.969 0.140 1.935"*

0.400 -0.257 0.130 - 1.015 0.130 - 1.170 0.190 -6,620'*

0.490 -0.236 0,150 - 1,157 0.150 - 1,153 0.250 -0.555

0.590 -0.234 0.200 -0,676 0.210 -0.756 0.400 -0.402

0,630 -0.240 0.250 -0.517 0.250 -0.582 0,490 -0.362

0.700 -0.266 0.260 -0.466 0,340 -0.487 0.580 -0.313

0.750 -0.246 0.280 -0.499 0.370 -0.474 0.650 -0.396

0.810 -0.246 0.290 -0.458 0.400 -0.428 0.700 -0.353

0,840 -0.229 0.310 -0.4t3 0.410 -0.408 0.750 -0.319

0.900 -O 140 0.320 -0.44 1 0.430 -0.421 0.800 -0.252

0.960 -0045 0.340 -0.441 0.440 -0,399 0.830 -0.252

0,350 -0.134** 0.460 -0.381 0.900 -0. I 19

0.370 -0.402 0.490 -0.379 0.960 -0.002

0.380 -0.364 0.500 -0.372

0.400 -0.354 0.520 -0.372

0.410 -0,364 0.540 -0.374

0.430 -0.333 0,550 -0.332

0.440 -0.312 0.580 -0.311

0.460 -0.362 0.600 -0.372

0.470 -0,353 0.610 -0.286

0.490 -0.326 0.650 -3.820"*

0.500 -0.313 0.700 -0.353

0.520 -0.304 0.750 -0.323

0.530 -0.296 0.820 -0.291

0.550 -0.307 0.890 -0.116

0.560 -0.318 0.900 -0.106

0.580 -0,278 0.960 -0.027

0.590 -0.324

0.600 -0.325

0.640 -3.654**

0.700 -0.313

0.750 -0.275

0.820 -3,833**

0.870 -0.206

0.930 -0083

0.960 -0.026

Lower Surface

0.020 -0,031 0.020 0,13 l 0.020 0.205 0.020 0.463"*

0.110 -0.011 0.060 0.223 0060 0.260 0.060 5.739**

0.230 0.096 0.090 0.136 0.090 0.180 0. I I0 0.172

0.400 0,008 0.120 O. 123 0.120 0,004 0.250 0.004

0.490 -0.037 0.200 0.100 0,200 0.055 0.400 -0,039

0.630 3.497"* 0.260 0.038 0,250 0.035 0A90 -0.095

0.750 0.025 0.400 -3,851 ** 0.400 -0.037 0.580 -0.131

0,850 0.055 0.490 -0,032 0.490 -0.009 0,650 -0.044

0,900 0.136 0.580 -0,008 0.580 -0.086 0.750 0.166

0,960 0.121 0.640 0.295 0.650 0.024 0.830 0.279

0.750 0,147 0.750 0.225 0,900 0.336

0.870 0.225 0.890 ******** 0.960 0.241

0.930 0.207 0.930 0.244

0.960 0.123 0.960 -3,850**

CN = 0.306 0.519 0.541 0.514

163
Table D-2. Continued.

Flight t95, Wing sweep = 26 °, Time = 8-34-2-000. MINF = 0.715, Camber = 5/2. ALPT = 9.12. BETA = 0.07. QINF = 312.3.

RNPU = 2.8E+06. CNWP = 0.4406

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0.667 0.000 0.784 0.000 -6.352"* 0.010 - 1.469

0.060 -0.609 0.020 -0.984 0.020 - 1.210 0.020 - 1.492

0.110 -0.631 0.040 -0.738 0.060 -1.453"* 0.060 -1,477

0.200 -0.534 0.060 - 1.049 0.090 - 1.295 0.110 - 1.584

0.230 -0.503 0.090 -1.180 0.110 -1.368 0.140 1.795"*

0.400 -0.287 0.130 - 1.259 0.130 - 1.485 0.190 -6.224**

0.490 -0.258 0.150 - 1.336 0.150 - 1.417 0.250 -0.568

0.590 -0.265 0.200 - 1.294 0.210 - 1.515 0.400 -0.398

0.630 -0.274 0.250 -0.511 0.250 -0.630 0.490 -0.361

0.700 -0.293 0.260 -0.450 0.340 -0.465 0.580 -0.308

0.750 -0.255 0.280 -0.457 0.370 -0.469 0.650 -0.373

0.810 -0.270 0.290 -0.459 0.400 -0.437 0.700 -0.322

0.840 -0.275 0.310 -0.429 0.410 -0.400 0.750 -0.294

0.900 -0.173 0.320 -0.431 0.430 -0.447 0.800 -0.25 I

0.960 -0.079 0.340 -0.438 0.440 -0.423 0.830 -0.209

0.350 -0.121 ** 0.460 -0.390 0.900 -0.094

0.370 -0.402 0.490 -0.364 0.960 -0.035

0.380 -0.401 0.500 -0.371

0.400 -0.347 0.520 -0.376

0.410 -0.396 0.540 -0.386

0.430 -0.352 0.550 -0.355

0.440 -0.331 0.580 -0.320

0.460 -0.380 0.600 -0.392

0.470 -0.363 0.610 -0.276

0,490 -0.341 0.650 -3.607**

0.500 -0.334 0.700 -0.349

0.520 -0.331 0.750 -0.328

0.530 -0.312 0.820 -0.280

0.550 -0.326 0.890 -0.103

0.560 -0.346 0.900 -0.094

0.580 -0.299 0.960 0.000

0.590 -0.339

0.600 -0.341

0.640 -3.453**

0.700 -0.326

0.750 -0.291

0.820 -3.619"*

0.870 -0.208

0.930 -0.083

0.960 -0.010

Lower Surface

0.020 0.077 0.020 0.278 0.020 0.331 0.020 0.574**

0.110 0.027 0.060 0.288 0.060 0.350 0.060 5.327**

0.230 0.130 0.090 0.214 0.090 0.248 0.110 0.194

0.400 0.023 0.120 0.191 0.120 0.075 0.250 0.049

0.490 -0.019 0.200 0.136 0.200 0.109 0.400 0.010

0.630 3.232"* 0.260 0.075 0.250 0.080 0.490 -0.056

0.750 0.024 0.400 -3.636** 0.400 -0.002 0.580 -0.118

0.850 0.049 0.490 -0.015 0.490 -0.004 0.650 -0.029

0.900 0.129 0.580 0.000 0.580 -0.075 0.750 0.178

0.960 0.109 0.640 0.287 0.650 0.041 0.830 0.296

0.750 0.158 0.750 0.229 0.900 0.350

0.870 0.224 0.890 ******** 0.960 0.243

0.930 0.223 0.930 0.247

0.960 0.123 0.960 -3.635 **

CN = 0.372 0.618 0.635 0.607

164
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-34-8-500, MINF = 0.715, Camber = 5/2, ALPT = 10.07, BETA = -0.08, Q1NF = 311.4,

RNPU = 2.8E+06, CNWP = 0.3911

fl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -1.161 0.000 0.659 0.000 -6.356** 0.010 -1.671

0.060 -0.740 0.020 - 1.366 0.020 - 1.399 0.020 - 1.659

0.110 -0.688 0.040 - 1.115 0.060 - 1.561 ** 0.060 - 1.644

0.200 -0.561 0.060 - 1.216 0.090 - 1.430 0.110 - 1.709

0.230 -0.523 0.090 -1.237 0.110 -1.511 0.140 1.817"*

0.400 -0.310 0.130 -1.423 0,130 -1.616 0.190 -6.228**

0.490 -0.270 0.150 - 1.489 0.150 - 1.542 0.250 -0.841

0.590 -0.292 0.200 - 1.487 0.210 - 1.194 0.400 -0.373

0.630 -0.301 0.250 -0.675 0.250 -0.871 0.490 -0.335

0.700 -0.310 0.260 -0.545 0.340 -0.512 0.580 -0.300

0.750 -0.304 0.280 -0.476 0.370 -0.487 0.650 -0.351

0.810 -0.314 0.290 -0.417 0.400 -0.432 0.700 -0.317

0.840 -0.305 0.310 -0,380 0.410 -0.409 0.750 -0.288

0.900 -0.202 0.320 -0.409 0.430 -0.435 0.800 -0.245

0,960 -0.100 0.340 -0.409 0.440 -0.400 0.830 -0.201

0.350 -0.107"* 0.460 -0.394 0.900 -0.112

0.370 -0.404 0.490 -0.387 0.960 -0.062

0.380 -0.380 0.500 -0.386

0.400 -0.328 0,520 -0.378

0.410 -0.380 0.540 -0.387

0.430 -0.365 0.550 -0.357

0.440 -0.349 0.580 -0.304

0.460 -0.388 0.600 -0.368

0.470 -0.377 0.610 -0,264

0.490 -0.347 0.650 -3.604"*

0.500 -0.341 0.700 -0.309

0.520 -0.325 0.750 -0.288

0.530 -0.317 0.820 -0.229

0.550 -0.350 0.890 -0.077

0.560 -0.362 0.900 -0.061

0.580 -0.308 0.960 -0.022

0.590 -0.345

0.600 -0.348

0.640 -3.449**

0.700 -0.324

0.750 -0.2%

0,820 -3.616"*

0.870 -0.206

0.930 -0.081

0.960 -0.021

Lower Surface

0.020 0.189 0.020 0.359 0.020 0.437 0.020 0.629**

0.110 0.058 0.060 0.349 0.060 0.389 0,060 5.355**

0.230 0.148 0.090 0.257 0.090 0.285 0.110 0.224

0.400 0.030 0.120 0.216 0.120 0.111 0,250 0.076

0.490 -0.006 0.200 0.174 0.200 0.122 0.400 0.034

0.630 3.254** 0.260 0.116 0.250 0.116 0,490 -0.028

0.750 0.020 0.400 -3.633"* 0.400 0.022 0.580 -0.085

0.850 0.059 0.490 -0.008 0.490 0.013 0.650 0.006

0.900 0.121 0.580 0.017 0.580 -0.055 0.750 0.192

0.960 0.079 0.640 0.296 0.650 0.047 0.830 0.288

0.750 0.158 0.750 0.237 0.900 0.344

0.870 0.215 0.890 ******** 0.960 0.226

0.930 0.209 0.930 0.246

0.960 0.116 0.960 -3.632 **

CN = 0.413 0.684 0.664 0.680

165
Table D-2, Continued.

Flight 195. Wing sweep = 26 °, Time = 8-34-12-500, MINF = 0.703, Camber = 5/2, ALPT = 11.06, BETA = 0.05, QINF = 299.5,

RNPU = 2.7E+06, CNWP = 0.3610

1"1= 0.93 0.76 0.59 0.40

Upper Surface

xA- CP x./c CP x/c CP x/c CP

0,020 -1.410 0.000 0.534 0.000 -6.599** 0.010 -1.812

0.060 - 1.213 0.020 - 1.616 0.020 - 1.644 0.020 - 1.842

O. 110 -0.695 0.040 - 1.405 0.060 - 1.770"* 0.060 - 1.827

0.200 -0.627 0,060 - 1.440 0.090 - 1.692 0.110 - 1.905

0.230 -0.571 0.090 -1.503 0.110 -1.702 0.140 1.905"*

0.400 -0.328 0.130 - 1.632 0.130 - 1.138 0.190 -6.466"*

0.490 -0.283 0.150 - 1.662 0.150 -0.994 0.250 -0.85 |

0.590 -0.306 0.200 - 1.641 0.210 - 1.044 0.400 -0.358

0.630 -0.319 0.250 -0.718 0.250 -0.882 0.490 -0.339

0.700 -0.327 0.260 -0.563 0.340 -0.708 0.580 -0.306

0.750 -0.304 0.280 -0.509 0.370 -0.631 0.650 -0.325

0.810 -0.318 0.290 -0.442 0.400 -0.556 0.700 -0.299

0.840 -03 30 0.310 -0.389 0.410 -0.548 0.750 -0.276

0.900 -0.218 0.320 -0.402 0.430 -0.536 0.800 -0.271

0.960 -0.138 0.340 -0.416 0.440 -0.496 0.830 -0.172

0.350 -0.091 ** 0.460 -0.460 0.900 -0.154

0.370 -0.411 0.490 -0.438 0.960 -0.137

0.380 -0.400 0.500 -0.416

0.400 -0.342 0.520 -0.418

0,410 -0.389 0.540 -0.421

0.430 -0.364 0.550 -0.372

0.440 -0.342 0.580 -0.325

0.460 -0.388 0.600 -0.374

0.470 -0.376 0.610 -0.266

0.490 -0.358 0.650 -3.738"*

0.500 -0.349 0.700 -0.277

0.520 -0.321 0.750 -0.237

0.530 -0.328 0.820 -0.178

0.550 -0.336 0.890 -0.107

0.560 -0.340 0.900 -0.107

0.580 -0.290 0.960 -0.099

0.590 -0.34t

0.600 -0.347

0.640 -3.576**

0.700 -0.306

0.750 -0.269

0.820 -3.750"*

0, 870 -0.176

0.930 -0.071

0.96O -0.O31

Lower Surface

0.020 0.255 0.020 0,457 0.020 0.511 0.020 0.729**

0.110 0.118 0.060 0.417 0.060 0.453 0.060 5.576"*

0.230 0.179 0.090 0.312 0.090 0.344 0.110 0.289

0.400 0.048 0.120 0.268 0.120 0.182 0.250 0.130

0.490 -0.011 0.200 0.190 0.200 0.170 0.400 0.067

0.630 3.392 * * 0.260 0.159 0.250 0.170 0.490 -0.012

0.750 0.026 0.400 -3.768** 0.400 0.028 0.580 -0.073

0.850 0.044 0.490 0.005 0.490 0.019 0.650 -0.007

0.900 0.102 0.580 0.016 0.580 -0.04 1 0.750 0.199

0.960 0.094 0.640 0.308 0.650 0.059 0.830 0.292

0.750 0.142 0.750 0.219 0.900 0.337

0.870 0.209 0.890 ******** 0.960 0.197

0.930 0.201 0.930 0.205

0.960 0.112 0.960 -3.766"*

CN = 0.478 0.743 0.686 0.734

166
Table D-2, Continued.

Flight 195, Wing sweep = 26 °, Time = 8-34-26-000, MINF = 0.697, Camber = 5/2, ALPT = 11.27, BETA = 0.05. QINF = 297.5,

RNPU = 2.7E+06, CNWP = 0.3728

r I = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0,020 - 1_478 0.000 0.502 0.000 -6.668" * 0.010 - 1.848

0.060 - 1.333 0.020 - 1.705 0.020 - 1.715 0.020 - 1.908

0.110 -0.722 0.040 - 1.484 0.060 - 1.761 ** 0.060 - 1.878

0.200 -0.640 0.060 - 1.491 0.090 - 1.73 l 0.110 - 1.979

0,230 -0,548 0.090 - 1.568 0,110 - 1.618 0.140 1,921 **

0.400 -0,349 0.130 - 1.668 0,130 - 1.133 0.190 -6.535 * *

0.490 -0.317 0.150 - 1.718 0.150 - 1.003 0.250 -0.782

0.590 -0.322 0.200 - 1.437 0.210 - 1.062 0.400 -0.371

0.630 -0.336 0.250 -0.681 0.250 -0.899 0.490 -0.357

0,700 -0,333 0,260 -0.537 0.340 -0,725 0.580 -0.279

0,750 -0.313 0.280 -0.481 0.370 -0.640 0.650 -0.329

0.810 -0.308 0,290 -0.447 0.400 -0.564 0.700 -0.308

0.840 -0.321 0.310 -0.412 0.410 -0.578 0.750 -0.288

0,900 -0.233 0.320 -0.433 0.430 -0,581 0.800 -0.265

0.960 -0.128 0.340 -0.444 0.440 -0.536 0.830 -0.212

0.350 -0.108"* 0.460 -0.496 0.900 -0.151

0,370 -0.421 0.490 -0.466 0,960 -0,149

0,380 -0.404 0,500 -0.449

0.400 -0,352 0.520 -0.458

0.410 -0,392 0.540 -0.434

0.430 -0.372 0.550 -0.396

0.440 -0.356 0.580 -0,355

0.460 -0.387 0.600 -0.399

0.470 -0.389 0.610 -0.278

0.490 -0.346 0.650 -3.788**

0.500 -0.347 0.700 -0.282

0.520 -0.327 0.750 -0.274

0.530 -0.330 0.820 -0.216

0.550 -0.335 0.890 -0.143

0.560 -0.347 0.900 -0.113

0,580 -0,288 0.960 -0.092

0.590 -0.345

0.600 -0,341

0.640 -3.626**

0.700 -0,304

0.750 -0.275

0.820 -3,801"*

0.870 -0,170

0.930 -0.064

0.960 -0.027

Lower Surface

0.020 0.256 0.020 0.488 0.020 0.519 0.020 0.742**

0.110 0,129 0,060 0,416 0.060 0.472 0.060 5.589"*

0.230 0.173 0.090 0.338 0.090 0.374 0.110 0,294

0.400 0.030 0,120 0,266 0,120 0.1 64 0.250 0.130

0.490 0.007 0.200 0.199 0.200 0,153 0,400 0.075

0.630 3.390"* 0,260 0,150 0,250 0.164 0.490 0.014

0.750 0.012 0.400 -3.818" * 0.400 0,037 0.580 -0,060

0.850 0,049 0.490 0.013 0.490 0.013 0.650 0.004

0.900 0.121 0.580 0.020 0.580 -0.048 0.750 0,190

0.960 0.090 0.640 0.299 0.650 0.048 0.830 0.297

0.750 0.147 0.750 0.231 0.900 0.343

0.870 0.220 0.890 ******** 0.960 0.188

0.930 0.180 0.930 0.207

0.960 0.094 0.960 -3.817"*

CN = 0.494 0.743 0,711 0,744

167
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-34-33-500, MINF = 0,697, Camber = 5/2, ALPT = 11.88, BETA = 0.13, QINF = 301.7,

RNPU = 2.7E+06, CNWP = 0.3778

•q = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

O.020 - 1.618 0.000 0.425 0.000 -6.623 * * 0.010 - 1.952

0.060 - 1.503 0.020 - 1.785 0.020 - 1,845 0.020 -1.976

O. 1 I 0 -0.769 0.040 - 1.610 0.060 - 1.874"* 0.060 -2.003

0.200 -0.634 0.060 - 1.644 0.090 - 1.300 0.110 -2.043

0.230 -0.586 0.090 -1.656 0.110 -1.208 0.140 1.871 **

0.400 -0.356 0.130 -1.698 0.130 -1,136 0.190 -6.491"*

0.490 -0.313 0.150 - 1.796 0.150 -0.986 0,250 -0.510

0.590 -0,322 0.200 - 1.176 0.210 - 1.027 0,400 -0.376

0.630 -0.332 0,250 -0.674 0.250 -0.875 0.490 -0,365

0.700 -0.332 0.260 -0,525 0,340 -0.764 0.580 -0.290

0.750 -0.309 0.280 -0.500 0.370 -0.689 0.650 -0.331

0.810 -0.331 0.290 -0.457 0.400 -0.632 0.700 -0.293

0,840 -0.335 0.310 -0.415 0.410 -0.622 0.750 -0.274

0.900 -0.228 0.320 -0.420 0.430 -0.639 0.800 -0.294

0.960 -0.137 0.340 -0.441 0.440 -0.601 0.830 -0,208

0.350 -0.101 * * 0.460 -0.568 0,900 -0.198

0.370 -0.411 0.490 -0.544 0.960 -0.194

0.380 -0.401 0,500 -0.518

0.400 -0.361 0.520 -0.518

0.410 -0.390 0.540 -0.487

0.430 -0.382 0.550 -0.455

0.440 -0.337 0.580 -0.409

0.460 -0.385 0.600 -0.444

0.470 -0.373 0.610 -0.305

0.490 -0.345 0.650 -3.782**

0.500 -0,332 0.700 -0.317

0.520 -0.326 0.750 -0.299

0.530 -0.301 0.820 -0.227

0.550 -0.311 0.890 -0.155

0.560 -0.319 0.900 -0.142

0.580 -0.275 0.960 -0.131

0.590 -0.313

0.600 -0.306

0.640 -3.622**

0.700 -0.249

0.750 -0.221

0.820 -3.795**

0.870 -0.136

0.930 -0,056

0.960 -0.023

Lower Surface

0.020 0.353 0.020 0.552 0.020 0.577 0.020 0.777**

0.110 0.144 0.060 0.458 0.060 0.490 0.060 5.465"*

0.230 0.200 0,090 0.360 0.090 0,397 0.110 0.321

0,400 0.055 0.120 0.303 0.120 0.207 0.250 0.168

0.490 0.003 0.200 0.211 0,200 0.182 0.400 0.085

0.630 3.296"* 0.260 0.180 0.250 0.202 0.490 0.025

0,750 0.018 0.400 -3.812"* 0.400 0.048 0.580 -0.043

0.850 0.051 0.490 0.031 0.490 0.027 0.650 0.026

0.900 0. I 10 0.580 0.020 0.580 -0.033 0.750 0.198

0.960 0.085 0.640 0.306 0,650 0.058 0.830 0.290

0.750 0.139 0.750 0.210 0.900 0.329

0.870 0.204 0.890 ******** 0.960 0.181

0.930 0.174 0.930 0.215

0.960 0.067 0.960 -3.811 **

CN = 0.522 0.735 0.712 0.744

168
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-35-52-000, MINF = 0.700, Camber = 5/6, ALPT = 5.12, BETA = -0.48, QINF = 297.3,

RNPU = 2.7E+06, CNWP = 0.3726

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.209 0.000 0.692 0.000 -6.652** 0.010 -0.516

0.060 -0.113 0.020 -0,014 0.020 -0.104 0.020 -0.348

0.110 -0.280 0.040 -0.l 15 0.060 -1.116"* 0.060 -0.673

0.200 -0.346 0.060 -0.334 0.090 -0.551 0.110 -0.789

0.230 -0.315 0.090 -0.438 0.110 -0.677 0.140 1,947"*

0.400 -0.227 0.130 -0.577 0.130 -0.784 0.190 -6.518 **

0.490 -0.225 0.150 -0.631 0.150 -0.559 0.250 -0.450

0.590 -0.284 0.200 -0.487 0.210 -0.588 0.400 -0,364

0.630 -0.309 0.250 -0.385 0.250 -0.443 0.490 -0.364

0.700 -0.385 0.260 -0.357 0.340 -0.421 0.580 -0.355

0.750 -0.455 0.280 -0.375 0.370 -0.409 0,650 -0.435

0.810 -0.454 0,290 -0.376 0.400 -0.380 0.700 -0.439

0.840 -0.446 0.310 -0.345 0.410 -0,375 0.750 -0.517

0.900 -0.206 0.320 -0.356 0.430 -0.411 0.800 -0.524

0.960 -0.063 0.340 -0.366 0.440 -0.387 0.830 -0.542

0,350 -0.148"* 0.460 -0,375 0.900 -0.204

0,370 -0.341 0.490 -0.362 0.960 -0.009

0,380 -0.333 0.500 -0,384

0.400 -0.293 0.520 -0.390

0.410 -0.343 0.540 -0.399

0.430 -0.316 0.550 -0.378

0.440 -0.299 0.580 -0.348

0.460 -0.358 0.600 -0.44 I

Q470 -0,362 0.610 -0.34 I

0.499 -0.333 0.650 -3.769"*

0.500 -0.329 0.700 -0.498

0.520 -0.319 0.750 -0.506

0.530 -0,326 0.820 -0.560

0.550 -0.345 0.890 -0.184

0.560 -0.371 0.900 -0.132

0.580 -0.335 0.960 -0.036

0.590 -0.389

0.600 -0.397

0.640 -3.606**

0.700 -0.506

0,750 -0.590

0,820 -3.782**

0,870 -0,343

0,930 -0.141

0,960 -0.056

Lower Surface

0.020 -0.388 0.020 -0.374 0.020 -0.262 0.020 0.016"*

0.110 -0.135 0.060 -0,017 0.060 0.026 0,060 5.615 * *

0,230 0.020 0.090 -0.052 0.090 -0.040 0.110 -0.027

0,400 0.004 0.120 -0,019 0.120 -0.177 0,250 -0,113

0.490 -0,007 0.200 0.036 0.200 -0.003 0.400 -0.091

0.630 3.415' * 0.260 -0.026 0.250 -0.044 0.490 -0.113

0.750 0.115 0.400 -3.799"* 0.400 -0.063 0.580 -0.104

0.850 0.175 0.490 -0.018 0.490 0.016 0.650 0.035

0.900 0.235 0.580 0.054 0.580 -0.037 0.750 0.266

0.960 0.174 0,640 0,389 0.650 0.151 0.830 0,368

0,750 0.230 0.750 0.340 0.900 0,434

0,870 0.352 0,890 ******** 0.960 0.303

0,930 0.291 0.930 0.341

0.960 O. 180 0,960 -3,798**

CN = 0.309 0.479 0.487 0,466

169
Table D-2. Continued.

Flight 195. Wing sweep = 26 °, Time = 8-35-59-000, MINF = 0.701, Camber = 5/6, ALPT = 6.97, BETA = -0.37, QINF = 297.2,

RNPU = 2.7E+06, CNWP = 0.4529

rI = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.130 0.000 0.855 0.000 -6.644** 0.010 -1.316

0,060 -0.336 0,020 -0.452 0.020 -0.542 0,020 -0.658

0.110 -0.431 0.040 -0,436 0,060 - 1.345"* 0.060 - l. 132

O.200 -0,441 0.060 -0.667 0.090 -0.848 O. 110 -0.978

0.230 -0.438 0.090 -0.718 0.110 -0.986 0.140 1.920 **

0,400 -0.279 0.130 -0,910 0.130 -1.165 0.190 -6.511 **

0.490 -0.260 0.150 -0.886 0.150 -0.785 0.250 -0.553

0.590 -0.321 0,200 -0.666 0.210 -0.731 0,400 -0.424

0.630 -0.346 0.250 -0.507 0.250 -0,559 0.490 -0.412

0.700 -0,424 0.260 -0,472 0.340 -0,497 0.580 -0.404

0,750 -0.500 0.280 -0,492 0,370 -0.487 0.650 -0.472

0.810 -0.513 0,290 -0.476 0.400 -0.451 0.700 -0.472

0.840 -0,500 0.310 -0.430 0.410 -0,444 0.750 -0.537

0,900 -0.245 0,320 -0,442 0,430 -0,479 0,800 -0,493

0.960 -0.111 0,340 -0,448 0,440 -0.456 0,830 -0.514

0.350 -0.154"* 0.460 -0.434 0,900 -0.158

0.370 -0.415 0.490 -0.412 0.960 -0.024

0,380 -0.409 0,500 -0.432

0.400 -0.360 0.520 -0.450

0.410 -0.409 0.540 -0.445

0,430 -0.391 0.550 -0.418

0,440 -0.357 0.580 -0.391

0,460 -0.421 0,600 -0,475

0,470 -0,405 0,610 -0.388

0.490 -0.382 0,650 -3.761 **

0,500 -0.379 0.700 -0.531

0.520 -0.379 0.750 -0.533

0,530 -0.376 0,820 -0.559

0,550 -0,408 0.890 -0.167

0.560 -0.411 0.900 -0.117

0.580 -0,372 0.960 -0,030

0.590 -0.435

0.600 -0,437

0.640 -3.598**

0,700 -0.540

0,750 -0.616

0.820 -3.773**

0.870 -0.355

0.930 -0.150

0,960 -0.065

Lower Surface

0.020 -0.173 0,020 -0,019 0.020 0,063 0.020 0,348"*

0.110 -0.038 0.060 0.149 0,060 0,209 0.060 5.627**

0.230 0,080 0.090 0,091 0.090 0.122 0.110 0.086

0,400 0.017 0.120 0.092 0.120 -0.054 0.250 -0.016

0.490 0.017 0.200 0.1 04 0.200 0.054 0.400 -0.019

0.630 3.426** 0.260 0,043 0,250 0.040 0.490 -0.058

0.750 0.105 0.400 -3.791 ** 0,400 -0.002 0.580 -0.053

0.850 0.158 0,490 0.022 0,490 0,026 0.650 0.067

0.900 0.225 0.580 0.093 0.580 0.002 0.750 0.286

0,960 0.143 0.640 0.402 0,650 0.168 0.830 0.378

0,750 0,240 0,750 0.354 0.900 0.450

0.870 0.334 0.890 ******** 0.960 0.310

0,930 0.294 0,930 0.343

0,960 0.178 0.960 -3.790"*

CN = 0.404 0.620 0.616 0,590

170
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-36-15-000, MINF = 0.705. Camber = 5/6, ALPT = 8.03, BETA = -0.11, QINF = 296.8,

RNPU = 2.7E+06, CNWP = 0.4727

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.393 0.000 0.772 0.000 -6.617"* 0.010 - 1.332

0.060 -0.461 0.020 -0.808 0.020 -0.878 0.020 - 1.377

O. 110 -0.516 0.040 -0.651 0.060 - 1.424" * 0.060 - I. 169

0.200 -0.487 0.060 -0.848 0.090 -0.938 0.110 - 1.072

0.230 -0.450 0.090 -0.853 0.110 - 1.025 0.140 1.929"*

0.400 -0.288 0.130 -1.018 0.130 -1.197 0.190 -6.483**

0.499 -0.265 0.150 - 1.165 0.150 - 1.183 0.250 -0.562

0.590 -0,326 0.200 -0.688 0.210 -0.745 0.400 -0.425

0.630 -0.347 0,250 -0.541 0.250 -0.575 0.490 -0.405

0.700 -0.418 0.260 -0.493 0.340 -0.530 0.580 -0.377

0.750 -0.486 0.280 -0.504 0.370 -0.497 0.650 -0.442

0.810 -0.477 0.290 -0.488 0.400 -0.460 0.700 -0.434

0.840 -0.494 0.310 -0.446 0.410 -0.453 0.750 -0.472

0.900 -0.263 0.320 -0.453 0.430 -0.495 0.800 -0.408

0.960 -0.133 0.340 -0.463 0.440 -0.450 0.830 -0.423

0.350 -0.142"* 0.460 -0.436 0.900 -0.160

0.370 -0.427 0.490 -0.406 0.960 -0.025

0.380 -0.408 0.500 -0.436

0.400 -0.365 0.520 -0.444

0.410 -0.412 0.540 -0.439

0.430 -0.396 0.550 -0.412

0.440 -0.366 0.580 -0.367

0.460 -0.427 0.600 -0.462

0.470 -0.406 0.610 -0.367

0.490 -0.384 0.650 -3.730* *

0.500 -0.378 0.700 -0.507

0.520 -0.373 0.750 -0.501

0.530 -0.366 0.820 -0.507

0.550 -0.402 0.890 -0.148

0.560 -0.41 l 0.900 -0.105

0.580 -0.366 0.960 -0.045

0.590 -0.420

0.600 -0.426

0.640 -3.567**

0.700 -0.512

0.750 -0.571

0.820 -3.742**

O.870 -0.331

0.930 -0.132

0.960 -0.066

Lower Surface

0.020 0.006 0.020 0.174 0.020 0.244 0.020 0.510"*

0.110 0.027 0.060 0.250 0.060 0.296 0.060 5.670**

0.230 0.117 0.090 0.175 0.090 0.204 0.110 0.154

0.400 0.050 0.120 0.148 0.120 0.022 0.250 0.041

0.490 0.024 O, 200 O. 140 0.200 0.092 0.400 0,032

0.630 3.466** 0.260 0.093 0.250 0.099 0.490 -0.006

O.750 O. 101 0.400 -3,760* * 0.400 0.036 0.580 -0.015

0.850 O. 142 0.490 0.040 0.490 0.018 0.650 0.089

0.900 0.202 0.580 0.092 0.580 0.028 0.750 0.283

0.960 O. 133 0.640 0,403 0.650 O. 175 0.830 0.368

0.750 0.230 0.750 0.338 0.900 0.436

0.870 0.313 0,890 ******** 0.960 0.296

0.930 0.271 0.930 0,327

0.960 O.156 0.960 -3.759**

CN = 0.438 0.670 0.657 0.632

171
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-36-33-000, MINF = 0,721, Camber = 5/6, ALPT = 9.17, BETA = 0.15, QINF = 332.1,

RNPU = 2.9E+06, CNWP = 0.4460

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.679 0,000 0.781 0.000 -6.088"* 0.010 -1.487

0.060 -0.723 0,020 -0.948 0.020 - 1.195 0.020 - 1.458

0.110 -0.666 0.040 -0,692 0.060 - 1.451 ** 0.060 - 1.482

0.200 -0.556 0.060 - 1.042 0.090 - 1.300 0.110 - 1.561

0.230 -0.529 0.090 - 1.166 0.110 - 1.344 0.140 1.728"*

0.400 -0.352 0.130 - 1.261 0.130 - 1.498 0.190 -5.968" *

0.490 -0.328 0.150 - 1.367 0.150 - 1.418 0.250 -0.902

0.590 -0.373 0.200 - 1.370 0.210 - 1.559 0.400 -0.44 1

0.630 -0.422 0.250 -0.804 0.250 -0.920 0.490 -0.432

0.700 -0.479 0.260 -0.648 0.340 -0,508 0.580 -0.392

0.750 -0.582 0.280 -0.563 0.370 -0.466 0,650 -0.437

0.810 -0.598 0.290 -0,472 0.400 -0.443 0.700 -0.444

0.840 -0.610 0.310 -0.401 0.410 -0.454 0.750 -0.474

0.900 -0.315 0.320 -0.417 0,430 -0.504 0.800 -0.402

0,960 -0.176 0.340 -0,422 0.440 -0.448 0.830 -0,375

0.350 -0.106"* 0.460 -0.448 0,900 -0.161

0.370 -0.416 0.490 -0.449 0,960 -0.047

0.380 -0.408 0.500 -0.468

0,400 -0.387 0.520 -0.454

0.410 -0.431 0.540 -0,473

0.430 -0.422 0,550 -0.450

0.440 -0.382 0.580 -0.403

0.460 -0.460 0.600 -0.494

0.470 -0.430 0.610 -0.422

0.490 -0.423 0.650 -3.508 * *

0.500 -0.414 0.700 -0.523

0.520 -0.395 0.750 -0.534

0,530 -0.398 0.820 -0.507

0.550 -0.427 0.890 -0.126

0.560 -0.448 0.900 -0.097

0.580 -0.402 0.960 -0.036

0.590 -0.463

0.600 -0.478

0.640 -3.362**

0.700 -0.575

0.750 -0.658

0.820 -3.519"*

0.870 -0.333

0.930 -0.147

0.960 -0.088

Lower Surface

0.020 0.095 0.020 0.375 0.020 0.352 0.020 0.592**

0.110 0.034 0.060 0.308 0.060 0.369 0.060 4.893**

0.230 0.170 0.090 0.252 0.090 0.265 0.110 0.201

0.400 0.059 0.120 0.233 0.120 0,082 0.250 0.084

0.490 0.035 0.200 0.175 0.200 0.146 0.400 0.043

0.630 2.923** 0.260 0,134 0.250 0.123 0.490 -0,005

0.750 O. 104 0.400 -3.534"* 0.400 0.023 0.580 -0.002

0.850 O. 134 0.490 0.064 0.490 0.037 0.650 0.094

0.900 0.213 0.580 0.090 0.580 0.003 0.750 0.314

0.960 O. 136 0.640 0.406 0.650 O. 164 0.830 0.386

0.750 0.251 0.750 0.063 0.900 0.466

0.870 0.329 0.890 ******** 0.960 0.318

0.930 0,286 0.930 0.335

0.960 0.170 0.960 -3.533 * *

CN = 0.538 0.797 0.740 0.774

172
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-36-45-500, MINF = 0.692, Camber = 5/6, ALPT = 11.00. BETA = 0.05, QINF = 313.4.

RNPU = 29E+06, CNWP = 0.4383

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -1.476 0,000 0.497 0.000 -6,524"* 0.010 -t.865

0,060 - 1.211 0.020 -1.689 0,020 -1.763 0.020 - 1.877

0.110 -0,793 0.040 - 1.484 0_060 -1.736** 0,060 - 1.903

0.200 -0.665 0.060 - 1.493 0.090 - 1.739 0,1 I0 - 1.965

0,230 -0,626 0,090 - 1.566 0.110 - 1.773 0,140 1,854"*

0.400 -0,413 0,130 - 1.590 0.130 - 1.494 0.190 -6.397"*

0.490 -0.379 0.150 - 1.726 0.150 - 1.104 0.250 -0.837

0.590 -0.413 0.200 -1.712 0.210 -1.196 0,400 -0,417

0,630 -0.452 0,250 -0.841 0.250 - 1.006 0.490 -0.433

0.700 -0.518 0.260 -0.669 0.340 -0.765 0.580 -0,385

0.750 -0,599 0.280 -0.590 0.370 -0.679 0,650 -0,379

0.810 -0.630 0,290 -0.507 0.400 -0.647 0,700 -0.389

0.840 -0,643 0,310 -0.447 0.410 -0.591 0,750 -0,394

0.900 -0,358 0,320 -0.459 0.430 -0.599 0.800 -0,394

0.960 -0.209 0.340 -0.480 0.440 -0.553 0.830 -0.297

0.350 -0.107"* 0.460 -0.524 0,900 -0,216

0,370 -0,452 0.490 -0.500 0.960 -0,189

0,380 -0.448 0.500 -0.490

0.400 -0.407 0.520 -0.487

0.410 -0.454 0,540 -0.477

0.430 -0.422 0.550 -0.464

0.440 -0,380 0.580 -0.416

0.460 -0.489 0.600 -0.464

0,470 -0.451 0.610 -0.356

0,490 -0.420 0.650 -3.789**

0,500 -0,413 0.700 -0.376

0.520 -0.423 0.750 -0,39 I

0.530 -0.398 0,820 -0.313

0.550 -0,416 0_890 -0.165

0,560 -0.435 0.900 -0,147

0,580 -0. 390 0,960 -0.141

0,590 -0.438

0.600 -0.450

0.640 -3.635"*

0,700 -0,491

0.750 -0.535

0.820 -3.801 **

0.870 -0.291

0.930 -0.117

0.960 -0.055

Lower Surface

0,020 0.308 0.020 0,546 0.020 0.518 0.020 0.748**

0.110 0.145 0.060 0,436 0.060 0.491 0.060 5.113"*

0.230 0.223 0.090 0.346 0.090 0.383 0.110 0.315

0.400 0.080 0.120 0.301 0,120 0,186 0.250 0.163

0.490 0.069 0.200 0.244 0.200 0.201 0.400 0.119

0.630 3.026** 0.260 0.197 0.250 0.211 0.490 0,048

0,750 0.103 0.400 -3.818 ** 0.400 0.105 0.580 0,038

0.850 0.138 0.490 0.089 0.490 0.056 0.650 0,128

0.900 0.200 0,580 0.124 0.580 0.062 0.750 0.315

0.960 0.115 0.640 0.417 0.650 0.191 0.830 0.397

0,750 0.255 0.750 0.098 0.900 0.460

0.870 0.329 0.890 ******** 0.960 0.273

0,930 0.279 0.930 0.321

0.960 0.162 0.960 -3,816"*

CN = 0.651 0,913 0,810 0.866

173
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-37-22-000, MINF = 0.691, Camber = 5/6, ALPT = 11.06, BETA = -0.19, QINF = 312.5,

RNPU = 2.9E+06, CNWP = 0,4411

rl = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0,020 - 1.516 0,000 0,461 0,000 -6.548"* 0,010 - 1.886

0.060 - 1.246 0,020 - 1.715 0.020 - 1.806 0,020 - 1.909

0.110 -0.768 0.040 -1.511 0,060 -1.764** 0.060 -1.914

0,200 -0,672 0.060 - 1.533 0,090 - 1.760 0.110 - 1.995

0.230 -0,633 0.090 - 1,585 0.110 - 1,792 0.140 1.859**

0.400 -0.413 0.130 - 1.559 0.130 - 1.342 0.190 -6.421 **

0.490 -0.389 0.150 - 1.745 0.150 - 1.113 0,250 -0,763

0,590 -0.431 0.200 - 1,723 0.210 - 1,205 0,400 -0,424

0.630 -0.467 0.250 -0,799 0.250 - 1.001 0.490 -0.440

0.700 -0,535 0.260 -0.651 0,340 -0.802 0,580 -0.392

0.750 -0.621 0.280 -0.563 0.370 -0.717 0.650 -0.386

0.810 -0,660 0.290 -0,506 0.400 -0,690 0.700 -0,406

0.840 -0.658 0.310 -0.461 0.410 -0.613 0.750 -0,401

0,900 -0,365 0,320 -0.470 0.430 -0.607 0.800 -0,408

0,960 -0.216 0.340 -0,497 0,440 -0.571 0.830 -0,295

0.350 -0.118"* 0,460 -0.531 0,900 -0.223

0.370 -0.469 0.490 -0,500 0,960 -0.195

0.380 -0,468 0.500 -0,497

0.400 -0.413 0.520 -0.502

0.410 -0.470 0.540 -0.497

0.430 -0,446 0,550 -0.460

0,440 -0.416 0.580 -0.423

0.460 -0.482 0.600 -0.471

0.470 -0.471 0.610 -0.362

0,490 -0.435 0.650 -3.806**

0.500 -0,435 0.700 -0.404

0.520 -0,437 0.750 -0.404

0.530 -0.411 0.820 -0.336

0.550 -0,423 0.890 -0.179

0,560 -0,454 0,900 -0.158

0,580 -0.403 0.960 -0.143

0,590 -0,453

0.600 -0.471

0.640 -3.651 **

0,700 -0.512

0,750 -0.560

0.820 -3,818"*

0,870 -0.298

0.930 -0.123

0.960 -0.061

Lower Surface

0,020 0.284 0,020 0.481 0,020 0.514 0.020 0.744**

0. I I 0 0.139 0,060 0.435 0,060 0.486 0.060 5.122"*

0,230 0.211 0.090 0.341 0.090 0.378 0.110 0.310

0,400 0,078 0.120 0.296 0,120 0.181 0.250 0.157

0,490 0.053 0.200 0.236 0.200 0.183 0,400 0.107

0.630 3,029"* 0.260 0.196 0.250 0.206 0.490 0,057

0.750 0.097 0.400 -3.834* * 0.400 0.100 0.580 0.032

0.850 0.132 0.490 0.091 0.490 0,058 0.650 0.126

0,900 0.193 0.580 0.122 0,580 0.056 0.750 0.315

0,960 0.106 0.640 0.419 0.650 0.207 0,830 0,393

0,750 0,262 0,750 0,099 0.900 0.456

0.870 0.333 0.890 ******** 0.960 0.265

0,930 0.278 0,930 0,323

0,960 0.160 0.960 -3.833 **

CN = 0,653 0.925 0.818 0.861

174
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time -- 8-39-31-500, MINF = 0.696, Camber = 5/10, ALPT = 3.95, BETA = -0.03, QINF = 282.6,

RNPU = 2.6E+06. CNWP = 0.3128

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.283 0.000 0.585 0.000 -6.880"* 0.010 -0.278

0,060 -0.038 0.020 O. 168 0.020 0.059 0.020 -0.214

O. 110 -0,226 0.040 -0,011 0.060 - 1.151 ** 0.060 -0.533

0.200 -0.312 0.060 -0.226 0.090 -0.461 O. 110 -0.693

0230 -0.356 0,090 -0.363 0.110 -0.585 0.140 2.044**

0.400 -0.243 0,130 -0.514 0,130 -0.701 0.190 -6.739.**

0.490 -0.260 0.150 -0.579 0,150 -0,513 0.250 -0.411

0.590 -0.327 0.200 -0.452 0.210 -0,537 0.400 -0.364

0.630 -0.382 0.250 -0.382 0,250 -0.423 0.490 -0.377

0.700 -0.499 0.260 -0.344 0.340 -0.414 0.580 -0.374

0.750 -0.685 0.280 -0.370 0.370 -0.394 0.650 -0.487

0.810 -0.699 0.290 -0.351 0,400 -0,381 0.700 -0.511

0.840 -0,691 0.310 -0.343 0,410 -0,375 0.750 -0.649

0,900 -0.205 0.320 -0.351 0,430 -0.428 0.800 -0.706

0.960 -0,070 0.340 -0.374 0.440 -0.390 0.830 -0.703

0.350 -0.155"* 0.460 -0.383 0.900 -0.180

0.370 -0.343 0.490 -0.385 0.960 -0.144

0.380 -0.345 0.500 -0.387

0.400 -0.301 0.520 -0.398

0.410 -0,365 0.540 -0.43 l

0_430 -0.349 0.550 -0.399

0,440 -0.319 0.580 -0407

0.460 -0,393 0,600 -0.494

0.470 -0.399 0,610 -0 407

0.490 -0,363 0,650 -3,847**

0.500 -0,361 0,700 -0.584

0.520 -0,364 0,750 -0.620

0.530 -0.365 0.820 -0,676

0.550 -0,386 0,890 -0,198

0.560 -0,420 0,900 -0,173

0,580 -0.378 0.960 -0.182

0.590 -0.425

0.600 -0.442

0.640 -3.676**

0.700 -0.613

0.750 -0.776

0.820 -3.860**

0.870 -0.452

0.930 -0.253

0.960 -0.149

Lower Surface

0.020 -0,519 0.020 -0,520 0.020 -0.413 0.020 -0,156"*

0,110 -0.138 0.060 -0,058 0,060 -0.017 0.060 6.027**

0.230 -0.003 0.090 -0.100 0.090 -0.094 0.110 -0.118

0.400 0.024 0.120 -0.048 0.120 -0.239 0.250 -0.137

0,490 0.027 0.200 0.022 0,200 -0.021 0.400 -0.073

0,630 3.711 ** 0.260 -0.031 0.250 -0,043 0.490 -0.084

0.750 0.189 0.400 -3.879** 0.400 -0.033 0.580 -0.048

0.850 0.261 0,490 0.033 0.490 0,022 0.650 0.120

0.900 0.318 0.580 0.115 0,580 0,027 0,750 0.349

0.960 0.201 0.640 0.488 0.650 0,251 0,830 0.438

0.750 0.316 0.750 0.059 0.900 0,518

0.870 0.396 0,890 ******** 0,960 0.340

0.930 0.337 0.930 0.387

0.960 0.185 0.960 -3.877"*

CN = 0.389 0.544 0.482 0.508

175
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-39-46-000. MINF = 0.691, Camber = 5/10, ALPT = 6.00, BETA = -0.32, QINF = 278.5,

RNPU = 2.5E+06, CNWP = 0.3859

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.025 0.000 0.841 0.000 -6,977** 0.010 -0,946

0.060 -0.236 0.020 -0.334 0.020 -0.391 0.020 -0.592

0.110 -0.419 0,040 -0.320 0.060 -1.315"* 0,060 -0.909

0.200 -0.439 0.060 -0.575 0.090 -0.766 0.110 -0.998

0.230 -0.423 0.090 -0.651 0.110 -0.913 0.140 2,078**

0.400 -0.294 0.130 -0.805 0.130 - 1.084 0.190 -6.834**

0.490 -0.293 0.150 -0.839 0.150 -0.726 0.250 -0.542

0.590 -0.360 0.200 -0.620 0.210 -0.736 0.400 -0.419

0.630 -0.422 0.250 -0.524 0.250 -0.553 0.490 -0.420

0.700 -0.536 0.260 -0.463 0.340 -0.518 0.580 -0.423

0.750 -0.739 0.280 -0.492 0.370 -0,499 0.650 -0.532

0.810 -0.757 0.290 -0.484 0.400 -0.478 0.700 -0.557

0.840 -0.748 0.310 -0.420 0.410 -0.470 0.750 -0.687

0,900 -0.240 0.320 -0.436 0.430 -0.499 0.800 -0.668

0.960 -0.138 0.340 -0.459 0.440 -0,483 0.830 -0.650

0.350 -0.172** 0.460 -0.472 0.900 -0.184

0.370 -0,427 0.490 -0.444 0.960 -0.146

0,380 -0.419 0.500 -0,478

0.400 -0.357 0.520 -0.476

0.410 -0.432 0.540 -0,487

0.430 -0.413 0.550 -0.469

0.440 -0.384 0.580 -0.452

0.460 -0.443 0.600 -0.536

0.470 -0.436 0.610 -0.455

0.490 -0.417 0,650 -3,900"*

0.500 -0.412 0.700 -0,602

0.520 -0,425 0,750 -0,654

0.530 -0.417 0.820 -0.673

0.550 -0.441 0.890 -0.196

0.560 -0,462 0.900 -0.180

0.580 -0.422 0.960 -0.195

0,590 -0,488

0.600 -0,520

0.640 -3.726**

0.700 -0.647

0.750 -0.677

0.820 -3.913"*

0.870 -0.514

0.930 -0.279

0.960 -0.193

Lower Surface

0.020 -0.281 0.020 -0.113 0.020 -0.006 0,020 0.260**

0.110 -0.043 0.060 0.115 0.060 0.170 0.060 6.116"*

0.230 0.060 0.090 0.063 0.090 0.079 0.110 0.051

0.400 0.050 0.120 0.073 0.120 -0.110 0.250 -0.028

0.490 0.038 0.200 0.091 0.200 0.032 0.400 -0.009

0.630 3.767"* 0,260 0.041 0.250 0.046 0.490 -0.035

0.750 0.173 0.400 -3.932 * * 0.400 0.018 0.580 0.003

0,850 0.225 0.490 0.056 0.490 0.047 0.650 0.148

0.900 0.291 0.580 0.154 0.580 0.061 0.750 0.372

0.960 0.180 0.640 0.491 0.650 0.292 0.830 0.469

0,750 0.296 0.750 0.078 0.900 0,536

0.870 0.429 0,890 ******** 0.960 0.344

0.930 0.336 0.930 0.394

0.960 0.198 0.960 -3.931 **

CN = 0.479 0.685 0.626 0.652

176
Table D-2. Concluded.

Fligh! 195, Wing sweep = 26 °, Time = 8-39-57-500, MINF = 0.690, Camber = 5/10, ALPT = 7.01, BETA = -0.37, QINF = 276.5,

RNPU = 2.5E÷06, CNWP = 0.4296

1] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.236 0.000 0.863 0.000 -7.018"* 0.010 -1.331

0.060 -0.427 0.020 -0,636 0.020 -0.653 0.020 -0.727

0.110 -0.497 0.040 -0.527 0.060 - 1.459"* 0.060 - 1.248

0.200 -0.501 0.060 -0.769 0.090 -0.908 0.1 I 0 - 1.015

0.230 -0.476 0.090 -0.814 0. l 10 - 1.064 0.140 2.085"*

0.400 -0.309 0.130 -0.999 0,130 - 1.238 0.190 -6.874**

0,490 -0.324 0.150 - 1.094 0.150 - I. 109 0.250 -0.595

0.590 -0.399 0.200 -0,725 0.210 -0.792 0.400 -0.471

0.630 -0.443 0.250 -0.587 0.250 -0.609 0.490 -0,474

0.700 -0.572 0.260 -0.522 0.340 -0.561 0.580 -0.477

0.750 -0.762 0.280 -0.553 0.370 -0.568 0.650 -0.551

0.810 -0.802 0.290 -0.536 0.400 -0.510 0.700 -0.585

0.840 -0.787 0.310 -0.482 0.410 -0.505 0.750 -0.705

0,900 -0.257 0.320 -0.493 0.430 -0,526 0.800 -0.662

0.960 -0.174 0.340 -0.505 0,440 -0.521 0.830 -0.669

0.350 -0.150** 0.460 -0.501 0.900 -0.214

0.370 -0.463 0,490 -0.468 0.960 -0.172

0.380 -0.459 0,500 -0.507

0.400 -0.408 0,520 -0.525

0.410 -0,467 0,540 -0.524

0.430 -0.431 0.550 -0.489

0.440 -0.411 0.580 -0.472

0.460 -0.490 0.600 -0.555

0.470 -0.463 0.610 -0.463

0490 -0.443 0.650 -3.918"*

0.500 -0.457 0.700 -0.638

0.520 -0.451 0.750 -0.667

0.530 -0.435 0.820 -0.626

0.550 -0.463 0.890 -0.208

0.560 -0.488 0.900 -0.187

0.580 -0.427 0.960 -0,201

0.590 -0.512

0.600 -0.523

0.640 -3.743**

0.700 -0.676

0,750 -0.74 l

0.820 -3.932**

0.870 -0.518

0.930 -0.242

0.960 -0.191

Lower Surface

0.020 -0.089 0.020 0.066 0.020 0.134 0.020 0.444**

0,110 -0.004 0.060 0.232 0.060 0.254 0.060 6.173 **

0.230 0.092 0.090 0.138 0.090 0.162 0.110 0.107

0.400 0,057 0.120 0.126 0.120 -0.034 0.250 0.019

0.490 0.053 0.200 0.130 0.200 0.073 0.400 0.026

0.630 3.807** 0.260 0.084 0.250 0.089 0.490 0,001

0.750 0.169 0.400 -3.951 * * 0.400 0.046 0.580 0.036

0.850 0.218 0.490 0.071 0.490 0.043 0,650 0.176

0.900 0.286 0.580 0.154 0.580 0.081 0.750 0.386

0,960 0.150 0.640 0.499 0.650 0.282 0.830 0.468

0.750 0.309 0.750 0.089 0.900 0.545

0.870 0.404 0.890 ******** 0.960 0.358

0.930 0.334 0.930 0.400

0.960 0.179 0.960 -3,949 * *

CN = 0.534 0.772 0.698 0.728

177
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-40-7-500, MINF = 0.701, Camber = 5/10, ALPT = 8.06, BETA = -0.11, QINF = 286.0,

RNPU = 2.6E+06, CNWP = 0.5042

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.489 0.000 0.823 0,000 -6.786"* 0.010 -1.281

0.060 -0.521 0.020 -0,978 0.020 -0.892 0,020 - 1.416

0.110 -0.631 0.040 -0.704 0.060 - 1.562"* 0.060 - 1.393

0.200 -0,559 0.060 - 1.007 0.090 - 1.257 0. 110 - 1.527

0.230 -0.530 0.090 - 1.024 0.110 - 1.300 0.140 2.031 **

0.400 -0,343 0.130 - 1.035 0.130 - 1.399 0.190 -6,647* *

0.490 -0.339 0.150 - 1.248 0.150 - 1.341 0.250 -0.621

0.590 -0.402 0.200 - 1.273 0.210 - 1.415 0,400 -0,487

0.630 -0.464 0.250 -0.582 0.250 -0.607 0.490 -0.465

0.700 -0.568 0.260 -0.520 0,340 -0.580 0.580 -0.466

0,750 -0.737 0,280 -0.544 0,370 -0.555 0.650 -0.521

0.810 -0.764 0.290 -0.537 0.400 -0.519 0.700 -0.586

0.840 -0.776 0.310 -0.494 0.410 -0.524 0.750 -0.662

0.900 -0.261 0.320 -0.504 0.430 -0.560 0.800 -0.590

0.960 -0.208 0,340 -0.519 0.440 -0.525 0.830 -0.561

0,350 -0.160"* 0.460 -0.525 0.900 -0.189

0.370 -0.476 0.490 -0.464 0.960 -0.1 04

0.380 -0.473 0.500 -0.508

0.400 -0.427 0.520 -0.531

0.410 -0.481 0.540 -0.538

0.430 -0.466 0.550 -0,490

0,440 -0.417 0.580 -0.490

0.460 -0.509 0.600 -0.560

0.470 -0.475 0.610 -0.494

0.490 -0.453 0.650 -3.790"*

0.500 -0448 0.700 -0.615

0,520 -0.424 0.750 -0.647

0.530 -0.440 0.820 -0.595

0.550 -0.481 0.890 -0.169

0.560 -0.490 0.900 -0.156

0.580 -0.449 0.960 -0.178

0.590 -0,499

0.600 -0.514

0.640 -3.621"*

0.700 -0.679

0.750 -0.749

0.820 -3.803**

0.870 -0.492

0.930 -0.244

0.960 -0.199

Lower Surface

0.020 0.061 0.020 0.263 0.020 0,296 0.020 0,556**

0.110 0.066 0,060 0.310 0.060 0.356 0.060 5.964"*

0.230 0,164 0.090 0.214 0.090 0.242 0.110 0.184

0.400 0.091 0.120 0.188 0.120 0.034 0.250 0.065

0.490 0.075 0.200 0.191 0.200 0.134 0.400 0.080

0.630 3.677** 0.260 0.143 0.250 0.149 0.490 0.029

0.750 0.183 0.400 -3.821 ** 0,400 0.093 0.580 0.084

0.850 0.230 0.490 0.097 0.490 0.054 0.650 0.206

0.900 0.293 0.580 0.184 0.580 0.106 0.750 0.406

0.960 0.151 0,640 0.519 0.650 0.300 0.830 0.483

0.750 0.344 0.750 0. 110 0.900 0.577

0.870 0.408 0.890 ******** 0.960 0.386

0.930 0.355 0.930 0.407

0.960 0.204 0.960 -3.820**

CN = 0.595 0.870 0,807 0.827

178
Table D-2. Continued,

Flight 195, Wing sweep = 26 °, Time = 8-41-2-000, MINF = 0,686, Camber = 5/10, ALPT = 6.99, BETA = -0.19, QINF = 283.2,

RNPU = 2.6E+06, CNWP = 0.4150

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/¢ CP x/c CP x/c CP

0.020 -0.198 0.000 0.879 0.000 -6.951 ** 0,010 - 1.292

0.060 -0.391 0.020 -0.594 0.020 -0.622 0.020 -0,759

0.110 -0.467 0.040 -0496 0.060 - 1.458" * 0,060 - 1,234

0.200 -0.483 0.060 -0.744 0.090 -0.935 0.110 -1.042

0.230 -0.458 0.090 -0.788 0,110 - 1.061 0.140 2.036"*

0.400 -0.311 0.130 -0,965 0.130 - 1.227 0,190 -6.811 **

0.490 -0.314 0.150 -0.938 0.150 -0,838 0,250 -0.582

0.590 -0.383 0.200 -0.706 0.210 -0.802 0.400 -0.468

0.630 -0.434 0,250 -0.580 0,250 -0.596 0.490 -0.461

0.700 -0.560 0.260 -0.503 0.340 -0.558 0.580 -0.459

0,750 -0.749 0.280 -0,533 0.370 -0.540 0.650 -0.539

0.810 -0.784 0.290 -0,516 0.400 -0.499 0.700 -0.575

0.840 -0.773 0.310 -0.470 0.410 -0.494 0.750 -0.697

0.900 -0,259 0.320 -0,475 0.430 -0.538 0.800 -0.662

0.960 -0,156 0.340 -0.493 0.440 -0.502 0.830 -0.666

0.350 -0,173** 0.460 -0.488 0.900 -0.193

0.370 -0,449 0.490 -0.458 0.960 -0.16 I

0.380 -0.446 0.500 -0.493

0.400 -0.391 0,520 -0.506

0.410 -0.456 0.540 -0.521

0.430 -0.439 0.550 -0.499

0.440 -0.398 0.580 -0.464

0.460 -0.484 0.600 -0.535

0470 -0.452 0.610 -0.460

0.490 -0.434 0.650 -3.925"*

0.500 -0.422 0.700 -0.627

0.520 -0.425 0.750 -0.660

0.530 -0.425 0.820 -0.635

0.550 -0.454 0.890 -0.179

0.560 -0.470 0.900 -0.168

0,580 -0.432 0.960 -0.181

0,590 -0.498

0.600 -0.509

0.640 -3.755**

0.700 -0.673

0.750 -0.740

0.820 -3.939**

0.870 -0.488

0,930 -0.268

0.960 -0.187

Lower Surface

0.020 -0.110 0.020 0,045 0.020 0.129 0.020 0,441 **

0.1 I 0 -0.004 0.060 0.225 0.060 0.255 0.060 5.926"*

0.230 0.113 0.090 0,135 0,090 0.165 0.110 0.133

0.400 0.059 0.120 0.137 0.120 -0.036 0.250 0.025

0.490 0.059 0.200 0,134 0.200 0.078 0.400 0.033

0.630 3.616"* 0,260 0,089 0.250 0.094 0.490 0.007

0.750 0.176 0.400 -3.957 ** 0.400 0.051 0.580 0.042

0,850 0.231 0.490 0.080 0.490 0.049 0.650 0.179

0.900 0.298 0.580 0,157 0.580 0.086 0.750 0.404

0.960 0.162 0.640 0.500 0.650 0.289 0.830 0.477

0.750 0.317 0.750 0.086 0.900 0.558

0.870 0,420 0.890 ******** 0,960 0.362

0.930 0.349 0.930 0.390

0.960 0.193 0.960 -3.956**

CN = 0.528 0.759 0.685 0.729

179
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-41-12-000, MINF = 0.700, Camber = 5/10, ALPT = 8.12, BETA = -0.08, QINF = 299.5,

RNPU = 2.7E+06, CNWP = 0.4919

rl = 0.93 076 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.491 0.000 0.810 0.000 -6.618"* 0.010 - 1.295

0.060 -0.505 0,020 -0.979 0.020 -0.913 0.020 - 1.403

0.110 -0.600 0.040 -0.712 0.060 - 1.506 ** 0.060 - 1.408

0.200 -0.576 0.060 -1.016 0.090 -1.272 0.110 -1.531

0.230 -0.514 0,090 -1.021 0.110 -1.312 0,140 1.925"*

0.400 -0.365 0,130 - 1.050 0.130 - 1.403 0.190 -6.485" *

0.490 -0.354 0.150 - 1.243 0.150 - 1.330 0.250 -0.644

0.590 -0.411 0.200 -1.273 0.210 -1.411 0.400 -0.479

0.630 -0.459 0.250 -0.589 0.250 -0,603 0.490 -0.471

0.700 -0.572 0.260 -0.539 0.340 -0.593 0.580 -0.489

0,750 -0.746 0.280 -0.559 0.370 -0.569 0.650 -0.530

0.810 -0.776 0.290 -0.557 0.400 -0.540 0.700 -0.596

0.840 -0.779 0.310 -0.505 0.410 -0.526 0.750 -0.676

0.900 -0.274 0.320 -0.521 0.430 -0.573 0.800 -0.586

0.960 -0.192 0.340 -0,525 0.440 -0.525 0.830 -0.572

0.350 -0.162"* 0.460 -0.532 0.900 -0.217

0.370 -0.481 0.490 -0.451 0.960 -0.116

0,380 -0.482 0.500 -0.522

0.400 -0.449 0.520 -0.518

0.410 -0.490 0.540 -0.536

0.430 -0.477 0.550 -0,521

0.440 -0.428 0,580 -0,479

0.460 -0.506 0.600 -0.555

0.470 -0.494 0.610 -0,493

0.490 -0.460 0.650 -3.757**

0.500 -0.462 0.700 -0.645

0.520 -0.466 0.750 -0.673

0.530 -0.449 0.820 -0.634

0,550 -0.471 0.890 -0.186

0.560 -0.501 0.900 -0.167

0,580 -0.463 0.960 -0.174

0.590 -0.510

0.600 -0,528

0.640 -3.596"*

0.700 -0.671

0.750 -0.734

0.820 -3.770**

0,870 -0.506

0.930 -0.267

0.960 -0.195

Lower Surface

0.020 0.040 0.020 0.267 0.020 0.283 0.020 0.569**

0.110 0.034 0.060 0.295 0.060 0.332 0.060 5.557"*

0.230 0.153 0.090 0.217 0.090 0.247 0.110 0.164

0.400 0.079 0.120 0.224 0.120 0.039 0.250 0.075

0.490 0.064 0.200 0.178 0.200 0.120 0.400 0.072

0.630 3.373** 0,260 0.132 0.250 0.123 0.490 0.019

0.750 0.174 0.400 -3.787"* 0.400 0.081 0.580 0,062

0,850 0.219 0.490 0.099 0.490 0.029 0.650 0.196

0.900 0.280 0.580 0.168 0.580 0.093 0.750 0.413

0.960 0.141 0.640 0.494 0.650 0.271 0.830 0.493

0.750 0.329 0.750 0.097 0,900 0.564

0,870 0.404 0.890 ******** 0.960 0.372

0,930 0.338 0.930 0.411

0.960 0.187 0.960 -3.786 * *

CN = 0.584 0.867 0.804 0,835

180
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-41-18-500, MINF = 0,703, Camber = 5/10, ALPT = 9.29, BETA = 0,10, QINF = 306.0,

RNPU = 2.8E+06, CNWP = 0.5275

"q = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.911 0.000 0.696 0.000 -6.520"* 0.010 - 1,659

0.060 -0.809 0.020 - 1.410 0.020 - 1.387 0,020 - 1.579

0.110 -0.731 0.040 - 1.052 0.060 - i .547"* 0.060 - 1.626

0.200 -0.610 0.060 - 1,084 0.090 - 1.404 0.110 - 1.711

0.230 -0.585 0.090 -1.240 0.110 -1,516 0.140 1.893"*

0.400 -0.401 0.130 - 1.386 0.130 - 1.595 0.190 -6.390"*

0.490 -0.396 0.150 -1,472 0.150 -1,538 0.250 -0.781

0.590 -0.453 0.200 - 1.448 0.210 - 1,633 0,400 -0.489

0.630 -0.504 0.250 -0,754 0.250 -0,882 0.490 -0.479

0.700 -0.595 0.260 -0.613 0.340 -0.549 0.580 -0.481

0,750 - 1.123 0.280 -0,545 0.370 -0.535 0.650 -0.512

0.810 - 1.213 0.290 -0.518 0.400 -0.535 0.700 -0.572

0.840 - 1.197 0.310 -0,458 0.410 -0.515 0.750 -0.626

0.900 -0.317 0.320 -0,468 0.430 -0.561 0.800 -0.544

0.960 -0.250 0.340 -0.509 0.440 -0,520 0.830 -0,504

0.350 -0,128** 0.460 -0.539 0.900 -0.211

0.370 -0,470 0.490 -0.44 1 0.960 -0.1 44

0.380 -0.488 0.500 -0.538

0.400 -0.445 0,520 -0.540

0.410 -0.501 0.540 -0.551

0.430 -0.473 0.550 -0.520

0.440 -0.436 0.580 -0,503

0.460 -0.530 0.600 -0,578

0.470 -0,546 0.610 -0.509

0.490 -0.469 0.650 -3,719"*

0.500 -0.474 0.700 -0,659

0,520 -0,486 0.750 -0.675

0.530 -0,473 0.820 -0.632

0.550 -0,504 0.890 -0.155

0.560 -0.518 0.900 -0,148

0.580 -0,485 0,960 -0,145

0.590 -0.543

0.600 -0,569

0.640 -3,561"*

0.700 -0.695

0.750 -0,707

0.820 -3.731"*

0.870 -0.519

0.930 -0.372

0.960 -0,272

Lower Surface

0.020 0.1 44 0,020 0.417 0.020 0,401 0.020 0.621 **

0,110 0.085 0.060 0.373 0.060 0,404 0.060 5,399**

0.230 0.184 0.090 0.271 0.090 0.319 0.110 0.235

0.400 0.082 0.120 0.257 0,120 0,090 0.250 0.121

0.490 0.063 0.200 0.207 0,200 0.151 0.400 0.093

0,630 3.260** 0,260 0.159 0.250 0.172 0,490 0.070

0.750 0,161 0.400 -3.748"* 0.400 0,114 0.580 0,071

0.850 0.211 0,490 0.113 0.490 0,075 0.650 0.214

0,900 0.262 0.580 0.173 0.580 0,117 0.750 0.401

0,960 0.129 0.640 0.487 0,650 0.288 0,830 0.484

0.750 0.323 0.750 0.114 0.900 0.559

0.870 0.406 0.890 ******** 0.960 0.368

0.930 0.328 0,930 0.410

0.960 0.177 0.960 -3.747*"

CN = 0.709 0.950 0.877 0.901

181
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-41-26-000, MINF = 0.697, Camber = 5/10, ALPT = 10.06, BETA = -0.06, QINF = 303.2,

RNPU = 2.8E+06, CNWP = 0.5327

11= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.351 0.000 0.557 0.000 -6,603"* 0,010 - 1.739

0.060 -0.679 0.020 - 1.588 0.020 - 1.605 0.020 - 1.783

0.110 -0.752 0.040 - 1.320 0.060 - 1.685"* 0,060 -1.789

0.200 -0.650 0.060 -1.364 0.090 -l.610 0.110 -1.863

0.230 -0.617 0.090 - 1.427 0.110 - 1.667 0.140 1.951 **

0.400 -0.431 0.130 - 1.519 0.130 - 1.772 0.190 -6.472"*

0.490 -0.413 O. 150 - 1.631 O. 150 - 1.673 0.250 -0.980

0.590 -0.475 0.200 - 1.638 0.210 - 1.504 0.400 -0.461

0.630 -0.528 0.250 -0.909 0.250 - 1.050 0.490 -0.465

0.700 -0.633 0.260 -0.768 0.340 -0.657 0.580 -0.470

0.750 - 1.053 0.280 -0.687 0.370 -0.597 0.650 -0.480

0.810 - 1.151 0.290 -0.566 0,400 -0,506 0.700 -0.527

0.840 - 1.171 0.310 -0.470 0.410 -0.530 0,750 -0.555

0,900 -0,335 0,320 -0.468 0.430 -0.563 0.800 -0.502

0.960 -0.275 0,340 -0,492 0.440 -0.530 0.830 -0.453

0.350 -0.120** 0.460 -0.525 0.900 -0.203

0.370 -0,470 0.490 -0.499 0.960 -0.160

0.380 -0.474 0.500 -0.505

0.400 -0.44 1 0.520 -0,526

0.410 -0.499 0.540 -0.537

0.430 -0.472 0.550 -0.518

0.440 -0.447 0.580 -0.488

0.460 -0.527 0.600 -0.565

0.470 -0.507 0.610 -0.48 l

0.490 -0.484 0.650 -3.777**

0.500 -0.495 0.700 -0.596

0.520 -0.479 0.750 -0.627

0,530 -0.472 0.820 -0,488

0.550 -0.499 0.890 -0.184

0.560 -0.531 0.900 -0.161

0.580 -0.483 0.960 -0.160

0.590 -0.538

0.600 -0555

0.640 -3.617"*

0.700 -0.697

0.750 -0,730

0.820 -3.789**

0.870 -0.515

0.930 -0,320

0.960 -0.231

Lower Surface

0.020 0.242 0.020 0.495 0.020 0.485 0.020 0.714"*

0.110 0.134 0.060 0.429 0.060 0.472 0.060 5,423" *

0.230 0,223 0.090 0.330 0.090 0.365 0.110 0.296

0.400 0.130 0.120 0.289 0.120 0.144 0.250 0.156

0.490 0.090 0.200 0.246 0.200 0.178 0.400 0.131

0.630 3,266"* 0.260 0.197 0.250 0.214 0.490 0.090

0.750 0.158 0.400 -3.806"* 0.400 0.130 0.580 0.101

0.850 O. 195 0.490 0.136 0.490 0.077 0,650 0.221

0,900 0,256 0.580 0.193 0.580 0.140 0.750 0,428

0,960 0.110 0,640 0.499 0.650 0.312 0.830 0.498

0,750 0.336 0.750 0.119 0.900 0.571

0.870 0,415 0,890 ******** 0.960 0,358

0.930 0,339 0.930 0.418

0.960 0.190 0.960 -3.805 **

CN = 0.732 1.024 0,923 0,959

182
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-41-50-000, MINF = 0.699. Camber = 5/10, ALPT = 11.06, BETA = -0.06, QINF = 313.7,

RNPU = 2.8E+06, CNWP = 0.5325

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

Q020 - 1.500 0,000 0.465 0.000 -6.463"* 0.010 - 1.846

0.060 - 1.396 0,020 - 1.720 0.020 - 1.791 0.020 - 1.869

0.110 - 1.021 0.040 - 1.494 0.060 - 1.731 ** 0.060 - 1.888

0.200 -0.662 0,060 - 1.524 0,090 - 1.720 0.110 - 1.974

0.230 -0.634 0.090 - 1.593 0.110 - 1.791 0.140 1.861 **

0.400 -0.437 0.130 - 1.548 0.130 - 1.269 0.190 -6.336"*

0.490 -0.404 0.150 - 1,766 0.150 - 1.084 0.250 - 1.208

0.590 -0.479 0.200 - 1,759 0.210 - 1.168 0.400 -0.403

0.630 -0.541 0.250 - 1.012 0.250 - 1.041 0.490 -0.433

0.700 -0.644 0.260 -0,870 0,340 -0.936 0.580 -0.418

0.750 - 1.268 0,280 -0,811 0.370 -0,855 0.650 -0.418

0.810 - 1.307 0.290 -0.677 0.400 -0.801 0.700 -0.443

0.840 - 1.317 0.310 -0.550 0.410 -0,773 0.750 -0.478

0.900 -0.326 0.320 -0.535 0,430 -0.792 0.800 -0,422

0.960 -0.297 0.340 -0.513 0.440 -0.733 0.830 -0.377

0.350 -0.115"* 0.460 -0.703 0.900 -0.242

0.370 -0.469 0.490 -0.649 0,960 -0.232

0.380 -0.476 0.500 -0.647

0.400 -0,445 0.520 -0.625

0.410 -0.491 0.540 -0.609

0.430 -0.475 0.550 -0.591

0.440 -0.442 0.580 -0.557

0.460 -0.517 0,600 -0.588

0.470 -Q492 0,610 -0.462

0.490 -0.463 0.650 -3.731 **

0.500 -0.468 0.700 -0,475

0.520 -0.469 0.750 -0.477

0.530 -0.450 0,820 -0.393

0.550 -0.466 0.890 -0.261

0.560 -0.497 0.900 -0.267

0.580 -0.451 0.960 -0.250

0.590 -0.496

0.600 -0.507

0.640 -3.577**

0.700 -0.592

0.750 -0.714

0.820 -3.743**

0.870 -0.298

0.930 -0.168

0.960 -0.168

Lower Surface

0.020 0.297 0.020 0.531 0.020 0.545 0.020 0.761 **

0, I 10 0.158 0.060 0.463 0.060 0.517 0.060 5,162"*

0.230 0.253 0.090 0.369 0.090 0.405 0.110 0.322

0.400 0.114 0.120 0.327 0.120 0.188 0.250 0.189

0.490 0.089 0,200 0.274 0.200 0.221 0.400 O.153

0.630 3.077"* 0,260 0.231 0.250 0.252 0.490 0.089

0,750 O. 155 0.400 -3.759"* 0.400 O. 151 0.580 O, 113

0.850 O. 197 0.490 O, 148 0.490 0.090 0.650 0.229

0.900 0,253 0.580 0,195 0.580 0.152 0.750 0.430

0.960 0.103 0.640 0.504 0.650 0.328 0.830 0.497

0.750 0.333 0.750 0.128 0.900 0.568

0.870 0.417 0.890 ******** 0.960 0.351

0.930 0.333 0.930 0.405

0.960 0.178 0.960 -3.758**

CN = 0.831 1.031 0.939 0.994

183
Table D-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 8-41-58-500. MINF = 0.700, Camber = 5/10, ALPT = 11.02, BETA = 0.28, QINF = 319.4,

RNPU = 2.9E+06, CNWP = 0.5307

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.506 0.000 0.469 0.000 -6,390** 0.010 - 1.845

0.060 - 1.377 0.020 - 1.708 0.020 - 1.780 0.020 - 1.877

0.110 -0,972 0.040 - 1.502 0.060 - 1.732"* 0.060 - 1.863

0.200 -0.665 0.060 -1.528 0.090 -1.712 0.110 -1.959

0,230 -0.634 0.090 -1.586 0.110 -I .773 0.140 1.837"*

0.400 -0.446 0.130 - 1.563 0.130 - 1.260 0.190 -6.265 **

0.490 -0.430 0.150 - 1.757 0.150 - 1.098 0,250 - 1,243

0.590 -0.466 0.200 - 1.774 0.210 - 1.167 0.400 -0,378

0.630 -0.541 0,250 - 1.045 0.250 - 1.038 0,490 -0.428

0.700 -0.632 0.260 -0.895 0,340 -0.944 0.580 -0.423

0.750 - 1.219 0.280 -0.858 0.370 -0.872 0.650 -0.420

0.810 - 1.308 0.290 -0,727 0.400 -0.809 0.700 -0.457

0.840 - 1.302 0.310 -0.584 0.410 -0.790 0.750 -0.472

0.900 -0.334 0.320 -0.577 0.430 -0.810 0.800 -0.443

0.960 -0.288 0.340 -0.525 0.440 -0.752 0.830 -0.373

0.350 -0.120"* 0.460 -0.735 0.900 -0.231

0.370 -0.467 0.490 -0.640 0,960 -0.215

0,380 -0.470 0,500 -0.674

0.400 -0,426 0.520 -0.665

0.410 -0.494 0,540 -0.653

0.430 -0.491 0.550 -0.594

0.440 -0.456 0.580 -0.549

0.460 -0.521 0.600 -0.592

0.470 -0.522 0.610 -0.489

0,490 -0.472 0.650 -3.707**

0.500 -0.472 0.700 -0.449

0.520 -0.434 0.750 -0.461

0.530 -0.458 0.820 -0.384

0.550 -0.485 0.890 -0.266

0.560 -0.502 0.900 -0.293

0.580 -0.458 0.960 -0.272

0.590 -0.50l

0.600 -0.518

0.640 -3.556**

0.700 -0.591

0.750 -0.707

0.820 -3.719"*

0.870 -0.272

0.930 -0.170

0.960 -0.164

Lower Surface

0.020 0.298 0.020 0.546 0.020 0.547 0.020 0.760**

0.110 0.159 0,060 0.459 0.060 0.518 0.060 5.027"*

0.230 0.246 0.090 0.369 0.090 0.404 0.110 0.333

0,400 0.109 0.120 0.319 0.120 0.190 0.250 0.190

0.490 0,088 0.200 0.270 0.200 0.221 0.400 0.148

0.630 2.979"* 0.260 0.224 0.250 0.245 0.490 0,099

0.750 0.164 0.400 -3.735** 0,400 0.146 0.580 0.109

0.850 0.195 0.490 0.139 0.490 0.093 0.650 0.230

0.900 0.251 0.580 O.190 0.580 O.147 0.750 0.438

0.960 O, 103 0.640 0.495 0.650 0.313 0.830 0.502

0.750 0.332 0.750 O.119 0.900 0.572

0.870 0.398 0.890 ******** 0.960 0.353

0.930 0.332 0.930 0.396

0.960 O, 180 0.960 -3.734"*

CN = 0,826 1.028 0.939 0.996

184
Table D-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 8-29-13-000, MINF = 0.695, Camber = 10/10. ALPT = 7.18, BETA = 0.17, QINF = 281.4,

RNPU = 2.6E+06, CNWP = 0.5226

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.179 0.000 0.721 0.000 1.492"* 0.010 -0.419

0.060 -0.321 0.020 0, l 11 0.020 -0.059 0.020 -0.398"*

0.110 -0.657 0.040 -0,121 0,060 -0,220"* 0.060 - 1.120"*

0.200 -0.586 0.060 -0,562 0.090 -0.857 0,110 - 1.394

0.230 -0.505 0.090 -0.789 0.110 - 1.098 0.140 - 1.720

0.400 -0.330 0.130 - 1.060 0.130 - 1.462 0.190 -2.960"*

0.490 -0.288 0.150 - 1.344 0,150 - 1.588 0.250 -0.660

0.590 -0.401 0.200 - 1.487 0.210 - 1.596 0.400 -0.479

0.630 -0.441 0.250 -0.722 0.250 -0.797 0.490 -0.446

0.700 -0.583 0.260 -0.596 0.340 -0.498 0.580 -0.460

0.750 -0.760 0.280 -0.511 0.370 -0.518 0.650 -0.587

0.810 -0.696 0.290 -0.470 0.400 -0.466 0.700 -0.564

0.840 -0.773 0.310 -0.454 0.410 -0.486 0.750 -0.667

0.900 -0.263 0.320 -0.476 0.430 -0.491 0.800 -0.572

0.960 -0.152 0.340 -0.475 0.440 -0.484 0.830 -0.567

0.350 -0.149** 0.460 -0.247 0.900 -0.183

0.370 -0.481 0.490 -0.461 0.960 -0.125"*

0.380 -0.483 0.500 -0.483

0.400 -0.440 0.520 -0.473

0.410 -0.444 0.540 -0.478

0.430 -0.436 0.550 -0.470

0.440 -0.434 0.580 -0.44.4

0.460 -0.451 0.600 -0.546

0.470 -0.458 0.610 -0.564

0.490 -0.461 0.650 0.064**

0,500 -0.439 0.700 -0.639

0.520 -0.439 0.750 -0.651

0.530 -0.452 0.820 -0.321

0.550 -0,447 0.890 -0.153

0.560 -0.484 0.900 -0.137

0.580 -0,428 0.960 -0.074

0.590 -0.517

0.600 -0.497

0.640 -0.623

0.700 -0.677

0.750 0.083**

0.820 -0.493

0.870 -0.503

0.930 -0.324

0.960 -0.225

Lower Surface

0.020 -0.238 0.020 -0.031 0.020 0.024 0.020 0.203

0.110 0.053 0.060 0.216 0.060 0.255 0.060 0.088

0.230 0.086 0.090 0.166 0.090 0.270 0.1 I 0 0.214

0.400 0.128 0.120 0.220"* 0.120 0.244 0.250 0.092

0.490 0.141 0.200 0.073 0.200 0.227 0.400 0.048

0.630 4.051 ** 0.260 0.173 0.250 0.142 0.490 0.076

0,750 0.201 0.400 0.117 0.400 0.086 0.580 0.067

0.850 0.223 0.490 0.118 0.490 0.062 0.650 0.197

0.900 0.302 0.580 0.126 0.580 0.108 0.750 0.423

0.960 0.159 0.640 0.324 0.650 0.062 0.830 0.505

0.750 0.379 0.750 0.070** 0.900 0.534

0.870 0.477 0.890 0.539 0.960 0.380

0.930 0.367 0.930 0.417

0.960 0.262 0.960 0.275

CN = 0.579 0.799 0.788 0.813

185
Table D-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 8-29-16-000, MINF = 0.691, Camber = 10/10, ALPT = 8.13, BETA = 0.25, QINF = 279.8,

RNPU = 2.6E÷06, CNWP = 0.5499

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0,023 0.000 0.822 0.000 1.506"* 0.010 -0.535

0,060 -0.456 0,020 -0.114 0.020 -0.274 0.020 -0.536**

0. 110 -0.734 0.040 -0.268 0.060 -0,432** 0.060 -1.270**

0.200 -0.779 0.060 -0.718 0,090 -1,043 0.110 -1.593

0.230 -0.529 0,090 -0.909 0.110 -1.202 0,140 -1.903

0,400 -0.366 0.130 - 1.173 0.130 - 1.545 0.190 -2.995 * *

0.490 -0.343 0.150 - 1.449 0.150 - 1.638 0.250 -0.741

0,590 -0,438 0.200 - 1.589 0.210 - 1.686 0.400 -0.514

0.630 -0.479 0,250 -0,973 0.250 - 1.005 0,490 -0.470

0,700 -0.609 0.260 -0.878 0.340 -0.519 0,580 -0.487

0.750 -0.796 0,280 -0.768 0.370 -0.515 0.650 -0.566

0.810 -0,732 0.290 -0.614 0.400 -0.471 0.700 -0,554

0.840 -0.819 0.310 -0.513 0.410 -0,508 0.750 -0.626

0.900 -0.294 0.320 -0.500 0.430 -0.512 0.800 -0.517

0,960 -0.185 0.340 -0.480 0,440 -0.527 0.830 -0.495

0,350 -0.131 ** 0.460 -0.262 0,900 -0.196

0.370 -0.467 0.490 -0.523 0.960 -0.130"*

0.380 -0.497 0.500 -0.508

0.400 -0.429 0,520 -0.513

0.410 -0.459 0,540 -0.512

0,430 -0.466 0.550 -0.501

0.440 -0.458 0.580 -0,486

0.460 -0.453 0.600 -0.533

0.470 -0,476 0.610 -0.568

0,490 -0.482 0.650 0,078**

0.500 -0,473 0.700 -0.649

0.520 -0,460 0.750 -0,653

0.530 -0.468 0.820 -0,303

0,550 -0.481 0.890 -0.156

0.560 -0,508 0.900 -0.128

0.580 -0.461 0.960 -0.061

0,590 -0.546

0,600 -0.549

0.640 -0.643

0.700 -0.710

0.750 0.077**

0.820 -0,526

0.870 -0.473

0.930 -0.292

0,960 -0.228

Lower Surface

0.020 -0.080 0.020 0.124 0.020 0.139 0.020 0,359

0.110 0,088 0.060 0.272 0,060 0.311 0.060 0,086

0,230 0.105 0.090 0.230 0.090 0.315 0.110 0.235

0.400 0.I 15 0.120 0,251"* 0.120 0,275 0.250 0.119

0,490 0.116 0,200 0.106 0,200 0.248 0.400 0.077

0.630 4,056** 0.260 0.211 0.250 0.188 0.490 0.087

0.750 0.183 0.400 0.143 0,400 0.121 0.580 0,087

0.850 0.201 0.490 0.141 0,490 0.045 0,650 0.220

0.900 0,290 0,580 0.144 0,580 0.134 0.750 0.424

0,960 0.147 0.640 0,328 0.650 0.080 0,830 0.497

0,750 0.361 0.750 0.060** 0,900 0,538

0.870 0,458 0.890 0.532 0.960 0.376

0.930 0.351 0.930 0.413

0.960 0.242 0.960 0.240

CN = 0.627 0.871 0.846 0.863

186
Table D-2. Continued.

Flight 204, Wing sweep = 26", Time = 8-29-23-000, MINF = 0.694, Camber = t0/10, ALPT = 11.25, BETA = 080, QINF = 290.0,

RNPU = 2.6E+06, CNWP = 0.5207

"fl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.474 0.000 0.773 0.000 1.316"* 0.010 - 1.355

0.060 -0.888 0.020 -0.763 0.020 -0.898 0.020 -1.393"*

0.110 - 1.072 0 040 -0.662 0.060 -0.673 ** 0.060 - 1.491 **

0.200 - 1.674 0.060 - 1.116 0.090 - 1.479 0.110 - 1.873

0.230 - 1.052 0.090 - 1.401 0.110 - 1.678 0.140 - 1.935

0.400 -0.477 0.130 - 1.570 0.130 - 1.180 0,190 -2.970"*

0.490 -0.447 0.150 - 1.773 0.150 - 1.126 0.250 - 1.515

0.590 -0,514 0.200 - 1.880 0.210 - I. 101 0.400 -0.488

0.630 -0.569 0.250 - 1,272 0.250 - 1.051 0.490 -0.451

0,700 -0.672 0.260 - 1.231 0.340 -0.975 0,580 -0.396

0.750 -0.891 0.280 - 1.180 0.370 -0.957 0.650 -0.437

0.810 -0.854 0.290 - 1.108 0.400 -0.881 0.700 -0.423

0.840 -0.975 0.310 - 1.024 0.410 -0.903 0.750 -0.423

0.900 -0.402 0.320 -1.044 0.430 -0.889 0.800 -0.463

0.960 -0.251 0,340 -0.916 0.440 -0.877 0.830 -0.352

0.350 -0.303** 0.460 -0.609 0.900 -0.372

0.370 -0.782 0,490 -0.776 0.960 -0,358**

0.380 -0.761 0.500 -0.769

0.400 -0,636 0.520 -0.746

0.410 -0,598 0.540 -0.697

0.430 -0,575 0.550 -0.680

0.440 -0550 0.580 -0.657

0.460 -0.542 0.600 -0.670

0.470 -0.526 0.610 -0.631

0.490 -0.498 0650 0.128"*

0.500 -0.491 0.700 -0.568

0.520 -0.458 0.750 -0.542

0.530 -0.473 0.820 -0.200

0.550 -0.456 0.890 -0.325

0.560 -0.491 0.900 -0.324

0.580 -0.451 0.960 -0.233

0.590 -0.492

0.600 -0.475

0.640 -0.508

0.700 -0.548

0.750 0.072"*

0.820 -0.448

0.870 -0.312

0.930 -0.204

0.960 -0.192

Lower Surface

0.020 0.164 0.020 0.479 0.020 0.433 0.020 0.660

0.110 0,167 0.060 0.423 0.060 0.470 0.060 0.107

0,230 0.138 0.090 0.354 0.090 0.441 0.110 0.337

0.400 0.119 0.120 0.341"* 0.120 0.383 0.250 0.210

0.490 0.157 0.200 0,197 0.200 0,268 0.400 0.143

0.630 3.832** 0.260 0.268 0.250 0.265 0.490 0,168

0.750 0.154 0.400 0,234 0.400 0,177 0.580 0.098

0,850 0.179 0.490 0.157 0.490 0.074 0,650 0.228

0,900 0.246 0.580 0.200 0.580 0.104 0.750 0.412

0.960 0.131 0.640 0,276 0.650 0,1 04 0,830 0.517

0.750 0.342 0,750 0.074** 0.900 0,521

0.870 0.435 0.890 0.522 0.960 0,284

0.930 0.328 0.930 0.365

0.960 0.197 0.960 0.155

CN = 0.852 1.024 0.966 1.001

187
Table D-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-6-25-000, MINF = 0.702, Camber = 5/15, ALPT = 3.12, BETA = 0.25, QINF = 288.0,

RNPU = 2.6E+06, CNWP = 0.3044

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.310 0.000 0.499 0.000 5.240"* 0.010 -0.103

0.060 -0.035 0.020 O. 144 0.020 O. 153 0.020 -0.105

O. 1 I0 -0.222 0.040 0.024 0.060 -3.690"* 0.060 -0.402

0.200 -0.280 0.060 -0.195 0.090 -0.385 O. 110 -0.603

0.230 -0.249 0.090 -0.304 O. 110 -0.542 O. 140 -0.575

0.400 -0.245 0.130 -0.447 0.130 -0.627 0.190 -2.895"*

0.490 -0.234 0.150 -0.544 0.150 -0.515 0.250 -0.374

0.590 -0.359 0.200 -0.425 0.210 -0.483 0.400 -0.387

0.630 -0.391 0.250 -0.388 0.250 -0.374 0.490 -0.352

0.700 -0.548 0.260 -0.347 0.340 -0.409 0.580 -0.371

0.750 -0.704 0.280 -0.379 0.370 -0.423 0.650 -0.537

0.810 -0.661 0.290 -0.364 0.400 -0.396 0.700 -0.540

0.840 -0.687 0.310 -0.354 0.410 -0.926** 0.750 -0.678

0.900 -0.279 0.320 -0.364 0.430 -0.419 0.800 -0.782"*

0.960 -0.294 0.340 -0.372 0.440 -0.391 0.830 -0.589

0.350 -0.220** 0.460 -0.409 0.900 -0.458

0.370 -0.317 0.490 -0.334 0.960 -0,457

0.380 -0.377 0.500 -0.428

0.400 -0.022 0.520 -0.435

0.410 -0.366 0.540 -0.424

0.430 -0.361 0.550 -0.382

0.440 -0.320 0.580 -0.385

0.460 -0.380 0.600 -0.482

0.470 -0.376 0.610 -0.488

0.490 -0.374 0.650 3.813"*

0.500 -0.388 0.700 -0.627

0.520 -0.394 0.750 -0.681

0.530 -0.387 0.820 -0.612"*

0.550 -0.440 0.890 -0.347

0.560 -0.442 0.900 -0.380

0.580 -0.405 0.960 -0.362

0.590 -0.487

0.600 -0.462

0.640 -0.583

0.700 -0.649

0.750 -0.016"*

0.820 -0.631

0.870 -0.403

0.930 -0.319

0.960 -0.321

Lower Surface

0.020 -0.566 0.020 -0.542 0.020 -0.397 0.020 -0.233

0. 110 -0.128 0.060 -0.114 0.060 -0.048 0.060 2.341 **

0.230 -0.030 0.090 -0.093 0.090 2.351 ** 0.1 I0 0.030

0.400 0.073 0.120 -0.039 0.120 -0.160 0.250 -0.124

0.490 0.121 0.200 -0.030 0.200 -0.016 0.400 -0.070

0.630 2.404** 0.260 0.016 0.250 -0.039 0.490 -0.024

0.750 0.265 0.400 0.050 0.400 -0.010 0.580 0.044

0.850 0.314 0.490 0.060 0.490 0.004 0.650 0.268

0.900 0.384 0.580 0.158 0.580 0.132 0.750 0.414

0.960 0.211 0.640 0.348 0.650 -0.025 0.830 0.529

0.750 0.418 0.750 0.005 0.900 0.573

0.870 0.498 0.890 0.508 0.960 0.393

0.930 0.405 0.930 0.429

0.960 0.254 0.960 -0.599"*

CN = 0.439 0.568 0.490 0.582

188
Table D-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-6-40-000, MINF = 0.702, Camber = 5/16, ALPT = 4.04, BETA = -0.21, QINF = 288.1,

RNPU = 2.6E+06, CNWP = 0.3618

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.218 0.000 0.650 0.000 5.232 * * 0.010 -0.334

0.060 -0.085 0.020 0.053 0.020 -0.021 0.020 -0.270

0.110 -0.298 0.040 -0,082 0.060 -3.696** 0.060 -0.535

0.200 -0.337 0.060 -0.315 0.090 -0.491 0.110 -0.702

0.230 -0.433 0.090 -0.397 0.110 -0.641 0.140 -0.659

0.400 -0.245 0.130 -0.554 0.130 -0.754 0.190 -2.902"*

0.490 -0.275 0.150 -0.630 0.150 -0.603 0.250 -0.394

0,590 -0.383 0.200 -0.499 0.210 -0.571 0.400 -0.414

0.630 -0.410 0.250 -0.417 0,250 -0.418 0.490 -0.383

0,700 -0.567 0.260 -0.403 0.340 -0.448 0.580 -0.363

0.750 -0.689 0.280 -0.410 0.370 -0.439 0.650 -0.571

0.810 -0.638 0.290 -0.416 0.400 -0.403 0.700 -0.564

0.840 -0.671 0.310 -0.399 0.410 -0.932** 0.750 -0.684

0.900 -0.318 0.320 -0.396 0.430 -0.457 0.800 -0.803**

0.960 -0.315 0.340 -0.398 0.440 -0.425 0.830 -0.581

0.350 -0.213** 0.460 -0.441 0.900 -0.450

0.370 -0.358 0.490 -0.435 0.960 -0.466

0.380 -0.417 0.500 -0.459

0.400 -0.025 0.520 -0.455

0.410 -0.402 0,540 -0.466

0.430 -0.373 0.550 -0.412

0.440 -0.354 0.580 -0.398

0.460 -0.394 0.600 -0.484

0.470 -0.374 0,610 -0.493

0.490 -0.387 0.650 3.805"*

0.500 -0.399 0.700 -0.641

0.520 -0.403 0.750 -0.696

0.530 -0.397 0.820 -0.591 **

0.550 -0.445 0.890 -0.360

0.560 -0.450 0.900 -0.382

0.580 -0.425 0.960 -0.365

0.590 -0.496

0.600 -0.484

0.640 -0.606

0.700 -0.663

0.750 -0.001 **

0,820 -0.631

0.870 -0.433

0.930 -0.356

0.960 -0.347

Lower Surface

0.020 -0.392 0.020 -0.370 0.020 -0.226 0.020 -0.017

0.110 -0.092 0.060 -0.032 0.060 0,043 0.060 2.334" *

0.230 0.010 0.090 -0.036 0.090 2.343 ** 0.110 0.028

0.400 0.070 0.120 0.015 0.120 -0.107 0.250 -0.085

0.490 0.132 0.200 0.012 0.200 0.006 0.400 -0.024

0.630 2.396"* 0,260 0.016 0.250 0,007 0.490 0.000

0.750 0.257 0.400 0.062 0.400 0.008 0.580 0.058

0.850 0.310 0.490 0.091 0.490 0.013 0.650 0.269

0.900 0.387 0.580 0.167 0,580 0.156 0.750 0.422

0.960 0.189 0.640 0.379 0.650 -0.040 0.830 0.552

0.750 0.435 0.750 0.024 0.900 0.581

0.870 0.516 0.890 0.535 0.960 0.410

0.930 0.409 0.930 0.460

0.960 0.262 0.960 -0,605"*

CN = 0.487 0.628 0.552 0.632

189
Table D-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-6-42-000, MINF = 0.704, Camber = 5/16, ALPT = 5.16, BETA = -0.07, QINF = 289.9,

RNPU = 2.6E+06, CNWP = 0.3858

rl = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.067 0.000 0.773 0.000 5.199** 0.010 -0.679

0.060 -0.14.4 0,020 -0.164 0,020 -0.245 0.020 -0.485

0. I 10 -0.405 0.040 -0.260 0.060 -3.675 * * 0.060 -0.739

0.200 -0.402 0.060 -0.507 0.090 -0.651 0.110 -0.861

0.230 -0.316 0.090 -0.557 0.110 -0.825 0.140 -0.841

0.400 -0.291 0.130 -0.707 0.130 -0.995 0.190 -2.885"*

0,490 -0.282 0.150 -0.786 0.150 -0.731 0,250 -0.509

0.590 -0.410 0.200 -0.614 0.210 -0.674 0.400 -0.456

0.630 -0.433 0.250 -0.508 0.250 -0.492 0,490 -0.411

0.700 -0.584 0.260 -0.465 0.340 -0.508 0.580 -0.426

0.750 -0.665 0.280 -0.480 0.370 -0.510 0,650 -0.600

0.810 -0.665 0.290 -0.462 0.400 -0.470 0.700 -0.578

0.840 -0.653 0.310 -0.454 0.410 -0,928"* 0.750 -0.703

0.900 -0.356 0,320 -0.459 0.430 -0.502 0.800 -0.784**

0.960 -0.365 0.340 -0.453 0.440 -0.477 0,830 -0,597

0.350 -0.219"* 0.460 -0.485 0.900 -0.485

0.370 -0.406 0.490 -0.426 0,960 -0.481

0.380 -0.467 0.500 -0.486

0.400 -0.060 0.520 -0.497

0.410 -0.444 0.540 -0.492

0.430 -0.420 0.550 -0.449

0.440 -0.388 0.580 -0.433

0.460 -0.442 0.600 -0.531

0.470 -0.453 0.610 -0.532

0.490 -0.423 0.650 3.781 **

0.500 -0.437 0.700 -0.661

0.520 -0.490 0.750 -0.719

0,530 -0,436 0.820 -0.575**

0,550 -0.434 0.899 -0,379

0.560 -0.487 0.900 -0.397

0.580 -0.451 0.960 -0.382

0.590 -0.531

0.600 -0.508

0.640 -0.634

0,700 -0.687

0.750 -0.009**

0.820 -0.640

0.870 -0.379

0.930 -0.340

0.960 -0.354

Lower Surface

0.020 -0.312 0.020 -0.173 0.020 -0.001 0.020 0.174

0.110 -0.059 0.060 0.061 0.060 0.137 0.060 2.318" *

0.230 0.032 0.090 0.032 0,090 2.328"* 0,110 0.068

0,400 0.068 0.120 0.105 0.120 -0.045 0,250 -0.045

0,490 0.134 0.200 0.037 0.200 0.033 0,400 -0.002

0.630 2.380** 0.260 0.060 0.250 0.040 0.490 0.014

0.750 0.246 0.400 0.076 0.400 0.043 0.580 0.061

0.850 0.291 0.490 0.093 0,490 0,019 0.650 0.274

0.900 0.372 0,580 0.168 0,580 0.161 0.750 0.444

0.960 0.152 0.640 0.368 0.650 -0.025 0,830 0.557

0250 0.423 0.750 0.027 0.900 0.583

0.870 0.502 0.890 0.535 0.960 0.401

0.930 0.402 0.930 0.448

0.960 0.252 0.960 -0.603**

CN = 0.507 0.698 0.630 0.721

190
TabLe D-2. Continued,

Flight 223, Wing sweep = 26 °, Time = 10-6-44-500, MINF = 0.705, Camber = 5/16, ALPT = 6,08, BETA = -0.27, QINF = 290.5,

RNPU = 2.6E+06, CNWP = 0.4093

rl = 093 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0,111 0.000 0.835 0,000 5.190"* 0.010 -1.063

0.060 -0.345 0.020 -0.434 0.020 -0.521 0.020 -0.632

0.110 -0.496 0.040 -0.433 0.060 - 3.664 ** 0.060 - 1.026

0.200 -0.463 0.060 -0.663 0.090 -0.787 0.110 -0.917

0.230 -0.427 0.090 -0.704 0.110 -0.968 0.140 - 1.332

0.400 -0,319 0.130 -0.864 0.130 - 1.109 0.190 -2.875"*

0.490 -0,321 0.150 - 1,007 0.150 - 1,151 0.250 -0.533

0.590 -0.422 0.200 -0.688 0.210 -0.708 0.400 -0.481

0,630 -0.449 0.250 -0,543 0.250 -0.541 0.490 -0.446

0.700 -0.591 0.260 -0.518 0.340 -0.536 0.580 -0,444

0.750 -0.685 0,280 -0.530 0.370 -0.539 0.650 -0.607

0.810 -0,601 0.290 -0.521 0.400 -0.497 0.700 -0.595

0.840 -0.633 0.310 -0.499 0.410 -0.923** 0.750 -0.714

0.900 -0.388 0.320 -0.501 0.430 -0.529 0.800 -0.758**

0.960 -0.405 0,340 -0.476 0.440 -0.505 0.830 -0.593

0.350 -0,226"* 0.460 -0,515 0.900 -0.444

0.370 -0.444 0.490 -0.422 0.960 -0,452

0.380 -0.486 0.500 -0.511

0.400 -0.057 0.520 -0,511

0.410 -0.480 0,540 -0.516

0,430 -0.452 0.550 -0.464

0,440 -0.413 0.580 -0.447

0.460 -0.447 0.600 -0.537

0.470 -0,456 0.610 -0.556

0.490 -0.452 0.650 3.775**

0.500 -0.461 0.700 -0.699

0.520 -0,478 0.750 -0.722

0.530 -0.454 0.820 -0.571 **

0.550 -0.495 0.890 -0.388

0.560 -0.515 0.900 -0.42 I

0.580 -0.481 0.960 -0.411

0.590 -0,545

0.600 -0.519

0.640 -0.647

0.700 -0.701

0,750 0.001"*

0.820 -0.628

0.870 -0.398

0.930 -0.371

0.960 -0.361

Lower Surface

0.020 -0,239 0.020 0.003 Q020 0.083 0.020 0.360

0.110 -0.015 0.060 0.133 0.060 0,207 0.060 2.316" *

0.230 0.066 0.090 0.092 0.090 2.325** 0.110 0.113

0.400 0.090 0.120 0.11 l 0.120 0,020 0.250 -0.001

0.490 0,118 0.200 0.070 0.200 0,063 0.400 0.020

0.630 2,378** 0.260 0.092 0250 0.077 0.490 0.048

0,750 0.241 0.400 0.110 0.400 0.056 0.580 0.079

0.850 0.286 0,490 0.123 0.490 0.022 0,650 0.283

0.900 0.357 0.580 0.171 0,580 0,179 0.750 0.461

0.960 0.150 0.640 0.378 0.650 -0.015 0.830 0.558

0.750 0.433 0.750 0.045 0.900 0.593

0.870 0.504 0,890 0.544 0.960 0.403

0.930 0.381 0.930 0.450

0,960 0.246 0.960 -0,599**

CN = 0.558 0.767 0.701 0.809

191
Table D-2. Continued.

Flight 223, Wing sweep = 26", Time = 10-6-48-000, MINF = 0.703, Camber = 5/16, ALPT = 7.02, BETA = -0.21, QINF = 288.2,

RNPU = 2.6E+06, CNWP = 0.4371

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0.312 0.000 0.817 0.000 5.240** 0.010 - 1.287

0.060 -0.393 0.020 -0.651 0.020 -0.726 0.020 - 1.243

0. I I0 -0.573 0.040 -0.590 0.060 -3.685 ** 0.060 - 1.146

0.200 -0.496 0.060 -0.806 0.090 -0.987 0.110 - 1.065

0.230 -0.436 0.090 -0.812 0.110 -0.981 0.140 - 1.335

0.400 -0.329 0.130 -0.997 0.130 - 1.184 0.190 -2.891 **

0.490 -0.323 0.150 - 1.182 0.150 - 1.251 0.250 -0.587

0.590 -0.426 0.200 - 1.117 0.210 -0.951 0.400 -0.521

0.630 -0.457 0.250 -0.590 0.250 -0.560 0.490 -0.455

0.700 -0.596 0.260 -0.556 0.340 -0.564 0.580 -0.457

0.750 -0.692 0.280 -0.572 0.370 -0.569 0.650 -0.631

0.810 -0.642 0.290 -0.529 0.400 -0.524 0.700 -0.620

0.840 -0.677 0.310 -0.520 0.410 -0.922"* 0.750 -0.757

0.900 -0.421 0.320 -0.523 0.430 -0.572 0.800 -0.741 **

0.960 -0.437 0.340 -0.514 0.440 -0.533 0.830 -0.612

0.350 -0.205"* 0.460 -0.531 0.900 -0.462

0.370 -0.462 0.490 -0.465 0.960 -0.44 1

0.380 -0.525 0.500 -0.551

0.400 -0.023 0.520 -0.527

0.410 -0.497 0.540 -0.525

0.430 -0.462 0.550 -0.477

0.440 -0.431 0.580 -0.473

0.460 -0.480 0.600 -0.574

0.470 -0.477 0.610 -0.581

0.490 -0.476 0.650 3.814"*

0.500 -0.470 0.700 -0.681

0.520 -0.515 0.750 -0.728

0.530 -0.460 0.820 -0.557**

0.550 -0.476 0.890 -0.380

0.560 -0.522 0.900 -0.385

0.580 -0.483 0.960 -0.380

0.590 -0.558

0.600 -0.536

0.640 -0.653

0.700 -0.699

0.750 0.024**

0.820 -0.610

0.870 -0.370

0.930 -0.358

0.960 -0.364

Lower Surlhce

0.020 -0.034 0.020 0.143 0.020 0.277 0.020 0.439

0.110 0.021 0.060 0.232 0.060 0.287 0.060 2.343 **

0.230 0.121 0.090 0.171 0.090 2.352** 0.110 0.179

0.400 0.091 0.120 0.207 0.120 0.079 0.250 0.046

0.490 0.153 0.200 0.124 0.200 0.115 0.400 0.047

0.630 2.405"* 0.260 0.124 0.250 0.131 0.490 0.072

0.750 0.246 0.400 0.130 0.400 0.100 0.580 0.114

0.850 0.287 0.490 O. 121 0.490 0.045 0.650 0.309

0.900 0.358 0.580 0.196 0.580 0.188 0.750 0.472

0.960 0.140 0.640 0.388 0.650 0.001 0.830 0.571

0.750 0.443 0.750 0.038 0.900 0.615

0.870 0.522 0.890 0.556 0.960 0.408

0.930 0.404 0.930 0.462

0.960 0.256 0.960 -0.595**

CN = 0.599 0.848 0.774 0.890

192
Table D-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-6-54-000, MINF = 0.702, Camber = 5/15, ALPT = 7.98, BETA = -0.21, QINF = 286.1,

RNPU = 2.6E+06, CNWP = 0.5183

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.647 0.000 0.719 0.000 5.288 ** 0.010 - 1.254

0.060 -0.612 0.020 - 1.024 0.020 - 1,223 0.020 - 1.417

0.1 I 0 -0.676 0.040 -0.790 0.060 -3,703 ** 0.060 - 1.392

0.200 -0.569 0.060 - 1.062 0.090 - 1.269 0.110 - 1.515

0.230 -0.537 0.090 - 1.125 0.110 - 1.362 0.140 - 1.694

0.400 -0,369 0.130 - 1.207 0.130 - 1.443 0.190 -2.902 **

0.490 -0.343 0.150 - 1.270 0.150 - 1.453 0.250 -0.626

0.590 -0.464 0.200 - 1.288 0.210 - 1.454 0.400 -0,536

0.630 -0.499 0.250 -0.598 0.250 -0.600 0.490 -0,489

0.700 -0.631 0,260 -0,550 0.340 -0.590 0.580 -0.484

0.750 -0.753 0,280 -0.579 0.370 -0.580 0,650 -0.647

0.810 -0.698 0.290 -0.560 0.400 -0.541 0.700 -0.648

0.840 -0.750 0.310 -0.551 0.410 -0.919"* 0.750 -0.776

0.900 -0.485 0.320 -0,550 0.430 -0.583 0.800 -0.689*"

0.960 -0.498 0.340 -0.544 0,440 -0.556 0.830 -0.607

0.350 -0.208** 0.460 -0.566 0.900 -0.333

0.370 -0.495 0,490 -0.427 0.960 -0.290

0.380 -0.563 0,500 -0.575

0.400 0.067 0.520 -0.556

0.410 -0.532 0.540 -0.562

0.430 -0.499 0.550 -0.509

0.440 -0.463 0.580 -0.495

0.460 -0.512 0.600 -0.59 I

0.470 -0.512 0.610 -0.602

0.490 " -0.492 0.650 3.851"*

0.500 -0.498 0.700 -0.769

0.520 -0.501 0.750 -0.763

0530 -0.495 0.820 -0.573**

0.550 -0.546 0.890 -0.369

0.560 -0.562 0.900 -0.384

0.580 -0.533 0.960 -0.351

0.590 -0.595

0.600 -0,566

0.640 -0.679

0.700 -0.725

0.750 0.023**

0820 -0.632

0.870 -0.352

0.930 -0.351

0.960 -0.357

Lower Surface

0.020 0.080 0.020 0297 0.020 0.378 0.020 0.578

0.110 0.074 0.060 0.294 0.060 0.368 0.060 2.369"*

0.230 0.155 0.090 0.230 0D90 2.379** 0.110 0.253

0.400 0.148 0.120 0.226 0.120 0.143 0.250 0.091

0.490 0.156 0.200 0.158 0.200 0.139 0.400 0.102

0.630 2.432** 0.260 0.172 0.250 0.172 0.490 0.097

0.750 0.217 0.400 0.145 0.400 0,126 0.580 0.135

0.850 0.271 0.490 0.150 0.490 0.047 0.650 0.305

0.900 0.344 0.580 0.202 0.580 0.207 0.750 0.480

0.960 0.120 0.640 0.393 0.650 0.003 0.830 0.595

0.750 0.464 0.750 0.071 0.900 0.623

0.870 0.506 0.890 0.555 0.960 0.429

0.930 0.397 0.930 0.459

0.960 0.249 0.960 -0.590**

CN = 0.676 0.929 0.877 0.982

193
Table D-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-6-58-500, MINF = 0,706, Camber = 5/15, ALPT = 9.99, BETA = 0.19, QINF = 292.3,

RNPU = 2.6E+06. CNWP = 0.6355

_q= 0.93 0.76 0.59 0.40

Upper Surface

.r./c CP x/c CP x/c CP x/c CP

0,020 -1.386 0.000 0.497 0,000 5.152"* 0.010 -1.623

0,060 - 1.078 0,020 - 1.601 0,020 - 1.615 0.020 - 1.685

0.110 -0.982 0,040 - 1.362 0.060 -3.646** 0,060 - 1.646

0.200 -1.301 0,060 -1.398 0.090 -1,561 0.110 -1.742

0.230 -0,578 0.090 - 1.423 0.110 - 1.654 0.140 - 1.909

0,400 -0.454 0.130 - 1.507 0.130 - 1.729 0.190 -2.863"*

0,490 -0.437 0.150 - 1.607 0.150 - 1,701 0.250 - 1.214

0,590 -0.538 0.200 - 1.615 0.210 - 1.562 0.400 -0.488

0.630 -0.568 0,250 - 1.174 0.250 - 1.065 0.490 -0.436

0.700 -0.675 0.260 -0.975 0,340 -0.956 0.580 -0.451

0,750 -0.829 0.280 -0,955 0.370 -0.875 0.650 -0.600

0.810 -0,822 0.290 -0.883 0,400 -0.780 0.700 -0.600

0.840 -0,828 0.310 -0.805 0.410 -0,922** 0,750 -0.655

0,900 -0.632 0.320 -0.756 0.430 -0.733 0.800 -0,570**

0,960 -0,657 0.340 -0.664 0.440 -0,680 0,830 -0.534

0.350 -0.225** 0.460 -0,662 0.900 -0.313

0.370 -0.484 0.490 -0.550 0.960 -0.295

0.380 -0.519 0.500 -0.627

0.400 -0,024 0,520 -0,625

0,410 -0,488 0.540 -0.611

0,430 -0,465 0.550 -0.55 I

0,440 -0,450 0.580 -0.551

0,460 -0,490 0,600 -0.623

0.470 -0.518 0.610 -0,594

0,490 -0,491 0.650 3.746 * *

0.500 -0.521 0.700 -0,722

0.520 -0492 0.750 -0,765

0.530 -0.513 0.820 -0.526**

0,550 -0.549 0,890 -0.335

0.560 -0.578 0.900 -0,304

0.580 -0,554 0,960 -0.271

0.590 -0.610

0,600 -0,547

0,640 -0.712

0.700 -0,773

0.750 0,037**

0,820 -0.584

0,870 -0.381

0,930 -0,310

0.960 -0,301

Lower Surface

0.020 0.153 0_020 0.511 0.020 0.552 0,020 0.712

0. I 10 0.149 0.060 0.418 0.060 0,477 0.060 2.296"*

0.230 0.221 0.090 0,338 0.090 2.306"* 0.110 0,354

0,400 0.133 0.120 0.349 0,120 0.237 0.250 0.169

0,490 0.168 0,200 0.229 0.200 0.221 0,400 0.156

0.630 2.358"* 0,260 0,236 0,250 0.259 0.490 0.156

0.750 0.227 0,400 0.191 0,400 0.181 0.580 0.175

0.850 0.252 0,490 0,200 0.490 0.047 0.650 0.344

0,900 0.315 0.580 0.225 0.580 0.263 0.750 0.507

0.960 0,085 0.640 0.407 0,650 0.018 0.830 0.609

0,750 0.451 0,750 0.092 0.900 0.638

0.870 0.518 0.890 0,573 0.960 0.443

0.930 0.396 0.930 0.479

0,960 0,255 0,960 -0.600"*

CN = 0,853 1.094 1.040 1.113

194
Table D-2, Continued.

Flight 223, Wing sweep = 26 °, Time = 10-7-4-000, MINF = 0.703, Camber = 5/16, ALP'I" = 11.03, BETA = -0,10, QINF = 295.0,

RNPU = 2.7E+06, CNWP = 0.6281

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 - 1,556 0.000 0,386 0.000 5.051 ** 0.010 - 1.716

0.060 - 1.363 0,020 - 1.856 0.020 - 1,735 0.020 - 1,819

0.1 l0 - 1.117 0,040 - 1.552 0,060 -3.668"* 0.060 - 1.818

0.200 -0.753 0.060 - 1.570 0.090 - 1,697 0.110 - 1,866

0.230 -0.553 0.090 - 1,557 0,110 - 1.770 0.140 - 1.890

0.400 -0.469 0.130 -1.617 0,130 -1.538 0,190 -2.891"*

0,490 -0.439 0.150 -1.729 0,150 -1.196 0.250 -1.285

0.590 -0,548 0.200 - 1.731 0.210 - 1.170 0.400 -0.400

0.630 -0.579 0.250 - 1,067 0.250 - 1.061 0.490 -0.413

0,700 -0.680 0.260 -0.981 0.340 - 1,035 0.580 -0.427

0.750 -0.897 0.280 -0.953 0.370 -0.975 0.650 -0.513

0.810 -0,816 0.290 -0.864 0.400 -0.881 0,700 -0.502

0.840 -0.865 0.310 -0.785 0.410 -0.968** 0,750 -0.533

0,900 -0.688 0,320 -0,712 0.430 -0.905 0.800 -0,524"*

0.960 -0.736 0,340 -0.680 0.440 -0.853 0.830 -0,473

0.350 -0.219** 0,460 -0.839 0,900 -0.336

0,370 -0,557 0.490 -0,755 0.960 -0,305

0.380 -0,611 0.500 -0.802

0.400 -0,082 0.520 -0.788

0.410 -0.565 0.540 -0.752

0.430 -0.535 0.550 -0.676

0.440 -0.491 0.580 -0.633

0.460 -0.539 0.600 -0.690

0.470 -0,540 0.610 -0.638

0.490 -0.511 0.650 3.658" *

0.500 -0.518 0.700 -0.606

0.520 -0.515 0.750 -0.611

0.530 -0.514 0.820 -0.488**

0.550 -0.552 0.890 -0.418

0,560 -0,565 0.900 -0.400

0.580 -0.536 0,960 -0.341

0.590 -0.584

0,600 -0.567

0.640 -0.630

0.700 -0,694

0.750 0.057**

0.820 -0.441

0,870 -0.265

0.930 -0,299

0.960 -0.301

Lower Surface

0.020 0.327 0.020 0.597 0.020 0.614 0,020 0.751

0.110 0.181 0.060 0.488 0.060 0,519 0.060 2,221 **

0.230 0,258 0.090 0,372 0.090 2.230** 0.110 0.411

0.400 0,151 0.120 0.343 0.120 0,285 0.250 0.207

0.490 O. 194 0.200 0.262 0.200 0.287 0.400 O.190

0.630 2,282"* 0.260 0.268 0.250 0,284 0.490 0.174

0,750 0.237 0.400 0.217 0.400 0.209 0.580 0,183

0.850 0.258 0.490 0.203 0.490 0.066 0.650 0,361

0.900 0.318 0,580 0.242 0,580 0.269 0.750 0.518

0.960 0.095 0.640 0,419 0.650 0,023 0.830 0.609

0.750 0.459 0,750 0.103 0.900 0.646

0,870 0.514 0,890 0.587 0,960 0.432

0.930 0.405 0,930 0.487

0.960 0,261 0.960 -0.649"*

CN = 0.883 1.116 1.057 1.124

195
Table D-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-7-12-500, MINF = 0.693, Camber = 5/16, ALPT = 11.95, BETA = -0.56, QINF = 296.7,

RNPU = 23E+06, CNWP = 0.6443

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 - 1.821 0.000 O. 183 0.000 4.925 ** 0.010 - 1.989

0.060 - 1.696 0.020 -2.007 0.020 - 1.927 0.020 -2.060

0.110 - 1.376 0.040 -1.790 0.060 -3.744** 0.060 - 1.985

0.200 -0.726 0.060 - 1.805 0.090 - 1.706 0.110 -2.022

0.230 -0.652 0.090 - 1.722 0.110 - 1.342 0.140 - 1,672

0.400 -0.497 0.130 - 1.602 0.130 - 1.227 0.190 -2.972 * *

0.490 -0.475 0.150 -1.281 0.150 -1.164 0.250 -1.387

0.590 -0.550 0.200 - 1.220 0.210 - 1.148 0.400 -0.484

0.630 -0.592 0.250 - 1.056 0.250 - 1.042 0.490 -0.447

0.700 -0.700 0.260 -0,929 0.340 - 1.037 0.580 -0.396

0.750 - 1.011 0.280 -0.930 0.370 -0.986 0.650 -0.488

0.810 -0.914 0.290 -0.842 0.400 -0.936 0.700 -0.502

0.840 - 1.047 0.310 -0.782 0.410 - 1.060"* 0.750 -0.484

0.900 -0.695 0.320 -0.766 0.430 -0.939 0.800 -0.536"*

0.960 -0.633 0.340 -0.739 0.440 -0.878 0.830 -0.470

0.350 -0.275"* 0.460 -0.870 0.900 -0.424

0.370 -0.654 0.490 -0.836 0.960 -0.418

0.380 -0.718 0.500 -0.844

0.400 -0.179 0.520 -0.827

0.410 -0.731 0.540 -0.811

0.430 -0.658 0.550 -0.743

0.440 -0.645 0.580 -0.709

0.460 -0.628 0.600 -0.755

0.470 -0.624 0.610 -0.711

0.490 -0.605 0.650 3.540* *

0.500 -0.607 0.700 -0.649

0.520 -0.513 0.750 -0,676

0.530 -0.580 0.820 -0.566**

0.550 -0.594 0.890 -0.424

0.560 -0.633 0.900 -0.425

0.580 -0.575 0.960 -0.352

0.590 -0.639

0.600 -0.607

0.640 -0.568

0.700 -0.585

0.750 0.048**

0.820 -0.318

0.870 -0.313

0.930 -0.362

0.960 -0.352

Lower Surface

0.020 0.432 0.020 0.666 0.020 0.665 0.020 0.783

0.110 0.205 0.060 0.495 0.060 0.554 0.060 2.111 **

0.230 0.263 0.090 0.403 0.090 2.120** 0.110 0.462

0.400 0, l 31 0.120 0.362 0.120 0.318 0.250 0.243

0.490 0.139 0.200 0.270 0.200 0.256 0.400 0.213

0.630 2.171 ** 0.260 0.283 0.250 0.303 0.490 0.187

0.750 0.227 0.400 0.226 0.400 0.209 0.580 0.198

0.850 0.244 0.490 0.205 0.490 0.090 0.650 0.358

0.900 0.300 0.580 0.240 0.580 0.270 0.750 0.511

0.960 0.086 0.640 0.412 0,650 0.029 0.830 0.626

0.750 0.447 0.750 0.102 0.900 0.634

0.870 0.512 0.890 0.568 0.960 0.417

0.930 0.383 0.930 0.476

0.960 0.243 0.960 -0.743**

CN = 0.940 1.097 1,091 1.176

196
Table D-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 8-30-51-000, MINF = 0.692, Camber = 5/15, ALPT = 3.04, BETA = -0.24, QINF = 282.6,

RNPU = 2.6E+06, CNWP = 0.3626

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.319 0.000 0.455 0.000 1.299"* 0.010 -0.203

0.060 -0.067 0.020 0.175 0,020 0.150 0.020 -0.107 **

0.110 -0222 0.040 0.138 0.060 -0.018"* 0.060 -0.508**

0.200 -0,296 0.060 -0.137 0.090 -0A20 0.110 -0.632

0.230 -O344 0.090 -0.277 0.110 -0.502 0.140 -0.579

0400 -0.221 0.130 -0.397 0.130 -0.684 0.190 -2.983 **

0.490 -0.229 0.150 -0.454 0.150 -0,566 0.250 -0.395

0.590 -0.423 0.200 -0.441 0.210 -0.472 0.400 -0.349

0.630 -0.410 0.250 -0.425 0.250 -0.390 0.490 -0.430

0.700 -0.562 0.260 -0,345 0.340 -0.372 0.580 -0.477

0.750 -0.779 0.280 -0,344 0.370 -0.463 0.650 -0.524

0.810 -0.621 0.290 -0.344 0.400 -0.381 0.700 -0.588

0.840 -0.703 0.310 -0.326 0.410 -0.389 0.750 -0.768

0.900 -0.346 0.320 -0.406 0.430 -0.397 0.800 -0.858

0.960 -0.323 0.340 -0.341 0.440 -0.401 0.830 -0.681

0.350 -0.168"* 0.460 -0.216 0.900 -0.499

0.370 -0.405 0.490 -0.428 0.960 -0.507**

0.380 -0.365 0.500 -0.448

0.400 -0.384 0.520 -0.460

0.410 -0.405 0.540 -0.395

0.430 -0.396 0.550 -0.397

0.440 -0.404 0.580 -0.428

0.460 -0.404 0.600 -0.457

0.470 -0.352 0.610 -0.542

0.490 -0.361 0.650 0.068**

0.500 -0.357 0.700 -0.614

0.520 -0.350 0.750 -0.630

0.530 -0.357 0.820 -0.334

0.550 -0.446 0.890 -0.403

0.560 -0.397 0.900 -0.419

0.580 -0.445 0.960 -0.390

0.590 -0.518

0.600 -0.513

0.640 -0.654

0.700 -0.648

0.750 0.013"*

0.820 -0.699

0.870 -0.439

0.930 -0.388

0.960 -0.310

Lower Surface

0,020 -0.608 0.020 -0.585 0.020 -0.409 0.020 -0.281

0,110 -0.107 0.060 -0.164 0.060 -0.135 0.060 0.052

0.230 -0.059 0.090 -0.145 0.090 -0.082 0.110 -0.141

0.400 0,015 0.120 -0.006"* 0.120 -0.063 0.250 -0.099

0.490 0.059 0.200 0.014 0.200 0.080 0.400 -0.042

0.630 3.997"* 0.260 0.022 0.250 -0.011 0.490 -0.064

0.750 0.226 0.400 -0.005 0.400 0.039 0.580 0.079

0,850 0.252 0,490 0.117 0.490 -0.004 0.650 0.202

0.900 0.336 0,580 0.105 0.580 0.157 0,750 0.467

0.960 0.143 0,640 0.395 0.650 0.064 0.830 0453

0.750 0,429 0.750 0.049** 0.900 0.536

0,870 0.533 0.890 0.586 0.960 0.365

0.930 0.357 0.930 0.405

0.960 0.2 l5 0.960 0.219

CN = 0.425 0.576 0.556 0.595

197
Table D-2. Continued.

Flight 204, Wing sweep = 26", Time = 8-30-57-500, MINF = 0.697, Camber = 5/15. ALPT = 5.04, BETA = -0.12. QINF = 284.6,

RNPU = 2.6E+06, CNWP = 0.4324

11= 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 0.070 0.000 0,829 0,000 1,366"* 0.010 -0.661

0,060 -0.167 0.020 -0.088 0.020 -0.249 0.020 -0.458"*

0.110 -0.293 0.040 -0.141 0.060 -0.166"* 0.060 -0.782"*

0.200 -0.392 0.060 -0.409 0.090 -0.631 0.110 -0.860

0.230 -0,400 0.090 -0.526 0.110 -0.762 0.1 40 -0.779

0.400 -0.258 0.130 -0.648 0.130 -0.918 0.190 -2.940"*

0.490 -0.252 0.150 -0.674 0.150 -0.670 0,250 -0.519

0,590 -0.371 0.200 -0,537 0.210 -0.633 0.400 -0.406

0.630 -0.410 0.250 -0.445 0.250 -0,485 0.490 -0.389

0.700 -0.572 0.260 -0.459 0.340 -0.474 0.580 -0.435

0.750 -0.644 0.280 -0.455 0.370 -0.461 0.650 -0.547

0.810 -0,618 0.290 -0.426 0.400 -0.397 0.700 -0.545

0.840 -0.692 0.310 -0.392 0.410 -0.435 0.750 -0.711

0.900 -0.320 0.320 -0.433 0.430 -0.452 0.800 -0.740

0.960 -0.306 0.340 -0.402 0.440 -0.438 0.830 -0.578

0.350 -0.103"* 0,460 -0.205 0.900 -0,431

0.370 -0.413 0.490 -0.422 0.960 -0.423"*

0.380 -0.413 0.500 -0.437

0,400 -0,349 0.520 -0.445

0.410 -0.379 0.540 -0.442

0.430 -0.396 0.550 -0.425

0.440 -0.375 0.580 -0,401

0.460 -0.366 0.600 -0.483

0.470 -0.389 0.610 -0.512

0.490 -0.389 0,650 0.085**

0.500 -0.381 0.700 -0.646

0.520 -0.391 0.750 -0.643

0.530 -0.389 0.820 -0.255

0,550 -0.393 0.890 -0.349

0,560 -0.431 0.900 -0,363

0.580 -0.393 0.960 -0.319

0.590 -0,463

0.600 -0.453

0.640 -0.582

0.700 -0.656

0.750 0.110"*

0.820 -0.640

0.870 -0.346

0,930 -0,307

0.960 -0,305

Lower Surface

0.020 -0.269 0.020 -0.121 0.020 -0,024 0,020 0,217

0.110 -0.018 0.060 0.112 0.060 0.136 0.060 0,104

0.230 0.072 0.090 0.061 0,090 0.153 0.110 0.107

0.400 0.120 0.120 0.104"* 0.120 0.076 0,250 -0,001

0.490 0.160 0,200 0.097 0.200 0.226 0.400 0.026

0.630 3,991 ** 0.260 0.089 0.250 0.087 0.490 0.065

0.750 0.286 0.400 0.105 0.400 0.076 0,580 0.110

0.850 0,327 0.490 0.138 0.490 0.116 0.650 0.314

0.900 0.403 0.580 0.206 0.580 0.189 0,750 0.526

0.960 0.196 0.640 0,398 0.650 0.1 04 0.830 0.566

0.750 0.439 0.750 0.055"* 0.900 0.633

0_870 0.551 0.890 0.618 0.960 0.433

0,930 0.441 0,930 0,500

0.960 0.300 0.960 0.311

CN = 0.525 0.689 0,667 0.721

198
Table D-2. Continued.

Flight 204, Wing sweep = 26", Time = 8-31-0-000, MINF = 0.692, Camber = 5/15, ALPT = 4.07, BETA = -0.07, QINF = 278.7,

RNPU = 2_5E+06, CNWP = 0.4111

I1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0,240 0.000 0.716 0.000 1.424"* 0.010 -0.399

0.060 -0.081 0,020 0.087 0.020 -0.039 0.020 -0.282"*

0.110 -0.262 0.040 0.020 0.060 -0.020** 0.060 -0.612**

0.200 -0.333 0060 -0.251 0.090 -0.472 O. I I0 -0.731

0.230 -0,290 0090 -0.436 O. 110 -0,624 O. 140 -0.712

0,400 -0.227 O.130 -0.511 O. 130 -0.781 O. 190 -2,988"*

0.490 -0,226 O. 150 -0.537 O. 150 -0.621 0.250 -0,471

0.590 -0.338 0,200 -0,439 0.210 -0.578 0.400 -0,378

0,630 -0.442 0.250 -0.400 0.250 -0,437 0.490 -0.358

0.700 -0.560 0.260 -0,373 0.340 -0,436 0,580 -0,396

0.750 -0.708 0.280 -0.431 0.370 -0,467 0.650 -0.548

0,810 -0,616 0,290 -0.390 0,400 -0,358 0,700 -0,540

0.840 -0.699 0.310 -0.361 0.410 -0.391 0.750 -0.696

0.900 -0.268 0.320 -0.381 0.430 -0.429 0.800 -0.741

0.960 -0.252 0.340 -0.368 0.440 -0.450 0.830 -0.552

0.350 -0.088** 0.460 -0.147 0.900 -0,453

0.370 -0.402 0.490 -0.375 0.960 -0.423**

0.380 -0.378 0.500 -0.401

0.400 -0.310 0.520 -0.404

0.410 -0.347 0.540 -0.424

0.430 -0.371 0.550 -0.401

0,440 -0.337 0.580 -0.422

0.460 -0.398 0.600 -0.455

0,470 -0.356 0.610 -0.494

0,490 -0.390 0,650 0,090**

0.500 -0.401 0,700 -0.621

0.520 -0,405 0,750 -0,676

0.530 -0,363 0.820 -0,230

0,550 -0,372 0.890 -0.309

0.560 -0,439 0,900 -0.33 I

0.580 -0.382 0,960 -0.281

0.590 -0.450

0.600 -0.468

0.640 -0.582

0.700 -0.655

0.750 0.077**

0.820 -0,622

0.870 -0.382

0.930 -0.290

0.960 -0.285

Lower Surface

0,020 -0.377 0,020 -0.317 0,020 -0.224 0.020 0.034

O. 110 -0.067 0.060 0.025 0.060 0.061 0.060 0.074

0.230 0.064 0.090 -0.010 0.090 0.073 0.110 0.021

0.400 0.118 0.120 0.058"* 0.120 0.031 0.250 -0.036

0.490 0.128 0.200 0.075 0.200 0.202 0.400 -0.005

0.630 4.090"* 0.260 0.052 0,250 0.003 0.490 0.011

0.750 0.311 0.400 0.075 0.400 0.067 0.580 0.066

0.850 0.338 0.490 0.117 0.490 0.099 0.650 0.312

0.900 0.373 0.580 0.174 0.580 0.137 0.750 0.485

0.960 0.222 0.640 0.418 0.650 0.086 0.830 0.574

0.750 0.445 0.750 0.102"* 0.900 0,636

0.870 0.521 0.890 0.607 0.960 0.457

0.930 0,450 0.930 0.498

0.960 0.313 0,960 0.321

CN = 0.484 0.629 0.598 0.658

199
Table D-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 8-3l-8-500, MINF = 0.692, Camber = 5/15, ALPT = 8.21, BETA = 0.25, QINF = 279.4,

RNPU = 2.6E+06, CNWP = 0.6380

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.962 0.000 0.676 0.000 1.224** 0.010 - 1.604

0.060 -0.707 0.020 -1.343 0.020 -1.467 0.020 -1.546"*

0.110 -0.728 0.040 -0.963 0.060 -0.694'* 0.060 -I .592"*

0.200 -0.615 0.060 -1.053 0.090 -1.338 0`110 -1.664

0.230 -0.538 0.090 -1.237 0.110 -1.448 0.140 -1.829

0.400 -0.376 0.130 -1.299 0.130 -1.557 0.190 -2.983**

0.490 -0.336 0.150 - 1.370 0.150 - 1.555 0.250 -0.667

0.590 -0.449 0.200 - 1.359 0.210 - 1.548 0.400 -0.521

0,630 -0.486 0.250 -0.603 0.250 -0.711 0.490 -0.470

0.700 -0.659 0.260 -0.556 0,340 -0,553 0.580 -0.528

0.750 -0,782 0.280 -0.551 0.370 -0.560 0.650 -0.644

0.810 -0.702 0.290 -0.548 0.400 -0.527 0,700 -0.612

0.840 -0.781 0.310 -0.533 0.410 -0.543 0.750 -0.743

0.900 -0.508 0.320 -0.542 0,430 -0.531 0,800 -0.599

0.960 -0.528 0.340 -0.529 0.440 -0.567 0.830 -0.523

0.350 -0.083"* 0.460 -0.306 0.900 -0.290

0.370 -0.526 0.490 -0.532 0.960 -0.255"*

0.380 -0.540 0.500 -0.543

0.400 -0.457 0.520 -0.534

0.410 -0.522 0.540 -0.532

0.430 -0.500 0.550 -0.517

0.440 -0.473 0.580 -0.493

0.460 -0.473 0.600 -0.583

0.470 -0.510 0.610 -0.611

0.490 -0.483 0.650 0.078"*

0.500 -0.471 0.700 -0.709

0.520 -0.479 0.750 -0.7 l0

0.530 -0.471 0.820 -0.229

0.550 -0.474 0.890 -0.306

0.560 -0.518 0.900 -0.297

0.580 -0.489 0.960 -0.287

0.590 -0.544

0.600 -0.550

0.640 -0.666

0.700 -0.727

0.750 0.120"*

0.820 -0.597

0.870 -0.286

0.930 -0.285

0.960 -0.284

Lower Surface

0.020 0.208 0.020 0.452 0.020 0.471 0.020 0.643

0.110 0.140 0.060 0.373 0.060 0.455 0.060 0.102

0.230 0.226 0.090 0.321 0.090 0.381 0.110 0.279

0.400 0.154 0.120 0.290"* 0.120 0.298 0.250 0.157

0.490 0.179 0.200 0.239 0.200 0.374 0.400 0.148

0.630 4.077"* 0.260 0.219 0.250 0.235 0.490 0` 178

0.750 0.270 0.400 0,223 0.400 0.211 0.580 0.178

0.850 0.275 0.490 0.221 0.490 0.146 0.650 0.355

0.900 0.363 0.580 0.250 0.580 0.251 0.750 0,542

0.960 0.123 0.640 0.437 0.650 0.114 0.830 0.615

0.750 0.481 0.750 0.053"* 0.900 0.676

0.870 0.553 0.890 0.626 0.960 0.456

0.930 0.426 0.930 0.497

0.960 0.305 0.960 0.310

CN = 0,730 0.996 0.962 0.964

20O
Table D-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 8-31-11-500, MINF = 0.692, Camber = 5/15, ALP'l" = 9,29, BETA = 0.34, QINF = 280,9,

RNPU = 2.6E+06, CNWP = 0.7725

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1,456 0.000 0.524 0.000 1.123 ** 0.010 - 1,756

0.060 -0.893 0.020 - 1.624 0.020 - 1.659 0.020 - 1.760"*

0,110 -0,799 0.040 -1.319 0.060 -0.921"* 0.060 -1.825"*

0.200 -0,639 0,060 - 1.351 0.090 - 1.586 0,110 - 1.837

0.230 -0.603 0.090 - 1.443 0,110 - 1,680 O. 140 - 1.568

0.400 -0.451 0.130 - 1.474 0.130 - 1.762 0,190 -2.986"*

0.490 -0,409 0.150 - 1,552 0.150 - 1.733 0,250 - 1.119

0.590 -0.517 0.200 - 1.613 0.210 - 1.657 0,400 -0.500

0.630 -0.562 0.250 -0.954 0.250 - 1,066 0.490 -0,466

0.700 -0.685 0.260 -0,868 0.340 -0,684 0.580 -0.498

0.750 -0.821 0,280 -0.770 0,370 -0.630 0.650 -0.597

0.810 -0.748 0.290 -0.639 0.400 -0.569 0.700 -0.602

0.840 -0.828 0.310 -0.537 0.410 -0.571 0,750 -0.697

0.900 -0,591 0,320 -0.508 0.430 -0.580 0,800 -0.562

0.960 -0,616 0.340 -0.456 0.440 -0,570 0.830 -0.533

0,350 -0.049"* 0,460 -0.317 0.900 -0.259

0,370 -0.466 0.490 -0.527 0.960 -0.260**

0.380 -0.512 0.500 -0,564

0,400 -0.467 0.520 -0.559

0.4 t 0 -0.491 0.540 -0,570

0.430 -0.483 0.550 -0,564

0,440 -0.501 0.580 -0.551

0.460 -0.482 0.600 -0,592

0.470 -0.508 0.610 -0.563

0.490 -0.503 0.650 0.166**

0.500 -0.504 0.700 -0.702

0.520 -0.490 0.750 -0.723

0.530 -0.503 0.820 -0.201

0.550 -0,505 0.890 -0.276

0.560 -0,566 0.900 -0.264

0.580 -0.518 0.960 -0.22 t

0.590 -0.582

0.600 -0.557

0.640 -0.700

0.700 -0.770

0.750 0.142"*

0.820 -0.630

0.870 -0.367

0.930 -0.296

0.960 -0.295

Lower Surface

0.020 0.327 0.020 0.584 0.020 0.563 0,020 0.738

0,1 l 0 0.179 0.060 0.457 0.060 0.492 0,060 0.067

0.230 0.268 0.090 0.371 0.090 0.455 0.110 0.378

0.400 0,168 0.120 0.331 ** 0.120 0.328 0,250 0.184

0.490 0,181 0.200 0,288 0.200 0.389 0.400 0.173

0,630 4.035** 0,260 0.275 0,250 0,268 0.490 0.177

0,750 0.278 0.400 0.171 0.400 O. 226 0.580 0.153

0.850 0.260 0.490 0.177 0.490 0,125 0.650 0.388

0.900 0.346 0.580 0.268 0.580 0,272 0.750 0.566

0.960 0,126 0.640 0,449 0.650 0,133 0.830 0.642

0.750 0.472 0.750 0.033'* 0.900 0.621

0.870 0.552 0.890 0.649 0.960 0,486

0.930 0,377 0.930 0.536

0.960 0,299 0,960 0.311

CN = 0.812 1.090 1.044 1.043

201
Table D-2. Concluded.

Flight 204, Wing sweep = 26 °, Time = 8-31-17-500, MINF = 0.687, Camber = 5/16, ALPT = 11.05, BETA = -0.41, QINF = 283.8,

RNPU = 2.6E+06, CNWP = 0.7577

rl = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x,/c CP

0.020 - 1.764 0.000 0.250 0.000 0.980"* 0.010 -2.028

0.060 - 1.649 0.020 - 1.944 0.020 - 1.912 0.020 - 1.998 **

0.110 - 1.106 0.040 - 1.675 0.060 - 1.055"* 0,060 -2.042"*

0.200 -0.732 0.060 - 1.708 0.090 - 1.840 0.110 -2.065

0.230 -0.686 0.090 -1.773 0. I 10 -1.581 0.140 -1.608

0.400 -0.464 0.130 - 1.702 0.130 - 1.231 0.190 -3.024 * *

0.490 -0.424 0,150 - 1.686 0.150 - 1.153 0.250 - 1.265

0.590 -0.526 0.200 - 1.289 0.210 - 1.151 0.400 -0.457

0.630 -0.574 0.250 - 1.040 0.250 - 1.086 0.490 -0.453

0.700 -0.691 0.260 -0.957 0.340 -0.965 0.580 -0.474

0.750 -0.943 0.280 -0.871 0.370 -0.933 0.650 -0.510

0.810 -0.861 0.290 -0.760 0.400 -0.875 0.700 -0.545

0.840 -0,952 0.310 -0.710 0.410 -0,844 0.750 -0.572

0.900 -0.668 0.320 -0.666 0.430 -0.822 0.800 -0.511

0.960 -0.755 0.340 -0.651 0.440 -0.8 |0 0.830 -0.436

0.350 -0.094** 0.460 -0.536 0,900 -0.303

0.370 -0.581 0.490 -0,762 0.960 -0.350"*

0.380 -0.599 0.500 -0.729

0.400 -0.536 0.520 -0.711

0,410 -0.532 0.540 -0.697

0.430 -0.538 0.550 -0.719

0.440 -0.537 0.580 -0.640

0.460 -0.517 0.600 -0.649

0.470 -0.526 0.610 -0.608

0.490 -0.523 0.650 0.131 **

0.500 -0.495 0.700 -0.548

0.520 -0.488 0.750 -0.537

0.530 -0,486 0.820 -0.155

0.550 -0.490 0.890 -0.337

0.560 -0.506 0,900 -0.383

0.580 -0.459 0.960 -0.274

0,590 -0.519

0.600 -0.497

0.640 -0.529

0.700 -0.585

0.750 0.149"*

0.820 -0.315

0,870 -0.209

0.930 -0.255

0.960 -0.253

Lower Surface

0,020 0.450 0.020 0.731 0.020 0.647 0.020 0.822

0.110 0.254 0.060 0.566 0.060 0.581 0.060 0.059

0.230 0.339 0,090 0.467 0.090 0.512 0.110 0.410

0.400 0.178 0.120 0.374"* 0.120 0.402 0.250 0.277

0.490 0.210 0.200 0.324 0.200 0.421 0.400 0.214

0.630 3.926"* 0.260 0.337 0.250 0.312 0.490 0.248

0.750 0,267 0.400 0.289 0,400 0.253 0.580 0.246

0.850 0.264 0.490 0.287 0.490 0.185 0.650 0.361

0.900 0.363 0.580 0.307 0.580 0.270 0.750 0.553

0.960 0.137 0.640 0.479 0.650 0.139 0.830 0.635

0.750 0.451 0.750 -0.036** 0.900 0.714

0.870 0.590 0.890 0.681 0.960 0.501

0.930 0.434 0.930 0.546

0.960 0.330 0.960 0.274

CN = 0.955 1.128 I. 100 1.097

202
APPENDIX E

Wing Pressure Coefficients for Nominal Dynamic Pressure

of 300 lb/ft 2 and Mach Number of 0.80.

Leading-edge wing sweep is 26 °. Table E-1 contains a summary of the data listing in table E-2. The asterisks (*)

in table E-2 indicate invalid values. Camber is _LE/TE" Refer to Nomenclature for definitions.

Table E- 1. Summary of listed data.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

216 10-34-46-000 0.805 0/2 4.96 -0.07 304.9 2.5E+06 0.2281

216 10-35-11-500 0.801 0/2 6.11 -0.67 302.0 2.5E+06 0.2931

216 10-35-16-500 0.800 0/2 7.12 -0.53 299.9 2.5E+06 0.3013

216 10-35-20-000 0.802 0/2 7.97 -0.18 299.8 2.5E+06 0.3300

216 10-35-23-500 0.801 0/2 10.12 -0.47 298.1 2.4E+06 0.4449

216 10-36-34-000 0.800 0/2 7.98 -0.15 296.7 2.4E+06 0.3491

216 10-36-38-500 0.802 0/2 9.01 0.43 297.4 2.4E+06 0.4157

216 10-36-44-000 0.812 0/2 10.15 -0.76 305.2 2.5E+06 0.4726

216 10-36-47-500 0.801 0/2 12.10 0.83 298.6 2.4E+06 0.2710

216 10-36-50-500 0.790 0/2 11.97 0.25 291.5 2.4E+06 0.2583

216 10-9-26-500 0.792 0/2 4.03 -0.12 283.0 2.3E+06 0.1794

224 10-3-54-500 0.802 0/2 8.01 0.11 292.5 2.4E+06 0.3170

224 10-4-3-000 0.807 0/2 10.17 0.19 298.9 2.4E+06 0.4287

216 10-32-45-500 0.803 5/2 5.49 0.05 303.4 2.5E+06 0.2974

216 10-33-21-500 0.806 5/2 6.89 -0.59 305.6 2.5E+06 0.3231

191 11-2-4-000 0.790 5/2 5.99 0.21 291.5 2.4E+06 0.3648

191 11-2-10-500 0.789 5/2 7.09 0.42 291.4 2.4E+06 0.3776

191 11-2-17-500 0.788 5/2 8.09 0.42 292.3 2.4E+06 0.4171

191 11-2-24-000 0.790 5/2 10.07 0.36 299.3 2.5E+06 0.4967

216 10-12-44-000 0.801 5/6 5.01 -0.10 302.1 2.5E+06 0.3585

216 10-13-5-500 0.811 5/6 6.08 0.11 308.1 2.5E+06 0.3883

195 9-49-26-500 0.811 5/6 7.02 0.13 280.8 2.3E+06 0.1721

195 9-49-39-500 0.800 5/6 8.11 0.02 275.5 2.3E+06 0.4730

195 9-49-45-000 0.798 5/6 9.07 0.10 276.4 2.3E+06 0.5332

195 9-49-52-000 0.797 5/6 10.01 -0.16 277.7 2.3E+06 0.6196

195 10-12-53-000 0.802 5/10 5.00 -0.24 292.2 2.4E+06 0.3467

195 10-13-9-500 0.797 5/10 7.05 -0.16 286.8 2.4E+06 0.4229

195 10-13-22-000 0.786 5/10 7.08 -0.19 276.7 2.3E+06 0.4066

195 10-13-56-500 0.795 5/10 8.14 -0.03 282.1 2.3E+06 0.5267

195 10-14-6-000 0.798 5/10 9.00 -0.01 284.3 2.3E+06 0.6346

203
TableE-1.Continued.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

195 10-14-10-500 0.798 5/10 10.22 -0.16 286.9 2.4E+06 0.7158

224 10-1 - 11-500 0.798 5/10 3.06 -0.07 296.9 2.4E+06 0.2403

224 10-1-36-500 0.800 5/11 8.07 -0.27 295.0 2.4E+06 0.5238

211 10-48-54-500 0.803 5/10 4.10 0.25 302.9 2.5E+06 0.3075

224 10-2-44-000 0.800 10/2 5.02 -0.59 294.7 2.4E+06 0.2869

224 10-2-52-500 0.805 10/2 10.29 -0.12 298.1 2.4E+06 0.3961

216 10-16-42-500 0.801 10/2 6.03 -0.01 303.1 2.5E+06 0.3208

216 10-17-12-500 0.808 10/2 4.04 -0.12 304.4 2.5E+06 0.2316

216 10-27-5-500 0.806 10/2 7.17 -0.47 307.6 2.5E+06 0.3778

216 10-27-8-500 0.806 10/2 8.10 -0.67 307.8 2.5E+06 0.4330

216 10-27-13-500 0.806 10/2 10.28 -0.36 307.4 2.5E+06 0.3816

216 10-27-18-000 0.794 10/2 12.15 -0.88 298.4 2.5E+06 0.1934

216 10-23-8-000 0.795 10/10 4.01 -0.21 297.0 2.5E+06 0.2962

216 10-28-48-500 0.805 10/10 4.06 -0.33 304.2 2.5E+06 0.3188

216 10-30-38-500 0.793 10/11 5.05 -0.50 295.7 2.4E+06 0.3418

216 10-29-6-000 0.803 10/I 1 6.26 -0.50 302.9 2.5E+06 0.4874

216 10-29-11-000 0.795 10/11 7.98 -0.10 296.7 2.4E+06 0.5321

204 9-13-37-500 0.797 10/10 7.25 0.19 277.2 2.3E+06 0.5409

204 9-13-41-500 0.794 10/10 8.13 -0.10 276.5 2.3E+06 0.6455

204 9-13-34-500 0.796 10/10 6.19 -0.56 275.6 2.3E+06 0.4409

204 9-13-48-500 0.788 10/I0 9.09 -0.04 277.2 2.3E+06 0.7290

204 9-13-51-500 0.789 10/10 10.08 0.80 281.5 2.3E+06 0.5351

201 8-31-7-500 0.814 10/10 4.04 -0.18 320.1 2.6E+06 0.3605

201 8-31-19-500 0.799 10/10 6.03 -0.04 306.9 2.5E+06 0.5275

201 8-31-27-000 0.800 10/10 6.99 0.28 307.5 2.5E+06 0.5905

201 8-31-42-000 0.810 10/10 8.08 0.34 321.9 2.6E+06 0.7250

201 8-31-47-000 0.809 10/10 9.21 0.11 324.0 2.6E+06 0.7585

214 9-0-54-000 0.794 0/11 4.01 -0.53 295.6 2.4E+06 0.3069

214 9-0-57-000 0.791 0/11 5.26 -0.44 292.9 2.4E+06 0.0833

214 9-1-13-500 0.800 0/11 7.09 -0.24 290.0 2.4E+06 0.7447

214 9-4-1-000 0.808 0/10 6.05 -0.07 297.8 2.4E+06 0.4134

214 9-4-8-500 0.819 0/11 7.18 -0.21 305.6 2.5E+06 0.5709

214 9-4-16-500 0.813 0/10 7.96 0.02 301.2 2.4E+06 0.6279

216 10-58-39-500 0.806 10/19 3.04 -0.56 305.3 2.5E+06 0.4224

216 10-58-52-500 0.811 10/19 8.22 -0.41 310.9 2.5E+06 0.7670

216 10-58-55-500 0.797 10/18 12.26 0.77 303.6 2.5E+06 0.4877

216 11-0-1-500 0.794 10/15 3.04 -0.15 295.3 2.4E+06 0.4146

204
TableE-I. Concluded.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

216 11-1-53-000 0.805 10/13 2.99 -0.44 304.4 2.5E+06 0.3791

216 11-2-1-000 0.808 10/13 6.08 -0.38 307.6 2.5E+06 0.5571

216 11-2-6-000 0.803 10/12 9.94 0.02 303.7 2.5E+06 0.6162

216 11-3-30-000 0.796 10/12 3.02 -0.21 297.9 2.5E+06 0.3846

216 11-3-39-500 0.804 10/13 8.04 -0.33 304.8 2.5E+06 0.7229

216 11-3-40-500 0.802 10/12 9.90 -0.30 304.3 2.5E+06 0.6857

216 11-5-2-000 0.804 10/9 3.15 -0.12 304.3 2.5E+06 0.3412

216 11-5-11-500 0.803 10/10 5.96 -0.56 304.2 2.5E+06 0.5427

216 11-5-14-000 0.805 10/9 8.32 0.22 306.8 2.5E+06 0.7148

216 11-6-47-000 0.795 10/6 3.02 -0.65 296.8 2.4E+06 0.3546

216 11-6-59-500 0.804 10/6 5.94 -0.10 304.5 2.5E+06 0.5619

216 11-7-3-000 0.807 10/7 8.29 -0.47 309.3 2.5E+06 0.7265

216 11-8-20-000 0.802 10/4 3.09 -0.62 302.2 2.5E+06 0.3607

216 11-8-28-000 0.810 10/4 6.06 -0.44 308.6 2.5E+06 0.5489

216 11-8-31-000 0.809 10/4 8.00 -0.41 307.0 2.5E+06 0.7208

216 11-10-2-500 0.806 10/0 3.02 -0.24 306.1 2.5E+06 0.3578

216 11-10-12-000 0.806 10/0 5.83 -0.38 306.9 2.5E+06 0.5499

216 11-10-16-000 0.803 10/0 8.04 -0.30 306.7 2.5E+06 0.7191

192 11-25-33-000 0.797 5/15 7.00 -0.06 233.9 1.9E+06 0.5904

192 11-25-40-000 0.786 5/15 8.08 0.42 224.2 1.9E+06 0.6774

192 11-25-43-500 0.784 5/15 9.25 -0.08 225.1 1.9E+06 0.7521

192 11-25-56-500 0.795 5/14 11.50 0.86 260.8 2.2E+06 0.5738

204 9-15-28-000 0.790 5/15 3.97 -0.18 266.4 2.2E+06 0.4161

204 9-15-38-500 0.794 5/15 4.99 -0.56 267.9 2.2E+06 0.6139

204 9-15-47-500 0.796 5/15 6.01 -0.33 270.1 2.2E+06 0.4391

204 9-15-50-500 0.797 5/15 7.18 -0.15 272.2 2.2E+06 0.7512

204 9-15-53-000 0.795 5/15 7.93 -0.24 271.9 2.2E+06 0.6265

205
Table E-2. Listing of data.

Flight 216, Wing sweep = 26 °, Time = 10-34-46-000, MINF = 0.805, Camber = 0/2, ALPT = 4.96, BETA = -0.07, QINF = 304.9,

RNPU = 2.5E+06, CNWP = 0.2281

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.297 0,000 0.856 0.000 0.434** 0.010 -0,845

0,060 -0,294 0,020 -0.770 0.020 -0.829 0.020 - 1.071

0.110 -0.304 0,040 -0.353 0.060 -0.281 ** 0.060 -0.999

0.200 -0.240 0,060 -0.553 0.090 -0.828 0.110 -0.932

0.230 -0.284 0.090 -0.504 0.110 -0.872 0.140 -0.925

0,400 -0.229 0.130 -0.439 0.130 -2.205** 0.190 -2,205 **

0.490 -0_201 0.150 -0,457 0.150 -0.428 0,250 -0.375

0,590 -0.249 0.200 -0.422 0.210 -0.510 0.400 -0.386

0.630 -0.252 0,250 -0.416 0.250 -0.431 0.490 -0.344

0.700 -0.211 0.260 -0,350 0.340 -0.391 0.580 -0,353

0,750 -0.252 0,280 -0.375 0.370 -0.387 0.650 -0.397

0.810 -0.237 0.290 -0.367 0.400 -0.379 0.700 -0.382

0.840 -0.223 0.310 -0.352 0.410 -3.184"* 0.750 -0.410

0.900 -0.133 0.320 -0.348 0.430 -0,378 0,800 -0.383

0.960 -0,026 0.340 -0.332 0.440 -0.347 0,830 -0.320

0,350 -0.206** 0,460 -0.353 0.900 -0.180

0.370 -0.312 0.490 -0,290 0.960 -0.018

0.380 -0.351 0,500 -0,352

0.400 -0.285 0,520 -0.330

0.410 -0,338 0.540 -0.336

0.430 -0.310 0.550 -0.326

0.440 -0.257 0.580 -0.330

0.460 -0.324 0,600 -0,336

0,470 -0.315 0.610 -0.337

0.490 -0.309 0.650 -0,649

0.500 -0,326 0,700 -0.399

0.520 -0.300 0.750 -0.431

0.530 -0.302 0.820 -0.343

0.550 -0.343 0.890 -0.128

0,560 -0.306 0.900 -0.089

0.580 -0.301 0,960 0,041

0.590 -0.338

0,600 -0.340

0,640 -0.372

0,700 -0.341

0.750 -0.033**

0.820 -0,275

0,870 -0.233

0.930 -0.103

0.960 -0.031

Lower Surface

0,020 -0.248 0.020 -0,069 0.020 0.051 0.020 0.395

0.110 -0.209 0,060 -0.017 0.060 0.074 0.060 -0.032

0.230 -0,077 0,090 -0,079 0,090 -0.011 0.110 -0.011

0,400 -0.075 0.120 -0.121 0.120 -0.334 0.250 -0.221

0.490 -0.060 0,200 -0.106 0.200 -0.157 0.400 -0.215

0,630 4.018"* 0.260 -0.205 0.250 -0.179 0.490 -0.255

0.750 0.016 0,400 -0.139 0.400 -0.171 0.580 -0.273

0.850 0.089 0,490 -0.158 0,490 -0,059 0.650 -0.133

0.900 0. t 69 0.580 -0,153 0.580 -0.196 0.750 0.123

0.960 0.146 0.640 0.027 0,650 -0.045 0.830 0.265

0.750 0.171 0,750 -0.037 0.900 0.312

0.870 0,208 0.890 0.289 0.960 0.250

0,930 0.215 0.930 0,247

0.960 0.173 0,960 0,368

CN = 0.185 0,308 0.330 0.391

206
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-35-11-500, MINF = 0,801, Camber = 0/2, ALPT = 6. ll, BETA = -0.67, QINF = 302.0,

RNPU = 2.5E+06, CNWP = 0,2931

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0,020 -0.828 0,000 0.783 0,000 0,371 ** 0.010 - 1.183

0,060 -0.370 0.020 - 1.096 0,020 - 1.017 0.020 - 1.182

0.110 -0.328 0.040 -0.783 0.060 -O406"* 0.060 - 1.158

0.200 -0,278 0.060 -0.956 0,090 - 1,016 0.110 - 1.056

0.230 -0.358 0.090 -0.923 0.110 - 1.078 0.140 - 1.074

0,400 -0.244 0.130 -0.934 0.130 -2.224* * 0.190 -2.224* *

0,490 -0.220 0.150 -0.890 0.150 -0.939 0.250 -0.459

0.590 -0.268 0.200 -0,334 0.210 -0.922 0.400 -0.367

0,630 -0.264 0,250 -0.365 0.250 -0.317 0.490 -0.346

0.700 -0.226 0.260 -0.331 0,340 -0.348 0.580 -0.339

0,750 -0.269 0,280 -0.368 0.370 -0.381 0,650 -0.389

0,810 -0.259 0.290 -0.364 0.400 -0.359 0.700 -0.368

0.840 -0.253 0.310 -0.353 0.410 -3.213" * 0.750 -0.398

0.900 -0.152 0.320 -0.363 0.430 -0.372 0.800 -0.365

0,960 -0.046 0.340 -0.340 0.440 -0,348 0.830 -0.312

0350 -0.212" * 0.46t7 -0.360 0,900 -0.163

0.370 -0,328 0.490 -0.298 0.960 -0.002

0,380 -0.362 0.500 -0.363

0.400 -0,286 0.520 -0.331

0.410 -0,355 0.540 -0.337

0.430 -0,314 0.550 -0.333

0.440 -0.274 0.580 -0.357

0.460 -0.337 0.600 -0.350

0.470 -0.329 0.610 -0.352

0.490 -0.326 0.650 -0.662

0.500 -0.355 0.700 -0.387

0.520 -0.340 0.750 -0.44 1

0.530 -0_317 0.820 -0.348

0.550 -0.354 0.890 -0.132

0.560 -0.344 0,900 -0.094

0.580 -0.315 0.960 0.040

0.590 -0.352

0.600 -0.356

0.640 -0.387

0.700 -0.357

0.750 -0,028**

0.820 -0.288

0.870 -0.237

0.930 -0.106

0.960 -0.037

Lower Surface

0,020 -0.013 0.020 0.099 0.020 0.192 0.020 0.484

0.110 -0.1 44 0.060 0.089 0.060 0.168 0.060 -0.026

0.230 -0.032 0,090 0.008 0.090 0.065 0.110 0.091

0.400 -0,060 0.120 -0.04 1 0.120 -0.259 0.250 -0.156

0,490 -0.044 0.200 -0.048 0.200 -0.063 0.400 -0.165

0.630 4.058"* 0.260 -0.147 0.250 -0.121 0,490 -0.211

0,750 0.014 0.400 -0.112 0.400 -0.131 0.580 -0.239

0.850 0,080 0.490 -0.131 0.490 -0.051 0.650 -0.110

0.900 0.176 0.580 -0.129 0.580 -0.160 0.750 0.126

0.960 0.137 0,640 0.044 0.650 -0.040 0.830 0.274

0.750 0.179 0.750 -0.036 0.900 0.323

0.870 0,235 0.890 0.293 0.960 0.254

0.930 0.219 0.930 0.251

0.960 0.172 0.960 0.358

CN = 0.234 0.416 0A 18 0.455

207
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-35-16-500, MINF = 0.800, Camber = 0/2, ALPT = 7,12, BETA = -0.53, QINF = 299.9,

RNPU = 2.5E+06, CNWP = 0.3013

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -1.039 0.000 0.682 0,000 0.311"* 0.010 -1.323

0.060 -0.999 0.020 - 1.261 0,020 - 1.150 0.020 - 1.364

0.110 -0.901 0.040 -0.989 0.060 -0.532** 0.060 -1.298

0.200 -0.248 0,060 - 1.139 0.090 - 1.191 0.110 - 1.207

0.230 -0.348 0.090 -1.116 0.110 -1.219 0.140 -1.230

0,400 -0,275 0.130 -1.116 0.130 -2.231 ** 0.190 -2.231 **

0.490 -0.249 0.150 -1.100 0.150 -1.129 0.250 -1.158

0.590 -0.277 0.200 - 1.012 0.210 - 1.087 0.400 -0.362

0.630 -0.291 0.250 - 1.034 0.250 - 1.086 0.490 -0.326

0.700 -0.242 0,260 -0.552 0.340 -0.387 0,580 -0.327

0.750 -0.304 0.280 -0.412 0.370 -0.319 0.650 -0.367

0.810 -0.295 0.290 -0.30 t 0.400 -0.272 0.700 -0.361

0,840 -0.268 0.310 -0.257 0.410 -3,227"* 0.750 -0.367

0,900 -0.197 0.320 -0.243 0.430 -0.261 0.800 -0.339

0,960 -0.073 0.340 -0.219 0.440 -0.264 0.830 -0.269

0.350 -0.161"* 0.460 -0.271 0.900 -0.119

0.370 -0.223 0.490 -0.246 0.960 -0.016

0.380 -0.269 0.500 -0.316

0.400 -0.229 0.520 -0.291

0.410 -0.290 0.540 -0.312

0.430 -0.244 0.550 -0.311

0.440 -0.226 0.580 -0.340

0.460 -0.304 0.600 -0.307

0.470 -0.305 0.610 -0.333

0.490 -0.303 0.650 -0.643

0.500 -0.320 0.700 -0.348

0,520 -0.309 0.750 -0.435

0.530 -0.304 0.820 -0.340

0.550 -0.344 0.890 -0.124

0.560 -0.340 0.900 -0.106

0,580 -0.295 0,960 0.023

0.590 -0.357

0.600 -0.360

0.640 -0.386

0.700 -0.366

0.750 -0.023**

0.820 -0.288

0.870 -0.255

0.930 -0.120

0.960 -0.051

Lower Surface

0.020 0.072 0,020 0.223 0.020 0.281 0.020 0.564

0.110 -0.1 04 0.060 0.163 0.060 0.242 0.060 -0.036

0.230 -0.023 0.090 0.072 0,090 0.129 0.110 0.157

0.400 -0.062 0.120 -0.004 0.120 -0.199 0.250 -0.111

0.490 -0.043 0.200 -0.014 0.200 -0.030 0.400 -0.129

0.630 4.096"* 0.260 -0,097 0.250 -0.070 0.490 -0.189

0.750 -0.008 0.400 -0.089 0.400 -0.099 0.580 -0.212

0.850 0.070 0.490 -0.115 0.490 -0.050 0.650 -0.102

0.900 0.149 0.580 -0.106 0.580 -0.149 0.750 0.145

0.960 0.107 0.640 0.046 0.650 -0.050 0.830 0.270

0.750 0.170 0.750 -0.042 0.900 0.313

0.870 0.240 0.890 0.282 0,960 0.238

0.930 0.207 0.930 0.243

0.960 0.160 0.960 0.338

CN = 0.325 0.511 0.509 0.585

208
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-35-20-000, MINF = 0.802, Camber = 0/2, ALPT = 7.97, BETA = -0.18, QINF = 299.8,

RNPU = 2.5E+06, CNWP = 0.3300

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.135 0.000 0.644 0.000 0.286" * 0.010 - 1.352

0.060 - 1.126 0,020 - 1.409 0.020 - 1.238 0.020 - 1.403

0.110 - 1.051 0.000 - 1.081 0.060 -0.477"* 0.060 - 1.379

0.200 -0.400 0.060 - 1.239 0.090 - 1.240 0.110 - 1,336

0.230 -0.214 0.090 -1,188 0.110 -1.324 0.140 -1.331

0,400 -0.251 0.130 - 1.184 0.130 -2.223"* 0.190 -2.223"*

0.490 -0.233 0.150 - 1.178 0.150 - 1.173 0.250 - 1.292

0.590 -0.283 0.200 - 1.102 0.210 - 1.181 0.400 -0.492

0.630 -0.305 0.250 - 1.163 0.250 - 1.179 0.490 -0.321

0.700 -0.248 0.260 - 1.098 0.340 -0.740 0.580 -0.300

0.750 -0.300 0.280 - 1.138 0.370 -0.616 0.650 -0.323

0.810 -0.293 0.290 - 1.129 0.400 -0.522 0.700 -0.332

0.840 -0.282 0.310 -0.930 0.410 -3,220** 0.750 -0.325

0.900 -0.206 0.320 -0.725 0.430 -0.448 0.800 -0.295

0.960 -0.092 0.340 -0.496 0.440 -0.364 0.830 -0.215

0.350 -0.259"* 0.460 -0.346 0.900 -0.101

0.370 -0.372 0.490 -0.215 0.960 -0.023

0.380 -0356 0.500 -0.273

0.400 -0.238 0.520 -0.249

0.410 -0.231 0.540 -0.241

0.430 -0.189 0.550 -0.238

0.440 -0.131 0.580 -0.246

0.460 -0.185 0.600 -0.238

0.470 -0.191 0.610 -0.242

0.490 -0.200 0.650 -0.553

0.500 -0.220 0.700 -0.303

0.520 -0.216 0.750 -0.368

0.530 -0.216 0.820 -0.297

0.550 -0.239 0.890 -0.103

0.560 -0.261 0.900 -0.077

0.580 -0.240 0.960 0.003

0.590 -0.293

0.600 -0.287

0.640 -0.320

0.700 -0.313

0.750 -0.029**

0.820 -0.283

0.870 -0.232

0.930 -0.104

0.960 -0.035

Lower Surface

0.020 0.096 0.020 0.320 0.020 0.383 0.020 0.664

0.110 -0.061 0.060 0.235 0.060 0.292 0.060 -0.013

0.230 0.009 0.090 0.137 0,090 0.184 0.110 0.231

0.400 -0.039 0.120 0.060 0.120 -0.132 0.250 -0.008

0.490 -0.00 1 0.200 0.039 0.200 0.013 0.400 -0.083

0.630 4.107** 0.260 -0.059 0.250 -0.024 0.490 -0.143

0.750 0.008 0.400 -0.054 0.400 -0.065 0.580 -0.193

0.850 0.060 0.490 -0.088 0.490 -0.026 0.650 -0.079

0.900 0.142 0.580 -0.101 0.580 -0.121 0.750 O. 139

0.960 0.110 0.640 0.058 0,650 -0.026 0.830 0.275

0.750 0.166 0.750 -0.019 0.900 0.33 I

0.870 0.227 0.890 0.284 0.960 0.250

0,930 0.213 0.930 0.255

0.960 0.169 0.960 0.362

CN = 0.352 0.589 0.573 0.657

209
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-35-23-500, MINF = 0.801, Camber = 0/2, ALPT = 10.12, BETA = -0.47, QINF = 298.L

RNPU = 2.4E+06, CNWP = 0.4449

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.388 0.000 0.445 0.000 0.058" * 0.010 - 1.592

0.060 - 1.349 0.020 - 1.674 0.020 - 1.452 0.020 - 1.590

0.110 - 1.314 0.040 - 1.255 0.060 -0.721 ** 0.060 - 1.609

0.200 -0.900 0.060 - 1.455 0.090 - 1.479 0. I 10 - 1.497

0.230 -0.707 0.090 - 1.402 0.110 - 1.511 0.140 - 1.544

0.400 -0.281 0.130 - 1.391 0.130 -2.226 * * 0.190 -2.226 * *

0.490 -0.265 0.150 - 1.379 0.150 - 1.356 0.250 - 1.476

0.590 -0.310 0,200 - 1.315 0.210 -0.944 0.400 -0.780

0.630 -0.317 0.250 - 1.147 0.250 -0.805 0.490 -0.370

0.700 -0.270 0.260 - 1.027 0.340 -0.749 0.580 -0.243

0.750 -0.319 0.280 -0.959 0.370 -0.729 0.650 -0.244

0.810 -0.321 0.290 -0.867 0.400 -0.708 0.700 -0.236

0.840 -0.326 0.310 -0.774 0.410 -3.228** 0.750 -0.236

0.900 -0,235 0.320 -0.755 0.430 -0.682 0.800 -0,272

0.960 -0.140 0.340 -0.674 0.440 -0.642 0.830 -0.197

0.350 -0.304"* 0.460 -0.644 0,900 -0.137

0.370 -0.533 0.490 -0,593 0.960 -0.072

0.380 -0.547 0.500 -0,633

0.400 -0.439 0.520 -0.613

0.410 -0.436 0.540 -0.602

0.430 -0.389 0.550 -0.588

0.440 -0.315 0.580 -0.572

0.460 -0.374 0.600 -0.544

0.470 -0.377 0.610 -0.545

0.490 -0.335 0.650 -0.749

0.500 -0.337 0.700 -0.505

0.520 -0.309 0.750 -0.515

0.530 -0.297 0.820 -0.351

0.550 -0.340 0.890 -0.227

0.560 -0.315 0.900 -0.206

0.580 -0.298 0.960 -0.176

0.590 -0.316

0.600 -0.314

0.640 -0.328

0.700 -O.335

0.750 -0.004**

0.820 -0.226

0,870 -0,216

0.930 -0.165

0.960 °0.143

Lower Surface

0.020 0.230 0.020 0.466 0.020 0.528 0.020 0.748

0.110 0.002 0.060 0.341 0,060 0.450 0.060 0.001

0.230 0.030 0.090 0.241 0.090 0.304 O. 110 0.344

0.400 -0.040 O. 120 O. 148 O. 120 -0.029 0.250 0.035

0.490 -0,035 0,200 0.115 0.200 0.106 0.400 -0.015

0.630 4.140"* 0.260 0.002 0.250 0.059 0.490 -0.081

0.750 -0.016 0.400 -0.014 0.400 -0.016 0.580 -0.139

0.850 0.028 0.490 -0.067 0.490 -0.016 0.650 -0.069

0.900 0.121 0.580 -0.096 0,580 -0.097 0.750 0.145

0.960 0.079 0.640 0.046 0.650 -0.016 0.830 0.275

0.750 0.151 0.750 -0.009 0.900 0.306

0.870 0.178 0.890 0.256 0.960 0.205

0.930 0.165 0.930 0.192

0.960 0.092 0.960 0.249

CN = 0.480 0.687 0.734 0.781

210
Table E-2, Continued.

Flight 216, Wing sweep = 26", Time = 10-36-34-000, MINF = 0.800, Camber = 0/2, ALPT = 7.98, BETA = -0.15, QINF = 296.7,

RNPU = 2.4E+06, CNWP = 0.349 [

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.165 0.000 0624 0.000 0.271 ** 0.010 - 1.395

0.060 - 1.117 0.020 - 1.388 0.020 - 1.253 0.020 - 1.436

0.110 -1.045 0.040 -1.092 0.060 -0.484** 0.060 -1.411

0.200 -0.384 0.060 - 1.255 0.090 - 1.271 O. l 10 - 1.333

0,230 -0.365 0.090 - 1.195 0.110 - 1.316 0.140 - 1.363

0,400 -0. 264 0.130 - 1.208 0.130 -2.234"* 0.190 -2.234"*

0.490 -0,257 0.150 - 1.185 0.150 - 1.203 0.250 - 1.323

0.590 -0.297 0.200 - 1.110 0.210 - 1.202 0.400 -0.487

0.630 -0.304 0.250 - 1.173 0.250 - 1.202 0.490 -0.333

0.700 -0.264 0.260 - 1.114 0.340 -0,704 0.580 -0.319

0.750 -0.317 0,280 - 1.159 0.370 -0.610 0.650 -0.319

0.810 -0.292 0.290 - 1.150 0.400 -0.530 0.700 -0,328

0,840 -0.295 0.310 -0.744 0.410 -3.241"* 0.750 -0.331

0.900 -0.223 0.320 -0.625 0.430 -0.440 0.800 -0.294

0.960 -0.096 0.340 -0.498 0.440 -0.391 0.830 -0.226

0.350 -0,269** 0.460 -0.335 0.900 -0.115

0.370 -0,345 0,490 -0.281 0.960 -0.022

0.380 -0.350 0,500 -0,275

0.400 -0.236 0.520 -0.237

0.410 -0.238 0.540 -0.247

0.430 -0.185 0.550 -0.246

0.440 -0,141 0.580 -0.213

0,460 -0.211 0.600 -0,232

0.470 -0.204 0.610 -0,249

0.490 -0.220 0.650 -0.58 I

0.500 -0.240 0.700 -0.324

0.520 -0.236 0.750 -0389

0.530 -0.240 0.820 -0.299

0.550 -0.272 0.890 -0.103

0.560 -0.275 0.900 -0.090

0.580 -0.245 0.960 0.033

0.590 -0.301

0.600 -0.318

0.640 -0.323

0.700 -0.334

0.750 -0.028**

0.820 -0.289

0.870 -0.248

0.930 -0.119

0.960 -0.034

Lower Surface

0.020 0.089 0.020 0.302 0.020 0.384 0.020 0.653

0. 110 -0.073 0.060 0.224 0,060 0.304 0.060 -0.031

0.230 -0.006 0.090 0.132 0.090 0.203 O.110 0.215

0.400 -0.046 0.120 0.047 0.120 -0.152 0.250 -0.059

0.490 -0.037 0.200 0.029 0.200 0.024 0.400 -0.080

0,630 4.161 ** 0.260 -0.062 0.250 -0.035 0.490 -0,151

0.750 -0.002 0.400 -0,065 0.400 -0.059 0.580 -0.173

0.850 0.046 0.490 -0.099 0.490 -0.044 0.650 -0,075

0.900 0.141 0.580 -0.112 0.580 -0.133 0.750 0.152

0.960 0.097 0.640 0.063 0.650 -0.044 0.830 0.283

0,750 0.169 0.750 -0.022 0.900 0.316

0.870 0.212 0.890 0,299 0.960 0.249

0.930 0.216 0,930 0.255

0.960 O. 157 0.960 O.344

CN = 0.367 0.588 0.582 0.667

211
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-36-38-500, MINF = 0,802, Camber = 0/2, ALPT = 9.01, BETA = 0.43, QINF = 297.4,

RNPU = 2.4E+06, CNWP = 0.4157

lq = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.275 0.000 0.558 0.000 O. 174"* 0.010 - 1.474

0.060 - 1.205 0.020 - 1.548 0.020 - 1.364 0.020 - 1.493

O. 110 - 1.205 0.040 - 1.222 0.060 -0.594"* 0.060 - 1.490

0.200 -0.958 0.060 - 1.354 0.090 - 1.371 O. 110 - 1.416

0.230 -0.844 0,090 -1.297 0.110 -1.403 0.140 -1.445

0.400 -0.233 0.130 - 1.294 0.130 -2.221 ** 0.190 -2.221 **

0,490 -0.226 0,150 -1.285 0.150 -1.312 0,250 -1.397

0.590 -0.285 0.200 - 1.231 0.210 - 1.297 0,400 -0,765

0,630 -0,300 0.250 - 1.295 0.250 - 1.285 0.490 -0.442

0.700 -0,249 0.260 - 1.211 0.340 -0.824 0,580 -0,290

0.750 -0,297 0.280 -1.265 0.370 -0.720 0,650 -0.259

0.810 -0.290 0.290 - 1,256 0.400 -0.677 0.700 -0.262

0.840 -0.294 0.310 -1.206 0.410 -3.225"* 0.750 -0.241

0.900 -0.233 0.320 - 1,208 0,430 -0.673 0.800 -0.221

0.960 -0.124 0.340 -0.776 0.440 -0.622 0,830 -0.166

0.350 -0.358"* 0.460 -0.622 0.900 -0.079

0.370 -0.617 0.490 -0.546 0,960 -0,003

0.380 -0.655 0,500 -0.592

0.400 -0.566 0.520 -0.568

0.410 -0.588 0.540 -0.539

0.430 -0.523 0,550 -0.507

0,440 -0.457 0.580 -0.455

0.460 -0.475 0.600 -0.441

0.470 -0.416 0.610 -0.402

0.490 -0.393 0.650 -0.540

0.500 -0.359 0.700 -0.292

0.520 -0.314 0.750 -0.332

0.530 -0,274 0.820 -0.169

0.550 -0.300 0.890 -0.071

0.560 -0.251 0,900 -0.062

0,580 -0.230 0.960 0.028

0.590 -0.246

0.600 -0.245

0.640 -0.217

0.700 -0,229

0.750 -0,005**

0.820 -0,205

0.870 -0,177

0.930 -0.077

0.960 -0.019

Lower Surface

0.020 0.174 0,020 0.413 0,020 0,485 0.020 0.732

0.110 -0.016 0.060 0.303 0.060 0.380 0.060 -0.008

0.230 0.025 0.090 0.202 0.090 0,272 0.110 0.299

0.400 -0.034 O. 120 O. 114 O. 120 -0.068 0.250 -0.003

0.490 -0.029 0.200 0.081 0.200 0,074 0.400 -0.035

0.630 4.159"* 0.260 -0.021 0,250 0.025 0.490 -0.101

0.750 -0,002 0.400 -0.027 0,400 -0.021 0.580 -0.155

0.850 0,046 0.490 -0,076 0.490 -0.021 0.650 -0.067

0.900 0.133 0.580 -0.101 0,580 -0.110 0.750 0.160

0.960 0.095 0,640 0.056 0.650 -0,014 0.830 0.297

0.750 0.171 0.750 -0.014 0.900 0.329

0.870 0,206 0,890 0.284 0.960 0,239

0,930 0.208 0.930 0.233

0.960 0.150 0.960 0,322

CN = 0.472 0.678 0.687 0.743

212
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-36-44-000, MINF = 0,812, Camber = 0/2, ALPT = 10.15, BETA = -0.76, QINF = 305.2,

RNPU = 2.5E+06. CNWP = 0.4726

= 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 - 1.341 0.000 0.462 0,000 0.096"* 0.010 - 1.543

0.060 - t .308 0.020 - 1.569 0.020 - 1,412 0.020 - 1.562

0. I 10 - 1.202 0.040 - 1.178 0.060 -0,606"* 0.060 - 1.560

0.200 -0.988 0.060 - 1.400 0,090 - 1,433 0.110 - 1.490

0.230 -0.736 0.090 - t .361 0.110 - 1,476 0.140 - 1.500

0,400 -0.276 0.130 -1.355 0.130 -2.168"* 0.190 -2.168"*

0.490 -0,268 0,150 -1.316 0.150 - 1.358 0.250 - 1.465

0.590 -0.319 0.200 -1.182 0.210 -1.342 0.400 -0.846

0.630 -0.330 0.250 -0.930 0250 -0.817 0.490 -0.509

0.700 -0,284 0.260 -0,832 0,340 -0.770 0.580 -0,308

0.750 -0.339 0.280 -0,809 0.370 -0.752 0.650 -0,257

0.810 -0.315 0.290 -0.762 0.400 -0,715 0.700 -0.245

0.840 -0,313 0.310 -0,753 0.410 -3.147"* 0,750 -0.239

0.900 -0,246 0.320 -0.746 0.430 -0.697 0.800 -0,261

0.960 -0.132 0,340 -0.700 0.440 -0.671 0,830 -0,206

0,350 -0.343 ** 0.460 -0.665 0,900 -0.134

0.370 -0.656 0.490 -0.611 0,960 -0.079

0,380 -0.705 0.500 -0.664

0.400 -0.535 0.520 -0.641

0.410 -0,565 0.540 -0.637

0.430 -0.594 0,550 -0.607

0.440 -0,492 0.580 -0.585

0460 -0.573 0.600 -0,553

0A70 -0.505 0.610 -0.555

0.490 -0.445 0.650 -0.773

0.500 -0488 0.700 -0,513

0.520 -0.402 0.750 -0.563

0.530 -0.418 0.820 -0.401

0,550 -0.421 0.890 -0.274

0.560 -0.383 0.900 -0.262

0.580 -0.372 0.960 -0.192

0,590 -0.379

0.600 -0.359

0.640 -0.310

0.700 -0.318

0.750 -0.016"*

0.820 -0.237

0,870 -0,209

0.930 -0.163

0.960 -0.130

Lower Surface

0.020 0.216 0.020 0,463 0.020 0.522 0.020 0.740

0.110 -0.010 0.060 0,354 0.060 0.418 0.060 -0.012

0,230 0.031 0.090 0.229 0.090 0.297 0.110 0.347

0.400 -0.048 0.120 0.135 0,120 -0.020 0.250 0.031

0.490 -0.011 0.200 0.107 0.200 0,081 0.400 -0.024

0.630 4,049"* 0,260 -0.015 0.250 0.049 0.490 -0.096

0.750 -0.021 0.400 -0.023 0.400 -0.015 0,580 -0.145

0.850 0,026 0.490 -0.074 0.490 -0.029 0.650 -0.069

0.900 0.120 0.580 -0.106 0.580 -0, l I 1 0.750 0,152

0.960 0,076 0.640 0.036 0.650 -0.025 0,830 0.277

0.750 0.1 46 0.750 -0.003 0.900 0.308

0.870 0.179 0,890 0.245 0,960 0,205

0.930 0.127 0,930 0.179

0.960 0.059 0.960 0,254

CN = 0.481 0.677 0.762 0.797

213
Table E-2. Continued.

Flight 216, Wing sweep = 26':, Time = 10-36-47-500, MINF = 0.801, Camber = 0/2, ALPT = 12.10, BETA = 0.83, QINF = 298.6,

RNPU = 2.4E+06, CNWP = 0.2710

rl = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 - 1.541 0.000 0.284 0.000 -0.171 ** 0.010 - 1.712

0.060 - 1.516 0.020 - 1.727 0.020 -0.772 0.020 - 1.710

0.110 - 1.457 0.040 - 1.508 0.060 -0.151 "* 0.060 - 1.630

0.200 -0.866 0.060 - 1.596 0.090 -0.668 0.110 - 1.335

0.230 -0.746 0.090 - 1.556 0.110 -0.747 0.140 - 1.202

0.400 -0.457 0,130 - 1.532 0,130 -2,226** 0.190 -2.226"*

0.490 -0.331 0.150 - 1.517 0.150 -0.705 0.250 - 1.148

0.590 -0.351 0.200 - 1.456 0.210 -0.686 0.400 -0.853

0.630 -0,347 0.250 - 1.074 0.250 -0.669 0.490 -0.552

0,700 -0.306 0.260 -0.962 0.340 -0.766 0.580 -0.470

0.750 -0.325 0.280 -0,958 0.370 -0.770 0.650 -0.435

0.810 -0,316 0,290 -0.862 0.400 -0.769 0,700 -0.431

0.840 -0.314 0.310 -0.823 0.410 -3.226"* 0.750 -0.444

0.900 -0.243 0.320 -0.830 0.430 -0.774 0.800 -0.450

0.960 -0,165 0,340 -0.636 0.440 -0.747 0.830 -0.388

0.350 -0.279** 0.460 -0.756 0.900 -0.354

0.370 -0.495 0.490 -0.717 0.960 -0.318

0,380 -0.454 0.500 -0,782

0.400 -0.302 0.520 -0.765

0.410 -0.379 0,540 -0.755

0.430 -0.360 0.550 -0.728

0.440 -0,286 0.580 -0.695

0.460 -0.379 0,600 -0.683

0.470 -0.330 0.610 -0.671

0.490 -0.361 0.650 -0.845

0.500 -0.355 0.700 -0.625

0.520 -0.350 0.750 -0.666

0.530 -0.355 0.820 -0.520

0.550 -0,394 0.890 -0.442

0.560 -0.351 0,900 -0.357

0.580 -0.328 0.960 -0.304

0.590 -0.378

0.600 -0.381

0.640 -0.346

0.700 -0.330

0.750 -0.033**

0.820 -0.221

0.870 -0.204

0.930 -0.231

0,960 -0.220

Lower Surface

0.020 0.264 0.020 0.577 0.020 0.626 0.020 0.811

0.110 0.072 0.060 0,420 0.060 0.513 0.060 -0.021

0.230 0,061 0,090 0.310 0,090 0.384 0.110 0,427

0.400 -0.025 0.120 0.217 0.120 0,039 0.250 0. l 11

0.490 -0.013 0.200 0.166 0.200 0.175 0,400 0.018

0.630 4.130"* 0.260 0.04 1 0.250 0.110 0.490 -0,062

0.750 -0.027 0.400 -0.002 0.400 0.006 0.580 -0.122

0.850 -0.002 0.490 -0.070 0.490 -0.038 0.650 -0.080

0.900 0.089 0,580 -0.114 0.580 -0.123 0.750 0.127

0.960 0.035 0,640 0.031 0.650 -0.034 0,830 0,248

0.750 0.149 0,750 -0.027 0.900 0.263

0.870 0,137 0.890 0.198 0.960 0.124

0.930 0.088 0.930 0.115

0.960 0.022 0.960 0.167

CN = 0.558 0.728 0.688 0,841

214
Table E-2. Continued.

Flight 216, Wing sweep = 26 °. Time = 10-36-50-500, MINF = 0.790, Camber = 0/2. ALPT = 11.97, BETA = 0.25, QINF = 291.5,

RNPU = 2.4E+06, CNWP = 0.2583

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 - 1.643 0.000 0,222 0.000 -0.146"* 0.010 - 1.774

0.060 - 1.565 0.020 - 1.801 0.020 - 1,152 0.020 - 1.772

0.110 - 1.521 0.040 - 1.387 0.060 -0,300** 0.060 - 1.807

0.200 -0.841 0,060 - 1.675 0.090 -0.966 0.110 - 1,446

0.230 -0.640 0.090 -1.631 0.110 -1.017 0.140 -1.086

0.400 -0.399 0.130 - 1.593 0.130 -2.287** 0.190 -2.287**

0.490 -0.332 0.150 - 1.584 0.150 - 1.034 0.250 -1.066

0.590 -0.325 0.200 - 1.519 0.210 - 1.044 0.400 -1.051

0.630 -0.344 0.250 - 1.145 0,250 -0.969 0.490 -0.884

0.700 -0.283 0.260 -0.971 0.340 -0.917 0.580 -0.620

0.750 -0.282 0,280 -0.988 0.370 -0.903 0.650 -0.490

0.810 -0.295 0,290 -0.914 0.400 -0.842 0.700 -0.466

0.840 -0.291 0.310 -0.876 0.410 -3.312** 0.750 -0.425

0.900 -0.229 0.320 -0.865 0.430 -0.832 0.800 -0.454

0.960 -0.177 0.340 -0,762 0.440 -0.779 0.830 -0.372

0.350 -0.350"* 0.460 -0.773 0.900 -0.323

0.370 -0.688 0.490 -0,680 0,960 -0.285

0.380 -0.693 0.500 -0.726

0.400 -0.381 0.520 -0.708

0.410 -0,368 0.540 -0.683

0.430 -0,350 0.550 -0.650

0.440 -0,222 0.580 -0.596

0.460 -0.345 0.600 -0.568

0.470 -0.284 0.610 -0.535

0.490 -0.244 0.650 -0.665

0.500 -0.289 0.700 -0.403

0.520 -0.231 0.750 -0.455

0.530 -0.264 0.820 -0.301

0.550 -0.266 0.890 -0.223

0.560 -0.250 0.900 -0.222

0.580 -0,234 0.960 -0.177

0.590 -0.271

0.600 -0.282

0.640 -0.224

0.700 -0.229

0.750 -0.016"*

0.820 -0.161

0.870 -0.157

0,930 -0.169

0.960 -0.146

Lower Surface

0.020 0.341 0.020 0.605 0.020 0.648 0.020 0.812

0.110 0.079 0.060 0.449 0.060 0.503 0.060 0.001

0.230 0.077 0.090 0.319 0.090 0.395 0.110 0.444

0.400 -0,014 0.120 0.222 0,120 0.062 0.250 0.112

0.490 -0.021 0.200 0.188 0.200 O. 194 0.400 0.056

0.630 4.221 ** 0.260 0.049 0,250 0.132 0.490 -0.026

0.750 -0.009 0.400 0.025 0.400 0,023 0,580 -0. I 13

0,850 0.009 0.490 -0.037 0.490 -0.028 0.650 -0.044

0.900 0.096 0.580 -0.082 0.580 -0.089 0.750 0.152

0,960 0.050 0.640 0,043 0.650 -0.013 0.830 0.257

0.750 0.158 0.750 -0.005 0.900 0.286

0.870 0.166 0.890 0.202 0.960 0,140

0.930 0.135 0.930 0.1 40

0.960 0.079 0.960 0.223

CN = 0.542 0.733 0.726 0.925

215
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-9-26-500, MINF = 0,792, Camber = 0/2, ALPT = 4.03, BETA = -0.12, QINF = 283.0,

RNPU = 2.3E+06, CNWP = 0.1794

I] = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0,020 -0.098 0.000 0.846 0,000 0.746** 0.010 - 1.018

0,060 -0.185 0,020 -0,385 0,020 -0,527 0.020 -0,974

0.110 -0.251 0,040 -0.234 0.060 -0.201 * * 0.060 -0.747

0.200 -0,209 0.060 -0,379 0.090 -0,415 0.110 -0,440

0,230 -0.244 0.090 -0.335 0.110 -0.441 0.140 -0.540

0.400 -0,204 0.I 30 -0,338 0.130 -2,278"* 0.190 -2,278**

0,490 -0.190 0.150 -0.352 0.150 -0.423 0.250 -0.415

0.590 -0,232 0.200 -0.325 0 210 -0.442 0.400 -0.353

0,630 -0,244 0,250 -0.306 0,250 -0.368 0.490 -0.308

0.700 -0.228 0.260 -0.308 0.340 -0.339 0.580 -0.295

0.750 -0.224 0.280 -0.318 0.370 -0.364 0.650 -0.381

0.810 -0.221 0.290 -0.302 0.400 -0.312 0.700 -0.353

0.840 -0.221 0.310 -0,289 0.410 -3.334** 0,750 -0.369

0.900 -0.126 0.320 -0.315 0,430 -0,340 0.800 -0,366

0,960 -0,010 0,340 -0.297 0.440 -0.338 0,830 -0.322

0.350 -0.213"* 0.460 -0.325 0,900 -0.185

0,370 -0,291 0,490 -0.293 0.960 -0.009

0,380 -0.312 0.500 -0.311

0,400 -0.242 0,520 -0.334

0.410 -0.296 0.540 -0,300

0.430 -0.266 0.550 -0.309

0,440 -0.248 0.580 -0.296

0.460 -0.254 0,600 -0.321

0,470 -0.288 0.610 -0.331

0,490 -0.284 0.650 -0,483

0.500 -0.291 0,700 -0.381

0.520 -0.271 0,750 -0.387

0,530 -0.281 0,820 -0.335

0,550 -0.318 0.890 -0.135

0,560 -0.307 0,900 -0.099

0.580 -0.278 0,960 0.032

0.590 -0.328

0.600 -0,306

0.640 -0,349

0,700 -0,326

0,750 -0,028**

0.820 -0274

0.870 -0.228

0.930 -0.104

0,960 -0.038

Lower Surface

0.020 -0.416 0.020 -0.316 0.020 -0.090 0,020 0.249

0.110 -0.256 0.060 -0.126 0,060 -0.028 0.060 -0.031

0.230 -0.128 0,090 -0.153 0.090 -0.097 0.110 -0,094

0.400 -0.125 0.120 -0.208 0.120 -0,348 0.250 -0.275

0,490 -0,077 0,200 -0.165 0.200 -0.209 0.400 -0.267

0,630 4,427** 0.260 -0,240 0,250 -0.236 0.490 -0.287

0,750 0.012 0.400 -0.178 0.400 -0,223 0.580 -0.291

0,850 0.071 0,490 -0.179 0.490 -0,072 0.650 -0.148

0.900 0.175 0.580 -0.177 0,580 -0.227 0.750 0,095

0,960 0,148 0,640 0.001 0.650 -0.056 0.830 0.236

0,750 0.1 64 0.750 -0.037 0.900 0.292

0.870 0.194 0.890 0,276 0.960 0.241

0.930 0.196 0.930 0.230

0.960 0.158 0.960 0.273

CN = 0.137 0.222 0.231 0.282

216
Table E-2. Continued,

Flight 224, Wing sweep = 26 °. Time = 10-3-54-500, MINF = 0.802, Camber = 0/2. ALPT = 8.01, BETA = 0.11, QINF = 292,5,

RNPU = 2.4E+06, CNWP = 0.3170

TI= 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.167 0.000 0.651 0.000 4.351 ** 0.010 - 1.294

0.060 - 1.139 0.020 - 1.410 0.020 - 1.225 0.020 - 1.293

0.110 - 1.141 0.040 -1.169 0.060 -5.239** 0.060 - 1.333

0.200 -0.674 0.060 - 1.212 0.090 - 1.212 0,110 - 1.259

0,230 -0,224 0,090 -1,167 0A 10 -1.307 0.140 -1.223

0.400 -0.209 0.130 -1.158 0.130 -1.199 0.190 -2.223**

0.490 -0.248 0.150 -1.159 0.150 -1.181 0.250 -1.241

0.590 -0.280 0.200 - 1.065 0.210 - 1.158 0.400 -0,467

0.630 -0.271 0.250 - 1.145 0,250 - 1.110 0.490 -0.257

0.700 -0,243 0.260 - 1.061 0.340 -0,863 0,580 -0,278

0.750 -0.303 0,280 - 1. 133 0,370 -0.612 0.650 -0.294

0.810 -0.295 0.290 - 1.133 0,400 -0.524 0.700 -0.287

0.840 -0.240 0.310 - 1.101 0,410 -3.244"* 0.750 -0.278

0.900 -0,182 0,320 - 1.066 0.430 -0.464 0,800 -0,300

0,960 -0,086 0.340 -0.541 0.440 -0.404 0.830 -0.222

0,350 -0,298** 0,460 -0,365 0.900 -0.105

0.370 -0.363 0.490 -0.210 0.960 -0.010

0.380 -0.370 0.500 -0.291

0.400 -0.192 0,520 -0.234

0.410 -0.238 0,540 -0,196

0.430 -0.175 0.550 -0.174

0.440 -0.122 0.580 -0.167

0.460 -0.179 0.600 -0.187

0.470 -0,134 0.610 -0.212

0.490 -0.149 0.650 2.946"*

0.500 -0.169 0,700 -0.296

0.520 -0.210 0.750 -0.352

0.530 -0.194 0.820 -0.264

0.550 -0.250 0.890 -0.086

0.560 -0.236 0.900 -0.051

0.580 -0.232 0.960 0.042

0,590 -0.260

0.600 -0284

0.640 -0.285

0.700 -0.296

0.750 -0.019"*

0,820 -0.238

0,870 -0.205

0,930 -0,092

0.960 -0.029

Lower Surface

0.020 0.167 0.020 0.338 0.020 0.451 0.020 0.695

0.110 -0.055 0.060 0.236 0.060 0.356 0.060 2.649"*

0.230 0,008 0.090 0,141 0,090 1,932** 0,110 0,196

0.400 0.020 0.120 0.098 0.120 -0.123 0.250 -0.027

0.490 0.006 0,200 0.031 0.200 -0,005 0,400 -0.068

0.630 2.710"* 0.260 -0.050 0.250 0.007 0.490 -0.136

0.750 0.015 0.400 -0.060 0.400 -0.067 0.580 -0.193

0.850 0.096 0.490 -0,099 0.490 -0.002 0,650 -0,062

0.900 0.167 0.580 -0.096 0,580 -0,092 0,750 0,137

0.960 0.122 0.640 0.078 0,650 -0.040 0.830 0.335

0.750 0.215 0.750 -0.009 0.900 0.352

0.870 0.266 0.890 0,279 0.960 0.260

0.930 0.202 0.930 0.249

0.960 0.168 0.960 -3.333 **

CN = 0.392 0.592 0.549 0.637

217
Table E-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 10-4-3-000, MINF = 0.807, Camber = 0/2, ALPT = 10.17, BETA = 0.19, QINF = 298.9,

RNPU = 2.4E+06, CNWP = 0.4287

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP xYc CP x/c CP x,/c CP

0.020 - 1.350 0.000 0.487 0,000 4.236"* 0.010 -1.488

0.060 - 1.342 0,020 - 1.580 0.020 - 1.406 0.020 - 1.487

0.110 - 1.281 0.040 - 1.394 0.060 -5.147"* 0.060 - 1.526

0.200 - 1.018 0.060 - 1.364 0.090 - 1,376 0.110 - 1.439

0.230 -0.859 0.090 - 1.335 0.110 - 1.469 0.140 - 1.438

0.400 -0.233 0.130 - 1.331 0.130 - 1.393 0.190 -2.196"*

0.490 -0.237 0.150 - 1.324 0.150 - 1.374 0.250 - 1.406

0.590 -0.304 0.200 - 1,249 0.210 - 1.218 0.400 -0.791

0.630 -0.295 0.250 - 1.137 0.250 -0.707 0.490 -0.441

0,700 -0.252 0.260 -0.908 0.340 -0.738 0.580 -0.274

0.750 -0.324 0.280 -0.997 0.370 -0.740 0,650 -0.249

0.810 -0.319 0.290 -0.910 0.400 -0.749 0.700 -0.252

0.840 -0.294 0.310 -0.842 0.410 -3.195"* 0.750 -0.220

0.900 -0.220 0.320 -0.799 0.430 -0,656 0.800 -0.249

0.960 -0.125 0.340 -0.725 0.440 -0.631 0.830 -0.202

0.350 -0,379** 0.460 -0.648 0900 -0.129

0.370 -0.633 0.490 -0.598 0.960 -0.066

0.380 -0.666 0.500 -0.637

0.400 -0.510 0.520 -0.583

0.410 -0.558 0,540 -0.607

0.430 -0.533 0.550 -0.555

0.440 -0.431 0.580 -0.506

0.460 -0.486 0.600 -0.525

0.470 -0.421 0.610 -0.536

0.490 -0.368 0.650 2.861 **

0.500 -0,370 0.700 -0.498

0.520 -0.368 0.750 -0.561

0.530 -0.303 0,820 -0.389

0.550 -0,363 0.890 -0.236

0.560 -0.282 0.900 -0.249

0.580 -0.310 0.960 -0.154

0,590 -0.268

0.600 -0,294

0.640 -0.207

0,700 -0.237

0.750 -0.003"*

0.820 -0.156

0.870 -0.188

0.930 -0.178

0.960 -0.163

Lower Surface

0.020 0.265 0.020 0.511 0.020 0.590 0.020 0.784

0.110 0.023 0.060 0,349 0.060 0.456 0.060 2.571 **

0,230 0,035 0.090 0.243 0.090 1.869"* 0.110 0.317

0.400 -0,020 0.120 0.170 0.120 -0.024 0,250 0.062

0.490 -0.008 0,200 0.108 0.200 0.065 0.400 0,001

0.630 2.631 ** 0.260 0.002 0.250 0,082 0.490 -0.087

0.750 -0.011 0.400 -0,024 0,400 -0.012 0.580 -0.150

0.850 0.072 0.490 -0.073 0,490 0.007 0.650 -0,038

0.900 0.137 0.580 -0.090 0.580 -0.081 0,750 0.158

0.960 0.106 0,640 0.051 0.650 -0.022 0.830 0.313

0.750 0.177 0.750 0.000 0,900 0.329

0.870 0.209 0,890 0.246 0.960 0.234

0.930 0.137 0,930 0.193

0.960 0,074 0.960 -3.282**

CN = 0.504 0.676 0.722 0.792

218
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-32-45-500, MINF = 0.803, Camber = 5/2, ALP'I" = 5.49, BETA = 0.05. QINF = 303.4,

RNPU = 2.5E+06, CNWP = 0.2974

1] = 0.93 0.76 0.59 0.40

Upper S,rface

x/c CP xA" CP x,/c CP x/c CP

0.020 0.138 0.000 0.728 0.000 0.463** 0.010 -0.548

0.060 -0.191 0.020 -0. [ 44 0.020 -0.073 0.020 -0.364

0.110 -0.419 0.040 -0.051 0.060 0.030"* 0.060 -0.750

0.200 -0.310 0.060 -0.406 0.090 -0.511 0.1 l0 -0.905

0.230 -0.310 0.090 -0,482 0.110 -0.707 0.140 - 1.1 I 1

0.400 -0.233 0.130 -0,629 0.130 -2.218 * * 0.190 -2.218 **

0.490 -0.212 0.150 -0.843 0.150 -0.933 0.250 -0.682

0.590 -0.234 0.200 -0.877 0.210 -0.963 0.400 -0.397

0.630 -0.252 0.250 -0.955 0.250 -0.951 0.490 -0.343

0.700 -0.211 0.260 -0.569 0.340 -0.336 0.580 -0.338

0.750 -0.253 0.280 -0.374 0.370 -0.345 0.650 -0.407

0.810 -0.247 0.290 -0.305 0.400 -0.333 0.700 -0.382

0.840 -0.226 0.310 -0.291 0.410 -3.202"* 0.750 -0.407

0.900 -0.136 0.320 -0.294 0.430 -0.360 0.800 -0.380

0.960 -0.028 0.340 -0.281 0.440 -0.316 0.830 -0.327

0.350 -0.174** 0.460 -0.343 0.900 -0.187

0.370 -0.287 0.490 -0.331 0.960 -0.007

0.380 -0.332 0.500 -0.351

0.400 -0.264 0.520 -0.352

0.410 -0.327 0.540 -0.326

0.430 -0.296 0.550 -0.327

0.440 -0.256 0.580 -0.319

0460 -0.325 0.600 -0,338

0.470 -0.323 0.610 -0,346

0490 -0.311 0.650 -0,586

0.500 -0.316 0,700 -0,404

0.520 -03 t2 0.750 -0.432

0.530 -0.305 0.820 -0.340

0.550 -0.351 0.890 -0.133

0.560 -0.332 0.900 -0,096

0.580 -0.303 0.960 0,046

0.590 -0.340

0.600 -0.344

0.640 -0.375

0.700 -0.342

0.750 -0.021 **

0.820 -0.276

0.870 -0.236

0.930 -0.102

0.960 -0.027

Lower Surface

0.020 -0.519 0.020 -0.400 0,020 -0.244 0.020 0.071

0.110 -0.179 0.060 -0.064 0.060 0,009 0.060 -0.016

0.230 -0.025 0.090 -0.108 0.090 -0.036 0.110 -0.039

0,400 -0.071 0.120 -0.081 0.120 -0.307 0.250 -0.158

0.490 -0.048 0.200 -0.026 0.200 -0.059 0.400 -0.182

0.630 4.035" * 0.260 -0.108 0.250 -0.103 0.490 -0.229

0.750 0.009 0.400 -0.101 0.400 -0.140 0.580 -0.252

0.850 0.082 0.490 -0.131 0.490 -0.040 0.650 -0.121

0.900 0.180 0.580 -0.134 0.580 -0.177 0.750 0.126

0.960 0.143 0.640 0.039 0.650 -0.048 0.830 0.270

0.750 0,180 0.750 -0.026 0.900 0.320

0.870 0.217 0.890 0.288 0.960 0.257

0.930 0.225 0.930 0.245

0.960 0.175 0.960 0.378

CN = 0.208 0.367 0.395 0.428

219
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-33-21-500, MINF = 0.806, Camber = 5/2. ALPT = 6.89, BETA = -0.59, QINF = 305.6,

RNPU = 2.5E+06, CNWP = 0.3231

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP .r./c CP

0.020 -0.058 0.000 0.817 0.000 0.432** 0.010 -0.830

0.060 -0.346 0.020 -0.347 0.020 -0.307 0.020 -0.708

0.1 I 0 -0.506 0.040 -0.243 0.060 -0.169'* 0.060 -0.887

0.200 -0.956 0,060 -0.585 0.090 -0.763 0.110 - 1.081

0.230 -0.815 0.090 -0,580 0.110 -0.870 0.140 - 1.295

0.400 -0.231 0.130 -0.746 0.130 -2.201 ** 0.190 -2.201 **

0.490 -0.221 0.150 -0.932 0.150 - 1.050 0.250 - 1.190

0.590 -0.281 0.200 -0.971 0.210 - 1.056 0.400 -0.421

0.630 -0.273 0.250 - 1.060 0.250 - 1.067 0.490 -0.359

0.700 -0.239 0.260 - 1.011 0.340 -0.821 0.580 -0.345

0.750 -0.285 0.280 - 1.046 0.370 -0.512 0,650 -0.393

0,810 -0.280 0.290 -1.029 0.400 -0.373 0.700 -0.378

0.840 -0.261 0.310 -0.985 0.410 -3.179"* 0.750 -0.390

0.900 -0.172 0.320 -0.996 0.430 -0.328 0.800 -0,353

0.960 -0.063 0.340 -0.706 0.440 -0.283 0.830 -0.306

0,350 -0.272"* 0,460 -0.297 0.900 -0.150

0,370 -0.357 0.490 -0.269 0.960 0.005

0.380 -0,342 0.500 -0,302

0.400 -0.240 0.520 -0.300

0.410 -0.258 0.540 -0.296

0.430 -0.214 0.550 -0.301

0.440 -0.178 0.580 -0,299

0,460 -0.252 0.600 -0.311

0.470 -0.225 0.610 -0.309

0.490 -0.253 0.650 -0.590

0.500 -0.270 0.700 -0.390

0.520 -0.272 0.750 -0.432

0.530 -0.271 0.820 -0.346

0.550 -0.321 0.890 -0,131

0.560 -0.311 0.900 -0.095

0.580 -0.281 0.960 0.036

0,590 -0.325

0.600 -0.332

0.640 -0.372

0.700 -0.353

0.750 -0,020**

0.820 -0.296

0.870 -0.248

0.930 -0.112

0.960 -0.037

Lower Surface

0.020 -0.376 0.020 -0.149 0,020 -0.028 0.020 0,309

O. 110 -0.125 0.060 0.047 0.060 O. 132 0.060 -0.019

0.230 0.013 0.090 -0.007 0.090 0.06 l O. 110 0.061

0.400 -0.059 O. 120 -0.008 O. 120 -0.212 0.250 -0.092

0.490 -0.032 0.200 0.017 0.200 -0.019 0.400 -0.127

0.630 4.007"* 0.260 -0,057 0.250 -0.045 0.490 -0.183

0.750 0.009 0.400 -0.067 0.400 -0.090 0.580 -0.211

0.850 0.067 0.490 -0.104 0.490 -0.039 0.650 -0.106

0.900 0.163 0.580 -0.106 0.580 -0.1 40 0.750 0.135

0.960 0.121 0.640 0.062 0.650 -0.032 0.830 0,277

0.750 0.179 0.750 -0.025 0.900 0.324

0.870 0.234 0.890 0.301 0.960 0.256

0,930 0.213 0.930 0.255

0.960 0.170 0.960 0.356

CN = 0.338 0,483 0.502 0.567

22O
Table E-2, Continued.

Flight 191, Wing sweep = 26 °. Time = 11-2-4-000, MINF = 0.790, Camber = 5/2, ALPT = 5.99, BETA = 0.21, QINF = 291.5,

RNPU = 2.4E+06, CNWP = 0.3648

rI = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.105 0.000 0.776 0.000 -5,299** 0,010 -0,636

0.060 -0.178 0.020 -0,237 0.020 -0.108 0.020 -0.421

0.110 -0.282 0.040 -0.139 0.060 -0.198"* 0.060 -0.839

0,200 -0.324 0.060 -0.433 0.090 -0,573 0,110 -0.990

0,230 -0.404 0.090 -0.527 0,110 -0,799 0,140 - 1,136

0.400 -0.237 0.130 -0.692 0.130 -0,869 0.190 -5.970"*

0.490 -0.213 0.150 -0.893 0.150 -0.991 0.250 -0.532

0.590 -0.248 0.200 -0.891 0.210 -1.062 0.400 -0.350

0.630 -0.242 0.250 -0.557** 0.250 -0.953 0.490 -0.376

0.700 -0,197 0.260 -0.2% 0.340 -0.331 0.580 -0.369

0.750 -0,245 0.280 -0.353 0.370 -0.339 0,650 -0.385

0.810 -0.292 0.290 -0.343 0,400 -0.372 0.700 -0.394

0.840 -0.216 0,310 -0,321 0.410 -0.314 0.750 -0.413

0.900 -0,120 0.320 -0.295 0.430 -0.360 0,800 -0,410

0.960 -0,049 0.340 -0.302 0.440 -0.336 0.830 -0.339

0.350 -0.221 ** 0.460 -0.342 0.900 -0.166

0.370 -0,295 0.490 -0.276 0.960 -0,002

0.380 -0,323 0,500 -0,361

0.400 -0,220 0.520 -0.299

0.410 -0.358 0.540 -0.322

0.430 -0.330 0.550 -0.340

0.440 -0,252 0,580 -0.345

0.460 -0.396 0,600 -0.324

0.470 -0.313 0.610 -0,276

0.490 -0.316 0.650 -3.158 **

0.500 -0.308 0.700 -0.427

0.520 -0.330 0.750 -0.490

0.530 -0.275 0.820 -0.342

0.550 -0.332 0.890 -0.132

0,560 -0,313 0.900 -0.106

0.580 -0.284 0.960 0.004

0.590 -0.323

0.600 -0.379

0.640 -2.992"*

0.700 -0.339

0.750 -0.272

0.820 -3.170"*

0.870 -0.225

0.930 -0.094

0.960 -0.015

Lower Surface

0.020 -0.449 0.020 -0.355 0.020 -0.231 0.020 0.094

0.1 t0 -0.160 0.060 -0.020 0.060 0.078 0.060 2.723"*

0.230 0.000 0.090 -0.085 0.090 -0,039 0,110 -0.071

0.400 -0.036 0.120 -0.021 0.120 -0.420** 0.250 -0.122

0.490 -0.078 0,200 0.015 0,200 -0.124 0,400 -0,14 I

0.630 2.748"* 0.260 -0.130 0.250 -0.052 0.490 -0.252

0.750 0.023 0A00 -3.188" * 0.400 -0.108 0.580 -0.229

0.850 0.107 0.490 -0.124 0.490 0.015 0,650 -0.112

0,900 0,192 0.580 -0,042 0.580 -0.149 0.750 0.138

0,960 0,151 0.640 0.286 0.650 0.024 0.830 0.292

0.750 0.174 0.750 0,268 0,900 0.380

0.870 0.221 0.890 ******** 0.960 0.283

0.930 0,231 0.930 0.268

0.960 0.147 0.960 -2.920 **

CN = 0.218 0.382 0.472 0.434

221
Table E-2. Continued.

Flight 191, Wing sweep = 26 °, Time = 11-2-10-500, MINF = 0,789, Camber = 5/2, ALPT = 7.09, BETA = 0.42, QINF = 291.4,

RNPU = 2.4E+06, CNWP = 0.3776

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0,020 -0.064 0,000 0,870 0.000 -5.307 ** 0.010 -0.996

0.060 -0.321 0.020 -0.505 0.020 -0.330 0.020 -0.586

0.110 -0.496 0.040 -0.288 0.060 -0,283"* 0.060 -0.960

0,200 -0,968 0,060 -0.582 0,090 -0.737 0.110 - 1.144

0,230 -0.366 0.090 -0,625 0.110 -0,930 0.140 - 1.279

0.400 -0,228 0.130 -0.791 0.130 -0,972 0.190 -5.978"*

0.490 -0.219 0.150 -0.977 0.150 - 1.059 0,250 -0,869

0.590 -0.251 0.200 -0,967 0.210 - 1.130 0,400 -0.348

0,630 -0.253 0,250 - 1.138** 0.250 - 1.079 0.490 -0.377

0,700 -0.199 0.260 -0.996 0,340 -0.448 0.580 -0.360

0.750 -0.252 0.280 - 1.081 0.370 -0,330 0,650 -0.376

0.810 -0.299 0.290 -0,960 0.400 -0,333 0.700 -0.379

0,840 -0,234 0.310 -0.480 0.410 -0,265 0,750 -0.389

0.900 -0.136 0,320 -0,407 0.430 -0.319 0.800 -0.371

0.960 -0.070 0,340 -0.315 0,440 -0.288 0.830 -0.306

0,350 -0.185"* 0.460 -0.319 0.900 -0.144

0.370 -0.222 0,490 -0.251 0.960 0.012

0,380 -0,245 0.500 -0.313

0.400 -0.155 0,520 -0.255

0.410 -0,289 0,540 -0,313

0.430 -0.272 0,550 -0.319

0.440 -0.209 0.580 -0.300

0.460 -0.350 0.600 -0.303

0.470 -0.271 0.610 -0.253

0.490 -0.283 0,650 -3.165**

0.500 -0.282 0.700 -0.385

0.520 -0,289 0.750 -0.473

0,530 -0.270 0,820 -0.333

0.550 -0.314 0.890 -0.127

0,560 -0.285 0,900 -0,099

0.580 -0.275 0,960 0.013

0.590 -0.314

0.600 -0.375

0.640 -2,999**

0.700 -0,330

0.750 -0,281

0,820 -3.177"*

0.870 -0.219

0,930 -0.096

0.960 -0,002

Lower Surface

0.020 -0.402 0.020 -0.135 0.020 -0.028 0.020 0.281

0.110 -0. I 11 0,060 0,096 0,060 0.196 0.060 2.718" *

0.230 0.044 0.090 0.003 0.090 0.069 0.110 0.022

0.400 0.003 0.120 0.011 0.120 -0.322 ** 0.250 -0.048

0,490 -0.054 0,200 0.061 0,200 -0.042 0.400 -0.079

0.630 2.743"* 0.260 -0.072 0,250 0.003 0.490 -0.196

0.750 0.051 0.400 -3.195"* 0,400 -0,057 0,580 -0.198

0. 850 0.105 0,490 -0.088 0.490 0.017 0.650 -0.088

0.900 0.188 0,580 -0.029 0.580 -0,118 0.750 0.157

0,960 0.147 0.640 0.301 0,650 0,044 0.830 0.315

0.750 0.166 0,750 0.270 0.900 0.380

0,870 0,230 0.890 ******** 0.960 0,284

0.930 0.232 0,930 0.270

0,960 0.164 0.960 -2,927"*

CN = 0.306 0.479 0.534 0.538

222
Table E-2. Continued.

Flight 191, Wing sweep = 26 °, Time = 11-2-17-500, MINF = 0.788, Camber = 5/2, ALPT = 8.09, BETA = 0.42, Q1NF = 292.3,

RNPU = 2.4E+06, CNWP = 0.4171

1"1= 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,287 0,000 0.912 0.000 -5.304"* 0.010 - 1.012

0.060 -0,498 0.020 -0.755 0.020 -0.506 0.020 - 1.015

0.110 -0.527 0.040 -0.431 0.060 -0.313"* 0.060 - 1,063

0.200 - 1.032 0.060 -0.768 0.090 -0.926 0. I 10 - 1.280

0.230 -0,927 0,090 -0.850 0.110 - 1.081 0.140 - 1.371

0.400 -0.240 0.130 -0.937 0.130 - 1.116 0.190 -5.973" *

0.490 -0.224 0.150 -1.083 0.150 - 1.199 0.250 - 1.394

0.590 -0.263 0.200 - 1.048 0.210 - 1.260 0.400 -0.367

0.630 -0.257 0.250 - 1.239"* 0.250 - 1.200 0.490 -0.364

0.700 -0.211 0.260 - 1,081 0.340 -0.999 0.580 -0.345

0.750 -0.268 0.280 - 1.185 0.370 -0.618 0.650 -0.347

0.810 -0,327 0,290 - 1.195 0,400 -0.546 0.700 -0.338

0.840 -0.247 0.310 -1.104 0.410 -0.430 0.750 -0.333

0.900 -0.161 0.320 - 1.079 0,430 -0,427 0,800 -0.309

0.960 -0,096 0.340 - 1.071 0.440 -0.329 0.830 -0.255

0.350 -0.331 ** 0.460 -0.316 0.900 -0.094

0.370 -0.460 0.490 -0.218 0.960 0.018

0.380 -0.417 0.500 -0.300

0.400 -0,253 0.520 -0.198

0.410 -0.337 0.540 -0,238

0.430 -0.245 0.550 -0.265

0.440 -0.174 0.580 -0.260

0.460 -0.285 0.600 -0.262

0.470 -0.194 0.610 -0,192

0.490 -0.215 0,650 -3.168"*

0.500 -0.224 0.700 -0.334

0,520 -0.231 0.750 -0.436

0.530 -0.220 0.820 -0.287

0.550 -0.264 0.890 -0.100

0.560 -0.243 0.900 -0.080

0.580 -0.231 0.960 0.015

0.590 -0.276

0.600 -0.341

0.640 -3,002"*

0.700 -0.308

0.750 -0.271

0.820 -3.181"*

0.8?0 -0.23 I

0.930 -0.078

0.960 -0.018

Lower Surface

0.020 -0.199 0.020 0.067 0.020 0.135 0.020 0.426

0. I 10 -0.053 0.060 0.197 0.060 0.293 0.060 2.698" *

0.230 0.085 0.090 0.099 0.090 0.158 0.110 0.087

0.400 0.013 0.120 0,105 0.120 -0.254"* 0.250 0.009

0.490 -0.051 0.200 0.085 0.200 -0,036 0.400 -0.031

0.630 2_723"* 0.260 -0.017 0.250 0.059 0.490 -0.155

0.750 0.022 0.400 -3.198"* 0.400 -0.013 0.580 -0.159

0.850 0.095 0.490 -0.062 0.490 0.004 0.650 -0.062

0.900 0.178 0.580 -0.011 0.580 -0.092 0.750 0.179

0.960 O. 132 0.640 0.313 0.650 0.061 0.830 0.320

0.750 0.193 0.750 0.264 0.900 0.373

0,870 0.231 0.890 ******** 0.960 0.279

0.930 0.245 0.930 0.257

0.960 0.158 0.960 -2.931 **

CN = 0.395 0.590 0.624 0.657

223
Table E-2, Continued.

Flight 191, Wing sweep = 26 °, Time = 11-2-24-000, MINF = 0.790. Camber = 5/2, ALPT = 10.07, BETA = 0.36, QINF = 299.3,

RNPU = 2.5E+06, CNWP = 0,4967

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x,/c CP

0.020 -0.833 0.000 0.819 0.000 -5.222"* 0.010 - 1.227

0.060 -0.766 0.020 -1.219 0.020 -0.995 0.020 - 1.229

0.110 -0.738 0,040 -0,816 0.060 -0.486"* 0.060 - 1.340

0.200 -1.148 0.060 -0.982 0.090 -I .141 0.110 -1.452

0.230 - 1.040 0.090 - 1.036 0.110 - 1.300 0.140 - 1.508

0.400 -0.235 0.130 - 1.176 0,130 - 1,316 0,190 -5.875"*

0.490 -0.204 0.150 - 1.285 0.150 - 1.356 0.250 - 1.588

0.590 -0,295 0.200 - 1.263 0.210 - 1.451 0.400 -0.863

0.630 -0.312 0.250 - 1.416"* 0.250 - 1.366 0,490 -0.378

0.700 -0.251 0.260 - 1.260 0.340 -0,790 0,580 -0.249

0.750 -0.316 0,280 - 1.366 0.370 -0.731 0.650 -0.257

0.810 -0.372 0.290 - 1.385 0.400 -0.759 0.700 -0.230

0.840 -0.316 0.310 -1.232 0.410 -0.670 0.750 -0.237

0.900 -0.226 0.320 -1.202 0.430 -0.710 0.800 -0.266

0.960 -0.158 0.340 -0.898 0.440 -0.662 0.830 -0,187

0.350 -0.345** 0.460 -0.672 0.900 -0.! 14

0.370 -0,692 0.490 -0.569 0.960 -0.038

0.380 -0,688 0.500 -0,643

0.400 -0.580 0.520 -0.577

0.410 -0.639 0.540 -0.580

0.430 -0.557 0.550 -0.590

0.440 -0.453 0.580 -0.555

0.460 -0.540 0.600 -0.510

0.470 -0.409 0.610 -0. 390

0.490 -0.414 0.650 -3.136**

0.500 -0.370 0,700 -0.404

0.520 -0,372 0.750 -0.497

0.530 -0,305 0.820 -0.270

0.550 -0.306 0.890 -0.155

0.560 -0,285 0.900 -0.174

0.580 -0,277 0,960 -0.141

0.590 -0.293

0.600 -0.362

0.640 -2,975**

0,700 -0.282

0.750 -0.228

0.820 -3.149"*

0.870 -0.196

0.93O -0.095

0.960 -0.047

Lower Surface

0.020 0.001 0.020 0.370 0,020 0.382 0.020 0.617

0.110 0,031 0.060 0.353 0,060 0.460 0.060 2,590**

0.230 0.151 0.090 0,218 0.090 0.287 0.110 0.212

0.400 0.017 0.120 0.207 0.120 -0.115"* 0,250 0,100

0.490 -0,035 0.200 0.167 0.200 0.041 0.400 0.032

0.630 2,615"* 0.260 0,049 0.250 0.146 0.490 -0,092

0.750 0.018 0,400 -3.166 ** 0.400 0.004 0.580 -0.109

0.850 0.073 0.490 -0.030 0.490 0.034 0,650 -0.046

0.900 0.154 0.580 0.000 0,580 -0.061 0.750 0.180

0.960 0.103 0.640 0.298 0,650 0.060 0.830 0.323

0.750 0.170 0.750 0.273 0.900 0.381

0.870 0.204 0,890 ******** 0.960 0.252

0.930 0,200 0.930 0,227

0.960 0.114 0.960 -2.905**

CN =

0,484 0.725 0.796 0.809

224
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-12-44-000, MINF = 0.801, Camber = 5/6, ALPT = 5.01, BETA = -0,10, QINF = 302A,

RNPU = 2.5E+06, CNWP = 0.3585

rl = 093 076 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 O. 184 0.000 0.692 0.000 0.625" * 0,010 -0.459

0.060 -0.177 0.020 0.001 0.020 -0.027 0.020 -0.315

O. 110 -0.498 0.040 -0.0 l5 0.060 -0.195"* 0.060 -0,724

0.200 -0.309 0.060 -0.347 0,090 -0.515 0,110 -0.856

0.230 -0,337 0.090 -0.446 0,110 -0.669 0.140 - 1.031

0,400 -0.257 0.130 -0.609 0,130 -2.228** 0.190 -2.228"*

0,490 -0,242 0.150 -0.816 0.150 -0.923 0.250 -0.643

0.590 -0.323 0.200 -0.855 0.210 -0.943 0.400 -0.404

0.630 -0,343 0.250 -0.630 0.250 -0,933 0.490 -0.362

0,700 -0.385 0.260 -0.394 0.340 -0.368 0,580 -0.377

0.750 -0,664 0.280 -0.329 0,370 -0,3% 0.650 -0.475

0.810 -0,525 0.290 -0.330 0,400 -0,364 0.700 -0.436

0.840 -0.520 0.310 -0.320 0.410 -3,216"* 0,750 -0.510

0.900 -0.202 0.320 -0.336 0.430 -0,392 0.800 -0.775

0.960 -0.056 0.340 -0,349 0.440 -0.385 0.830 -0.945

0.350 -0.182** 0.460 -0.376 0.900 -0.150

0.370 -0.336 0.490 -0.371 0.960 -0.081

0.380 -0,382 0.500 -0.394

0.400 -0.327 0.520 -0,392

0.410 -0.357 0,540 -0,379

0.430 -0.341 0.550 -0,361

0.440 -0.311 0.580 -0.341

0.460 -0.344 0.600 -0.402

0.470 -0.368 0.610 -0.420

0.490 -0.368 0.650 -0.716

0.500 -0.353 0.700 -0.642

0.520 -0.376 0.750 -0595

0.530 -0.359 0.820 -0.892

0.550 -0,419 0,890 -0.167

0.560 -0.405 0.900 -0.123

0.580 -0.370 0,960 -0.043

0.590 -0.420

0.600 -0.395

0.640 -0,608

0700 -0.463

0.750 -0.021"*

0.820 -0.487

0.870 -0.433

0.930 -0,312

0,960 -0.227

Lower Surface

0.020 -0.479 0.020 -0.432 0.020 -0.293 0.020 0_025

O. 110 -0.163 0.060 -0.065 0.060 -0.015 0,060 -0.005

0.230 -0.014 0.090 -0.106 0.090 -0.044 0,110 -0.030

0.400 -0.038 0.120 -0.067 0,120 -0,268 0.250 -0.170

0.490 0.018 0.200 -0.023 0.200 -0.024 0,400 -0.169

0.630 4.053** 0.260 -0.065 0.250 -0.089 0.490 -0.179

0,750 0,092 0,400 -0.065 0.400 -0,092 0.580 -0.145

0,850 0.143 0,490 -0.065 0.490 -0.033 0.650 -0.008

0.900 0,258 0.580 -0.040 0.580 -0.069 0,750 0.226

0.960 0.176 0.640 0.162 0.650 -0.018 0.830 0.359

0.750 0.267 0,750 -0.011 0.900 0.410

0,870 0,306 0.890 0.397 0.960 0,279

0.930 0.265 0.930 0.327

0.960 0.183 0.960 0.311

CN = 0.342 0.486 0.517 0,526

225
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-13-5-500, MINF = 0.811, Camber = 5/6, ALPT = 6.08, BETA = 0.1 l, QINF = 308.1,

RNPU = 2.5E+06, CNWP = 0.3883

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.052 0.000 0.781 0.000 0.657** 0.0 l0 -0.719

0.060 -0.265 0.020 -0.155 0.020 -0.180 0.020 -0.415

0.110 -0.467 0.040 -0.115 0.060 -0.371 ** 0.060 -0.806

0.200 -0.913 0.060 -0.451 0.090 -0.642 0.110 -0.963

0.230 -0.767 0.090 -0.522 0.110 -0.716 0.140 - 1.143

0,400 -0.257 0.130 -0.684 0.130 -2.175"* 0.190 -2.175"*

0.490 -0.260 0.150 -0.858 0.150 -0.952 0.250 - 1.101

0.590 -0.334 0.200 -0.912 0.210 -0.969 0.400 -0.434

0,630 -0.370 0.250 -0.978 0.250 -0.997 0.490 -0.396

0.700 -0.379 0.260 -0.960 0.340 -1.011 0.580 -0.390

0.750 -0.800 0.280 -0.980 0.370 -0.560 0.650 -0.485

0.810 -0.735 0.290 -0.940 0.400 -0.390 0.700 -0.463

0.840 °0.742 0.310 -0.905 0.410 -3.144"* 0.750 -0.533

0.900 -0.249 0.320 -0.930 0.430 -0.345 0.800 -0.882

0.960 -0.094 0.340 -0.936 0.440 -0.313 0.830 -0.962

0.350 -0.303** 0.460 -0.325 0.900 -0.137

0.370 -0.401 0.490 -0.295 0.960 -0.070

0.380 -0.347 0.500 -0.349

0.400 -0.243 0.520 -0.356

0.410 -0.261 0.540 -0.336

0.430 -0.234 0.550 -0.334

0.440 -0.211 0.580 -0.342

0.460 -0.250 0.600 -0.367

0.470 -0.288 0.610 -0.402

0.490 -0.282 0.650 -0.692

0.500 -0.303 0.700 -0.616

0.520 -0.299 0.750 -0.602

0.530 -0.301 0.820 -0,879

0.550 -0.365 0.890 -0.165

0.560 -0.349 0.900 -0.135

0.580 -0.340 0.960 -0.054

0.590 -0.385

0.600 -0.387

0.640 -0.600

0.700 -0.470

0.750 -0.014'*

0.820 -0.500

0.870 -0.468

0.930 -0.314

0.960 -0.227

Lower Surface

0.020 -0.294 0.020 -0.250 0.020 -0.126 0.020 0.169

0.110 -0.139 0.060 0.005 0.060 0.084 0.060 0.005

0.230 0.007 0.090 -0.031 0.090 0.021 0.110 0.006

0.400 -0.021 0,120 -0.027 0.120 -0.195 0.250 -0.112

0.490 -0.009 0.200 0.023 0.200 -0.002 0.400 -0.127

0.630 3.984** 0.260 -0.026 0.250 -0.049 0.490 -0.144

0.750 0.104 0.400 -0.032 0.400 -0.075 0.580 -0.137

0.850 0.143 0.490 -0.043 0.490 -0.015 0.650 0.013

0.900 0.241 0.580 -0.025 0.580 -0.044 0.750 0.250

0.960 0.152 0.640 0.187 0.650 -0.029 0.830 0.364

0.750 0.266 0.750 0,002 0.900 0.412

0.870 0.328 0.890 0.392 0.960 0.309

0.930 0.266 0.930 0.323

0.960 0.200 0.960 0,311

CN = 0.458 0.586 0.592 0.647

226
Table E-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 9-49-26-500, MINF = 0.811, Camber = 5/6, ALPT = 7.02, BETA = 0.13, QINF = 280.8,

RNPU = 2.3E÷06, CNWP = 0.1721

"q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP xA" CP

0.020 -0.056 0.000 0.859** 0.000 -6.122"* 0.010 -0.894

0.060 -0.316 0.020 -0.436 0.020 -0.290 0.020 -0.671

O. 110 -0.411 0.040 -0.264 0.060 - 1.006** 0.060 -0.902

0.200 -0.955 0.060 -0.577 0.090 -0.749 O. 110 - 1.076

0.230 -0.825 0.090 -0.575 0.110 -0.880 0.140 2.019"*

0.400 -0.209 0.130 -0.752 0.130 -0,927 0.190 -5.980"*

0,490 -0.240 0.150 -0,903 0.150 - 1,001 0.250 - 1.179

0.590 -0.310 0.200 -0,902 0.210 - 1.080 0.400 -0.476

0_630 -0.337 0.250 - 1.069 0.250 - 1.069 0.490 -0.445

0.700 -0.366 0.260 -0.977 0.340 - 1.098 0.580 -0.413

0.750 -0.776 0.280 - 1.040 0.370 - 1.057 0.650 -0.478

0.810 -0.791 0.290 - 1,051 0.400 - 1.057 0.700 -0.474

0.840 -0.748 0.310 -0.962 0.410 -0,805 0.750 -0.541

0.900 -0.222 0.320 -0.954 0.430 -0,616 0.800 -0.762

0,960 -0.129 0.340 - 1.000 0.440 -0,453 0.830 -0.952

0.350 -0.419"* 0.460 -0.397 0.900 -0.121

0.370 -0.953 0.490 -0,282 0.960 -0.053

0.380 -0.982 0.500 -0.308

0.400 -0.895 0,520 -0.277

0.410 -0.721 0,540 -0.281

0.430 -0.426 0.550 -0.297

0.440 -0.310 0.580 -0.303

0.460 -0.375 0.600 -0.330

0.470 -0.219 0.610 3.568

0.490 -0.229 0.650 -3,070"*

0.500 -0.220 0.700 -0.509

0.520 -0.208 0.750 -0.522

0.530 -0.208 0.820 -0.880

0.550 -0.241 0.890 -0.140

0,560 -0.262 0.900 -0.104

0.580 -0.251 0.960 -0.059

0.590 -0.308

0.600 -0.336

0.640 -2.898**

0.700 -0.459

0.750 -0.664

0.820 -3.084**

0.870 -0.414

0.930 -0.280

0.960 -0.222

Lower Surface

0.020 -0.321 0.020 -0.172 0.020 -0.019 0.020 0.267"*

0.110 -0.102 0.060 0.111 0.060 0.188 0.060 6.865" *

0.230 0.057 0.090 0.030 0.090 0,082 0.110 0.044

0.400 0.003 0.120 0.042 0.120 -0.250 0,250 -0,051

0.490 -0.009 0.200 0,098 0.200 -0,004 0,400 -0.059

0.630 4,535 ** 0.260 -0.005 0,250 0,030 0.490 -0.113

0.750 0.092 0.400 -3.102"* 0.400 -0,016 0.580 -0.108

0.850 0.192 0.490 -0,004 0.490 0.071 0.650 0.036

0.900 0.242 0.580 0,060 0.580 -0.017 0.750 0.289

0.960 0.145 0.640 0,432 0,650 0,189 0.830 0.406

0.750 0,253 0,750 0,062 0.900 0.470

0.870 0,324 0.890 ******** 0.960 0.318

0.930 0.291 0,930 0.348

0.960 0.173 0.960 -3.101 **

CN = 0.469 0.681 0.477 0.711

227
Table E-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 9-49-39-500, MINF = 0.800, Camber = 5/6, ALPT = 8.11, BETA = 0.02, QINF = 275.5,

RNPU = 2.3E+06, CNWP = 0.4730

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0,290 0.000 0,886"* 0,000 -6.2634" 0.010 -0,979

0.060 -0.519 0.020 -0.731 0.020 -0,522 0.020 -0.981

0,110 -0,608 0.040 -0.428 0,060 - l. 190* 4 0.060 - 1.056

0,200 - 1,022 0,060 -0.749 0.090 -0.933 0.110 - 1.223

0.230 -0,894 0,090 -0.828 0.110 - 1.069 0.140 2.082 **

0.400 -0.239 0.130 -0.935 0,130 -1.095 0,190 -6,119"*

0.490 -0.232 0.150 -1,056 0.150 -1,123 0,250 -1.351

0.590 -0.325 0.200 - 1,038 0.210 - 1.236 0.400 -0.665

0,630 -0,360 0.250 - 1.209 0,250 - 1,200 0.490 -0.481

0.700 -0.385 0.260 - 1.076 0,340 - 1,245 0.580 -0.415

0,750 -0.792 0.280 - 1.169 0.370 - 1.198 0,650 -0,463

0,810 -0,840 0,290 - 1.175 0.400 - 1.188 0,700 -0.482

0.840 -0.788 0.310 -1,078 0,410 -1,171 0,750 -0,544

0.900 -0.271 0.320 - 1.077 0,430 - 1.224 0,800 -0.481

0.960 -0.154 0,340 - 1.133 0.440 -0.860 0.830 -0.439

0,350 -0,42644 0.460 -0,660 0.900 -0.126

0,370 - 1.069 0,490 -0,505 0.960 -0.03 l

0.380 - 1.099 0.500 -0,514

0,400 - 1.022 0.520 -0.453

0.410 -1.118 0,540 -0,416

0,430 -1.088 0,550 -0.380

0,440 -0.771 0.580 -0.323

0.460 -0,646 0.600 -0.342

0.470 -0.447 0.610 -0,216

0.490 -0.387 0.650 -3.153"*

0,500 -0.335 0.700 -0.414

0.520 -0.321 0.750 -0,504

0.530 -0.230 0.820 -0.545

0,550 -0.232 0,890 -0.123

0,560 -0,229 0.900 -0.088

0.580 -0.196 0.960 -0.012

0,590 -0.253

0,600 -0.287

0.640 -2.977 *,

0.700 -0.436

0.750 -0,708

0.820 -3.166"*

0.870 -0.293

0.930 -0.213

0.960 -0.150

Lower Surface

0,020 -0,100 0,020 0.093 0,020 0.141 0,020 0.4564"

0.110 -0,022 0.060 0.230 0.060 0.295 0,060 6.973 *4

0.230 0.119 0.090 0.141 0.090 0,176 0.110 0.108

0.400 0,039 0.120 0.131 0,120 -0,186 0.250 0.030

0.490 0.015 0,200 0,147 0.200 0,037 0.400 0,008

0.630 4.598 *4 0,260 0.034 0.250 0,087 0,490 -0.067

0.750 0.114 0.400 -3.185** 0.400 0.024 0,580 -0.053

0,850 0,179 0.490 0,024 0.490 0.049 0,650 0.076

0.900 0,247 0,580 0,092 0,580 0,023 0,750 0.302

0,960 0.145 0.640 0,445 0,650 0,209 0.830 0,412

0,750 0,272 0.750 0.071 0.900 0,496

0.870 0,344 0,890 ,4*****4 0,960 0,342

0.930 0.313 0.930 0.374

0,960 0.188 0.960 -3.184**

CN = 0.559 0.794 0,764 0,799

228
Table E-2, Continued.

Flight 195, Wing sweep = 26 °, Time = 9-49-45-000, MINF = 0.798, Camber = 5/6, ALPT = 9.07, BETA = 0,10, QINF = 276.4.

RNPU = 2,3E+06, CNWP = 0.5332

rl = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.497 0.000 0.849** 0.000 -6.260** 0.010 -1.030

0.060 -0.607 0.020 -0.877 0.020 -0.808 0.020 - 1.074

0.110 -0.736 0.040 -0.523 0.060 - 1.177" * 0.060 - 1.198

0.200 - 1.075 0.060 -0.816 0.090 - 1.025 0.110 - 1.317

0.230 -0.957 0.090 -0.952 0.110 -1.180 0,140 2.083**

0.400 -0.519 O, 130 - 1.058 O. 130 - 1.208 O. 190 -6.116" *

0.490 -0.233 0,150 - 1.153 0.150 - 1,223 0,250 - 1.458

0.599 -0.310 0.200 - 1.154 0.210 - 1.340 0.400 -0.879

0.630 -0.354 0,250 - 1.303 0.250 - 1.283 0.490 -0.624

0.700 -0.381 0.260 - 1.184 0.340 - 1.328 0.580 -0.450

0.750 -0.816 0.280 - 1.271 0.370 - 1.308 0.650 -0.431

0,810 -0.865 0.290 - 1,294 0.400 - 1.272 0.700 -0.427

0.840 -0.827 0.310 - 1.175 0.410 - 1,256 0.750 -0.464

0.900 -0.305 0.320 - 1.167 0.430 - 1.339 0.800 -0.372

0.960 -0.193 0.340 - 1.251 0.440 - 1.289 0.830 -0.352

0.350 -0.428" * 0.460 - 1.055 0.900 -0.125

0.370 - 1.177 0.490 -0.665 0.960 -0.027

0.380 - 1.203 0.500 -0.711

0.400 -1.118 0.520 -0.674

0.410 - 1.230 0.540 -0.672

0.430 - 1.199 0.550 -0.603

0.440 -1.084 0.580 -0.573

0.460 - 1.307 0.600 -0.549

0.470 - 1.023 0.610 -0.398

0.490 -0.658 0650 -3.160"*

0.500 -0.57 t 0.700 -0.371

0.520 -0.530 0.750 -0445

0.530 -0.465 0.820 -0.360

0.550 -0.443 0.890 -0.126

0.560 -0.381 0.900 -0.080

0.580 -0.346 0.960 -0.029

0.590 -0.332

0.600 -0.319

0.640 -2.985**

0.700 -0,361

0.750 -0.601

0,820 -3.173"*

0.870 -0.328

0.930 -0.123

0.960 -0.024

Lower Surface

0.020 0.002 0.020 0.262 0.020 0.257 0.020 0.582**

0.110 0,022 0.060 0.312 0.060 0.389 0,060 6.933**

0.230 0.162 0,090 0.200 0.090 0.241 0. I 10 0.193

0.400 0.069 0.120 0.178 0.120 -0.089 0.250 0.066

0.490 0.037 0.200 0.185 0.200 0.093 0,400 0,046

0.630 4.566** 0.260 0.072 0.250 0.133 0.490 -0.036

0.750 0.123 0.400 -3.192"* 0,400 0,065 0.580 -0.027

0,850 0.172 0.490 0.058 0.490 0.063 0.650 0.09 I

0.900 0.231 0.580 0,127 0.580 0.045 0.750 0.326

0,960 0.139 0.640 0.454 0,650 0.215 0,830 0,416

0.750 0.311 0,750 0,085 0.900 0.519

0.870 0.338 0.890 ******** 0.960 0.345

0,930 0.319 0.930 0,363

0.960 0,214 0.960 -3.191 **

CN = 0.647 0.894 0.863 0.879

229
Table E-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 9-49-52-000, MINF = 0.797, Camber = 5/6, ALPT = 10.01, BETA = -0.16, QINF = 277.7,

RNPU = 2.3E+06, CNWP = 0.6196

1] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.858 0.000 0.775** 0.000 -6.245"* O.OlO -1.251

0.060 -0.798 0.020 - 1.153 0.020 - 1.008 0.020 - 1.193

O. 110 -0.793 0.040 -0.824 0.060 - 1.234** 0.060 - 1.290

0.200 -1.168 0.060 -0.961 0.090 -1.121 0.110 -1.410

0.230 - 1.017 0.090 - 1.031 0.110 - 1.286 0.140 2.068"*

0.400 -0.703 0.130 - 1.140 0.130 - 1.299 0.190 -6.102"*

0.490 -0.231 0.150 - 1,254 0.150 - 1.281 0.250 - 1.545

0.590 -0.311 0,200 - 1.239 0.210 - 1.424 0.400 - 1.008

0.630 -0.383 0,250 - 1.350 0.250 - 1.362 0.490 -0.758

0.700 -0.414 0.260 - 1.235 0.340 - 1.437 0.580 -0.431

0.750 -0.799 0.280 - 1.322 0.370 - 1.403 0.650 -0.385

0.810 -0.851 0.290 - 1.361 0.400 - 1.352 0.700 -0.371

0.840 -0.822 0.310 - 1.237 0.4 l0 - 1.334 0.750 -0.346

0.900 -0.329 0.320 - 1.248 0.430 - 1.049 0,800 -0.331

0.960 -0.199 0.340 - 1.319 0.440 -0.827 0.830 -0.309

0.350 -0.446** 0.460 -0.786 0.900 -0.123

0.370 - 1.264 0.490 -0.700 0.960 -0.042

0.380 -1.294 0.500 -0.769

0.400 - 1.209 0.520 -0.707

0.410 -1.268 0.540 -0.712

0.430 -0.859 0.550 -0.695

0.440 -0.759 0.580 -0,648

0.460 -0.833 0.600 -0,637

0.470 -0.707 0.610 -0.524

0.490 -0.665 0.650 -3.160**

0.500 -0.664 0.700 -0.468

0.520 -0.617 0.750 -0.484

0.530 -0,582 0,820 -0.315

0,550 -0.552 0,890 -0.189

0.560 -0.519 0.900 -0.195

0.580 -0.493 0.960 -0.151

0.590 -0.491

0.600 -0.453

0.640 -2.985**

0.7OO -0.307

0.750 -0.400

0.820 -3.173"*

0.870 -0.206

0.930 -0.133

0.960 -0.114

Lower Surface

0.020 0.070 0.020 0.353 0.020 0.358 0.020 0.628"*

0.110 0.059 0.060 0.352 0.060 0.438 0.060 6.886**

0.230 0.183 0,090 0.245 0.090 0.294 0.110 0.237

0.400 0.046 0.120 0.202 0.120 -0.066 0.250 0.102

0.490 0.014 0.200 0.212 0.200 0.115 0.400 0.087

0,630 4.530 ** 0.260 0.112 0.250 0.166 0.490 0.005

0.750 0.096 0.400 -3.192"* 0.400 0.067 0.580 -0.009

0.850 0.160 0.490 0.048 0.490 0.072 0.650 0.100

0.900 0.217 0.580 0.103 0.580 0.046 0.750 0.315

0.960 0.119 0.640 0.459 0.650 0.211 0.830 0.431

0.750 0.259 0.750 0.086 0.900 0,495

0.870 0.308 0.890 ******** 0.960 0.338

0.930 0.271 0,930 0.353

0.960 0.143 0.960 -3.190"*

CN = 0.696 0,898 0.922 0.938

230
Table E-2. Continued.

Flight t95, Wing sweep = 26 °, Time = 10-12-53-000, MINF = 0.802, Camber = 5/10, ALPT = 5,00, BETA = -0.24, QINF = 292,2,

RNPU = 2.4E+06, CNWP = 0.3467

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.203 0.000 0.715"* 0.000 -6.019"* 0.010 -0.389

0.060 -0.108 0.020 -0.067 0.020 0.026 0,020 -0.262

0.110 -0.360 0.040 -0.041 0.060 -0.932** 0.060 -0.678

0.200 -0.306 0.060 -0.318 0.090 -0.479 0.110 -0.776

0.230 -0.343 0.090 -0.431 0.110 -0.682 0,140 1.968"*

0.400 -0.240 0,130 -0.607 0.130 -0.792 0,190 -5.883 **

0.490 -0,238 0,150 -0.811 0.150 -0.870 0.250 -0.595

0,590 -0.306 0.200 -0.793 0.210 -0.961 0.400 -0.371

0.630 -0.343 0.250 -0.453 0.250 -0.737 0.490 -0.393

0.700 -0.389 0.260 -0.273 0,340 -0.375 0.580 -0,393

0,750 -0.840 0.280 -0,329 0,370 -0.410 0.650 -0.460

0.810 -0.902 0.290 -0.325 0.400 -0.380 0.700 -0.462

0.840 -0.934 0.310 -0,318 0.410 -0.359 0.750 -0.542

0.900 -0.220 0,320 -0,316 0.430 -0.404 0.800 -0.98 l

0.960 -0,233 0,340 -0.345 0.440 -0.382 0.830 -0.593

0.350 -0.186** 0.460 -0,376 0.900 -0.400

0.370 -0.322 0.490 -0,316 0.960 -0.399

0.380 -0.337 0500 -0.384

0.400 -0.270 0.520 -0.355

0.410 -0.363 0.540 -0.385

0.430 -0.328 0.550 -0.366

0.440 -0.276 0,580 -0.348

0.460 -0.419 0.600 -0.405

0.470 -0.369 0.610 -0.326

0.490 -0.345 0.650 -3.085**

0,500 -0.339 0.700 -0,617

0.520 -0.365 0.750 -0.626

0.530 -0.332 0.820 -0.614

0.550 -0.373 0.890 -0.284

0.560 -0.371 0.900 -0.313

0,580 -0.342 0.960 -0.305

0.590 -0.394

0.600 -0.423

0.640 -2.920**

0.700 -0.549

0.750 -0.649

0.820 -3.098**

0.870 -0.310

0.930 -0.254

0.960 -0.247

Lower Surface

0.020 -0.501 0.020 -0.395 0.020 -0.325 0.020 -0.010"*

O, 110 -0.145 0.060 -0.023 0.060 0.033 0.060 6.464**

0,230 0.027 0.090 -0.080 0,090 -0.060 0,110 -0.083

0.400 0,041 0.120 -0.028 O. 120 -0.352 0.250 -0.122

0.490 0.029 0.200 0,046 0,200 -0.067 0.400 -0.090

0.630 4.224** 0.260 -0.057 0.250 -0.039 0.490 -0.124

0.750 0.189 0.400 -3,116"* 0.400 -0.037 0.580 -0,067

0.850 0,259 0.490 0.015 0.490 0,046 0.650 0.126

0.900 0,323 0.580 0.117 0.580 0.036 0,750 0,368

0.960 0.146 0.640 0.479 0.650 0.271 0.830 0.456

0.750 0.322 0.750 0.067 0.900 0.542

0.870 0,402 0.890 ******** 0,960 0.352

0.930 0,344 0.930 0.400

0.960 0.185 0.960 -3.115"*

CN = 0.430 0.548 0.542 0.582

231
Table E-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-13-9-500, MINF = 0.797, Camber = 5/10, ALPT = 7.05, BETA = -0.16, QINF = 286.8,

RNPU = 2.4E+06, CNWP = 0.4229

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.096 0.000 0.878"* 0.000 -6.120** 0.0 [ 0 -0.944

0.060 -0.336 0.020 -0.481 0.020 -0.335 0.020 -0.792

0.110 -0.424 0.040 -0.315 0.060 - 1.092 ** 0.060 -0.908

0.200 -0.993 0.060 -0.604 0.090 -0.791 0.110 - 1.130

0.230 -0.821 0.090 -0.595 0.110 -0.905 0.140 2.003**

0.400 -0.250 0.130 -0.770 0.130 -0,977 0.190 -5.982 **

0.490 -0.255 0.150 -0.950 0.150 - 1.017 0.250 - 1.204

0.590 -0.326 0,200 -0.944 0.210 - 1.136 0.400 -0.425

0.630 -0.368 0.250 - 1. I 17 0.250 - 1.089 0.490 -0.424

0.700 -0.413 0,260 - 1.001 0.340 - 1.129 0.580 -0,408

0.750 - 1.022 0.280 - 1.077 0.370 -0.746 0,650 -0.490

0.810 - 1.087 0.290 - 1.073 0.400 -0.537 0,700 -0.500

0.840 - 1.080 0.310 -0.974 0.410 -0.420 0.750 -0.596

0.900 -0.300 0.320 -0.970 0.430 -0,417 0.800 -0.847

0.960 -0.316 0,340 - 1.026 0.440 -0.341 0.830 -0,667

0.350 -0.402** 0.460 -0.327 0.900 -0,391

0.370 -0.612 0.490 -0.281 0.960 -0.304

0.380 -0.430 0.500 -0.315

0.400 -0.294 0,520 -0.317

0.410 -0,329 0.540 -0.345

0.430 -0.234 0.550 -0.349

0.440 -0.205 0.580 -0.344

0460 -0.313 0.600 -0.387

0.470 -0.248 0.610 -0.32 I

0.490 -0,252 0.650 -3.132**

0.500 -0.264 0.700 -0.596

0.520 -0.275 0.750 -0.616

0.530 -0.276 0.820 -0.660

0.550 -0.326 0.890 -0.247

0,560 -0.326 0,900 -0.261

0.580 -0.309 0.960 -0.262

0.590 -0.371

0.600 -0.4 [ 0

0.640 -2.964**

0.700 -0.488

0.750 -0.673

0.820 -3.146"*

0,870 -0.398

0.930 -0.248

0.960 -0.241

Lower Surface

0.020 -0.283 0.020 -0.037 0,020 0.031 0.020 0.323**

0.110 -0.045 0.060 0.161 0,060 0.232 0.060 6.595"*

0.230 0.109 0.090 0.086 0.090 0.117 0.110 0.047

0.400 0.067 0.120 0.098 0.120 -0.197 0.250 -0,002

0.490 0.048 0.200 0.126 0.200 0.032 0.400 0.003

0.630 4.314"* 0,260 0.036 0.250 0,063 0.490 -0.042

0.750 0.187 0.400 -3.164"* 0.400 0.036 0.580 0.000

0.850 0.246 0.490 0.042 0.490 0,065 0.650 0.166

0.900 0,304 0.580 0.153 0,580 0.082 0.750 0.385

0.960 0.123 0.640 0.508 0.650 0.302 0.830 0.486

0.750 0.332 0.750 0.071 0.900 0.571

0.870 0.397 0,890 ******** 0.960 0.378

0.930 0.349 0.930 0.418

0.960 0.188 0.960 -3.162**

CN = 0.599 0.723 0.722 0.808

232
Table E-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-13-22-000, MINF = 0.786, Camber = 5/10, ALFT = 7.08, BETA = -0.19, QINF = 276.7,

RNPU = 2.3E+06, CNWP = 0.4066

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 -0.142 0.000 0 884"* 0.000 -6.322"* 0.010 - 1.010

0.060 -0.307 0.020 -0.533 0.020 -0.398 0.020 -0.853

O. 110 -0.522 0,040 -0.354 0.060 - 1.161 ** 0.060 -0.950

0.200 -1.008 0.060 -0.635 0.090 -0.840 0.110 -1.165

0.230 -0.779 0.090 -0.625 0.110 -0.957 0.140 2.084"*

0.400 -0.269 0.130 -0.807 O. 130 - 1.015 0.190 -6.178"*

0.490 -0.269 0.150 -0.985 0.150 - 1.054 0.250 - 1.024

0.590 -0.342 0.2130 -0.982 0.210 - 1.160 0.400 -0.426

0.630 -0.386 0.250 - 1.151 0.250 -I.130 0.490 -0.438

0.700 -0.433 0,260 - 1.017 0.340 -0,729 0.580 -0.397

0.750 - 1.051 0.280 - 1.115 0.370 -0.483 0.650 -0.500

0.810 - 1.119 0.290 - 1.101 0.400 -0.352 0.700 -0.522

0.840 -1.089 0.310 -1,001 0.410 -0.361 0.750 -0.610

0.900 -0.278 0.320 -0.996 0.430 -0.392 0.800 -0.832

0.960 -0.313 0.340 -0.656 0.440 -0.351 0,830 -0.669

0,350 -0.213** 0.460 -0.351 0900 -0.354

0.370 -0.341 0.490 -0.308 0.960 -0.279

0.380 -0.309 0.500 -0.377

0.400 -0.220 0.520 -0.356

0.410 -0.288 0.540 -0.389

0.430 -0.264 0.550 -0.381

0.440 -0.214 0.580 -0.387

0.460 -0.372 0.600 -0.423

0.470 -0.308 0.610 -0.341

0.490 -0.312 0.650 -3,225**

0.500 -0.323 0.700 -0.638

0520 -0.343 0.750 -0.643

0.530 -0.329 0.820 -0.631

0.550 -0366 0.890 -0.243

0.560 -0.387 0.900 -0.263

0.580 -0.357 0.960 -0.261

0.590 -0.416

0.600 -O.460

0.640 -3.050"*

0.700 -0.519

0.750 -0.706

0.820 -3.238**

0.870 -0.437

0.930 -0.254

0.960 -0.247

Lower Surface

0.020 -0.222 0.020 -0.025 0.020 0.049 0.020 0.333**

0.110 -0.041 0.060 0.167 0.060 0.239 0.060 6.860"*

0.230 0.104 0.090 0.093 0.090 0.123 0.110 0.062

0.400 0.069 0.120 0.101 0.120 -0.203 0,250 -0,003

0.490 0.049 0.200 0.126 0.200 0.029 0.400 0.010

0.630 4.495"* 0.260 0.033 0.250 0.073 0.490 -0.040

0.750 0.173 0.400 -3.257** 0.400 0.034 0.580 0.002

0.850 0.242 0.490 0.055 0.490 0.059 0.650 0.168

0.900 0,303 0.580 0.150 0.580 0.080 0.750 0.385

0.960 0, l 19 0.640 0.515 0.650 0.297 0.830 0.486

0.750 0.327 0,750 0.081 0.900 0.571

0.870 0.413 0.890 ******** 0.960 0.370

0.930 0.346 0.930 0.408

0.960 0.186 0.960 -3.255**

CN = 0.603 0.740 0.705 0.787

233
Table E-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-13-56-500, MINF = 0.795, Camber = 5/10, ALPT = 8.14, BETA = -0.03, QINF = 282.1.

RNPU = 2.3E+06, CNWP = 0.5267

_q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.343 0,000 0.876"* 0,000 -6.194"* 0.010 -0.969

0,060 -0,553 0.020 -0.782 0.020 -0.568 0.020 - 1.016

0.110 -0,658 0.040 -0.472 0.060 - 1,185"* 0.060 - 1.089

0,200 - 1,036 0.060 -0.781 0.090 -0.969 0.110 - 1.246

0.230 -0.920 0.090 -0.878 0.110 - 1.097 O. 140 2.072"*

0,400 -0.273 0.130 -0,979 0.130 - 1.127 0.190 -6,053" *

0.490 -0.245 0.150 - 1.093 0.150 - 1.154 0,250 - 1.380

0.590 -0.354 0.200 - 1.065 0.210 - 1.266 0.400 -0.698

0.630 -0.392 0,250 - 1.218 0.250 - 1.225 0,490 -0.518

0.700 -0.430 0.260 - 1.113 0.340 - 1.266 0.580 -0,457

0.750 - 1.094 0,280 - 1.196 0.370 - 1.222 0.650 -0.485

0.810 - 1.141 0.290 - 1.212 0.400 - 1.206 0.700 -0.540

0.840 -1,101 0.310 - 1.105 0.410 - 1.199 0,750 -0.646

0.900 -0,402 0.320 - 1.103 0,430 - 1.261 0.800 -0.612

0,960 -0,457 0.340 - 1.164 0.440 - 1.040 0.830 -0.605

0.350 -0.433** 0.460 -0.742 0.900 -0.218

0,370 - 1.093 0.490 -0.555 0,960 -0.164

0.380 - 1.127 0,500 -0,557

0,400 - 1.047 0.520 -0.493

0.410 -1,142 0,540 -0,463

0.430 - 1.119 0.550 -0.404

0,440 -0.963 0,580 -0,357

0,460 -0,733 0.600 -0,367

0,470 -0,508 0,610 -0.253

0,490 -0,424 0,650 -3.156**

0,500 -0.369 0.700 -0.459

0.520 -0.339 0,750 -0,544

0.530 -0.264 0.820 -0,653

0.550 -0.251 0,890 -0.182

0,560 -0.258 0.900 -0.175

0.580 -0,223 0,960 -0.183

0,590 -0.273

0,600 -0.320

0,640 -2,985**

0,700 -0,475

0,750 -0.872

0.820 -3.169"*

0.870 -0,474

0.930 -0.254

0.960 -0,232

Lower Surface

0,020 -0,066 0_020 0.142 0.020 0,186 0.020 0,498"*

0.110 0.011 0.060 0,261 0.060 0.355 0.060 6.735**

0,230 0,152 0.090 0,170 0.090 0.207 0,110 0.127

0.400 0.074 0.120 0.165 0.120 -0.131 0,250 0,054

0.490 0.062 0.200 0.172 0.200 0.090 0.400 0.055

0.630 4.416"* 0.260 0,074 0.250 0.125 0.490 -0.001

0,750 0.172 0,400 -3.188"* 0.400 0.078 0.580 0.035

0,850 0.231 0,490 0.080 0.490 0,080 0.650 0.195

0.900 0.285 0.580 0.169 0,580 0.113 0.750 0.421

0,960 0.091 0.640 0.521 0,650 0.317 0.830 0.499

0,750 0.343 0,750 0.105 0.900 0.582

0.870 0,408 0.890 ******** 0.960 0.385

0,930 0.353 0.930 0.430

0,960 0.193 0.960 -3.186**

CN = 0.688 0.905 0866 0,914

234
Table E-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-14-6-000, MINF = 0.798, Camber = 5/t0, ALPT = 9.00, BETA = -0.01, QINF = 284.3,

RNPU = 2.3E+06, CNWP = 0.6346

"q = 0,93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.520 0.000 0,833"* 0.000 -6.150"* 0.010 -0.994

0.060 -0.625 0.020 -0.882 0.020 -0.836 0.020 - 1.086

0.110 -0.774 0,040 -0.535 0.060 - 1.151 ** 0D60 - 1.203

0.200 - 1.043 0.060 -0.830 0.090 - 1.039 0.110 - 1.329

0.230 -0.961 0.090 -0.952 0.110 - 1.181 0.140 2.048"*

0.400 -0.851 0.130 -1.086 0.130 -1.209 0.190 -6.01 I**

0.490 -0,294 0.150 -1.171 0,150 -1.221 0.250 -1.442

0.590 -0.344 0.200 - 1.159 0.210 - 1.329 0.400 -0.935

0.630 -0.402 0.250 - 1.278 0.250 - 1.295 0.490 -0.737

0.700 -0.435 0,260 - 1.187 0,340 - 1.359 0,580 -0,598

0.750 -1.079 0.280 - 1.279 0.370 - 1.318 0.650 -0.512

0.810 - 1.146 0.290 -1.272 0.400 - 1.277 0.700 -0.569

0.840 - 1.144 0.310 - 1.189 0.410 - 1.266 0.750 -0.622

0.900 -0.482 0,320 - 1.182 0.430 -1.338 0,800 -0.475

0.960 -0,545 0.340 - 1,254 0.440 - 1.282 0.830 -0.412

0.350 -0,409** 0.460 - 1.314 0.900 -0.199

0.370 - 1.172 0.490 - 1.198 0.960 -0 152

0,380 -1.182 0,500 -1.318

0.400 -1.142 0.520 -1.298

0.410 -1.228 0.540 -1.197

0430 -1.199 0.550 -0.834

0.440 - 1.106 0.580 -0.679

0.460 - 1.305 0.600 -0.661

0.470 - 1,206 0.610 -0.535

0.490 - 1.148 0.650 -3.136**

0.500 - 1.167 0.700 -0.471

0.520 -1.144 0.750 -0.513

0.530 - 1.060 0.820 -0.441

0.550 -0.708 0.890 -0.136

0.560 -0.586 0.900 -0.130

0.580 -0.502 0.960 -0,128

0.590 -0.479

0.600 -0.461

0.640 -2.966"*

0.700 -0.387

0.750 -0.831

0.820 -3.149**

0.870 -0.369

0.930 -0.183

0.960 -0.130

Lower Surface

0.020 0.031 0.020 0,258 0.020 0.279 0.020 0.573**

0.110 0.043 0.060 0.317 0.060 0,364 0.060 6,679" *

0,230 0.186 0.090 0,217 0.090 0.259 0.110 0.180

0.400 0.081 0.120 0.186 0.120 -0.082 0.250 0.086

0.490 0.065 0,200 0.209 0,200 0,104 0.400 0.082

0.630 4.377 ** 0.260 0.115 0.250 0.159 0.490 0.026

0.750 0.153 0.400 -3.167"* 0.400 0.093 0.580 0.057

0.850 0.212 0,490 0.102 0,490 0,090 0.650 0,204

0.900 0,281 0.580 0,187 0.580 0.135 0.750 0.434

0.960 0.078 0.640 0.534 0,650 0,330 0.830 0.515

0.750 0,342 0.750 O. 112 0.900 0.604

0.870 0.425 0.890 ******** 0.960 0.393

0.930 0.393 0.930 0.454

0.960 0.237 0.960 -3.166**

CN = 0.799 1.026 0.995 1.002

235
Table E-2. Continued.

Flight 195, Wing sweep = 26", Time = 10-14-10-500, MINF = 0.798. Camber = 5/10, ALPT = 10.22, BETA = -0.16, QINF = 286.9,

RNPU = 2.4E+06, CNWP = 0.7158

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.892 0.000 0.765** 0,000 -6.113"* 0.010 -1.224

0.060 -0.853 0.020 - 1.209 0.020 - 1.034 0.020 - 1.249

0.110 -0.860 0.040 -0.822 0.060 -1.261"* 0.060 -1,321

0.200 -I .188 0.060 -0.973 0.090 -1.146 0.110 -1.415

0.230 -1.004 0.090 -1.044 0.110 - 1.293 0.140 2.048**

0.400 -0.982 0.130 - 1.155 0.130 - 1.324 0.190 -5.974"*

0.490 -0.536 0.150 - 1.258 0.150 - 1.297 0.250 - 1.580

0.590 -0.295 0.200 - 1.248 0,210 - 1.414 0.400 - 1.065

0.630 -0.377 0,250 - 1.371 0.250 - 1.363 0.490 -0.948

0.700 -0.416 0.260 - 1.257 0,340 - 1.434 0.580 -0.759

0.750 - 1.047 0.280 - 1.344 0.370 - 1.395 0.650 -0.523

0.810 -1.101 0.290 -1.365 0.400 -1.308 0.700 -0.527

0.840 - 1.103 0.310 - 1.256 0.410 - 1.359 0.750 -0.469

0.900 -0.559 0.320 - 1.252 0.430 - 1.412 0.800 -0.424

0.960 -0.595 0.340 - 1.333 0,440 - 1.387 0.830 -0.392

0.350 -0.421 ** 0.460 - 1.408 0.900 -0.168

0,370 -1.260 0.490 -1.275 0,960 -0.114

0.380 -1.294 0.500 -1,381

0.400 - 1.219 0.520 - 1.368

0.410 - 1.319 0.540 -0.985

0.430 - 1.299 0.550 -0.839

0.440 - 1.190 0.580 -0.736

0.460 - 1.386 0.600 -0.719

0.470 - 1.291 0.610 -0.592

0.499 - 1.212 0.650 -3.126" *

0.500 - I. 153 0.700 -0.560

0.520 -1.123 0,750 -0.581

0.530 -0.802 0.820 -0.381

0.550 -0.722 0.890 -0.238

0.560 -0.653 0.900 -0.254

0.580 -0.623 0.960 -0.239

0.590 -0.616

0.600 -0.589

0.640 -2.958**

0.700 -0.388

0,750 -0.499

0.820 -3,139"*

0,870 -0.161

0.930 -0.182

0.960 -0.172

Lower Surface

0.020 0.106 0.020 0.398 0.020 0.432 0.020 0.653**

O. 110 0.081 0.060 0.390 0.060 0.469 0.060 6.596"*

0.230 0.238 0.090 0,296 0.090 0.333 0.110 0.257

0.400 0,098 0.120 0.265 O.120 -0.002 0.250 O. 152

0.490 0.083 0.200 0.267 0.200 0.1 64 0.400 0.130

0.630 4.316"* 0.260 0.154 0.250 0.218 0.490 0.067

0.750 O. 178 0.400 -3.157" * 0.400 0.134 0.580 0.093

0.850 0.224 0,490 0.112 0.490 0.108 0.650 0.236

0.900 0.274 0.580 0.203 0,580 0.144 0.750 0.450

0.960 0.075 0.640 0.542 0.650 0.345 0.830 0.512

0.750 0.347 0.750 0.121 0.900 0.609

0.870 0.423 0.890 ******** 0.960 0.394

0.930 0.36l 0.930 0.436

0.960 0.207 0,960 -3.156**

CN = 0,895 1.057 1.089 1,103

236
Table E-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 10-1-11-500, MINF = 0.798, Camber = 5/10, ALPT = 3.06, BETA = -0.07, QINF = 296.9,

RNPU = 2.4E+06, CNWP = 0.2403

rI = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.348 0.000 0,475 0.000 4.229** 0.010 0.031

0.060 -0.038 0.020 O, 126 0.020 0,292 0.020 0.028

O. 110 -0.271 0.040 O. 135 0.060 -5.217"* 0.060 -0.323

0.200 -0.264 0.060 -0.128 0.090 -0.260 O. 110 -0.524

0.230 -0.236 0.090 -0.237 0.110 -0.482 0.140 -0.827

0.400 -0.217 0.130 -0,392 0.130 -0,638 0.190 -2.246"*

0.490 -0.203 0.150 -0.562 0.150 -0,507 0,250 -0.324

0.590 -0.319 0.200 -0.427 0.210 -0.467 0.400 -0.329

0.630 -0.323 0.250 -0.366 0.250 -0.299 0.490 -0.302

0.700 -0.370 0.260 -0.321 0.340 -0.361 0.580 -0.329

0.750 -0.811 0.280 -0.344 0.370 -0,356 0,650 -0.451

0.810 -0.804 0.290 -0.326 0.400 -0,349 0.700 -0.422

0.840 -0.804 0.310 -0.353 0.410 -3.252** 0.750 -0.498

0.900 -0.204 0.320 -0.326 0.430 -0,363 0.800 -1.064

0.960 -0.181 0.340 -0.330 0.440 -0.334 0,830 -0.580

0.350 -0.242** 0.460 -0.358 0,900 -0,404

0.370 -0.281 0,490 -0.364 0.960 -0.404

0.380 -0.337 0.500 -0.386

0.400 -0.242 0.520 -0.346

0.410 -0.334 0.540 -0.340

0.430 -0.306 0.550 -0.317

0.440 -0.274 0.580 -0.288

0.460 -0.336 0.600 -0.364

0.470 -0.325 0.610 -0.409

0.490 -0.316 0.650 2.845**

0.500 -0.313 0.700 -0.625

0.520 -0.330 0.750 -0.588

0.530 -0.313 0.820 -0.660

0,550 -0.371 0.890 -0.296

0.560 -0.352 0.900 -0.325

0.580 -0.351 0.960 -0.260

0.590 -0,383

0.600 -0,391

0.640 -0.562

0.700 -0.477

0.750 -0.016"*

0.820 -0.561

0.870 -0.306

0.930 -0.282

0.960 -0.281

Lower Surface

0.020 - 1.065 0.020 - 1.311 0.020 - 1.172 0.020 -0.366

0.110 -0.175 0.060 -0.310 0.060 -0.170 0.060 2.553"*

0.230 -0.062 0.090 -0.249 0.090 1.846"* 0.110 -0.162

0.400 0.001 0.120 -0.136 0.120 -0.414 0.250 -0.214

0.490 0.047 0.200 -0.073 0.200 -0.116 0.400 -0.166

0.630 2,613 ** 0.260 -0.116 0.250 -0.137 0.490 -0.169

0.750 0,158 0.400 -0.030 0.400 -0.093 0.580 -0,096

0.850 0.256 0,490 -0.014 0.490 0,002 0.650 0.115

0.900 0.313 0.580 0.040 0.580 0.023 0.750 0,298

0.960 0.179 0.640 0.251 0.650 -0.027 0.830 0.436

0.750 0.298 0.750 0.032 0.900 0.484

0,870 0.381 0.890 0.424 0,960 0,337

0.930 0.283 0.930 0.335

0.960 0.199 0.960 -3.340**

CN = 0.360 0.413 0,376 0.444

237
Table E-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 10-1-36-500, MINF = 0.800, Camber = 5/11, ALPT = 8.07, BETA = -0.27, QINF = 295.0,

RNPU = 2.4E+06, CNWP = 0.5238

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.347 0.000 0.847 0,000 4.284'* 0.010 -0.847

0.060 -0.50 t 0.020 -0.706 0,020 -0.573 0.020 -0.953

0 110 -0.658 0.040 -0.503 0,060 -5.225 ** 0.060 -0.991

0.200 -0.978 0.060 -0.733 0.090 -0,904 0.110 - 1.133

0.230 -0,842 0.090 -0.813 0.110 - 1.042 0.140 - 1.319

0.400 -0.368 0.130 -0.914 0.130 - 1.090 0.190 -2.234* *

0.490 -0.230 0.150 -I .057 0.150 -1.181 0.250 -1.300

0.590 -0.335 0.200 -1.055 0.210 - 1.177 0.400 -0.834

0.630 -0.373 0.250 -1.176 0.250 -1.135 0.490 -0.534

0.700 -0.404 0.260 - 1.101 0.340 - 1.217 0.580 -0.461

0.750 -1.096 0.280 - 1.161 0.370 - 1.218 0,650 -0.526

0.810 - 1.043 0.290 - 1.148 0.400 - 1.173 0.700 -0.546

0.840 -1.066 0.310 -1.115 0.410 -3,247** 0.750 -0.615

0.900 -0.452 0.320 - 1.099 0.430 - 1.209 0.800 -0.582

0.960 -0.456 0.340 - 1.119 0.440 - 1.181 0.830 -0.508

0.350 -0.468"* 0.460 - 1.204 0.900 -0,215

0.370 - 1.062 0.490 - 1.022 0,960 -0.193

0.380 -1.175 0.500 -0.799

0.400 - 1.04 1 0.520 -0,645

0.410 -1.134 0.540 -0.589

0.430 - 1.097 0.550 -0.496

0.440 - 1.041 0.580 -0.411

0.460 -1.139 0.600 -0.416

0.470 -1.098 0.610 -0.381

0.490 - 1.036 0.650 2.891 **

0.500 -0.652 0.700 -0.450

0.520 -0.543 0.750 -0.532

0.530 -0.410 0.820 -0.639

0,550 -0.403 0.890 -0.165

0.560 -0.320 0.900 -0.148

0.580 -0,282 0.960 -0.107

0.590 -O291

0.600 -0.277

0.640 -0,345

0.700 -0.434

0.750 0,045**

0,820 -0,550

0.870 -0.432

0.930 -0.264

0.960 -0.248

Lower Surface

0.020 -0.076 0.020 0.140 0.020 0.269 0.020 0.507

0.110 0.015 0.060 0.241 0,060 0.314 0.060 2.597**

0.230 0.129 0,090 0.150 0.090 1.886"* 0.110 0.202

0.400 0.069 0.120 0.165 0. ] 20 -0.055 0.250 0.056

0.490 0.164 0.200 0.128 0.200 0.054 0.400 0.038

0.630 2.658"* 0.260 0.091 0.250 0.127 0.490 0.005

0.750 0.177 0.400 0.096 0.400 0.074 0.580 0.032

0.850 0.248 0.490 0.078 0.490 0.059 0.650 0.195

0,900 0.288 0.580 0.128 0.580 0.125 0.750 0.391

0.960 0.097 0.640 0.325 0.650 0.022 0.830 0.528

0.750 0.389 0,750 0,089 0.900 0.559

0.870 0.461 0.890 0.492 0.960 0.390

0.930 0.342 0.930 0.413

0.960 0.239 0.960 -3.335**

CN = 0.690 0.902 0.858 0,927

238
Table E-2. Continued.

Flight 211. Wing sweep 26 °, TIME = 10-48-54-500. MINF = 0.803, Camber = 5/10, ALPT = 4.10, BETA = 0.25, QINF = 302.9,

RNPU = 2.5E+06, CNWP = 0.3075

i"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0,020 0.315 0.000 0.607 0.000 0.859"* 0.010 -0.224

0,060 -0.073 0.020 0.228 0,020 O. 135 0.020 -0.185

O. 110 -0.305 0.040 0.096 0,060 1.038"* 0.060 -0.55 [

0.200 -0.331 0.060 -0,188 0,090 -0,405 O. 110 -0.58 l

0.230 -0.349 0.090 -01341 0.110 -0.530 0,140 -0,955

0,400 -0.254 O. 130 -0.537 0,130 -2,216"* O. 190 -2,216"*

0,490 -0.239 O, 150 -0.722 O, 150 -0.825 0,250 -0.434

0.590 -0.317 0.200 -0.720 0.210 -0.829 0.400 -0.390

0.630 -0.363 0,250 -0.369 0.250 -0.386 0.490 -0,346

0.700 -0.430 0.260 -0.387 0.340 -0.406 0.580 -0.366

0.750 -0.708 0.280 -0.383 0.370 -0.420 0.650 -0.483

0.810 -0.674 0.290 -0.374 0.400 -0.364 0.700 -0.440

0.840 -0.759 0.310 -0.367 0,410 0.181 ** 0.750 -0.531

0.900 -0.248 0.320 -0.387 0,430 -0.400 0.800 -0.787

0.960 -0,211 0.340 -0.368 0,440 -0.404 0,830 -0,563

0.350 -0.145"* 0.460 -0.386 0.900 -0.402

0.370 -0.358 0.490 -0.372 0.960 -0.397

0.380 -0.375 0.500 -0.391

0.400 -0.327 0.520 -0.402

0.410 -0.348 0.540 -0.386

0.430 -0.331 0.550 -0.366

0.440 -0.322 0.580 -0.346

0460 -0.344 0.600 -0.399

0.470 -0.366 0.610 -0.412

0.490 -0.347 0.650 -0.598

0500 -0.346 0.700 -0.638

0.520 -0.340 0.750 -0.573

0.530 -0.352 0.820 -0.647

0.550 -0379 0.890 -0.293

0.560 -0.390 0.900 -0.353

0.580 -0.348 0.960 -0.270

0.590 -0.403

0600 -0.383

O.64O -0619

0.700 -0.551

0.750 -0.014"*

0.820 -0.573

0,870 -0.41 t

0.930 -0.294

0.960 -0.297

Lower Surface

0.020 -0.729 0.020 -0.643 0,020 -0.780 0.020 -0.149

0.110 -0.1 64 0.060 -0.107 0.060 -0. l I 1 0.060 0.019

0.230 -0.027 0.090 -0.137 0.090 -0.107 0.1 I 0 -0.124

0400 -0.003 0.120 -0.097 0.120 -0.112 0.250 -0.195

0.490 0.038 0.200 -0.024 0.200 -0.005 0.400 -0.162

0.630 3.524"* 0.260 -0.052 0.250 -0.123 0.490 -0.128

0.750 0.166 0.400 -0.033 0.400 -0.076 0.580 -0.089

0.850 0.194 0.490 0.001 0.490 -0.027 0.650 0.105

0.900 0.288 0.580 0.038 0.580 -0.006 0.750 0.331

0.960 0.136 0.640 0.257 0.650 -0.033 0.830 0.414

0.750 0.313 0.750 0.013 0.900 0.480

0.870 0.389 0.890 0.463 0.960 0.322

0.930 0.314 0.930 0.368

0.960 0.199 0.960 0.232

CN = 0.382 0.503 0.479 0.511

239
Table E-2, Continued.

Flight 224, Wing sweep = 26 °, Time = 10-2-44-000, MINF = 0.800, Camber = 10/2, ALPT = 5.02, BETA = -0.59, QINF = 294.7,

RNPU = 2.4E+06, CNWP = 0.2869

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.473 0.000 0.142 0.000 4.290* * 0,010 0.334

0.060 -0.021 0.020 0.342 0,020 0,474 0.020 0.173

0.110 -0.363 0,040 0.227 0.060 -5.228** 0.060 -0.350

0.200 -0.581 0.060 -0.144 0.090 -0.335 0.110 -0.693

0.230 -0.216 0.090 -0.322 0.110 -0.637 0.140 -1.136

0.400 -0.212 0.130 -0.592 0.130 -0.893 0.190 -2.234 **

0.490 -0.198 0.150 -0.931 0.150 - 1.106 0.250 -0.585

0.590 -0.243 0.200 -0.988 0.210 - 1.049 0.400 -0.319

0.630 -0.238 0.250 -0.751 0.250 -0.865 0.490 -0.312

0.700 -0.208 0.260 -0.445 0.340 -0.310 0,580 -0.299

0,750 -0.251 0.280 -0.366 0.370 -0.349 0.650 -0.377

0.810 -0.251 0.290 -0.306 0,400 -0.323 0.700 -0.361

0.840 -0.198 0.310 -0.297 0.410 -3.247"* 0.750 -0.385

0,900 -0.127 0.320 -0.277 0.430 -0.335 0.800 -0.380

0.960 -0.029 0.340 -0.257 0.440 -0.319 0.830 -0.319

0.350 -0.237** 0.460 -0.345 0.900 -0.209

0,370 -0.269 0.490 -0.252 0.960 -0.033

0.380 -0.319 0.500 -0.343

0.400 -0.215 0.520 -0,305

0.410 -0.315 0.540 -0.304

0.430 -0.292 0.550 -0.281

0.440 -0.239 0.580 -0.250

0.460 -0.294 0.600 -0.309

0.470 -0.286 0,610 -0.333

0,490 -0.301 0.650 2,896**

0.500 -0.306 0.700 -0.370

0.520 -0.316 0.750 -0.444

0.530 -0.278 0.820 -0.348

0.550 -0.349 0.890 -0.123

0.560 -0.295 0.900 -0.074

0.580 -0,282 0,960 0.044

0.590 -0.335

0.600 -0.350

0.640 -0.364

0.700 -0.344

0.750 -0.028**

0.820 -0.271

0.870 -0.213

0.930 -0.116

0.960 -0.034

Lower Surface

0.020 -0.774 0.020 -0.804 0.020 -0.626 0.020 -0.740

0.110 -0.459 0,060 -0.565 0.060 -0.375 0.060 2,601 **

0.230 -0.082 0.090 -0.386 0.090 1.889** 0.110 -0,065

0.400 -0,004 0.120 -0.086 0,120 -0.346 0.250 -0.153

0.490 0.009 0.200 -0.093 0.200 -0.155 0.400 -0.183

0.630 2.662"* 0.260 -0.063 0.250 -0.065 0.490 -0.246

0.750 0.027 0.400 -0.080 0.400 -0.160 0.580 -0.280

0.850 0.121 0.490 -0. l 14 0.490 -0.022 0.650 -0.120

0.900 0.152 0.580 -0.093 0.580 -0.156 0.750 0.110

0,960 0.138 0.640 0.065 0,650 -0.029 0,830 0.283

0.750 0.184 0.750 -0.022 0.900 0.310

0,870 0.232 0.890 0.264 0.960 0.272

0.930 0.180 0.930 0.220

0.960 0.147 0.960 -3.336**

CN = 0.175 0.306 0.323 0.348

240
Table E-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 10-2-52-500, MINF = 0.805, Camber = 10/2, ALPT = 1029, BETA = -0.12, QINF = 298.1.

RNPU = 2.4E+06, CNWP = 0.3961

11 = 0.93 0.76 0_59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0020 O.101 0.000 0.770 0.000 4.247"* 0.010 -0.401

0,060 -0.397 0.020 -0.160 0.020 -0.090 0.020 -0.324

O. 110 -0.634 0.040 -0.200 0,060 -5.163"* 0.060 -0.907

0.200 - 1.212 0.060 -0.560 0,090 -0.836 O. 110 - 1.228

0.230 - 1.127 0.090 -0,752 O. 110 - 1.039 O, 140 - 1.498

0.400 -0.432 O.130 -0.924 O, 130 - 1.229 O. 190 -2.203" *

0.490 -0.261 0.150 - 1.172 0.150 - 1.382 0.250 - 1.526

0.590 -0,291 0.200 - 1.260 0.2 I0 -1.086 0.400 -0.954

0.630 -0.279 0.250 - 1.094 0.250 -0.769 0.490 -0.363

0.700 -0.224 0.260 -0.828 0.340 -0.757 0.580 -0.214

0.750 -0.257 0.280 -0.890 0.370 -0.752 0.650 -0.267

0,810 -0.270 0.290 -0.820 0.400 -0.708 0.700 -0.249

0.840 -0.243 0.310 -0.796 0.410 -3.205** 0.750 -0.243

0.900 -0.174 0,320 -0.765 0,430 -0.674 0.800 -0.285

0.960 -0.090 0,340 -0.741 0,440 -0.640 0.830 -0.217

0.350 -0.393** 0.460 -0,659 0.900 -0.148

0.370 -0.684 0.490 -0,593 0.960 -0.064

0.380 -0.770 0.500 -0.644

0.400 -0.608 0.520 -0.614

0.410 -0.698 0.540 -0.594

0.430 -0_661 0.550 -0.555

0.440 -0.601 0.580 -0.529

0.460 -0.653 0.600 -0.537

0.470 -0.611 0.610 -0.538

0.490 -0.590 0.650 2868**

0.500 -0.566 0.700 -0.482

0.520 -0.567 0.750 -0.534

0.530 -0.505 0,820 -0.390

0.550 -0.551 0.890 -0.296

0.560 -0,506 0.900 -0.273

0.580 -0.479 0,960 -0.204

0,590 -0.4%

0.600 °0.469

0.640 -0.351

0.700 -0.338

0.750 0.004**

0.820 -0.188

0.870 -0.175

0.930 -0.187

0.960 -0,179

Lower Surface

0.020 -0.177 0.020 0.033 0.020 0.167 0.020 0.377

0.110 0.025 0.060 0,235 0.060 0.338 0.060 2.577 * *

0.230 0.045 0.090 0.172 0.090 1.873"* 0.110 0,270

0.400 0.012 0A20 0.199 0,120 -0.010 0.250 0.100

0.490 -0.002 0,200 0.046 0,200 0.032 0.400 0.018

0.630 2.637"* 0.260 O. I 11 0.250 O. 140 0.490 -0.074

0.750 -0,009 0.400 0,024 0.400 0.011 0.580 -0.137

0. 850 0.062 0.490 -0.055 0.490 0.009 0.650 -0.039

0.900 0.115 0.580 -0.073 0.580 -0.068 0.750 0,138

0.960 0.099 0.640 0.065 0.650 -0.031 0.830 0.317

0.750 0,183 0.750 0.013 0.900 0.317

0,870 0,218 0.890 0.231 0.960 0.233

0.930 0.140 0.930 0.170

0.960 0,085 0.960 -3.293**

CN = 0.459 0.632 0.675 0.758

241
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-16-42-500, MINF = 0.801, Camber = 10/2, ALPT = 6.03, BETA = -0.01, QINF = 303.1,

RNPU = 2.5E+06, CNWP = 0.3208

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.434 0.000 0.331 0.000 0.529"* 0.010 0.120

0.060 -0.092 0.020 0.340 0.020 0.373 0.020 0.004

0.110 -0.434 0.040 0.221 0,060 -0.012** 0.060 -0.588

0.200 -1.144 0.060 -0.226 0.090 -0,464 0.110 -0.910

0.230 - 1.026 0.090 -0.426 0.110 -0.711 0,140 - 1.292

0.400 -0.207 0.130 -0.672 0.130 -2.224"* 0.190 -2.224**

0.490 -0.205 0.150 -0.992 0.150 - 1.137 0.250 -0.965

0.590 -0.253 0.200 - 1.095 0.210 - 1.142 0.400 -0.401

0.630 -0.252 0.250 - 1.123 0.250 - 1.130 0.490 -0.338

0.700 -0.226 0.260 - 1.077 0.340 -0.638 0.580 -0.331

0.750 -0.249 0.280 - 1.102 0.370 -0.473 0.650 -0.380

0.810 -0.229 0.290 - 1.076 0.400 -0.344 0.700 -0.375

0.840 -0.230 0.310 -1.028 0.410 -3.210"* 0.750 -0.389

0.900 -0.147 0.320 - 1.048 0.430 -0.305 0.800 -0.356

0.960 -0.035 0.340 -0.555 0.440 -0.269 0.830 -0.304

0,350 -0.267"* 0.460 -0.270 0.900 -0.164

0,370 -0.356 0,490 -0.231 0.960 0.005

0.380 -0.326 0.500 -0.304

0.400 -0.235 0.520 -0.290

0.410 -0.239 0.540 -0.289

0.430 -0.197 0.550 -0.283

0.440 -0.195 0.580 -0.288

0.460 -0.211 0.600 -0.306

0.470 -0.231 0.610 -0.317

0.490 -0.240 0.650 -0.475

0.500 -0.244 0.700 -0.364

0.520 -0.247 0.750 -0.392

0.530 -0.256 0.820 -0.319

0.550 -0.291 0.890 -0.124

0.560 -0.293 0.900 -0.097

0.580 -0.267 0.960 0.039

0.590 -0.309

0.600 -0.309

0.640 -0.346

0.700 -0.324

0.750 -0.024"*

0.820 -0.272

0.870 -0.225

0.930 -0.106

0.960 -0.030

Lower Surface

0.020 - 1.086 0.020 -0.684 0.020 -0.587 0,020 -0.292

0.110 -0.149 0.060 -0.201 0.060 -0.007 0.060 -0.016

0.230 -0.051 0.090 -0.106 0.090 -0.018 0.110 -0.062

0.400 -0.034 0.120 -0.034 0.120 -0.196 0.250 -0.106

0.490 -0.022 0.200 -0.051 0.200 -0.076 0.400 -0.150

0.630 4.037"* 0.260 -0.026 0.250 -0.042 0.490 -0.196

0.750 0.017 0.400 -0.064 0.400 -0.114 0.580 -0.226

0.850 0.064 0.490 -0.094 0.490 -0.044 0.650 -0.103

0.900 0.158 0.580 -0.103 0.580 -0.159 0.750 0.132

0.960 0.123 0.640 0.047 0.650 -0.036 0.830 0.276

0.750 0.169 0.750 -0.029 0.900 0.317

0.870 0.214 0.890 0.292 0.960 0.254

0.930 0.207 0.930 0.242

0.960 0.164 0.960 0.304

CN = 0.325 0,418 0.436 0.466

242
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-17-12-500, MINF = 0.808, Camber = 10/2. ALPT = 4.04, BETA = -0.12, QINF = 304.4,

RNPU = 2.5E+06, CNWP = 0.2316

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.560 0.000 0.1 04 0,000 0.377"* 0.010 0.332

0.060 0,024 0.020 0.464 0,020 0,547 0.020 0.215

0,110 -0.312 0,040 0.374 0.060 0.153 ** 0,060 -0.323

0.200 -0.471 0.060 -0.047 0.090 -0.323 0.110 -0.683

0.230 -0,229 0.090 -0.297 0.110 -0.570 0.140 - 1,151

0.400 -0.218 0,130 -0.571 0.130 -2.190** 0.190 -2.190"*

0.490 -0,197 0.150 -0.861 0.150 - 1.013 0,250 -0,466

0.590 -0.237 0.200 -0.946 0.210 -0986 0,400 -0.348

0.630 -0,248 0.250 -0,433 0.250 -0,506 0,490 -0.322

0.700 -0.218 0.260 -0.318 0,340 -0,328 0.580 -0.314

0.750 -0.230 0,280 -0.320 0,370 -0,330 0.650 -0.393

0,810 -0.219 0.290 -0.303 0.400 -0,332 0.700 -0.368

0,840 -0.219 0.310 -0.304 0.410 -3.171 ** 0,750 -0.407

0.900 -0.126 0.320 -0.310 0.430 -0.352 0.800 -0.387

0.960 -0.022 0,340 -0.305 0.440 -0.323 0,830 -0.325

0.350 -0.197"* 0.460 -0.333 0.900 -0,218

0.370 -0.302 0.490 -0.279 0.960 -0,015

0.380 -0.329 0.500 -0.344

0.400 -0.271 0,520 -0.326

0,410 -0.318 0.540 -0.326

0,430 -0.269 0.550 -0.310

0.440 -0,263 0.580 -0.309

0.460 -0.297 0.600 -0.333

0.470 -0,296 0.610 -0.347

0.490 -0.302 0.650 -0.498

0.500 -0.312 0.700 -0.396

0.520 -0.282 0.750 -0.406

0.530 -0,298 0.820 -0.329

0.550 -0.339 0.890 -0.132

0.560 -0.327 0.900 -0.098

0.580 -0.291 0.960 0.035

0.590 -0.334

0.600 -0.346

0.640 -0.366

0,700 -0,338

0.750 -0.036**

0.820 -0,257

0.870 -0.222

0,930 -0.099

0,960 -0,035

Lower Surface

0.020 -0.830 0.020 - 1.127 0.020 -0,927 0.020 - 1.016

0.110 -0.558 0.060 -0,564 0.060 -0,563 0.060 -0.024

0.230 -0.088 0.090 -0.408 0.090 -0,359 0.110 -0.27 I

0.400 -0.053 0, | 20 -0.268 0.120 -0,415 0.250 -0.222

0.490 -0,012 0.200 -0.088 0.200 -0.087 0.400 -0.261

0,630 4,044** 0.260 -0,144 0.250 -0.140 0.490 -0.295

0,750 0,027 0.400 -0,124 0.400 -0.186 0,580 -0.299

0.850 0.067 0,490 -0.120 0.490 -0.062 0.650 -0,158

0,900 0,1 40 0.580 -0,107 0,580 -0.184 0.750 0.1 04

0,960 0.122 0.640 0.031 0.650 -0.055 0.830 0.251

0.750 0.123 0.750 -0.019 0.900 0.308

0.870 0,1 64 0.890 0.251 0.960 0,243

0.930 0.173 0,930 0,215

0.960 0.137 0,960 0.298

CN = 0,I 34 0.241 0.276 0.291

243
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-27-5-500, MINF = 0,806, Camber = 10/2, ALPT = 7.17, BETA = -0.47, QINF = 307.6,

RNPU = 2.5E+06, CNWP = 0.3778

r I = 0.93 0.76 0.59 0.40

Upper Surface

x.,/c CP x/c CP x/c CP x/c CP

0,020 0.35t 0,000 0,456 0.000 0.501 ** 0,010 -0.082

0,060 -0.138 0,020 0.180 0.020 0.25 t 0,020 -0.064

0.110 -0.465 0,040 0.146 0,060 0,095"* 0.060 -0,729

0.200 - 1.169 0.060 -0,335 0.090 -0.541 O. 110 - 1.056

0.230 - 1.076 0,090 -0,498 0.110 -0,787 0.140 - 1.384

0,400 -0.174 0.130 -0.764 0.130 -2.198"* 0.190 -2.198"*

0.490 -0.173 0.150 - 1.047 0.150 - 1.185 0,250 - 1.276

0.590 -0.256 0.200 -1.146 0.210 -1.204 0.400 -0,552

0.630 -0.249 0.250 -1.200 0.250 -1.187 0.490 -0,386

0,700 -0.233 0.260 -1.147 0,340 -1.193 0.580 -0,354

0,750 -0.279 0,280 -1.177 0.370 -1.192 0,650 -0.377

0.810 -0.264 0,290 - 1.169 0,400 -0,727 0.700 -0.367

0.840 -0.255 0.310 -1.117 0.410 -3.169** 0.750 -0.373

0.900 -0.179 0.320 - 1.138 0,430 -0.585 0,800 -0.338

0.960 -0.073 0.340 -1.124 0.440 -0.513 0.830 -0,280

0,350 -0,508** 0.460 -0.453 0.900 -0.129

0,370 - 1.093 0,490 -0.323 0,960 -0.002

0.380 -1.104 0.500 -0.324

0,400 -0,609 0,520 -0.292

0.410 -0.553 0,540 -0.265

0,430 -0,449 0.550 -0.256

0,440 -0,372 0.580 -0,243

0,460 -0,366 0.600 -0,250

0,470 -0.291 0.610 -0.239

0490 -0.240 0.650 -0,495

0,500 -0.242 0,700 -0,305

0,520 -0_205 0,750 -0.376

0.530 -0.175 0,820 -0.301

0,550 -0.215 0.890 -0.107

0.560 -0.205 0,900 -0,092

0.580 -0.192 0.960 0.035

0,590 -0.255

0,600 -0,249

0,640 -0,300

0,700 -0,287

0,750 -0,027"*

0.820 -0,271

0.870 -0.240

0.930 -0.108

0.960 -0.037

Lower Surface

0.020 -0.943 0.020 -0.507 0.020 -0,283 0,020 -0.133

0.110 -0.096 0.060 -0.030 0.060 0,088 0.060 -0.026

0.230 -0.046 0.090 -0.020 0.090 0.073 O. l I 0 0.011

0.400 -0.033 O. 120 0.059 O. 120 -0.155 0.250 -0.057

0,490 -0.021 0.200 -0.040 0.200 -0.072 0,400 -0.112

0.630 3,970"* 0.260 0.010 0,250 -0,005 0.490 -0.171

0.750 0.013 0.400 -0.022 0.400 -0.071 0,580 -0.211

0.850 0.060 0,490 -0,084 0.490 -0,046 0.650 -0.087

0.900 0.146 0.580 -0,097 0.580 -0.136 0,750 0.142

0.960 0.124 0,640 0.061 0.650 -0.036 0.830 0.277

0,750 0.190 0.750 -0,036 0.900 0,322

0.870 0.222 0.890 0.295 0.960 0.249

0.930 0.201 0,930 0.246

0.960 0.176 0.960 0.359

CN = 0,343 0.526 0.548 0.575

244
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-27-8-500, MINF = 0.806, Camber = 10/2, ALPT = 8,10, BETA = -0.67, QINF = 307.8,

RNPU = 2.5E+06, CNWP = 0.4330

r I = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x./c CP x/c CP x/c CP

0.020 0.280 0.000 0.564 0.000 0.562 ** 0.010 -0.129

0.060 -0.212 0.020 0.083 0.020 0A 18 0.020 -0.192

0.110 -0.510 0.040 0.050 0.060 0.026** 0.060 -0,837

0.200 - 1.193 0.060 -0.41 I 0.090 -0.673 0.1 I0 - 1,137

0.230 -1.147 0.090 -0.572 0,110 -0.842 0.140 -1,438

0.400 -0.262 0.130 -0.813 0,130 -2.197"* 0.190 -2.197"*

0.490 -0.158 0.150 -1,087 0.150 -1.243 0.250 -1.386

0.590 -0.238 0.200 - 1,192 0.210 - 1.243 0.400 -0.734

0,630 -0,256 0,250 - 1.259 0.250 - 1.249 0.490 -0,435

0.700 -0.229 0.260 - 1,191 0.340 - 1.266 0,580 -0.359

0.750 -0.280 0.280 - 1.243 0.370 - 1.261 0.650 -0.357

0.810 -0,267 0.290 - 1.230 0.400 - 1.201 0.700 -0,342

0.840 -0.270 0,310 -1.186 0.410 -3,167"* 0.750 -0.333

0,900 -0.196 0,320 - 1.197 0.430 -0,717 0.800 -0.289

0,960 -0.093 0.340 - 1.195 0.440 -0.649 0.830 -0.230

0.350 -0.535"* 0.460 -0.636 0.900 -0,101

0.370 - 1.163 0.490 -0,558 0.960 -0.011

0.380 - 1.245 0.500 -0,598

0.400 - 1.143 0.520 -0,540

0.410 -0.972 0.540 -0,516

0.430 -0.632 0,550 -0.462

0.440 -0.566 0.580 -0.396

0.460 -0.560 0,600 -0.352

0.470 -0.510 0.610 -0,304

0.490 -0.468 0.650 -0.423

0.500 -0.429 0,700 -0.255

0.520 -0.395 0.750 -0.318

0.530 -0.318 0.820 -0.241

0.550 -0,306 0.890 -0.092

0.560 -0.257 0.900 -0.070

0.580 -0.210 0,960 0.033

0.590 -0.223

0.600 -0.216

0.640 -0.220

0.700 -0.243

0.750 -0.013"*

0.820 -0.235

0.870 -0.204

0.930 -0.089

0.960 -0,029

Lower Surface

0.020 -0.498 0.020 -0.250 0.020 -0.161 0.020 0.096

0.110 -0.049 0.060 0.076 0,060 0.147 0.060 -0.008

0.230 -0,013 0,090 0.051 0.090 0. I 19 0,110 0,084

0.400 -0.026 0.120 0,123 0.120 -0.107 0,250 -0.011

0.490 -0.021 0,200 -0.015 0.200 -0.048 0.400 -0,077

0.630 3.967** 0.260 0.031 0,250 0,037 0.490 -0.135

0.750 -0.002 0.400 -0,019 0.400 -0.047 0.580 -0,176

0,850 0_048 0.490 -0.066 0.490 -0.035 0.650 -0.087

0.900 0.142 0.580 -0.090 0,580 -0.121 0,750 0.147

0.960 0.104 0,640 0.061 0.650 -0.028 0.830 0.287

0.750 0.174 0.750 -0.021 0.900 0,325

0.870 0,209 0.890 0.288 0.960 0,246

0.930 0.208 0.930 0,246

0.960 0.169 0.960 0. 346

CN = 0.380 0.590 0.632 0.650

245
Table E-2. Continued.

Flight 216. Wing sweep = 26 °, Time = 10-27-13-500, MINF = 0.806, Camber = 10/2, ALPT = 10.28, BETA = -0.36, QINF = 307.4,

RNPU = 2.5E+06, CNWP = 0.3816

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.108 0.000 0.777 0,000 0.511 ** 0.010 -0.466

0.060 -0.365 0.020 -0.145 0,020 -0.108 0.020 -0.400

0.110 -0.686 0.040 -0.038 0.060 -0.240"* 0.060 -0.971

0.200 - 1.227 0.060 -0.592 0,090 -0.892 0.110 - 1.262

0.230 - 1.137 0.090 -0.778 0.110 - 1.064 0.140 - 1.550

0.400 -0,423 0.130 -0.964 0.130 -2,199"* 0.190 -2.199 **

0.490 -0.268 0.150 - 1.182 0.150 - 1.289 0.250 - 1.568

0.590 -0.301 0.200 - 1.247 0.210 -0.926 0.400 -0.942

0.630 -0.316 0.250 -0.921 0.250 -0.806 0.490 -0.351

0.700 -0.255 0,260 -0.800 0.340 -0.753 0.580 -0.222

0.750 -0.277 0.280 -0.836 0.370 -0.720 0.650 -0.283

0.810 -0.252 0.290 -0.794 0,400 -0.698 0.700 -0.262

0.840 -0.277 0.310 -0.795 0.410 -3.171 ** 0.750 -0.275

0.900 -0.198 0.320 -0.779 0.430 -0.673 0.800 -0.287

0.960 -0.126 0.340 -0,762 0.440 -0.640 0.830 -0.218

0.350 -0,355** 0.460 -0.640 0.900 -0.155

0.370 -0.699 0.490 -0.580 0.960 -0.076

0380 -0.754 0,500 -0.633

0.400 -0.644 0.520 -0.626

0.410 -0.701 0.540 -0.612

0.430 -0.679 0.550 -0.600

0.440 -0.614 0.580 -0.589

0.460 -0.658 0,600 -0.569

0.470 -0.620 0.610 -0.525

0.490 -0.600 0.650 -0.659

0.500 -0,570 0.700 -0.483

0.520 -0.570 0.750 -0.515

0.530 -0.517 0.820 -0,405

0.550 -0.557 0.890 -0.316

0.560 -0.493 0.900 -0.327

0.580 -0.488 0.960 -0.253

0.590 -0.467

0.600 -0.426

0.640 -0.343

0.700 -0.354

0.750 -0.004"*

0.820 -0.238

0.870 -0.206

0.930 -0200

0.960 -0,182

Lower Surface

0.020 -0.171 0.020 0.039 0.020 0.097 0.020 0.378

0.110 0.005 0.060 0.246 0.060 0.312 0.060 0.015

0.230 0.050 0.090 0.172 0.090 0.249 0.110 0.223

0.400 -0.014 0.120 0.196 0.120 -0.008 0.250 0.075

0.490 -0.020 0.200 0.047 0.200 -0.003 0.400 0.003

0.630 3.974"* 0.260 0.096 0.250 0.117 0.490 -0.083

0.750 -0.010 0.400 0.022 0.400 -0.003 0.580 -0.142

0,850 0.011 0.490 -0.044 0.490 -0.020 0.650 -0,064

0.900 0.127 0.580 -0.090 0.580 -0.098 0.750 0.144

0.960 0.081 0.640 0.047 0.650 -0.019 0.830 0.284

0.750 0.147 0,750 0.009 0.900 0.317

0.870 0.181 0.890 0.234 0.960 0.213

0,930 0.128 0.930 0.161

0.960 0.053 0,960 0.197

CN = 0.459 0.621 0.673 0.747

246
Table E-2. Continued.

Flig ht 216, Wing sweep = 26 °, Time = 10-27-18-000, MINF = 0.794, Camber = 10/2, ALPT = 12.15, BETA = -0.88, QINF = 298.4,

RNPU = 2.5E+06, CNWP = 0.1934

r I = 093 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.173 0,000 0,849 0.000 0,453** 0.010 -0.910

0.060 -0.573 0.020 -0.462 0.020 -0_436 0.020 -0,988

0.110 -0.878 0.040 -0.262 0,060 -0.394** 0.060 - 1.157

0.200 -0.807 0.060 -0.818 0.090 - I. 102 0.110 - 1.481

0.230 -0.766 0.090 - 1.022 0.110 - 1.282 0.140 - 1.442

0.400 -0.591 0.130 - 1,164 0.130 -2.269"* 0.190 -2.269"*

0.490 -0.428 0.150 - 1.385 0,150 -0.801 0.250 - 1,230

0.590 -0.373 0.200 - 1.482 0.210 -0.774 0.400 -0.987

0.630 -0.334 0.250 - 1.206 0.250 -0.717 0.490 -0.757

0,700 -0.286 0.260 - 1.037 0.340 -0,674 0.580 -0.58 I

0.750 -0.270 0.280 - 1.049 0.370 -0,652 0.650 -0.521

0.810 -0.270 0.290 -0.997 0.400 -0.559 0.700 -0.487

0.840 -0.252 0.3 l0 -0.952 0.410 -3.270** 0.750 -0.434

0.900 -0.223 0,320 -0.930 0.430 -0.622 0.800 -0A31

0.960 -0.182 0.340 -0.911 0,440 -0.597 0.830 -0.369

0.350 -0.376** 0.460 -0.592 0.900 -0.331

0.370 -0.809 0.490 -0.526 0.960 -0.287

0.380 -0.816 0.500 -0.584

0.400 -0.652 0.520 -0.566

0.410 -0.630 0.540 -0.545

0.430 -0.406 0.550 -0.521

0.440 -0.366 0.580 -0560

0.460 -0.356 0.600 -0.527

0470 -0,283 0.610 -0.489

0.490 -0.242 0.650 -0.668

0.500 -0.242 0,700 -0.464

0.520 -0.248 0,750 -0.523

0.530 -0.243 0.820 -0.461

0.550 -0.274 0.890 -0.383

0.560 -0.260 0.900 -0.374

0.580 -0.229 0.960 -0.306

0.590 -0.273

0.600 -0.274

0.640 -0.276

0.700 -0.261

0.750 -0.008**

0.820 -0.174

0.870 -0.161

0,930 -0.191

0,960 -0.187

Lower Surface

0D20 0.014 0.020 0.269 0.020 0.345 0.020 0.538

0.110 0.076 0.060 0.347 0.060 0.411 0.060 0.026

0.230 0.074 0.090 0.261 0.090 0,339 0.110 0.373

0.400 0.011 0.120 0.257 0.120 0.086 0.250 0,169

0.490 0.005 0,200 0.063 0.200 0.025 0.400 0.050

0.630 4.090"* 0.260 0.146 0.250 0.183 0.490 -0,030

0.750 -0.0| 1 0.400 0.057 0.400 0.048 0.580 -0.080

0.850 0.014 0.490 -0,007 0.490 -0.024 0.650 -0.025

0,900 0.084 0.580 -0.063 0.580 -0.083 0.750 0.155

0.960 0.017 0.640 0.067 0.650 -0,024 0,830 0.266

0.750 O, 155 0.750 0.005 0.900 0.284

0.870 O. 175 0.890 O. 194 0.960 O. 153

0,930 0.114 0.930 0,132

0,960 0.040 0.960 O. 154

CN = 0.489 0.655 0.663 0.904

247
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-23-8-000, MINF = 0.795, Camber = 10/10, ALPT = 4.01, BETA = -0.21, QINF = 297.0,

RNPU = 2.5E+06, CNWP = 0.2962

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.522 0.000 0.128 0.000 0.322** 0.010 0.325

0.060 0.024 0.020 0.408 0.020 0.508 0.020 0.195

0.110 -0.374 0.040 0.333 0.060 0.137** 0.060 -0.366

0,200 -0.443 0.060 -0.114 0.090 -0.356 0.110 -0.737

0.230 -0.297 0.090 -0,333 0.110 -0.621 0.140 - 1.205

0.400 -0,272 0.130 -0.603 0.130 -2.261 ** 0.190 -2.261 **

0.490 -0.256 0.150 -0.911 0.150 - 1.061 0.250 -0.451

0.590 -0.332 0.200 -1.002 0.2 l0 -1.039 0.400 -0.393

0.630 -0.362 0.250 -0.457 0.250 -0.461 0.490 -0.369

0.700 -0.421 0.260 -0.355 0.340 -0.385 0.580 -0.378

0.750 -0.934 0.280 -0.353 0.370 -0.4 l 3 0.650 -0.478

0.8 l0 -0.884 0.290 -0.344 0.400 -0.373 0.700 -0.464

0.840 -0.924 0,310 -0.352 0.410 -3.267** 0.750 -0.551

0.900 -0,208 0.320 -0.352 0.430 -0.409 0,800 -0.931

0.960 -0.174 0.340 -0.350 0.440 -0.387 0.830 -0.571

0,350 -0.212"* 0.460 -0.392 0.900 -0.390

0.370 -0.344 0.490 -0.342 0.960 -0.397

0.380 -0.384 0.500 -0.405

0.400 -0.327 0,520 -0.392

0.410 -0.380 0.540 -0.395

0.430 -0.342 0.550 -0.377

0.440 -0.320 0.580 -0.377

0.460 -0.373 0.600 -0.398

0,470 -0.370 0.610 -0,423

0,490 -0.366 0.650 -0.825

0,500 -0.369 0.700 -0.641

0.520 -0,370 0,750 -0.626

0.530 -0.372 0.820 -0.633

0.550 -0.421 0.890 -0.302

0.560 -0.394 0.900 -0.306

0.580 -0.378 0.960 -0.260

0.590 -0.427

0.600 -0.426

0.640 -0.611

0.700 -0.4%

0.750 -0,023"*

0.820 -0.581

0.870 -0.373

0.930 -0.256

0.960 -0.270

Lower Surface

0.020 -0,840 0.020 - 1.102 0.020 -0.702 0.020 -0.981

0.110 -0.337 0.060 -0.281 0.060 -0.392 0.060 0.000

0.230 -0.059 0,090 -0.232 0.090 -0.200 0. 110 -0.204

0.400 0.045 0.120 -0.144 0.120 -0.320 0.250 -0.162

0.490 0.076 0.200 -0.055 0,200 -0.089 0.400 -0.145

0.630 4.127 ** 0,260 -0.040 0.250 -0.049 0.490 -0.147

0.750 0.149 0.400 0.000 0.400 -0.054 0.580 -0.077

0,850 0.181 0.490 0,008 0.490 -0.043 0,650 0.091

0.900 0.250 0.580 0.061 0.580 0.018 0.750 0.321

0.960 0.119 0.640 0.220 0.650 -0.039 0,830 0.424

0.750 0.270 0.750 -0,007 0.900 0.482

0.870 0.307 0.890 0.394 0.960 0.318

0.930 0.245 0.930 0.322

0.960 0.154 0.960 0.353

CN = 0.392 0.483 0.479 0.526

248
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-28-48-500, MINF = 0.805, Camber = 10/10, ALPT = 4.06, BETA = -0.33, QINF = 304,2,

RNPU = 2.5E+06, CNWP = 0.3188

TI = 0,93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0,528 0.000 0.131 0.000 0,241 ** 0.010 0.340

0.060 0.044 0.020 0.400 0.020 0.530 0.020 0.183

0.110 -0,340 0.040 0.360 0,060 0,259** 0.060 -0.355

0.200 -0.678 0.060 -0.109 0,090 -0,335 0.110 -0.708

0.230 -0.324 0.090 -0.315 0.110 -0.604 0,140 -1.157

0,400 -0.255 0.130 -0.574 0.130 -2.206"* 0.190 -2,206"*

0.490 -0.241 0.150 -0,884 0.150 - 1.025 0,250 -0.583

0.590 -0.322 0.200 -0,976 0.210 - 1.012 0.400 -0.381

0.630 -0.352 0.250 -0,844 0,250 -0.849 0.490 -0.358

0.700 -0,397 0.260 -0.439 0,340 -0.344 0.580 -0.377

0.750 -0.844 0.280 -0.360 0370 -0.362 0,650 -0.464

0.810 -0.853 0.290 -0.317 0.400 -0.354 0.700 -0,451

0,840 -0.892 0.310 -0.313 0.410 -3.187** 0.750 -0,542

0,900 -0.216 0.320 -0.315 0.430 -0.382 0.800 -0.996

0.960 -0.189 0.340 -0.313 0.440 -0.365 0.830 -0.583

0.350 -0.210"* 0,460 -0.381 0.900 -0.396

0.370 -0.316 0.490 -0,339 0.960 -0.393

0.380 -0.359 0.500 -0.389

0.400 -0,285 0,520 -0,380

0.410 -0.359 0.540 -0.370

0.430 -0.320 0.550 -0.354

0.440 -0.295 0.580 -0.383

0.460 -0.350 0.600 -0.387

0.470 -0.346 0.610 -0.397

0490 -0.351 0.650 -0.799

0.500 -0.353 0.700 -0.652

0.520 -0.359 0.750 -0.639

0.530 -0.36 t 0,820 -0.637

0.550 -0.409 0.890 -0.289

0.560 -0.389 0.900 -0.328

0.580 -0.367 0.960 -0.276

0.590 -0.414

0.600 -0.414

0.640 -0.626

0.700 -0.540

0.750 -0.017"*

0.820 -0.565

0,870 -0.376

0.930 -0.266

0.960 -0,276

Lower Surface

0.020 -O 862 0,020 -0.995 0.020 -0,713 0.020 -0.962

O.I I0 -0.333 0.060 -0.342 0.060 -0.406 0.060 0.002

0.230 -0.059 0.090 -0.270 0.090 -0.230 O.I 10 -0.217

0.400 0.039 0.120 -0.145 0.120 -0.327 0.250 -0.162

0.490 0.069 0.200 -0.055 0.200 -0.104 0.400 -0.146

0.630 4.032** 0.260 -0.051 0.250 -0.046 0.490 -0.141

0.750 0,140 0.400 0.002 0.400 -0,050 0,580 -0.087

0.850 0.179 0.490 0,010 0.490 -0.033 0.650 0.095

0.900 0.249 0.580 0.062 0.580 0.024 0.750 0.325

0.960 0.127 0.640 0.224 0.650 -0.032 0.830 0.424

0.750 0.274 0.750 0.000 0.900 0.485

0.870 0.302 0.890 0.401 0.960 0.324

0.930 0.249 0.930 0.324

0.960 O. 152 0.960 0.375

CN = 0.389 0.482 0.494 0,535

249
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-30-38-500, MINF = 0.793, Camber = 10/11, ALPT = 5.05, BETA = -0.50, QINF = 295.7,

RNPU = 2.4E+06, CNWP = 0.3418

= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 0.456 0.000 0.233 0.000 0.322 ** 0.010 O. 191

0.060 -0.030 0.020 0.287 0.020 0,426 0.020 0.040

O. I 10 -0.409 0.040 0.269 0.060 O. 197 * * 0.060 -0.525

0.200 -1. I 11 0.060 -0.180 0.090 -0,429 0.1 I 0 -0.797

0.230 -0.436 0.090 -0.410 0. l 10 -0.702 0.140 - 1.252

0.400 -0.268 0.130 -0.673 0.130 -2.273 * * 0.190 -2.273 * *

0,490 -0.260 0.150 -0.981 0.150 -l.130 0.250 -0.910

0.590 -0.337 0.200 -1.075 0.210 -1.125 0.400 -0.418

0.630 -0.375 0.250 - 1.089 0.250 - 1.082 0.490 -0.396

0.700 -0.425 0.260 - 1.013 0.340 -0.374 0.580 -0.399

0,750 -0.973 0.280 -0.952 0.370 -0.362 0.650 -0.498

0.810 -0.933 0.290 -0.519 0.400 -0.332 0.700 -0.485

0.840 -0,982 0.310 -0.399 0.410 -3.283 * * 0.750 -0.570

0.900 -0.252 0.320 -0.382 0.430 -0.383 0.800 -1.085

0.960 -0.227 0.340 -0.305 0.440 -0.365 0.830 -0.709

0.350 -0.190"* 0.460 -0.382 0.900 -0.397

0.370 -0.285 0.490 -0.323 0,960 -0.353

0.380 -0.336 0.500 -0.389

0.400 -0.283 0.520 -0.381

0.410 -0.350 0.540 -0.398

0.430 -0.319 0.550 -0.391

0.440 -0.290 0.580 -0.402

0.460 -0.362 0.600 -0.412

0.470 -0.359 0.610 -0.426

0.490 -0.363 0.650 -0.867

0.500 -0.369 0.700 -0.657

0.520 -0.367 0.750 -0.639

0.530 -0.375 0.820 -0.632

0.550 -0.429 0.890 -0.287

0.560 -0.409 0,900 -0.322

0.580 -0.380 0.960 -0.270

0.590 -0.434

0.600 -0.441

0.640 -0,621

0,700 -O512

0.750 -0.004"*

0.820 -0.583

0.870 -0.406

0.930 -0.297

0.960 -0.296

Lower Surface

0.020 -0.990 0.020 -0.754 0.020 -0.598 0.020 -0.452

O. 110 -0.144 0,060 -0.201 0,060 -0.078 0,060 0,020

0.230 -0.028 0,090 -0.132 0.090 -0.038 O, 110 -0.110

0.400 0.061 0. | 20 -0.029 0.120 -0.239 0.250 -0.1 O0

0.490 0.081 0.200 -0.028 0,200 -0.070 0.400 -0.096

0.630 4.142"* 0.260 0.009 0.250 -0.007 0,490 -0.105

0.750 0.150 0.400 0.028 0.400 -0.021 0.580 -0.065

0.850 0.191 0.490 0.025 0.490 -0.016 0,650 0.112

0.900 0.261 0.580 0.089 0.580 0.038 0,750 0.335

0.960 0.115 0.640 0.256 0.650 -0.023 0.830 0.438

0.750 0.309 0.750 0.006 0.900 0.494

0.870 0.358 0.890 0.441 0.960 0.326

0.930 0.285 0.930 0.363

0.960 0.171 0.960 0.416

CN = 0.492 O581 0.584 0.654

25O
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-29-6-000, MINF = 0.803, Camber = 10/11, ALPT = 6.26, BETA = -0.50, QINF = 302.9,

RNPU = 2.5E+06, CNWP = 0.4874

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.412 0.000 0.384 0,000 0.452"* 0.010 0.068

0,060 -0.098 0.020 0.249 0,020 0,327 0.020 -0.059

0.1 I 0 -0.440 0.040 0.200 0.060 0.052"* 0.060 -0,662

0,200 - 1.142 0.060 -0,262 0,090 -0,496 0.1 l 0 -0.967

0.230 - 1.042 0,090 -0,454 0. l 10 -0.734 0.140 - 1.305

0.400 -0.196 0.130 -0.716 0,130 -2.214"* 0,190 -2.214"*

0.490 -0.237 O. 150 - 1.004 O.150 - 1.164 0.250 -0.953

0.590 -0.331 0.200 - I. 106 0.2 lO - 1.157 0.400 -0.513

0.630 -0,368 0.250 - 1.146 0.250 - 1.144 0.490 -0.428

0.700 -0.413 0,260 - 1,091 0.340 - 1.127 0.580 -0.405

0.750 - 1.071 0.280 - I. 131 0,370 - 1.109 0,650 -0.491

0.810 - 1.026 0,290 - 1.096 0,400 -0,735 0.700 -0,489

0.840 - 1.055 0.310 - 1.052 0.410 -3.201 ** 0.750 -0,594

0,900 -0,325 0,320 - 1,074 0,430 -0,487 0.800 -0.799

0.960 -0,307 0.340 - 1.054 0,440 -0,423 0,830 -0.615

0,350 -0,479** 0.460 -0.378 0,900 -0.382

0.370 - 1.026 0,490 -0,302 0.960 -0,307

0.380 - 1.088 0,500 -0,333

0400 -0.640 0.520 -0,333

0,410 -0,505 0.540 -0.323

0,430 -0.374 0.550 -0,327

0.440 -0.305 0.580 -0.335

0.460 -0.300 0.600 -0.349

0.470 -0.255 0.610 -0.370

0.490 -0,243 0.650 -0,783

0,500 -0.225 0.700 -0,582

0,520 -0.238 0.750 -0,582

0.530 -0.255 0,820 -0.78 l

0.550 -0.314 0.890 -0.263

0.560 -0.302 0,900 -0,298

0.580 -0,293 0,960 -0,233

0,590 -0.326

0.600 -0.357

0.640 -0.483

0.700 -0.490

0.750 0.006**

0.820 -0,593

0.870 -0.438

0.930 -0.285

0.960 -0.291

Lower Surface

0,020 - 1,037 0.020 -0.537 0,020 -0.377 0.020 -0.182

0.110 -0,089 0,060 -0,042 0,060 0.072 0,060 0.017

0.230 -0,021 0.090 -0,019 0,090 0.052 0.110 -0.002

0.400 0.043 0.120 0,053 0.120 -0.160 0,250 -0,043

0.490 0.063 0,200 -0.011 0.200 -0,042 0.400 -0.052

0,630 4,051 ** 0.260 0,036 0.250 0,035 0.490 -0.067

0,750 0.160 0,400 0,051 0.400 0.014 0,580 -0,028

0.850 0.192 0,490 0.045 0.490 -0.010 0,650 0.129

0,900 0,266 0.580 0,089 0.580 0.054 0,750 0.361

0.960 0.093 0.640 0.282 0.650 -0,010 0,830 0,459

0.750 0.332 0.750 0.011 0.900 0.512

0,870 0,392 0.890 0483 0,960 0.341

0.930 0.323 0.930 0,378

0,960 0,208 0.960 0.416

CN = 0,570 0.691 0.703 0.714

251
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-29-11-000, MINF = 0.795, Camber = 10/11, ALPT = 7.98, BETA = -0.10, Q1NF = 296.7,

RNPU = 2.4E+06, CNWp = 0.5321

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.267 0000 0.599 0.000 0.471 ** 0.010 -0.174

0.060 -0.231 0.020 0.055 0.020 0.083 0.020 -0.240

0.110 -0.592 0.040 0.028 0.060 -0.058 ** 0.060 -0.846

0.200 - 1.237 0.060 -0.456 0.090 -0.696 0.110 - 1.194

0.230 -1.163 0.090 -0.607 0.110 -0882 0.140 -1.463

0.400 -0.511 0.130 -0.851 0.130 -2.259** 0.190 -2.259**

0.490 -0.241 0.150 - 1.121 0.150 - 1.284 0.250 - 1.460

0.590 -0.330 0.200 - 1.229 0.210 - 1.281 0.400 -0.816

0.630 -0.387 0.250 - 1.293 0.250 - 1.289 0.490 -0.615

0.700 -0.425 0.260 - 1.232 0.340 - 1.294 0.580 -0.540

0.750 - 1.117 0.280 - 1.273 0.370 - 1.307 0.650 -0.563

0.810 - 1.052 0.290 - 1.247 0.400 - 1.256 0.700 -0.572

0.840 - 1.098 0.310 - 1.217 0.410 -3.266"* 0.750 -0.671

0.900 -0.471 0.320 - 1.226 0.430 - 1.286 0.800 -0.531

0.960 -0.469 0.340 - 1.231 0.440 - 1.265 0.830 -0.458

0.350 -0.528** 0.460 - 1.267 0.900 -0.204

0.370 - 1.190 0.490 - 1.169 0.960 -0.176

0.380 - 1.277 0.500 -0.869

0.400 - 1.165 0.520 -0.734

0.410 - 1.224 0.540 -0.676

0.430 - 1.181 0.550 -0.619

0.440 - 1.131 0.580 -0.558

0.460 - 1.225 0.600 -0.507

0.470 - 1.198 0.610 -0.455

0.490 - 1.173 0.650 -0.624

0.500 -0.953 0.700 -0.455

0.520 -0.721 0.750 -0.555

0,530 -0,552 0.820 -0.559

0.550 -0.528 0.890 -0.172

0.560 -0A64 0.900 -0.155

0.580 -0.396 0.960 -0.104

0.590 -0.396

0.600 -0.353

0.640 -0.352

0.700 -0.436

0.750 0.026**

0.820 -0.635

0.870 -0.464

0.930 -0.271

0.960 -0.218

Lower Surface

0.020 -0.300 0.020 -0.113 0.020 -0.087 0.020 0.142

0.1 I0 0.007 0.060 0.155 0.060 0.2 l I 0.060 0.049

0.230 0.047 0.090 0.117 0.090 O. 176 0.110 0.132

0.400 0.060 0.120 0.163 0.120 -0.055 0.250 0.044

0.490 0.080 0.200 0.046 0.200 0.001 0.400 0.015

0.630 4.136"* 0.260 0.108 0.250 0.118 0.490 -0.007

0.750 0.160 0.400 0.099 0.400 0.066 0.580 0.023

0.850 0.196 0.490 0.081 0.490 -0.002 0.650 0.167

0.900 0.264 0.580 0.111 0.580 0.101 0.750 0.380

0.960 0.072 0.640 0.319 0.650 0.006 0.830 0.482

0.750 0.362 0.750 0.043 0.900 0.535

0.870 0.422 0.890 0.495 0.960 0.359

0.930 0.357 0.930 0.413

0.960 0.244 0.960 0.439

CN = 0.704 0,908 0.880 0.916

252
Table E-2, Continued.

Flight 204, Wing sweep = 26 °, Time = 9-13-37-500, MINF = 0.797, Camber = 10/10, ALPT = 7.25, BETA = 0.19, QINF = 277.2,

RNPU = 2.3E÷06, CNWP = 0.5409

rl = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.340 0.000 0,565 0.000 1.418"* 0,010 -0,143

0.060 -0.150 0.020 0.203 0.020 0.134 0.020 -0.101 **

0.110 -0.452 0.040 0.058 0.060 0.009** 0.060 -0.760**

0,200 - 1.208 0.060 -0.268 0.090 -0.522 0.110 - 1.109

0.230 - 1,044 0.090 -0.508 0.110 -0.826 0.140 - 1.421

0.400 -0.345 0.130 -0.734 0.130 - 1.030 0.190 -2,249"*

0.490 -0.185 0.150 - 1.078 0.150 -1.227 0.250 - 1.420

0.590 -0.283 0_200 - 1, l 17 0,210 - 1,309 0.400 -0,672

0.630 -0.357 0.250 - 1.240 0.250 - 1.219 0.490 -0.520

0.700 -0,378 0.260 - 1.253 0,340 - 1,235 0,580 -0.456

0.750 - 1,087 0.280 - 1,204 0.370 - 1.217 0.650 -0.527

0.810 -0.989 0.290 -1.196 0.400 -1.164 0.700 -0,514

0,840 -1.036 0.310 -1.154 0.410 -1.173 0.750 -0.611

0.900 -0.388 0.320 - 1.162 0.430 -1.194 0.800 -0,622

0.960 -0,366 0.340 - 1.228 0.440 - 1.162 0.830 -0.588

0.350 -0.408** 0.460 -0,665 0.900 -0.227

0.370 - 1.131 0.490 -0.579 0.960 -0.185**

0.380 - 1.204 0.500 -0.554

0.400 - 1.072 0.520 -0.474

0.410 - 1,140 0.540 -0.438

0.430 - 1.103 0.550 -0.410

0.440 - 1.077 0.580 -0.334

0.460 - 1,085 0.600 -0.419

0.470 -0.659 0.610 -0.352

0.490 -0.487 0.650 0.096**

0,500 -0.434 0.700 -0.443

0.520 -0.399 0.750 -0.478

0530 -0.305 0.820 -0.323

0.550 -0.299 0,890 -0.190

0.560 -0,242 0.900 -0.137

0.580 -0.223 0.960 -0. 110

0.590 -0.264

0.600 -0.235

0.640 -0.438

0.700 -0.427

0.750 -0.027**

0.820 -0.537

0.870 -0,472

0.930 -0,265

0.960 -0.236

Lower Surface

0.020 -0,558 0.020 -0,230 0.020 -0.252 0,020 0.023

0. I 10 0.035 0.060 0,118 0.060 0.196 0.060 0.108

0.230 0.083 0.090 0.111 0.090 0.112 0.110 0. 139

0.400 0.085 0.120 0.175"* 0.120 0.030 0.250 0,042

0.490 0.114 0.200 -0,013 0,200 0,185 0.400 -0.098

0.630 4.867"* 0.260 0.046 0,250 0.060 0.490 -0.122

0,750 0,187 0.400 0. I 17 0.400 -0.009 0.580 0.008

0.850 0.226 0.490 0.094 0.490 0.003 0.650 0.187

0.900 0.300 0.580 0.131 0,580 0.105 0.750 0.391

0.960 0.115 0.640 0.341 0.650 0.085 0.830 0.430

0.750 0.367 0.750 -0.543** 0.900 0.489

0.870 0.472 0.890 0.519 0,960 0.392

0,930 0.368 0,930 0.348

0.960 0.258 0.960 0.269

CN = 0.655 0.813 0.792 0.836

253
Table E-2. Continued.

Flight 204, Wing sweep = 26", Time = 9-13-41-500, MINF = 0.794, Camber = 10/10, ALPT = 8.13, BETA = -0.10, QINF = 276.5,

RNPU = 2.3E+06, CNWP = 0.6455

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.240 0.000 0.688 0.000 1.411 ** 0.010 -0.153

0.060 -0.232 0.020 0.059 0.020 0.069 0.020 -0.217"*

O. 1 I0 -0.533 0,040 0.031 0.060 -0.073** 0.060 -0.889**

O.200 - 1.246 0.060 -0.398 0.090 -0.695 O.110 - 1.198

0.230 -1.167 0.090 -0.595 0.110 -0.925 0.140 -1.491

0.400 -0.777 0.130 -0.823 0.130 - 1.102 0.190 -2.266"*

0.490 -0.266 0.150 - 1.045 0.150 - 1.292 0.250 - 1.495

0.590 -0.296 0.200 - 1.180 0.210 - 1.294 0.400 -0.865

0.630 -0.362 0.250 - 1.305 0.250 - 1.288 0.490 -0.640

0.700 -0.407 0.260 - 1.252 0.340 - 1.331 0.580 -0.573

0.750 - 1.103 0.280 - 1.287 0.370 - 1.311 0.650 -0.569

0.810 - 1.003 0.290 - 1.278 0.400 - 1.243 0.700 -0.585

0.840 - 1.098 0.310 - 1.234 0.410 - 1.265 0.750 -0.647

0.900 -0.459 0.320 - 1.241 0.430 - 1.290 0.800 -0.484

0.960 -0.455 0.340 - 1.243 0.440 - 1.284 0.830 -0.406

0.350 -0.445"* 0.460 - 1.036 0.900 -0.179

0.370 - 1.217 0.490 - 1.222 0.960 -0.124"*

0.380 - 1.285 0.500 - 1.281

0.400 -1.162 0.520 -1.131

0.410 - 1.212 0.540 -0.833

0.430 - 1.201 0.550 -0.724

0.440 - 1.160 0.580 -0.619

0.460 - 1.222 0.600 -0.595

0.470 - 1.210 0.610 -0.565

0.490 - I. 164 0.650 0.120"*

0.500 - I_ 162 0.700 -0,444

0.520 - 1.162 0.750 -0.499

0.530 -0.881 0.820 -0.178

0.550 -0.635 0.890 -0.131

0.560 -0.536 0.900 -0.103

0.580 -0.471 0.960 -0.048

0.590 -0.485

0.600 -0.434

0.640 -0.308

0.700 -0.396

0.750 0.119'*

0.820 -0.931

0.870 -0.315

0.930 -0.146

0.960 -0.102

Lower Surface

0.020 -0.229 0.020 -0.001 0.020 -0.019 0.020 0.227

0. I 10 0.071 0.060 0.240 0.060 0.297 0.060 0.097

0.230 0.100 0.090 0.182 0.090 0.278 0.110 0.204

0.400 0.121 0.120 0.223** 0.120 0.081 0.250 0.091

0.490 0.110 0.200 0.105 0.200 0.213 0.400 0.040

0.630 4.867"* 0.260 0.160 0.250 0.191 0.490 0.056

0.750 0.191 0.400 0.130 0.400 0.127 0.580 0.054

0.850 0.222 0.490 0.127 0.490 0.102 0.650 0.216

0.900 0.303 0.580 0.151 0.580 0.133 0.750 0.428

0.960 0.115 0.640 0.346 0.650 0.125 0.830 0.537

0.750 0.402 0.750 -0.556** 0.900 0.582

0.870 0.483 0.890 0.548 0.960 0.403

0.930 0.392 0.930 0.440

0.960 0.290 0.960 0.283

CN = 0.775 0.965 0.953 0.960

254
Table E-2, Continued,

Flight 204, Wing sweep = 26 °, Time = 9-13-34-500, MINF = 0.796, Camber = 10/10, ALPT = 6.19, BETA = -0.56, QINF = 275.6,

RNPU = 23E+06, CNWP = 0A409

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.418 0.000 O.362 0.000 1.261 ** 0.010 0.073

0,060 -0.128 0.020 O. 143 0.020 0.279 0.020 -0.062"*

O. 110 -0.414 0.040 0.057 0.060 0.080"* 0.060 -0.666"*

0.200 - 1.203 0.060 -0.225 0.090 -0.514 O.110 - 1.040

0.230 - 1.084 0.090 -0.437 O. 110 -0.759 O. 140 - 1.313

0.400 -0.180 0.130 -0.742 0.130 - 1.001 0.190 -2.256"*

0.490 -0.205 0,150 -0,941 0.150 - 1.194 0.250 -0.957

0,590 -0,375 0,200 - 1,130 0.210 - 1,236 0.400 -0.507

0.630 -0.380 0.250 - 1.178 0.250 - 1.135 0.490 -0.459

0.700 -0.410 0.260 - 1.096 0.340 - 1.295 0.580 -0.564

0.750 - 1,074 0,280 - 1.191 0,370 -0.922 0.650 -0,516

0.810 - 1,046 0,290 - 1,288 0.400 -O570 0,700 -0.49 [

0.840 - 1,219 0,310 - 1.056 0.410 -0.507 0.750 -0.609

0,900 -0.442 0.320 - 1.068 0.430 -0.457 0.800 -0.806

0.960 -0.232 0.340 - 1.048 0.440 -0.405 0.830 -0.646

0.350 -0.413" * 0.460 -0.245 0.900 -0.391

0.370 -1.000 0.490 -0.311 0.960 -0.442**

0.380 -0.669 0_500 -0.456

0.400 -0.472 0.520 -0.317

0.410 -0,424 0,540 -0.367

0,430 -0356 0.550 -0.477

0.440 -0.298 0.580 -0.349

0.460 -0.222 0.600 -0.384

0,470 -0.293 0.610 -0.425

0.490 -0.214 0.650 0.018"*

0.500 -0.222 0.700 -0.770

0.520 -0.409 0.750 -0.603

0.530 -0.308 0.820 -0.449

0.550 -0,325 0.890 -0.291

0.560 -0.365 0.900 -0.301

0.580 -0.271 0.960 -0.230

0.590 -0.518

0.600 -0 369

0.640 -0.525

0.700 -0.551

0.750 0.085**

0.820 -0.606

0.870 -0.497

0.930 -0.308

0,960 -0,295

Lower Surface

0.020 -0.567 0.020 -0.659 0.020 -0.354 0,020 -0,275

0.110 -0.161 0.060 -0.078 0.060 0.038 0,060 0.051

0.230 0.001 0.090 -0.047 0.090 0.058 0.110 -0.067

0,400 O.1O0 O.120 0.023"* O. 120 -0.131 0.250 -0.074

0.490 0,045 0,200 0.044 0,200 0,058 0,400 -0.061

0.630 4.901 ** 0.260 0.004 0.250 0.042 0.490 -0.094

0.750 0.203 0.400 0.008 0.400 -0,089 0.580 -0.024

0.850 0.198 0.490 0.017 0.490 -0,103 0.650 0.138

0,900 0.306 0.580 -0.058 0.580 0.071 0.750 0.330

0.960 0,146 0.640 0.300 0.650 0,032 0.830 0.422

0.750 0,189 0.750 -0.540"* 0,900 0.560

0.870 0.438 0,890 0.353 0.960 0.387

0.930 0.284 0,930 0.351

0.960 0.170 0.960 0.229

CN = 0.603 0.668 0.683 0.724

255
Table E-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 9-13-48-500, MINF = 0.788, Camber = 10/10, ALPT = 9.09, BETA = -0.04, QINF = 277.2,

RNPU = 2.3E+06, CNWP = 0.7290

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.108 0.000 0.831 0.000 1.424"* 0.010 -0.371

0,060 -0.336 0.020 -0.082 0.020 -0,080 0,020 -0.350**

0. I 10 -0.633 0.040 -0.107 0.060 -0.158"* 0.060 -0,977"*

0.200 - 1.304 0,060 -0,541 0,090 -0.839 0.110 - 1.342

0.230 -1.221 0.090 -0,772 0.110 -1.064 0.140 -1.596

0.400 -0,991 0,130 -0.911 0.130 - 1.233 0.190 -2.300"*

0.490 -0.361 0.150 - 1.136 0,150 - 1.384 0.250 -I.577

0.590 -0.314 0.200 - 1.246 0.210 - 1.378 0.400 - 1,072

0.630 -0.380 0.250 - 1.375 0.250 - 1.367 0.490 -0.767

0.700 -0.420 0.260 - 1.313 0,340 - 1,403 0.580 -0.616

0.750 - 1.090 0.280 - 1.365 0.370 - 1.403 0.650 -0.549

0.8 t 0 - 1,008 0,290 - 1.365 0.400 - 1,345 0.700 -0.515

0.840 -1,104 0.310 -1.315 0.410 -1.355 0.750 -0.560

0.900 -0,548 0.320 - 1.321 0.430 - 1.378 0.800 -0,437

0.960 -0.522 0.340 - 1.327 0.440 - 1,369 0.830 -0.368

0.350 -0,443"* 0,460 -1.118 0.900 -0.155

0.370 - 1.305 0.490 - 1,302 0.960 -0,098 **

0.380 -1.382 0.500 -1.378

0.400 - 1.255 0.520 - 1.196

0.410 - 1.313 0.540 -0.895

0.430 - 1.288 0,550 -0.805

0.440 - 1.251 0.580 -0.723

0.460 - 1.325 0.600 -0.727

0.470 - 1.267 0.610 -0.686

0.490 - 1.268 0.650 0,139"*

0.500 - 1.275 0,700 -0.554

0,520 - 1.270 0,750 -0,539

0.530 - 1.239 0.820 -0.082

0.550 -0.855 0,890 -0,190

0.560 -0.708 0.900 -0,171

0.580 -0.627 0,960 -0.105

0.590 -0,638

0.600 -0.611

0.640 -0.395

0.700 -0.399

0.750 0,146"*

0.820 -0,474

0.870 -0.204

0.930 -0,106

0,960 -0,102

Lower Surface

0.020 -0.090 0.020 0.158 0.020 0.140 0.020 0.395

0,110 0.107 0.060 0.311 0.060 0.375 0.060 0,042

0.230 0.156 0,090 0,249 0.090 0.340 0. I 10 0.249

0,400 0.124 0,120 0,278"* 0,120 0.126 0.250 0.153

0.490 0.118 0.200 0.152 0.200 0.240 0,400 0.087

0.630 4,817"* 0.260 0.207 0.250 0.230 0.490 0.088

0.750 0.202 0,400 0,165 0.400 0.145 0.580 0.099

0.850 0.228 0,490 0.154 0,490 0.110 0.650 0.247

0.900 0.306 0.580 0.170 0.580 0.1 64 0.750 0.451

0.960 0.109 0.640 0.360 0.650 0.133 0.830 0.543

0.750 0.406 0.750 -0.594** 0.900 0.598

0.870 0,495 0,890 0.555 0.960 0.419

0.930 0.392 0.930 0.438

0,960 0.285 0.960 0.306

CN = 0,861 1,021 1,051 1.040

256
Table E-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 9-13-51-500, MINF = 0.789, Camber = 10/10, ALPT = 10.08, BETA = 0.80, QINF = 281.5,

RNPU = 2.3E+06, CNWP = 0.5351

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.038 0.000 0.888 0.000 1.379"* 0.010 -0.455

0.060 -0.401 0.020 -0.359 0.020 -0.164 0.020 -0.390**

0.110 -0.697 0.040 -0.161 0.060 -0.298** 0.060 -1.030"*

0.200 - 1.283 0,060 -0.800 0.090 -0.905 0.110 - 1.467

0,230 - 1.252 0.090 -0.835 0.110 - 1.105 0.140 - 1.613

0,400 -0.580 0.130 -0.988 0.130 - 1,290 0.190 -2.296"*

0.490 -0.238 0.150 - 1.184 0,150 - 1.417 0.250 - 1.645

0.590 -0.334 0,200 -1.294 0.210 -1.318 0.400 -1.144

0.630 -0.407 0.250 - 1.381 0.250 -0.886 0.490 -0.636

0.700 -0.442 0.260 - 1.329 0.340 -0.869 0,580 -0.329

0.750 -1.062 0.280 -1.307 0.370 -0.839 0.650 -0.422

0.810 - 1.016 0.290 - 1.168 0.400 -0.774 0.700 -0.409

0.840 -1.111 0.310 -1.119 0.410 -0.801 0.750 -0.525

0.900 -0.420 0.320 - 1.112 0.430 -0.797 0.800 -0.490

0.960 -0.421 0.340 -1.068 0.440 -0.777 0.830 -0.460

0.350 -0.302'* 0.460 -0.524 0,900 -0.211

0.370 -0.834 0.490 -0.737 0.960 -0.140"*

0.380 -0.872 0,500 -0.774

0.400 -0.745 0.520 -0.748

0.410 -0.768 0.540 -0.752

0.430 -0.751 0.550 -0.754

0.440 -0.709 0.580 -0.731

0.460 -0.722 0.600 -0.742

0.470 -0.717 0.610 -0.719

0.490 -0.676 0.650 0.085"*

0.500 -0.653 0.700 -0.621

0.520 -0.656 0.750 -0.594

0.530 -0.622 0.820 -0.180

0.550 -0,572 0.890 -0.461

0.560 -0.599 0.900 -0.406

0,580 -0.547 0.960 -0.336

0.590 -0.577

0.600 -0,540

0.640 -0.400

0.700 -0.413

0.750 0.136"*

0.820 -0.291

0.870 -0.279

0.930 -0,310

0.960 -0.288

Lower Surface

0.020 -0.016 0,020 0.252 0.020 0.211 0.020 0.470

0.110 0.119 0.060 0.346 0.060 0.364 0.060 O. 118

0.230 0.156 0.090 0.273 0.090 0.379 0.110 0.352

0.400 0. l 18 0.120 0.304"* 0.120 0.159 0.250 0.175

0.490 0.123 0.200 0.161 0.200 0.246 0.400 0.116

0.630 4.712"* 0.260 0.226 0.250 0.249 0.490 0.094

0.750 0.210 0.400 0.166 0.400 0.153 0.580 0.097

0.850 0.232 0.490 0.147 0.490 0.115 0.650 0,234

0.900 0.320 0.580 0.159 0.580 0.153 0.750 0.443

0.960 0.147 0.640 0.346 0.650 0.122 0.830 0.534

0.750 0.391 0.750 0.069"* 0.900 0.591

0.870 0.487 0.890 0.538 0.960 0.406

0.930 0.358 0.930 0.411

0,960 0.230 0.960 0.232

CN = 0.800 0.918 0.937 1.055

257
Table E-2. Continued.

Flight 201, Wing sweep = 26 °, Time = 8-31-7-500, MINF = 0.814, Camber = 10/10, ALPT = 4.04, BETA = -0.18, QINF --- 320.1,

RNPU = 2.6E+06, CNWP = 0.3605

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.561 0.000 0.134 0.000 0.888** 0.010 0.402

0.060 0.071 0,020 0.552 0.020 0.563 0.020 0.291 **

0.110 -0.294 0,040 0.402 0.060 0.516"* 0.060 -0.308**

0.200 - 1.019 0.060 -O016 0.090 -0.279 0.110 -0.680

0.230 -0.331 0.090 -0.254 0.110 -0,544 0.140 -1.121

0.400 -0.214 0.130 -0.535 0.130 -0.816 0.190 -2.156 * *

0.490 -0.217 0.150 -0.841 0.150 - 1.008 0.250 -0.768

0.590 -0.298 0.200 -0.947 0.210 -0.967 0.400 -0.346

0.630 -0.341 0.250 -0.927 0.250 -0.933 0.490 -0.329

0.700 -0,394 0.260 -0.897 0.340 -0.298 0.580 -0,329

0.750 -0.638 0.280 -0.484 0,370 -0.322 0,650 -0,450

0.810 -0,574 0.290 -0.333 0.400 -0.300 0.700 -0.409

0.840 -0.625 0.310 -0.280 0.410 -0.326 0.750 -0.517

0.900 -0.204 0.320 -0.275 0,430 -0.334 0.800 - 1.04 1

0.960 -0.170 0.340 -0,255 0.440 -0.332 0.830 -0.576

0.350 -0.126"* 0.460 -0.115 0.900 -0.398

0,370 -0.271 0.490 -0.300 0.960 -0.390**

0.380 -0.308 0.500 -0.336

0.400 -0.252 0.520 -0.332

0.410 -0.297 0.540 -0.336

0.430 -0.286 0.550 -0,330

0.440 -0.280 0.580 -0.302

0.460 -0.303 0,600 -0.361

0.470 -0.312 0.610 -0.386

0.490 -0.312 0.650 0.035**

0.500 -0.306 0.700 -0.612

0.520 -0.319 0.750 -0.588

0.530 -0.323 0.820 -0.353

0.550 -0.334 0.890 -0.298

0.560 -0.364 0.900 -0.322

0.580 -0.319 0.960 -0.279

0,590 -0.381

0.600 -0.378

0_640 -0.591

0.700 -0.535

0.750 0.047**

0.820 -0.543

0.870 -0.352

0.930 -0.245

0.960 -0,244

Lower Surface

0.020 -0.814 0.020 -0.919 0.020 -0.780 0.020 -0.958

0.110 -0,486 0.060 -0.553 0.060 -0.491 0,060 - 1.142

0.230 -0.031 0.090 -0.326 0.090 -0.272 0.110 -0.082

0.400 0.080 0.120 -0.116'* 0.120 -0.217 0.250 -0.149

0.490 0.102 0.200 -0.023 0.200 -0,032 0.400 -0.137

0.630 1.889"* 0,260 -0.006 0,250 -0,028 0.490 -0.119

0.750 0.180 0.400 0.006 0.400 -0.042 0.580 -0.077

0.850 0.185 0.490 0.035 0.490 0,032 0.650 0.123

0.900 0.258 0.580 0.088 0.580 0.042 0.750 0.356

0.960 O.142 0.640 0.246 0.650 0.038 0.830 0.464

0.750 0.298 0.750 0.018"* 0.900 0.527

0.870 0.372 0.890 0.451 0.960 0.359

0.930 0.290 0.930 0.351

0.960 O.184 0.960 0.378

CN = 0.355 0.465 0_481 0.486

258
Table E-2. Continued.

Flight 201, Wing sweep = 26 °, Time = 8-31-19-500. MINF = 0.799, Camber = 10/10, ALPT = 6.03, BETA = -0,04, QINF = 306.9,

RNPU = 2.5E+06, CNWP = 0.5275

rl = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.429 0.000 0.401 0.000 1.045" * 0,010 0.115

0.060 -0.077 0.020 0,395 0.020 0.369 0,020 0.04 l **

0.110 -0.418 0.040 0.242 0,060 0_326"* 0,060 -0636**

0.200 - 1.151 0.060 -0.175 0,090 -0.451 0,110 -0.949

0.230 - 1,026 0.090 -0.402 0.110 -0.703 0.140 - 1.293

0.400 -0,185 0.130 -0.681 0.130 -0.980 0.190 -2.240"*

0.490 -0.221 0.150 -0,988 0.150 - I, 143 0.250 -0.957

0.590 -0.310 0.200 - 1.102 0,210 - 1.140 0.400 -0.461

0.630 -0,355 0.250 - 1.130 0,250 - 1.154 0.490 -0.375

0,700 -0,421 0.260 -1,104 0.340 -1.1 I l 0,580 -0,371

0.750 - 1.053 0.280 - 1.112 0.370 - 1.071 0,650 -0,486

0,810 -0.981 0.290 - 1.086 0.400 -0.492 0,700 -0.454

0,840 - 1,050 0.310 - 1.043 0.410 -0.460 0.750 -0.562

0.900 -0.268 0,320 - 1.060 0.430 -0,399 0.800 -0.770

0.960 -0.230 0.340 - 1.035 0,440 -0,338 0.830 -0,657

0.350 -0.398** 0.460 -0.088 0.900 -0.321

0.370 -1.021 0.490 -0.267 0.960 -0.257**

0.380 -0,688 0,500 -0.290

0.400 -0.443 0.520 -0,257

0.410 -0.369 0.540 -0.300

0.430 -0.286 0.550 -0.297

0.440 -0,244 0.580 -0.292

0.460 -0.223 0.600 -0.347

0.470 -0.226 0.610 -0.380

0.490 -0.217 0.650 0.060"*

0.500 -0.216 0.700 -0.589

0.520 -0,242 0,750 -0.539

0,530 -0.245 0.820 -0.472

0.550 -0.281 0.890 -0.240

0,560 -0,302 0.900 -0.240

0,580 -0.277 0.960 -0.182

0.590 -0353

0.600 -0.347

0.640 -0.480

0.700 -0.481

0.750 0.076**

0.820 -0.573

0.870 -0,444

0.930 -0.250

0,960 -0,231

Lower Surface

0,020 -0.564 0.020 -0.614 0,020 -0.441 0,020 -0.260

0.110 -0.140 0.060 -0.065 0.060 0.071 0.060 - 1.010

0.230 0,017 0.090 0.008 0.090 0.071 0.110 0.076

0.400 0.103 0.120 0.091 ** 0.120 -0.003 0,250 -0.017

0.490 0.104 0.200 0.03 ! 0,200 0,016 0.400 -0_034

0.630 1,980"* 0.260 0.095 0,250 0.058 0.490 -0,035

0.750 0.193 0.400 0.056 0,400 0.023 0.580 -0.009

0.850 0.213 0.490 0.071 0.490 0.064 0.650 0,166

0.900 0.295 0,580 0.108 0.580 0.077 0,750 0.395

0.960 0.139 0,640 0.302 0.650 0.070 0,830 0.499

0.750 0,358 0.750 0,035** 0.900 0,561

0.870 0.452 0,890 0.529 0.960 0.384

0,930 0.347 0.930 0.419

0.960 0.223 0.960 0,421

CN = 0.579 0.677 0.696 0.642

259
Table E-2. Continued.

Flight 201, Wing sweep = 26 °, Time = 8-31-27-000, MINF = 0,800, Camber = 10/10, ALPT = 6.99, BETA = 0.28, QINF = 307.5,

RNPU = 2.5E+06, CNWP = 0.5905

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.386 0.000 0.513 0.000 1.145"* 0.010 -0.018

0.060 -0.130 0,020 0.303 0.020 0.271 0.020 -0.041 **

0.110 -0.442 0.040 0.158 0.060 0.352** 0.060 -0.706"*

0.200 - 1.191 0.060 -0.245 0.090 -0.512 O.110 - 1.048

0.230 - 1.094 0.090 -0,457 O. 110 -0.753 O.140 - 1.384

0.400 -0.231 0.130 -0.717 0.130 -1.014 0,190 -2.230**

0.490 -0.186 0.150 - 1.030 0.150 - 1.179 0.250 - 1.297

0.590 -0.297 0.200 -1.141 0.210 -1.186 0.400 -0.671

0.630 -0.349 0.250 - 1.182 0.250 - 1.195 0.490 -0.501

0.700 -0.404 0.260 - l. 167 0.340 - 1.191 0.580 -0.422

0.750 - 1.076 0.280 - 1.175 0.370 - 1.187 0.650 -0.505

0.g 10 -0.980 0.290 - 1.158 0.400 - 1.148 0.700 -0.484

0.840 - 1.053 0.310 - 1.121 0.410 - 1.153 0.750 -0.598

0,900 -0.345 0,320 - 1.133 0.430 - 1.169 0.800 -0.647

0.960 -0.321 0.340 -1.113 0.440 -1.143 0.830 -0.583

0.350 -0,424** 0.460 -0.611 0.900 -0.274

0.370 - 1.099 0.490 -0,549 0.960 -0.197* *

0.380 -1.155 0.500 -0.489

0.400 - 1.064 0.520 -0.434

0.410 -1.103 0.540 -0.399

0.430 - 1.066 0.550 -0.348

0.440 - 1.049 0.580 -0.306

0,460 -0.980 0.600 -0.321

0,470 -0.597 0,610 -0.319

0.490 -0.452 0.650 0.084**

0.500 -0.382 0.700 -0.440

0.520 -0,342 0.750 -0.483

0.530 -0.276 0.820 -0,375

0.550 -0.251 0.890 -0.185

0.560 -0.233 0.900 -0.176

0.580 -0.205 0.960 -0.134

0.590 -0.246

0.600 -0.221

0.640 -0.369

0.700 -0.439

0.750 0.092**

0.820 -0.574

0.870 -0.466

0.930 -0.226

0,960 -0.214

Lower Surface

0.020 -0.675 0.020 -0.382 0.020 -0.238 0.020 -0.065

0.110 0.028 0.060 0.064 0.060 0.155 0.060 -0.960

0.230 0.059 0.090 0.085 0.090 0.143 0.110 0.125

0.400 0.072 0.120 0.157** 0.120 0.059 0.250 0,035

0.490 0.105 0.200 0.065 0.200 0.049 0.400 0.000

0,630 1.982* * 0.260 0.136 0.250 0.107 0.490 -0.001

0.750 0.201 0.400 0.079 0.400 0.063 0.580 0.021

0.850 0.213 0.490 0.095 0.490 0.076 0.650 0.193

0.900 0.296 0.580 0.124 0.580 0.108 0.750 0.414

0.960 O.118 0.640 0.317 0.650 0.083 0.830 0.518

0.750 0.385 0.750 0.059** 0.900 0.566

0.870 0.471 0.890 0.548 0.960 0.406

0.930 0.373 0.930 0.438

0.960 0.249 0.960 0,464

CN = 0.630 0.792 0.789 0.772

260
Table E-2. Continued.

Flight 201, Wing sweep = 26 °, Time = 8-31-42-000, MINF = 0.810, Camber = 10/10, ALPT = 8,08, BETA = 0,34, QINF = 321.9,

RNPU = 2.6E+06, CNWP = 0.7250

rl = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP xffc CP

0,020 0.312 0.000 0.649 0.000 1.098" * 0.010 -0.071

0.060 -0.180 0.020 0,225 0.020 0.143 0.020 -0,141 **

0.110 -0.477 0.040 0.093 0,060 0.209"* 0.060 -0.749* *

0.200 - 1,179 0.060 -0.326 0,090 -0.616 0,110 - 1.123

0.230 -1.125 0.090 -0.523 0A 10 -0.801 0,140 -1.415

0.400 -0.861 0.130 -0,756 0.130 - 1.033 0.190 -2.175"*

0.490 -0,608 0.150 - 1,060 0.150 - 1,204 0.250 - 1.443

0.590 -0.317 0,200 - 1.176 0.210 - 1.200 0.400 -0.935

0.630 -0.359 0.250 - 1.212 0,250 - 1.238 0.490 -0.697

0.700 -0.393 0,260 - 1.199 0,340 - 1.254 0.580 -0.623

0.750 - 1,023 0.280 - 1.218 0.370 - 1.255 0650 -0.690

0.810 -0.960 0.290 - 1.196 0.400 - 1.190 0.700 -0.674

0.840 - 1.037 0.310 - 1.167 0.410 - 1.221 0,750 -0.743

0.900 -0.447 0.320 - 1,188 0.430 - 1,247 0.800 -0.433

0.960 -0.435 0.340 - 1,160 0.440 - 1.235 0.830 -0.386

0.350 -0.426* * 0.460 - 1.009 0.900 -0.205

0,370 -1.156 0.490 -1.182 0.960 -0.178"*

0.380 -1,229 0,500 -1.218

0.400 -1,116 0.520 -1.221

0.410 -1.173 0.540 -1.213

0.430 -1.138 0,550 -1.189

0.440 -1.112 0.580 -1.166

0.460 - 1.168 0.600 - 1.193

0.470 -1.156 0.610 -t.148

0.490 -1,133 0.650 0.086**

0.500 - 1.152 0,700 -0.540

0.520 -1.128 0.750 -0.489

0.530 -1.121 0,820 -0.065

0.550 - 1.096 0.890 -0.156

0.560 -1.141 0.900 -0.t27

0.580 - 1,099 0.960 -0,088

0.590 -1.154

0.600 -1.113

0.640 -0.474

0.700 -0.416

0.750 0.108"*

0.820 -0.553

0.870 -0.214

0.930 -0,117

0.960 -0.113

Lower Surface

0,020 -0.444 0.020 -0.133 0.020 -0.101 0.020 0.180

0,110 0.037 0.060 0.170 0.060 0,239 0.060 -0.838

0.230 0.098 0.090 0.159 0.090 0.219 0.110 0.209

0.400 0.082 0.120 0.214"* 0.120 0.119 0.250 0.074

0.490 0.110 0.200 0,106 0.200 0.092 0.400 0,037

0,630 1.849"* 0.260 0.153 0.250 0.153 0,490 0.023

0.750 0.212 0.400 0.100 0,400 0.088 0,580 0.026

0,850 0.203 0.490 0.118 0.490 0.107 0.650 0, 201

0.900 0.304 0.580 0.132 0,580 0.130 0,750 0.423

0,960 0.109 0.640 0,327 0.650 0.099 0.830 0.507

0.750 0.393 0.750 0,056"* 0.900 0.586

0.870 0.503 0,890 0.547 0.960 0.422

0,930 0.400 0.930 0.435

0.960 0.292 0.960 0.470

CN = 0.789 0.949 0.975 0.904

261
Table E-2. Continued.

Flight 201, Wing sweep = 26 °, Time = 8-31-47-000, M1NF = 0.809, Camber = 10/10, ALPT = 9.21, BETA = 0.11, QINF = 324.0,

RNPU = 2.6E+06, CNWP = 0.7585

'q = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 O. 193 0.000 0.770 0.000 1.099** 0.010 -0.262

0060 -0.290 0.020 0.033 0.020 -0.005 0.020 -0.283"*

O. I 10 -0.565 0.040 -0.044 0.060 0.093** 0.060 -0.896"*

0.200 -1.223 0,060 -0.451 0.090 -0.788 0.110 -1.223

0.230 - 1.167 0.090 -0.647 0.110 -0.954 0,140 - 1.503

0.400 -0.986 0.130 -0.842 0.130 - 1.156 0.190 -2.185"*

0.490 -0,767 0,150 - 1.124 0.150 - 1.295 0.250 - 1.538

0.590 -0.285 0.200 - 1.231 0.210 - 1.293 0.400 - 1.085

0.630 -0.349 0.250 - 1.296 0,250 - 1.308 0.490 -0.872

0.700 -0.400 0.260 - 1.263 0.340 - 1.328 0.580 -0.723

0.750 - 1.025 0.280 - 1,283 0,370 - 1.333 0.650 -0.764

0,810 -0.951 0.290 - 1.291 0.400 - 1.297 0.700 -0.730

0.840 - 1.042 0.310 - 1.252 0.410 - 1.305 0.750 -0,763

0.900 -0.634 0.320 - 1.264 0.430 - 1.320 0.800 -0.395

0.960 -0.518 0.340 - 1.258 0,440 - 1.307 0.830 -0.342

0.350 -0,426"* 0.460 -1.030 0.900 -0.185

0,370 - 1.244 0,490 - 1,249 0.960 -0,124**

0.380 -1.311 0.500 -1.304

0.400 - 1.208 0.520 - 1.306

0.410 - 1.257 0.540 - 1.310

0,430 - 1.222 0.550 - 1.292

0.440 - 1.213 0.580 - 1.269

0,460 - 1.257 0.600 - 1,13 t

0.470 - 1.243 0.610 -0.789

0.490 - 1.195 0.650 0.101 **

0.500 - 1.220 0,700 -0.568

0.520 - 1.061 0.750 -0.580

0.530 -0.839 0.820 -0,177

0,550 -0.658 0.890 -0.317

0.560 -0,625 0,900 -0.335

0.580 -0.595 0.960 -0.281

0.590 -0,610

0.600 -0,562

0.640 -0.469

0.700 -0.473

0.750 0.119"*

0,820 -0.265

0.870 -0.238

0.930 -0,275

0.960 -0.246

Lower Surface

0.020 -0.178 0.020 0.042 0.020 0.074 0.020 0.341

0.110 0.071 0.060 0.260 0.060 0.300 0.060 -0.763

0.230 0.127 0.090 0.208 0.090 0.274 0.110 0.266

0.400 0.094 0.120 0.252** 0.120 0.168 0.250 0.126

0.490 0.098 0.200 0.131 0.200 0.122 0.400 0.079

0.630 1.812"* 0.260 0.195 0.250 0.188 0,490 0,059

0.750 0.177 0.400 0.125 0.400 0.121 0.580 0.069

0.850 0.200 0.490 O.119 0,490 0.105 0.650 0.219

0.900 0.297 0.580 0.136 0.580 0.134 0.750 0.436

0.960 0.126 0.640 0.327 0.650 0.111 0.830 0.533

0.750 0.376 0.750 0.085** 0.900 0.593

0.870 0.472 0.890 0.539 0.960 0.416

0.930 0,353 0.930 0.427

0.960 0.235 0.960 0.436

CN = 0,852 0.951 1.064 1.007

262
Table E-2. Continued.

Flight 214, Wing sweep = 26 °, Time = 9-0-54-000, MINF = 0,794, Camber = 0/11, ALPT = 4.01, BETA = -0,53, Q1NF = 295.6,

RNPU = 24E+06. CNWP = 0.3069

"q = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 - 1,078 0.000 0.701 0.000 -0.533"* 0.010 -2,175

0.060 -0.335 0.020 -0,576 0.020 -0.847 0,020 - 1.944

0.110 - 1.157 0.040 -0.424 0.060 -0.970 ** 0.060 - 1.749

0.200 -0.482 0.060 -0.556 0.090 -0,590 0.110 -0,417

0.230 - 1,218 0.090 - 1.292 0.110 - 1,387 0.140 -0,738

0.400 -1.191 0.130 -1.311 0.130 -1,395 0.190 -2.267**

0.490 - 1.184 0.150 - 1.553 0.150 -0,577 0.250 -0,469

0.590 - 1.259 0.200 - 1.308 0,210 - 1.436 0.400 -1.337

0.630 -0.507 0.250 -0.610 0,250 -0.449 0,490 - 1.308

0,700 - 1.379 0.260 -0.609 0.340 - 1.359 0,580 - 1.316

0.750 - 1.666 0,280 - 1,533 0.370 -0.665 0.650 - 1.416

0.810 - 1,627 0.299 - 1.303 0.400 -0.511 0.700 -0.599

0.840 - 1.705 0,310 -0.499 0.410 -3.197"* 0.750 -0,798

0.900 - 1.214 0.320 - 1.302 0.430 - 1.337 0.800 -2,037

0.960 - 1.175 0.340 -0.368 0.440 -0.537 0.830 - 1.549

0.350 - I. 143"* 0,460 -0.638 0.900 - 1.358

0.370 -0.364 0.490 - 1.262 0.960 - 1,363

0.380 -0.508 0.500 -1.335

0.400 - 1.483 0.520 -0.643

0.410 - 1.296 0.540 - 1.557

0.430 - 1,265 0.550 - 1,323

0.440 - 1.262 0.580 - 1.549

0.460 - 1.513 0.600 -0.559

0470 -1.302 0,610 -1.354

0.490 -0.380 0.650 - 1.794

0.500 - 1.311 0.700 - 1.590

0,520 - 1.313 0.750 -0,743

0.530 -0.607 0.820 - 1.563

0,550 - 1,306 0.890 - 1.273

0.560 - 1.353 0,900 - 1.307

0.580 -1,309 0.960 -1.253

0.590 -1.372

0.600 -1.350

0.640 - 1.564

0,700 -0.517

0.750 -0.279**

0.820 -1.522

0.870 -0.504

0.930 - 1+241

0.960 -0.438

Lower Surface

0.020 - 1.278 0.020 - 1.372 0,020 -0.983 0.020 -0.651

0.1 I0 - 1.378 0.060 -0.197 0.060 -0.901 0.060 -0,957

0.230 -0.989 0.090 -0.146 0.090 -0.071 0.110 -0.956

0.400 -0.957 0.120 - 1.065 0.120 - 1.165 0.250 -0.246

0.490 -0,918 0.200 -0,100 0.200 - 1.059 0.400 -0.226

0.630 0.781 ** 0.260 -0.150 0.250 -1.102 0.490 -1,082

0.750 -0,772 0.400 - 1,214 0,400 -0.096 0.580 -0.111

0,850 0.062 0,490 -0,072 0.490 -0,192 0,650 -0,850

0.900 -0.634 0.580 -0,907 0,580 -0.144 0,750 -0.855

0.960 -0.795 0,640 O. 115 0.650 - 1.216 0.830 -0.522

0,750 0.180 0.750 0.103 0.900 0.332

0.870 -0.564 0.890 0,318 0.960 O. 173

0.930 O. 176 0.930 -0.569

0.960 -0.060 0.960 O. 125

CN = 0.272 0.676 0.630 0.665

263
Table E-2. Continued.

Flight 214, Wing sweep = 26 °, Time = 9-0-57-000, MINF = 0.791, Camber = 0/11, ALPT = 5.26, BETA = -0.44, QINF = 292.9,

RNPU = 2.4E+06, CNWP = 0.0833

rl = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x./c CP

0.020 -0.694 0.000 0.537 0.000 0.093"* 0.010 - 1.420

0.060 -0.614 0.020 - 1.168 0.020 -1.265 0.020 - 1.430

0.110 -0.594 0.040 - 1.006 0.060 -0.651 ** 0.060 - 1.362

0.200 -1.473 0.060 -1.091 0.090 -1,231 0.110 -1.261

0.230 -0.601 0.090 -0.716 0.110 - 1.178 0.140 - 1.248

0.400 -0.386 0.130 -0.727 0.130 -0.753 0.190 -2.281 **

0.490 -0.530 0.150 - 1.199 0.150 -0.650 0.250 -0.684

0.590 -0.599 0.200 - 1.186 0.210 -0.746 0.400 -0.465

0.630 -0.634 0,250 - 1.616 0.250 - 1.202 0.490 -0.504

0.700 -0.700 0.260 -0.686 0,340 -0.490 0.580 -0.657

0.750 -0.947 0.280 -0,692 0.370 -0.569 0.650 -0.543

0.810 -0.983 0.290 - 1.138 0.400 -0.671 0.700 -0.733

0.840 - 1.078 0.310 -0.659 0.410 -3.220* * 0.750 -0.828

0.900 -0.543 0.320 -0.674 0.430 - 1.172 0.800 - 1.207

0.960 -0.990 0.340 -0.501 0.440 - 1.616 0.830 -0.870

0.350 -0.440"* 0,460 -0.525 0.900 -0.649

0.370 - 1.102 0.490 -0.648 0.960 -0.61 I

0.380 -0.671 0.500 - 1.147

0.400 -0.617 0.520 -0.694

0.410 -I.112 0.540 -0.525

0.430 -0.621 0.550 - 1.587

0.440 -0.609 0.580 -0.645

0,460 -0.404 0.600 -0.69 I

0.470 -0.637 0.610 - I. 169

0.490 - 1.102 0.650 - 1.142

0,500 -0.648 0.700 -0.920

0.520 -0.405 0.750 - 1.358

0.530 -0.643 0.820 -0.823

0,550 -0,690 0.890 -0.544

0.560 -0.682 0.900 -0,606

0.580 -0.646 0.960 -0.537

0.590 -0.700

0.600 -0.660

0,640 -1.373

0.700 -0.773

0.750 -0.279**

0.820 - 1.305

0.870 -0.670

0.930 -0.560

0.960 -0,548

Lower Surface

0.020 -0.388 0,020 -0.910 0,020 -0.578 0,020 0.173

0.110 -0.387 0.060 -0.650 0.060 0.013 0,060 -0.031

0.230 -0.261 0.090 -0.235 0.090 -0.203 0.110 -0.200

0,400 -0.255 0.120 -0.753 0.120 -0,403 0.250 -0.877

0.490 -0.209 0,200 -0.742 0.200 -0.270 0.400 -0.372

0.630 0.794** 0.260 -0.789 0.250 -0.806 0.490 -0.358

0.750 -0.556 0,400 -0.731 0.400 -0.155 0.580 -0.779

0.850 -0.527 0.490 -0.250 0.490 -0,756 0.650 -0.143

0.900 0.035 0.580 -0.208 0.580 -0.704 0.750 0,083

0.960 0.019 0.640 0.006 0.650 -1.221 0.830 0.328

0.750 0.067 0.750 -0.586 0.900 0.230

0.870 0.133 0.890 -0.718 0,960 0.060

0.930 0.068 0.930 0.197

0.960 -0.530 0.960 0.100

CN = 0.381 0.523 0.330 0.505

264
Table E-2. Continued,

Flight 214, Wing sweep = 26 °, Time = 9-1-13-500, MINF = 0.800, Camber = 0/11, ALPT = 7.09, BETA = -0.24, QINF = 290.0,

RNPU = 2.4E+06, CNWP = 0,7447

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -2.203 0.000 -0.498 0,000 -0.897"* 0.010 -2.464

0.060 -2.255 0.020 -2.361 0.020 -2.335 0.020 -2.506

0.110 - 1.185 0.040 - 1.996 0.060 - 1.694" * 0.060 -2.481

0.200 - 1.456 0.060 -2.274 0.090 -2.370 0.110 - 1.446

0.230 -0.556 0.090 -2.277 O. 110 -2.363 0.140 -2.386

0.400 - 1.458 0.130 -2.277 0.130 -2.319 0.190 -2.233"*

0.490 -1.445 0.150 - 1.312 0.150 -2.246 0.250 -2.382

0.590 -0.582 0.200 - 1.251 0.210 -2.260 0.400 - 1.644

0,630 - 1.572 0.250 -2.204 0.250 -2.287 0.490 -0.602

0.700 - 1.611 0.260 -2.200 0.340 -2.305 0.580 - 1.548

0.750 -2.093 0.280 -2.225 0.370 - 1.783 0.650 - 1.419

0.810 -2.031 0.290 - 1.277 0.400 - 1.599 0.700 - 1.641

0.840 -2.079 0.310 -2.174 0.410 -3.181 ** 0.750 - 1.768

0.900 - 1.577 0.320 -2.145 0.430 - 1.536 0.800 - 1.957

0.960 - 1.561 0.340 - 1.647 0.440 - 1.486 0.830 - 1.869

0.350 -1.339"* 0.460 - 1.455 0.900 - 1,481

0.370 - 1.455 0.490 - 1.421 0.960 - 1.380

0.380 - 1.441 0.500 - 1.451

0,400 - 1.366 0.520 - 1.482

0.410 - 1.379 0.540 -0.346

0.430 -1.375 0.550 -1.481

0.440 - 1.361 0.580 - 1.501

0.460 - 1.404 0.600 - 1.528

0.470 -1.424 0.610 -0.533

0.490 - 1.438 0.650 - 1.961

0.500 - 1.460 0.700 - 1.744

0.520 - 1.456 0.750 - 1.706

0.530 -0.535 0.820 -1.885

0.550 - 1.527 0.890 - 1.409

0.560 - 1.531 0.900 - 1,444

0.580 -1.499 0.960 - 1.385

0.590 - 1.570

0,600 - 1.565

0.640 -1.718

0.700 -1.675

0.750 -0.218"*

0.820 -1.760

0,870 -1.594

0.930 - 1.434

0.960 - 1.448

Lower Surface

0.020 - 1.053 0.020 - 1.310 0.020 -0.821 0.020 -0.532

0.110 -0.265 0.060 -0.935 0.060 0.052 0.060 -0.898

0.230 -1.115 0.090 -1.006 0.090 -0.029 0.110 -0.944

0.400 - 1.133 0.120 - 1.085 0.120 -0.150 0.250 - 1.210

0.490 - 1.094 0.200 - 1.092 0.200 - 1.085 0.400 - 1,191

0,630 0.873** 0.260 - 1.136 0.250 -0.009 0.490 - I. 191

0.750 -0,058 0.400 - 1.122 0.400 - 1.137 0.580 - 1.160

0.850 -0.979 0.490 -0.174 0.490 - 1.170 0.650 0.135

0.900 -0.885 0.580 -0.140 0.580 - 1.095 0.750 O. 154

0.960 - 1.071 0.640 -0.869 0.650 -1.177 0.830 0,446

0.750 -0.813 0.750 0,372 0.900 0.500

0.870 -0.752 0.890 -0.662 0.960 0.335

0.930 -0.829 0.930 -0.757

0.960 -0.953 0.960 -0.787

CN = 0.680 0.837 1,133 1.152

265
Table E-2. Continued.

Flight 214, Wing sweep = 26 °, Time = 9-4-1-000. MINF = 0.808, Camber = 0/10, ALPT = 6.05, BETA = -0.07, QINF = 297.8,

RNPU = 2.4E+06. CNWP = 0.4134

"q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.880 0.000 0.760 0.000 0,288"* 0.010 - 1.175

0.060 -0.887 0.020 - 1.027 0,020 - 1.050 0,020 - 1.237

0.110 -0.681 0.040 -0.820 0.060 -0.342"* 0.060 - 1.184

0.200 -0.288 0,060 -0.976 0.090 - 1.074 0.110 - 1.099

0.230 -0.336 0.090 -0,968 0.110 - 1.065 0.140 - 1.096

0.400 -0.289 0.130 -0.981 0.130 -1.023 0,190 -2.190"*

0.490 -0.269 0.150 -0.964 0.150 -0.963 0,250 - 1.107

0.590 -0.352 0.200 -0,852 0.210 -0,969 0,400 -0.390

0,630 -0.388 0.250 -0.913 0.250 - 1.005 0.490 -0.366

0.700 -0.429 0,260 -0,866 0.340 -0.397 0,580 -0.393

0,750 -0.880 0.280 -0.433 0,370 -0.323 0.650 -0.486

0.810 -0.865 0.290 -0,279 0.400 -0.266 0,700 -0.471

0,840 -0.942 0,310 -0.238 0,410 -3.113"* 0,750 -0.591

0.900 -0,328 0.320 -0.256 0.430 -0,330 0,800 -0.968

0.960 -0.322 0.340 -0,237 0.440 -0,307 0.830 -0,654

0,350 -0.110"* 0,460 -0.334 0.900 -0.418

0.370 -0,264 0.490 -0.310 0.960 -0,347

0,380 -0.312 0.500 -0,360

0.400 -0.255 0,520 -0.357

0.410 -0,325 0.540 -0,386

0.430 -0.301 0.550 -0.362

0,440 -0.284 0.580 -0.360

0.460 -0.353 0.600 -0.414

0.470 -0.339 0.610 -0.405

0.490 -0.341 0.650 -0,844

0,500 -0.352 0.700 -0,638

0.520 -0.353 0.750 -0.627

0,530 -0.369 0.820 -0.636

0.550 -0,404 0.890 -0.285

0.560 -0.410 0.900 -0,343

0.580 -0.367 0.960 -0,278

0.590 -0.428

0.600 -0.384

0.640 -0.626

0.700 -0.574

0.750 0.000"*

0.820 -0.604

0.870 -0,400

0.930 -0,280

0,960 -0.291

Lower Surface

0.020 0.012 0.020 0.214 0.020 0.227 0.020 0.516

0.110 -0.086 0.060 0.178 0,060 0.204 0.060 0.019

0.230 0.022 0.090 0,068 0.090 0.126 0.110 0.159

0.400 0,002 0.120 0.005 0.120 -0,096 0.250 -0,120

0.490 0,047 0,200 0,027 0,200 0,023 0.400 -0.091

0.630 0.835** 0.260 -0,045 0.250 -0.047 0,490 -0,092

0.750 0.169 0.400 -0,005 0.400 -0.017 0,580 -0.052

0,850 0.183 0.490 0.010 0,490 -0,048 0.650 0.141

0,900 0.293 0.580 0,062 0,580 0,042 0,750 0.351

0.960 0. l 10 0.640 0.277 0,650 -0,041 0.830 0,442

0,750 0.344 0.750 0,376 0,900 0.518

0,870 0.384 0.890 0,482 0,960 0.35 I

0,930 0,309 0,930 0,368

0,960 0.185 0.960 0,409

CN = 0.523 0.675 0.696 0,775

266
Table E-2. Continued.

Flight 214, Wing sweep = 26 °, Time = 9-4-8-500, MINF = 0.819, Camber = 0/11, ALPT = 7A8, BETA = -0.21, QINF = 305.6,

RNPU = 2.5E*06, CNWP = 0.5709

= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0_971 0.000 0.695 0.000 0.319" * 0.010 - 1.271

0.060 - 1,059 0.020 - 1,141 0,020 - 1.097 0,020 - 1.298

0.110 -0.991 0.040 -0.416 0.060 -0.429"* 0,060 - 1.247

0,200 -0.713 0.060 -1.062 0.090 -1.169 0.110 -1,176

0.230 -0.664 0.090 - 1.072 0.110 - 1.148 0.140 ° 1.180

0.400 -0.267 0.130 -1.074 0.130 -l.114 0.190 -2.131"*

0.490 -0.251 0,150 - 1.052 0.150 - 1.059 0,250 - 1.180

0.590 -0,351 0.200 -0.997 0.210 - 1.054 0.400 -0.875

0.630 -0.403 0.250 - 1.010 0,250 - 1,093 0.490 -0,577

0.700 -0.415 0.260 - 1.014 0.340 - 1,137 0.580 -0.424

0.750 - 1,060 0.280 - 1.025 0.370 - 1.104 0.650 -0.461

0.810 - 1.008 0.290 - 1,024 0.400 - 1.030 0.700 -0.449

0.840 -1.052 0,310 -0,995 0.410 -3.030** 0.750 -0.583

0,900 -0.477 0.320 -0.995 0.430 - 1.086 0.800 -0.770

0.960 -0.470 0.340 - 1.024 0.440 - 1.074 0.830 -0.595

0.350 -0.430** 0,460 -1.044 0.900 -0,326

0.370 - 1.001 0.490 -0.616 0.960 -0.277

0.380 - 1,068 0.500 -0.517

0,400 -0.966 0.520 -0.44 1

0.410 -1.011 0.540 -0.385

0.430 -0.914 0.550 -0.333

0.440 -0.586 0.580 -0.306

0.460 -0.406 0.600 -0.311

0.470 -0,348 0.610 -0.273

0.490 -0.292 0.650 -0.653

0.500 -0.257 0.700 -0.409

0.520 -0.218 0.750 -0.463

0.530 -0.212 0.820 -0.893

0.550 -0.244 0.890 -0.238

0.560 -0.224 0.900 -0.269

0.580 -0.238 0.960 -0.195

0.590 -0.288

0.600 -0.293

0.640 -0.426

0.700 -0.456

0.750 -0.014"*

0,820 -0.582

0.870 -0.515

0,930 -0.327

0.960 -0.301

Lower Surface

0.020 0.062 0.020 0.280 0.020 0.344 0,020 0.585

0.110 -0.068 0.060 0.200 0.060 0.265 0.060 0,033

0.230 0.018 0.090 0.129 0.090 0,174 0.110 0.204

0.400 0.019 0.120 0.051 0.120 -0.048 0,250 -0.061

0.490 0.049 0.200 0.052 0.200 0.051 0.400 -0.057

0.630 0.817 ** 0.260 -0.012 0.250 0.000 0.490 -0,054

0.750 0,139 0.400 0.019 0.400 0.002 0,580 -0.020

0.850 0.180 0.490 0.031 0.490 -0.002 0.650 0.138

0,900 0.256 0.580 0.057 0.580 0,048 0.750 0,378

0.960 0.081 0,640 0.267 0.650 -0,022 0.830 0.457

0.750 0.346 0.750 0.391 0.900 0.534

0,870 0.401 0.890 0.488 0.960 0.364

0.930 0.319 0,930 0.405

0.960 0.211 0.960 0.368

CN = 0.640 0.803 0.862 0.885

267
Table E-2. Continued.

Flight 214, Wing sweep = 26 °, Time = 9-4-16-500, MINF = 0,813, Camber = 0/10, ALPT = 7.96, BETA = 0.02. QINF = 301.2,

RNPU = 2.4E+06, CNWP = 0.6279

11 = 0.93 0,76 0.59 0.40

Upper Surface

x,/c CP x/c CP x,/c CP x/c CP

0,020 - 1.097 0.000 0.637 0.000 0,228 ** 0.010 - 1,337

0.060 - 1.148 0.020 - 1.197 0.020 - 1.218 0.020 - 1.356

0.110 - 1.072 0,040 -0.015 0.060 -0,413"* 0,060 - 1.353

0.200 -0,834 0,060 - 1.180 0.090 - 1.239 0.110 - 1.307

0,230 -0,729 0.090 - 1.145 0.110 - 1,240 0.140 - 1.296

0.400 -0.360 0.130 -1,144 0.130 -1,195 0,190 -2,160"*

0,490 -0,255 0.150 -1.135 0.150 -1.155 0.250 -1.302

0.590 -0.339 0.200 - 1.076 0.210 - 1.123 0.400 -0,934

0.630 -0.399 0.250 - 1.109 0.250 - 1.176 0,490 -0.767

0.700 -0,432 0,260 - 1.086 0,340 - 1.221 0,580 -0.633

0.750 - 1.061 0,280 - 1.113 0.370 - 1.200 0.650 -0.531

0.810 -0.993 0.290 -1.113 0,400 -1.163 0,700 -0.515

0,840 - 1.066 0.310 - 1.069 0.410 -3.073"* 0,750 -0.609

0.900 -0.480 0.320 - 1.105 0.430 - 1.183 0.800 -0,488

0.960 -0.511 0.340 - 1.097 0.440 - 1.154 0.830 -0.373

0,350 -0.438"* 0,460 - 1.146 0,900 -0.197

0.370 - 1.077 0,490 - 1.098 0,960 -0.171

0,380 -1.142 0.500 -1.170

0.400 - 1.078 0.520 - 1.163

0.410 -1.104 0.540 -0.923

0.430 - 1.069 0.550 -0.732

0.440 - 1.018 0,580 -0.556

0.460 - 1.102 0.600 -0.530

0.470 -1.103 0.610 -0.435

0.490 - 1.061 0650 -0.596

0.500 -0.723 0,700 -0,375

0.520 -0.555 0,750 -0,447

0.530 -0.413 0.820 -0.532

0,550 -0,409 0,890 -0.148

0,560 -0,329 0.900 -0.168

0,580 -0.297 0,960 -0.102

0.590 -0,296

0,600 -0,260

0,640 -0,320

0.700 -0.400

0.750 0,023**

0.820 -0.748

0,870 -0.438

0,930 -0.258

0,960 -0,257

Lower Surface

0.020 0.173 0.020 0,380 0.020 0.397 0.020 0.656

0.110 -0.013 0.060 0.256 0,060 0.318 0.060 0.042

0.230 0,037 0.090 0.176 0.090 0,225 0.110 0,257

0,400 0.024 0.120 0.114 0,120 0,001 0.250 -0.020

0,490 0.051 0.200 0.086 0.200 0.088 0.400 -0,006

0,630 0.830** 0.260 0.025 0,250 0.052 0.490 -0.013

0.750 0.155 0.400 0.064 0,400 0,048 0.580 0.005

0.850 0.172 0,490 0.072 0.490 0,006 0.650 0.183

0.900 0.257 0,580 0,095 0,580 0,089 0.750 0,392

0.960 0.057 0.640 0.290 0,650 -0.007 0,830 0.485

0.750 0.351 0.750 0.398 0.900 0.539

0.870 0,404 0.890 0,496 0,960 0.359

0.930 0,349 0.930 0.419

0.960 0.220 0.960 0.430

CN = 0.691 0.915 0.948 0,964

268
Table E-2. Continued.

Flight 216. Wing sweep = 26 °, Time = 10-58-39-500, MINF = 0,806, Camber = 10/19, ALPT = 3,04, BETA = -0.56, QINF = 305.3,

RNPU = 2.5E+06, CNWP = 0.4224

= 093 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP xJc CP x/c CP

0.020 0,548 0.000 0.027 0.000 -0.002* * 0,010 0.419

0.060 0.097 0.020 0.378 0.020 0.573 0.020 0.272

0.110 -0.193 0.040 0.415 0.060 0.593** 0.060 -0.253

0.200 -0.295 0.060 -0.049 0.090 -0.274 0.110 -0.649

0.230 -0.343 0.090 -0.265 0.110 -0.568 0.140 -1.102

0.400 -0.242 0.130 -0.542 0.130 -2.199"* 0.190 -2,199"*

0.490 -0.235 0.150 -0.858 0.150 - 1.023 0.250 -0.343

0.590 -0.338 0.200 -0.902 0.210 -0.937 0.400 -0.368

0.630 -0.356 0.250 -0.394 0.250 -0.327 0.490 -0.359

0.700 -0.424 0.260 -0.332 0.340 -0.374 0.580 -0.388

0.750 -0.473 0.280 -0.378 0.370 -0.401 0.650 -0.465

0.810 -0.437 0.290 -0.378 0.400 -0.369 0.700 -0.451

O.840 -0.436 O.310 -0,364 0.410 -2.236 ** 0.750 -0.567

0.900 -0.414 0.320 -0.360 0.430 -0.383 0,800 -0.700

0.960 -0.441 0.340 -0.347 0,440 -0.366 0.830 -0.547

0.350 -0.242** 0.460 -0.381 0.900 -0.547

0.370 -0.331 0.490 -0.310 0.960 -0.568

0.380 -0.382 0.500 -0.403

0.400 -0.297 0.520 -0.364

0.410 -0.382 0.540 -0.371

0.430 -0.343 0.550 -0.366

0.440 -0.287 0.580 -0.384

0.460 -0.385 0.600 -0.375

0.470 -0.353 0.610 -0.398

0.490 -0.356 0.650 -0.954

0.500 -0.359 0.700 -0648

0.520 -0.337 0.750 -0.689

0.530 -0365 0.820 -0.583

0.550 -0.409 0.890 -0.522

0,560 -0.383 0.900 -0.568

0.580 -0.367 0,960 -0.511

0.590 -0.415

0.600 -0.429

0.640 -0.639

0700 -0.601

0.750 -0.019"*

0.820 -0473

0.870 -0.395

0,930 -0.409

0.960 -0.411

Lower Surface

0.020 -0.980 0.020 -0.849 0,020 -0.759 0.020 - 1.068

0.110 -0.275 0.060 -0.402 0.060 -0.509 0.060 0.000

0.230 -0.057 0.090 -0.306 0.090 -0.323 0.110 -0.277

0.400 0.095 0.120 -0.165 0.120 -0.462 0.250 -0,150

0.490 0.147 0.200 -0.057 0,200 -0.112 0.400 -0.091

0.630 1.629"* 0.260 -0.056 0.250 -0,001 0.490 -0.055

0.750 0,236 0.400 0.078 0.400 0.045 0.580 0,073

0.850 0.264 0.490 0.116 0.490 -0.0 l 3 0.650 0,301

0.900 0,321 0.580 0.207 0.580 0.204 0.750 0.462

0.960 0.124 0_640 0.347 0.650 -0.041 0.830 0.529

0.750 0.365 0.750 -0.006 0.900 0.597

0,870 0.398 0.890 0.497 0,960 0.469

0.930 0.375 0.930 0.430

0.960 0.269 0.960 0.583

CN = 0.377 0.537 0.529 0.577

269
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-58-52-500, MINF = 0.811, Camber = 10/19, ALPT = 8.22, BETA = -0.41, QINF = 310.9,

RNPU = 2.5E+06, CNWP = 0.7670

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.241 0.000 0.666 0.000 0.277** 0.010 -0.176

0.060 -0.219 0.020 -0.047 0.020 0.089 0.020 -0.239

0.110 -0.555 0.040 0.040 0.060 0.150"* 0.060 -0.837

0.200 - 1.177 0.060 -0.455 0.090 -0.695 0.110 - 1.148

0.230 -1.135 0.090 -0.586 0.110 -0.892 0.140 -1.438

0.400 -0.883 0.130 -0.827 0.130 -2.174"* 0.190 -2.174"*

0A90 -0.675 0.150 - 1.099 0.150 - 1.281 0.250 - 1.425

0.590 -0.393 0.200 -1.185 0.210 - 1.240 0.400 -0.909

0.630 -0.400 0.250 - 1.272 0.250 - 1.234 0.490 -0.686

0.700 -0.435 0.260 - 1.179 0.340 - 1.261 0.580 -0.667

0.750 -0.857 0.280 - 1.238 0.370 - 1.260 0.650 -0.683

0.810 -0.752 0.290 - 1.230 0.400 - 1.210 0.700 -0.696

0.840 -0.768 0.310 -1.176 0.410 -2.211"* 0.750 -0.769

0.900 -0.749 0.320 - 1.181 0.430 - 1.246 0.800 -0.597

0.960 -0.752 0.340 - 1.187 0.440 - 1.217 0.830 -0.498

0.350 -0.504** 0.460 - 1.236 0.900 -0.419

0.370 - 1.147 0.490 - 1,164 0.960 -0.462

0.380 - 1.244 0.500 - 1.257

0.400 -0.309 0.520 -1.227

0.410 - 1.202 0.540 - 1.225

0,430 - 1.150 0.550 - 1.202

0.440 - 1.093 0.580 - 1.198

0.460 - 1.228 0.600 - 1.089

0.470 -1.164 0.610 -0.918

0.490 - 1.124 0.650 - 1.094

0.500 -1.163 0.700 -0.771

0.520 -1.142 0.750 -0.748

0.530 - 1.124 0.820 -0.350

0.550 - 1.160 0.890 -0.340

0.560 - 1.1 44 0.900 -0.353

0.580 - 1.114 0.960 -0.313

0.590 -1.159

0.600 -1.151

0.640 -0.599

0.700 -0.470

0.750 0.073**

0.820 -0.270

0.870 -0.292

0.930 -0.302

0.960 -0.300

Lower Surface

0.020 -0.248 0.020 -0.007 0.020 -0.013 0.020 0.195

0.110 0.055 0.060 0.231 0.060 0.287 0.060 0.057

0.230 0.084 0.090 0.178 0.090 0.239 0.1 I0 0.214

0.400 0.147 0.120 0.229 0.120 -0.034 0.250 0.096

0.490 0.187 0.200 0.082 0.200 0.024 0.400 0.094

0.630 1.585"* 0.260 0.172 0.250 0.201 0.490 0.097

0.750 0.311 0.400 0.202 0.400 0.178 0.580 0.187

0.850 0.334 0.490 0.208 0.490 0.079 0.650 0.374

0.900 0.398 0.580 0.279 0.580 0.274 0.750 0.557

0.960 0.151 0.640 0.486 0.650 0.054 0.830 0.633

0.750 0.514 0.750 0.008 0.900 0.689

0.870 0.554 0.890 0.629 0.960 0.497

0.930 0.492 0.930 0.572

0.960 0.367 0.960 0.668

CN = 0.875 1.043 1.073 1.097

270
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-58-55-500, MINF = 0.797, Camber = 10/18, ALPT = 12.26, BETA = 0.77, QINF = 303.6,

RNPU = 2.5E+06, CNWP = 0.4877

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.240 0.000 0.837 0.000 0.223"* 0.010 -0.937

0.060 -0.569 0.020 -0.677 0.020 -0.539 0.020 - 1.019

O.110 -0.914 0.040 -0.372 0.060 -0.046"* 0.060 - 1.180

0.200 - 1.393 0.060 -0,840 0.090 - 1.105 O. 110 - 1.459

0.230 - 1.283 0.090 - 1,044 0,1 l0 - 1.302 0.140 - 1.712

0.400 -0.830 0,130 - 1,214 0,130 -2,248"* 0.190 -2.248**

0.490 -0,504 0,150 - 1.425 0.150 -1.138 0.250 - 1.296

0.590 -0.494 0.200 -1.475 0.210 -1,033 0.400 -1,141

0.630 -0.497 0.250 - 1.383 0,250 -0.944 0.490 -0,974

0.700 -0.557 0.260 - 1.365 0.340 -0.935 0,580 -0,820

0.750 -0.705 0.280 - 1.252 0.370 -0,903 0,650 -0.763

0.810 -0.961 0.290 - 1.192 0.400 -0.860 0.700 -0.746

0.840 - 1.005 0.310 - 1.134 0.410 -2.286"* 0.750 -0,680

0.900 -0.492 0,320 - 1.132 0.430 -0.868 0.800 -0.762

0.960 -0.665 0.340 - 1.010 0.440 -0.811 0.830 -0,664

0.350 -0.435** 0.460 -0.826 0.900 -0.520

0.370 -0.993 0.490 -0.775 0.960 -0.514

0.380 - 1.082 0.500 -0.822

0.400 -0.352 0.520 -0,783

0.410 - 1.022 0.540 -0.764

0.430 -0.942 0.550 -0.751

0.440 -0.886 0.580 -0.735

0.460 -0.944 0.600 -0,728

0.470 -0.820 0.610 -0.680

0.499 -0,756 0.650 - 1.010

0,500 -0,758 0.700 -0.652

0.520 -0.771 0.750 -0.733

0.530 -0,693 0.820 -0.640

0.550 -0,633 0,890 -0.543

0.560 -0.577 0.900 -0.542

0.580 -0.547 0.960 -0.459

0590 -0.500

0.600 -0.502

0.640 -0.401

0.700 -0.427

0.750 0.072**

0.820 -0.306

0.870 -0.356

0.930 -0.444

0.960 -0.464

Lower Surface

0.020 0.093 0.020 0,446 0,020 0,44 1 0.020 0.596

0.110 0.182 0.060 0.455 0.060 0.511 0,060 0_066

0.230 0.146 0.090 0.369 0.090 0.445 0,110 0,406

0.400 0.187 0.120 0.344 0.120 0.117 0.250 0.252

0.490 0.199 0.200 0.145 0.200 0.083 0.400 0.216

0.630 1,602** 0.260 0.277 0.250 0.329 0.490 0.191

0.750 0.299 0.400 0.267 0.400 0.268 0,580 0.238

0,850 0,320 0,490 0.254 0.490 0.099 0.650 0.398

0.900 0.394 0.580 0.301 0,580 0.310 0.750 0.578

0,960 0.150 0.640 0.486 0,650 0.038 0.830 0,648

0.750 0.510 0.750 -0.013 0.900 0.708

0.870 0.553 0.890 0.645 0.960 0.494

0.930 0.479 0.930 0.557

0.960 0.333 0.960 0.637

CN = 0.967 1.092 1,033 1.318

271
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-0-1-500, MINF = 0.794, Camber = 10/15, ALPT = 3.04, BETA = -0.15, QINF = 295.3,

RNPU = 2AE+06, CNWP = 0.4146

"q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 0.527 0.000 0.079 0.000 0.106** 0.010 0.389

0.060 0.080 0.020 0.361 0.020 0,552 0.020 0,290

0.110 -0.273 0.040 0.389 0.060 0.368** 0.060 -0.317

0.200 -0.324 0.060 -0.090 0.090 -0.306 0.110 -0.698

0.230 -0.365 0.090 -0,306 0.110 -0.597 0.140 - 1.164

0.400 -0.264 0.130 -0.593 0.130 -2.265 * * 0.190 -2.265 * *

0.490 -0.238 0.150 -0.895 0.150 - 1.04 1 0.250 -0.403

0.590 -0.329 0.200 -0,953 0.210 -0.989 0.400 -0.401

0.630 -0.359 0.250 -0.399 0.250 -0.344 0.490 -0.372

0.700 -0.422 0.260 -0.334 0.340 -0.378 0.580 -0.393

0.750 -0.504 0.280 -0.397 0.370 -0.398 0.650 -0,472

0.810 -0.487 0.290 -0.391 0.400 -0.403 0.700 -0.468

0.840 -0,477 0.310 -0.371 0.410 -2.303"* 0.750 -0.582

0,900 -0,368 0.320 -0.383 0.430 -0.418 0.800 -0.681

0.960 -0.389 0.340 -0.372 0.440 -0.385 0.830 -0.520

0.350 -0.226** 0.460 -0.397 0.900 -0.511

0.370 -0.341 0.490 -0.358 0.960 -0.530

0.380 -0.392 0.500 -0.408

0.400 -0.320 0.520 -0.368

0.410 -0.408 0.540 -0.404

0.430 -0.352 0.550 -0.376

0.440 -0.291 0.580 -0,388

0.460 -0.417 0.600 -0.407

0.470 -0.383 0.610 -0.417

0.490 -0.382 0.650 -0.870

0.500 -0.379 0,700 -0.647

0.520 -0.379 0.750 -0.719

0.530 -0.368 0.820 -0.551

0.550 -0,415 0.890 -0,478

0.560 -0.403 0.900 -0.530

0.580 -0.378 0.960 -0.463

0.590 -0.420

0.600 -0.440

0.640 -0.664

0.700 -0,602

0.750 -0.037**

0.820 -0,358

0.870 -0.366

0.930 -0.380

0.960 -0.401

Lower Surface

0,020 -0.869 0.020 -0.936 0,020 -0.728 0.020 - 1.067

0.110 -0.316 0.060 -0.335 0.060 -0.440 0.060 0.008

0.230 -0.039 0,090 -0.260 0.090 -0.211 0.110 -0.252

0.400 0.103 0.120 -0.129 0.120 -0.374 0.250 -0.142

0.490 0.108 0.200 -0.061 0.200 -0.114 0.400 -0.063

0.630 1.692** 0.260 -0.024 0.250 0.019 0.490 -0.033

0.750 0.206 0.400 0.085 0.400 0.045 0.580 0.069

0.850 0.238 0.490 0.110 0.490 -0.042 0.650 0.312

0.900 0.302 0.580 0.173 0.580 0.208 0.750 0.462

0.960 0.116 0.640 0.337 0,650 -0.075 0.830 0.532

0.750 0.335 0.750 0.006 0.900 0.604

0.870 0.341 0.890 0,497 0.960 0.466

0.930 0.270 0,930 0,438

0.960 0.163 0.960 0.530

CN = 0,372 0,528 0.542 0.605

272
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-1-53-000, MINF = 0.805, Camber = 10/13, ALPT = 2,99, BETA = -0.44, QINF = 304.4,

RNPU = 2.5E+06, CNWP = 0.3791

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.551 0.000 0,034 0.000 -0.028 ** 0.010 0.423

0.060 0.099 0.020 0.381 0,020 0.577 0.020 0.295

0.110 -0.260 0.040 0.418 0.060 0.528** 0.060 -0,252

0,200 -0.293 0.060 -0.032 0.090 -0.263 0.110 -0.664

0.230 -0.315 0.090 -0.264 0,110 -0.567 0,140 - 1,104

0.400 -0.240 0.130 -0.541 0.130 -2.204"* 0,190 -2.204"*

0.490 -0.233 0,150 -0,855 0.150 - 1.000 0,250 -0.369

0.590 -0.325 0.200 -0.903 0.210 -0,947 0.400 -0.367

0,630 -0_351 0.250 -0.393 0.250 -0.319 0.490 -0.372

0.700 -0.393 0.260 -0.317 0.340 -0.373 0,580 -0.377

0.750 -0.514 0.280 -0.368 0,370 -0.385 0.650 -0.454

0.810 -0.479 0,290 -0.368 0.400 -0,368 0.700 -0.435

0.840 -0.476 0.310 -0,360 0,410 -2.241 ** 0.750 -0,564

0,900 -0.337 0.320 -0.354 0.430 -0.397 0.800 -0,687

0.960 -0.349 0.340 -0.346 0.440 -0,355 0.830 -0.555

0.350 -0.246** 0.460 -0,380 0.900 -0.538

0.370 -0.326 0.490 -0.302 0.960 -0.560

0.380 -0.377 0.500 -0.393

0.400 -0.274 0.520 -0363

0.410 -0.378 0.540 -0.385

0.430 -0.342 0.550 -0.365

0.440 -0.267 0.580 -0.366

0.460 -0.399 0.600 -0.389

0.470 -0,346 0.610 -0.383

0490 -0,355 0.650 -0.926

0.500 -0.358 0700 -0.652

0.520 -0.366 0.750 -0.689

0.530 -0.360 0.820 -0,492

0.550 -0,409 0.890 -0.486

0.560 -0,376 0.900 -0.458

0.580 -0.360 0.960 -0.428

0.590 -0.414

0.600 -0.423

0.640 -0.629

0.700 -0.593

0.750 -0.074**

0.820 -0.324

0.870 -0.343

0.930 -0.383

0.960 -0.363

Lower Surface

0.020 - 1.006 0,020 -0.880 0.020 -0,759 0.020 - 1.057

0.110 -0. 300 0.060 -0.409 0,060 -0.495 0.060 0.002

0,230 -0,059 0.090 -0.299 0.090 -0.308 0.110 -0.256

0.400 0.072 0.120 -0.188 0.120 -0.445 0.250 -0,149

0,490 0.106 0.200 -0,059 0.200 -0.117 0.400 -0.082

0.630 1.636"* 0.260 -0.065 0.250 0,001 0.490 -0,038

0.750 0,159 0.400 0.058 0,400 0.038 0,580 0.085

0.850 0.187 0.490 0.100 0.490 -0.040 0.650 0,319

0.900 0.244 0.580 0.176 0.580 0.210 0.750 0.466

0,960 0.073 0.640 0.306 0.650 -0.081 0.830 0.533

0,750 0.270 0.750 -0.019 0.900 0.606

0.870 0.220 0.890 0,501 0.960 0.469

0.930 0.206 0.930 0441

0.960 O. 102 0.960 0.591

CN = 0.330 0.460 0.503 0.586

273
Table E-2. Continued.

Flight 216, Wing sweep = 26 °. Time = l 1-2-1-000, MINF = 0.808, Camber = 10/13, ALPT = 6.08, BETA = -0.38, QINF = 307.6,

RNPU = 2.5E+06, CNWP = 0.5571

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.375 0.000 0,419 0.000 0.303** 0.010 0.055

0.060 -0.098 0.020 0.124 0.020 0.307 0.020 -0,049

0.110 -0.469 0.040 0.148 0.060 0.234"* 0.060 -0.674

0.200 - 1.128 0.060 -0.295 0.090 -0.470 0.110 -0.982

0.230 - 1.035 0.090 -0.464 0.110 -0.749 0.140 - 1.320

0.400 -0.207 0.130 -0.722 0.130 -2.186 ** 0.190 -2.186"*

0.490 -0.218 0.150 -1.020 0.150 -1.170 0.250 -1.082

0.590 -0.324 0.200 - 1.102 0.210 - 1.167 0.400 -0.585

0.630 -0.372 0,250 - 1.169 0.250 - 1.132 0.490 -0.495

0.700 -0.406 0.260 - 1.078 0.340 - 1.123 0.580 -0.472

0.750 - 1.122 0.280 - 1.130 0.370 - 1.114 0.650 -0.534

0.810 -0.876 0.290 - 1.113 0.400 - 1.082 0,700 -0.523

0.840 -0.823 0,310 -1.055 0,410 -2.223"* 0.750 -0.647

0.900 -0.515 0.320 - 1.062 0.430 -0.881 0.800 -0,662

0.960 -0.529 0.340 - 1.059 0.440 -0.599 0.830 -0.526

0.350 -0.499"* 0.460 -0.520 0,900 -0.526

0.370 - 1.027 0.490 -0.377 0.960 -0.530

0.380 -1.116 0.500 -0.411

0.400 -0.301 0.520 -0.352

0.410 - 1.067 0.540 -0.342

0.430 -0.935 0.550 -0.338

0.440 -0.594 0.580 -0.338

0.460 -0.519 0.600 -0.335

0.470 -0.419 0.610 -0.356

0490 -0.312 0.650 -0,783

0.500 -0.298 0.700 -0.596

0.520 -0.271 0.750 -0.636

0.530 -0,239 0.820 -0.565

0.550 -0.283 0.890 -0.438

0.560 -0.276 0.900 -0.492

0.580 -0.261 0.960 -0.420

0.590 -0.299

0.600 -0.333

0.640 -0.464

0.700 -0.499

0.750 -0.028"*

0.820 -0.355

0.870 -0.341

0.930 -0.395

0.960 -0.371

Lower Surface

0.020 -0.896 0.020 -0.387 0.020 -0.242 0.020 -0.133

0.110 -0.041 0.060 0.022 0.060 0.131 0.060 0.026

0.230 0.017 0.090 0.046 0.090 0.110 0.110 0.027

0.400 0,088 0.120 0.093 0.120 -0.149 0.250 0.005

0.490 0.106 0.200 0.012 0.200 -0.059 0.400 0.025

0.630 1.6t4"* 0.260 0.086 0.250 0.107 0.490 0.037

0.750 0.181 0.400 0.125 0.400 0.109 0.580 0.137

0.850 0.209 0.490 0.138 0.490 0.002 0.650 0.339

0.900 0.286 0,580 0.205 0.580 0.232 0.750 0.522

0.960 0.072 0.640 0.396 0.650 -0.043 0.830 0.592

0.750 0.335 0.750 0.020 0.900 0.653

0.870 0.322 0.890 0.604 0,960 0.477

0.930 0.249 0.930 0.547

0.960 0.139 0.960 0.613

CN = 0.609 0,738 0.803 0.875

274
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-2-6-000, MINF = 0.803, Camber = 10/12, ALPT = 9.94, BETA = 0.02, QINF = 303.7,

RNPU = 2.5E+06, CNWP = 0,6162

r1 = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.001 0.000 0.808 0.000 0.390"* 0.010 -0.515

0.060 -0.424 0.020 -0.333 0.020 -0.204 0.020 -0.434

O. 110 -0.789 0.040 -0.208 0.060 -0.120"* 0.060 - 1.027

0.200 - 1.239 0.060 -0.654 0.090 -0.932 O. 110 - 1.345

0.230 -1.185 0.090 -0.851 0.110 -1.121 0.140 -1.583

0.400 -0,909 0.130 - 1,032 0.130 -2,216"* 0,190 -2,216"*

0,490 -0.331 0.150 -1,253 0,150 -1,424 0.250 -1,577

0,590 -0.366 0.200 - 1.330 0.210 - 1.416 0.400 - 1.194

0.630 -0.433 0,250 -1,408 0.250 -1.396 0.490 -0.948

0,700 -0.462 0.260 - 1,304 0.340 - 1,415 0.580 -0.636

0.750 -1.147 0.280 -I .376 0.370 -1.132 0.650 -0.474

0,810 - 1.143 0.290 -1.376 0,400 -0.901 0.700 -0.461

0,840 - 1.190 0, 310 - 1.329 0.410 -2.253"* 0.750 -0.521

0900 -0.689 0.320 - 1.328 0.430 -0.895 0,800 -0,623

0.960 -0.565 0,340 - 1.298 0.440 -0.834 0.830 -0,658

0350 -0,520** 0,460 -0.838 0.900 -0.416

0.370 -0.893 0.490 -0.750 0.960 -0.446

0.380 -0.905 0,500 -0,816

0.400 -0.299 0.520 -0.747

0.410 -0.824 0.540 -0.776

0.430 -0.771 0.550 -0.751

0.440 -0.722 0.580 -0.747

0,460 -0.792 0,600 -0,716

0.470 -0.736 0.610 -0.685

0.490 -0.714 0.650 -0,914

0.500 -0.702 0,700 -0.631

0,520 -0.722 0.750 -0.697

0.530 -0,684 0,820 -0.528

0.550 -0,699 0.890 -0.499

0.560 -0.668 0,900 -0,513

0.580 -0.651 0.960 -0.436

0.590 -0.657

0.600 -0,630

0.640 -0.514

0,700 -0.496

0.750 0,017"*

0.820 -0.381

0.870 -0.397

0.930 -0.391

0.960 -0.396

Lower Surface

0.020 -0.086 0.020 0.206 0.020 0.198 0.020 0.402

0.110 0.078 0.060 0.317 0.060 0.368 0.060 0.053

0,230 0.101 0.090 0.241 0.090 0.313 0.110 0.254

0,400 0.090 0.120 0.266 0.120 0.028 0.250 0.155

0.490 0,099 0,200 0.101 0.200 0.027 0.400 0.135

0,630 1.633"* 0.260 0,186 0.250 0.244 0,490 0,131

0.750 0,150 0.400 0,188 0.400 0.187 0.580 0.196

0.850 0.186 0.490 0.171 0.490 0.040 0.650 0,371

0.900 0,277 0.580 0.216 0,580 0,255 0.750 0.56 I

0.960 0.059 0.640 0.399 0,650 -0.016 0.830 0.619

0.750 0,335 0.750 0.018 0.900 0.677

0.870 0.299 0.890 0.625 0,960 0,475

0.930 0.244 0,930 0.523

0.960 0.1 I0 0.960 0,565

CN = 0.856 0,953 1,048 1.197

275
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-3-30-000, MINF = 0.796, Camber = 10/12, ALPT = 3.02, BETA = -0.21, QINF = 297.9,

RNPU = 2.5E+06, CNWP = 0.3846

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.535 0.000 0,034 0.000 -0,005"* 0.010 0.427

0,060 0,097 0.020 0,423 0.020 0.561 0.020 0,255

0.110 -0.293 0.040 0,393 0,060 0.535** 0.060 -0.283

0.200 -0.317 0.060 -0.069 0.090 -0.304 0.110 -0.668

0.230 -0.335 0,090 -0.291 0.110 -0.593 0.140 -1.150

0.400 -0,265 0.130 -0.577 0.130 -2.257"* 0.190 -2,257"*

0,490 -0.254 0.150 -0.890 0.150 - 1.034 0,250 -0.389

0.590 -0.337 0,200 -0.944 0.210 -0.982 0,400 -0.387

0.630 -0.367 0.250 -0.419 0.250 -0,352 0,490 -0.380

0.700 -0.414 0,260 -0.342 0.340 -0A01 0.580 -0.390

0.750 -0.546 0,280 -0.398 0.370 -0.398 0.650 -0.479

0.810 -0.544 0,290 -0.381 0,400 -0.351 0.700 -0.465

0.840 -0.547 0.310 -0.382 0.410 -2.294"* 0.750 -0.580

0.900 -0.311 0.320 -0,376 0,430 -0.410 0.800 -0.664

0,960 -0.326 0,340 -0,358 0,440 -0.372 0,830 -0,535

0,350 -0.246** 0.460 -0,393 0.900 -0.518

0,370 -0.345 0.490 -0,320 0.960 -0.536

0.380 -0.399 0.500 -0.406

0,400 -0,284 0.520 -0.376

0,410 -0.394 0.540 -0.383

0,430 -0,354 0,550 -0.390

0.440 -0.299 0.580 -0.3%

0,460 -0.397 0.600 -0,399

0.470 -0.364 0.610 -0.423

0.490 -0.371 0,650 -0.989

0.500 -0.381 0.700 -0.663

0,520 -0.379 0.750 -0.708

0,530 -0.376 0.820 -0,490

0.550 -0.422 0.890 -0.449

0.560 -0,395 0,900 -0.457

0,580 -0.379 0,960 -0.399

0,590 -0,428

0.600 -0,447

0,640 -0.654

0,700 -0.578

0,750 -0.084"*

0.820 -0.324

0,870 -0.355

0.930 -0,373

0.960 -0.346

Lower Surface

0,020 -0.963 0,020 -0.929 0.020 -0,749 0,020 - 1,091

0.110 -0.348 0.060 -0.399 0,060 -0.433 0,060 -0,003

0,230 -0.065 0,090 -0.292 0,090 -0.277 0.110 -0,307

0.400 0,050 0.120 -0.153 0.120 -0.416 0,250 -0.143

0.490 0,088 0.200 -0.057 0.200 -0.118 0,400 -0.081

0.630 t .667** 0,260 -0.042 0.250 -0.007 0.490 -0.044

0.750 0.143 0.400 0,055 0,400 0,024 0.580 0.072

0,850 0.179 0.490 0,083 0.490 -0.060 0.650 0,299

0.900 0,239 0.580 0.152 0.580 0.188 0,750 0,462

0.960 0.083 0.640 0.293 0.650 -0.102 0.830 0.523

0.750 0.251 0,750 -0,009 0.900 0.603

0.870 0.211 0.890 0.478 0,960 0,457

0,930 0.191 0,930 0,424

0,960 0,092 0,960 0,563

CN = 0.333 0.468 0.516 0.589

276
Table E-2, Continued.

Flight 216, Wing sweep = 26 °, Time = 11-3-39-500, MINF = 0.804, Camber = 10/13, ALPT = 8.04, BETA = -0.33, QINF = 304.8,

RNPU = 2.5E+06, CNWP = 0_7229

11 = 0.93 0,76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x./c CP

0,020 0.215 0.000 0.663 0.000 0.199"* 0.010 -0.208

0.060 -0.268 0,020 -0.055 0.020 0.075 0.020 -0,272

0.110 -0.529 0.040 0.019 0,060 0.215"* 0.060 -0.821

0.200 - 1.214 0.060 -0.471 0.090 -0.727 0.110 - 1.179

0.230 - 1.148 0.090 -0.622 0, 110 -0.917 0.140 -1.483

0.400 -0,894 0.130 -0.858 0,130 -2,211 ** 0.190 -2.211 **

0.490 -0,495 0,150 - 1.132 0.150 - 1.281 0.250 - 1.454

0.590 -0.360 0.200 - 1.211 0.210 - 1.281 0.400 -0.908

0.630 -0,401 0.250 - 1.293 0.250 - 1.273 0.490 -0.698

0.700 -0.419 0.260 - 1,203 0.340 - 1.287 0.580 -0.657

0.750 - 1,192 0.280 - 1,271 0.370 - 1.285 0.650 -0.685

01810 - 1.149 0.290 - 1.262 0.400 - 1.257 0.700 -0.697

0.840 - 1.203 0.310 - 1.207 0.410 -2.248"* 0,750 -0.764

0.900 -0.653 0,320 - 1,217 0.430 - 1.293 0,800 -0.576

0.960 -0.684 0.340 - 1.222 0,440 - 1,239 0.830 -0.462

0,350 -0.527** 0.460 - 1.274 0,900 -0.418

0,370 -1.177 0.490 - 1,195 0,960 -0.431

0.380 -1.276 0,500 -1.280

0.400 -0.290 0.520 - 1.242

0.410 -1.233 0.540 -1.258

0.430 - 1,181 0.550 - 1.221

0.440 -1.122 0.580 -1.161

0.460 - 1,260 0.600 -0.953

0.470 - 1.202 0.610 -0398

0.490 - 1.170 0.650 -0.976

0.500 - 1.226 0.700 -0.625

0,520 - 1.173 0.750 -0.636

0,530 -1.155 0.820 -0.327

0.550 - 1.182 0.890 -0.315

0.560 - 1.174 0.900 -0.305

0.580 - 1.138 0.960 -0.254

0.590 -1.181

0.600 -1.172

0.640 -0467

0.700 -0.458

0.750 0.021"*

0.820 -0.309

0,870 -0.266

0.930 -0.276

0.960 -0.260

Lower Surface

0.020 -0.280 0.020 -0.011 0.020 -0,005 0,020 0.203

0.1 I0 0.035 0.060 0,224 0.060 0.285 0.060 0.050

0.230 0.071 0.090 0.163 0.090 0.231 0.110 0.150

OAO0 O. 120 O. 120 0.219 O. 120 -0.042 0,250 0.093

0.490 O. 1 I 0 0.200 0.069 0.200 0.011 0.400 0.088

0.630 1.624"* 0.260 0.147 0.250 0.190 0.490 0.098

0.750 O.181 0.400 O.169 0.400 O.173 0.580 O. 183

0.850 0.208 0.490 O. 171 0.490 0.044 0.650 0.367

0.900 0.281 0.580 0.228 0.580 0.251 0.750 0.542

0.960 0.048 0.640 0.420 0.650 0.002 0.830 0.613

0.750 0.355 0.750 0.001 0.900 0.675

0.870 0.331 0.890 0.634 0.960 0.488

0.930 0.297 0.930 0.562

0.960 O. [61 0.960 0.682

CN = 0.842 0.977 1.042 1.089

277
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-3-40-500. MINF = 0.802, Camber = 10/12, ALPT = 9,90, BETA = -0.30, QINF = 304,3,

RNPU = 2,5E+06, CNWP = 0.6857

rl = 0,93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.005 0,000 0.826 0.000 0.215"* 0.010 -0.619

0.060 -0.428 0.020 -0.332 0,020 -0.201 0.020 -0.435

0.110 -0.803 0.040 -0.203 0,060 0.114"* 0.060 - 1.020

0.200 - 1.246 0.060 -0.664 0.090 -0,936 0.110 - 1.323

0.230 -1.215 0.090 -0.839 0,110 -1,108 0.140 -1.592

0.400 -0.769 0.130 - 1,024 0.130 -2.222 * * 0.190 -2,222 **

0.490 -0.485 0.150 - 1.247 0,150 - 1.410 0.250 - 1.597

0.590 -0.350 0.200 -1.319 0.210 -1,422 0.400 -1.172

0.630 -0.432 0,250 - 1.073 0.250 - 1.388 0.490 -0.918

0.700 -0.441 0.260 - 1,037 0.340 - 1,430 0.580 -0.615

0.750 -0.930 0.280 - 1.036 0.370 - 1,234 0.650 -0.454

0.810 -0.811 0,290 -0.989 0,400 -0.851 0,700 -0.441

0.840 -0.879 0.310 -0.844 0,410 -2,259"* 0,750 -0.507

0.900 -0.568 0.320 -0,839 0.430 -0.889 0,800 -0,568

0.960 -0,509 0.340 - 1,034 0,440 -0.813 0,830 -0.574

0.350 -0,463"* 0,460 -0.817 0.900 -0.379

0,370 -0.753 0.490 -0.736 0,960 -0.424

0.380 -0.840 0.500 -0.799

0.400 -0.268 0.520 -0.772

0.410 -0.845 0.540 -0.770

0.430 -0.750 0.550 -0.730

0.440 -0,785 0.580 -0.735

0.460 -0.771 0.600 -0.719

0.470 -0.779 0.610 -0,686

0.490 -0.682 0,650 -0,959

0,500 -0.744 0.700 -0650

0.520 -0.694 0,750 -0,706

0.530 -0,688 0.820 -0.578

0.550 -0.678 0.890 -0.530

0.560 -0.642 0.900 -0.492

0.580 -0.631 0.960 -0.423

0,590 -0.650

0.600 -0.624

0,640 -0.494

0.700 -0.480

0.750 0.000"*

0.820 -0.342

0,870 -0,341

0.930 -0,393

0,960 -0408

Lower Surface

0020 -0,057 0.020 0.228 0.020 0.232 0.020 0.430

0,110 0,097 0.060 0,310 0,060 0,399 0.060 0.080

0,230 0.119 0.090 0.271 0.090 0.336 0.110 0,293

0.400 0.113 0.120 0.285 0,120 0,047 0.250 0.181

0,490 0,118 0,200 0.116 0,200 0,040 0,400 0.158

0,630 1,620"* 0.260 0.205 0.250 0.256 0,490 0.150

0.750 0.151 0,400 0,199 0,400 0.206 0,580 0.215

0.850 0.197 0,490 0.164 0,490 0.037 0.650 0.390

0.900 0.274 0.580 0.224 0,580 0,274 0.750 0,574

0.960 0.062 0.640 0.410 0.650 0,003 0.830 0,637

0.750 0.345 0,750 0,067 0,900 0.681

0.870 0,327 0,890 0,622 0.960 0.485

0.930 0.248 0.930 0,519

0.960 0.111 0.960 0,628

CN = 0.814 0.905 1.072 1.199

278
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-5-2-000, MINF = 0.804, Camber = 10/9, ALPT = 3.15, BETA = -0.12, QINF = 304.3,

RNPU = 2.5E+06, CNWP = 0.3412

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x./c CP x/c CP

0.020 0.521 0.000 0.040 0.000 -0.056"* 0.010 0.390

0.060 0.068 0.020 0.378 0.020 0.554 0.020 0,267

0.110 -0.279 0.040 0.399 0.060 0.567" * 0.060 -0,254

0.200 -0.341 0.060 -0.071 0.090 -0.305 0.110 -0.657

0,230 -0.328 0.090 -0.286 0.110 -0.590 0.140 - 1, l 12

0.400 -0.255 0.130 -0.577 0.130 -2.212 ** 0.190 -2.212"*

0.490 -0.252 0.150 -0.871 0.150 - 1.016 0.250 -0.392

0,590 -0.348 0.200 -0.934 0.210 -0.979 0.400 -0.390

0.630 -0.355 0,250 -0.389 0.250 -0.334 0.490 -0.366

0.700 -0.405 0.260 -0.333 0.340 -0.381 0,580 -0.410

0.750 - 1.001 0.280 -0.382 0.370 -0.407 0.650 -0.466

0.810 -0.960 0,290 -0.391 0.400 -0.398 0.700 -0.448

0.840 -0.972 0.310 -0.376 0.410 -2.249** 0.750 -0.571

0.900 -0,275 0.320 -0.373 0.430 -0,397 0.800 -0640

0.960 -0.239 0.340 -0.347 0.440 -0,362 0.830 -0.509

0.350 -0.258"* 0.460 -0.403 0.900 -0.510

0.370 -0.352 0.490 -0.309 0.960 -0,527

0,380 -0.385 0,500 -0.416

0.400 -0.340 0.520 -0.371

0.410 -0.401 0,540 -0.378

0.430 -0.359 0550 -0.388

0.440 -0.308 0.580 -0.405

0.460 -0.392 0.600 -0.397

0.470 -0.381 0.610 -0.413

0.490 -0.359 0.650 -0.947

0500 -0.380 0.700 -0.671

0.520 -0,389 0.750 -0.711

0.530 -0.376 0.820 -0.477

0.550 -0.416 0. 890 -0.430

0.560 -0.399 0.900 -0.418

0.580 -0,389 0.960 -0.367

0.590 -0.432

0.600 -0.456

0.640 -0.637

0300 -0.609

0.750 -0.114"*

0,820 -0.328

0.870 -0.333

0.930 -0.405

0.960 -0.425

Lower Surface

0.020 -0.986 0,020 -0,903 0.020 -0.782 0.020 - 1.059

0.110 -0,362 0,060 -0.405 0,060 -0.499 0.060 -0.006

0.230 -0.078 0.090 -0.310 0.090 -0.284 0.110 -0.279

0.400 0.027 0.120 -0.161 0.120 -0.425 0.250 -0.152

0.490 0.047 0.200 -0.077 0.200 -0.133 0.400 -0.082

0.630 1.628'* 0,260 -0,073 0,250 -0.018 0.490 -0.061

0.750 0.076 0.400 0.024 0.400 0.006 0,580 0,063

0,850 0.137 0.490 0.077 0.490 -0.077 0.650 0.285

0.900 0.195 0.580 0.131 0.580 0.188 0.750 0.458

0.960 0.076 0.640 0.257 0,650 -0.139 0.830 0.533

0.750 0.179 0.750 -0.012 0.900 0.611

0.870 0.158 0.890 0.468 0.960 0.447

0.930 0,151 0.930 0.411

0.960 0.069 0.960 0.553

CN = 0.357 0.445 0.491 0.578

279
Table E-2. Continued.

Flight 216, Wing sweep = 26", Time = 11-5-11-500, MINF = 0.803, Camber = 10/10, ALPT = 5.96, BETA = -0.56, QINF = 304.2,

RNPU = 2.5E+06, CNWP = 0.5427

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.381 0.000 0.393 0.000 0.114"* 0.010 0.070

0.060 -0.086 0.020 0.176 0.020 0.336 0.020 -0.036

0.110 -0.458 0.040 0.194 0.060 0.423"* 0.060 -0.688

0,200 - 1.147 0.060 -0.274 0.090 -0.491 0.110 -0.960

0.230 -1.053 0.090 -0.458 0.110 -0,764 0.140 -1.315

0.400 -0.223 0.130 -0.726 0.130 -2.217"* 0.190 -2.217"*

0.490 -0.237 0.150 - 1.025 0.150 - 1.165 0.250 -0.974

0.590 -0.346 0.200 - 1.109 0.210 - 1.168 0.400 -0.529

0.630 -0.383 0.250 - 1.1 64 0.250 - 1.136 0.490 -0.461

0.700 -0.413 0.260 - 1.083 0.340 - 1.112 0,580 -0.462

0.750 - 1.037 0.280 - 1.132 0.370 - 1.101 0.650 -0.526

0.810 -0.991 0.290 -1.106 0.400 -0.758 0.700 -0.515

0.840 - 1.034 0.310 - 1.051 0.410 -2.254"* 0.750 -0.639

0,900 -0.381 0.320 - 1.062 0.430 -0,498 0.800 -0.649

0.960 -0.359 0.340 - 1.054 0.440 -0.408 0.830 -0.529

0.350 -0.522** 0.460 -0.385 0.900 -0.511

0.370 - 1.016 0.490 -0.284 0.960 -0.527

0.380 - 1.094 0.500 -0.357

0.400 -0.353 0.520 -0.329

0.410 -0.573 0.540 -0.339

0.430 -0.404 0.550 -0.348

0.440 -0.328 0.580 -0.365

0,460 -0.343 0.600 -0.357

0.470 -0.270 0.610 -0.366

0.490 -0.259 0.650 -0,926

0.500 -0.265 0.700 -0.613

0.520 -0.265 0.750 -0.671

0.530 -0.269 0.820 -0.565

0.550 -0.328 0.890 -0.445

0.560 -0.304 0.900 -0.456

0.580 -0.309 0,960 -0.417

0.590 -0.357

0.600 -0.391

0.640 -0.537

0.700 -0.525

0.750 -0.067**

0.820 -0.347

0.870 -0.372

0,930 -0,453

0.960 -0,414

Lower Surface

0.020 -0.989 0.020 -0.425 0.020 -0.312 0.020 -0.172

0.110 -0.067 0.060 0.009 0.060 0.113 0.060 0.020

0.230 0.000 0.090 0.012 0.090 0.096 0.110 0.001

0.400 0.064 0.120 0.088 0.120 -0.166 0.250 -0.002

0.490 0.072 0.200 -0.001 0.200 -0,060 0.400 0.015

0.630 1.626"* 0.260 0.074 0.250 0.095 0.490 0.031

0.750 0.113 0.400 0.117 0.400 0.100 0.580 0.133

0.850 0.148 0.490 0.118 0.490 -0.029 0.650 0.341

0.900 0.224 0.580 0.175 0.580 0.206 0.750 0.512

0.960 0.055 0.640 0.369 0.650 -0.081 0.830 0.589

0.750 0.268 0.750 -0.001 0.900 0.649

0.870 0.238 0,890 0.598 0.960 0.470

0.930 0.210 0.930 0.540

0.960 0.116 0.960 0.664

CN = 0.573 0.694 0.772 0,837

280
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-5-14-000, MINF = 0.805, Camber = 10/9, ALPT = 8.32, BETA = 0.22, QINF = 306.8,

RNPU = 2.5E+06. CNWP = 0,7148

r I = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 0.188 0.000 0.698 0.000 0.353"* 0.010 -0.217

0.060 -0.267 0.020 -0.083 0.020 0.050 0.020 -0.259

0.110 -0.558 0.040 -0.009 0.060 0.021 ** 0.060 -0.886

0.200 - 1.229 0.060 -0.493 0.090 -0.742 0, | 10 - l. 186

0.230 -1.154 0.090 -0.641 0,110 -0,948 0.140 -1.510

0.400 -0.942 0.130 -0.875 0.130 -2,207"* 0.190 -2.207"*

0A90 -0,737 0.150 - 1.151 0.150 - 1.299 0.250 - 1.489

0.590 -0,379 0.200 - 1.235 0.210 - 1.292 0,400 -0.979

0,630 -0.408 0.250 - 1.319 0.250 - 1,289 0.490 -0.740

0.700 -0,415 0,260 - 1.225 0.340 - 1.318 0.580 -0.703

0.750 - 1.016 0.280 - 1.289 0.370 - 1.302 0.650 -0.696

0.8 l 0 -0.990 0.290 - 1.281 0,400 - 1.251 0.700 -0.717

0.840 - 1.005 0.310 - 1.225 0.410 -2.243 ** 0.750 -0.769

0.900 -0.558 0.320 - 1.232 0.430 - 1.310 0.800 -0.56 I

0.960 -0.554 0.340 - 1.244 0.440 - 1.271 0.830 -0.486

0.350 -0,538"* 0.460 - 1.289 0.900 -0.425

0.370 - 1.201 0,490 - 1.212 0.960 -0.438

0.380 - 1,300 0,500 - 1.300

0,400 -0.341 0.520 - 1.261

0.410 - 1.257 0.540 - 1.286

0.430 - 1.206 0.550 - 1.233

0.440 - 1.145 0.580 - 1.214

0,460 - 1.285 0.600 - 1.239

0.470 -1.202 0.610 -1.106

0.490 - 1.199 0.650 -0.869

0.500 -1.228 0.700 -0.623

0.520 - 1.198 0.750 -0.617

0.530 -1.188 0.820 -0.339

0.550 -1.210 0.890 -0.319

0.560 - 1.207 0.900 -0,318

0.580 - 1.173 0.960 -0.283

0,590 -1.218

0.600 -1.204

0.640 -0.483

0.700 -0.447

0.750 -0.024"*

0.820 -0.250

0.870 -0.263

0.930 -0.316

0.960 -0.333

Lower Surface

0.020 -0.231 0.020 0.006 0.020 0.038 0.020 0.221

0.110 0.025 0.060 0,227 0.060 0.287 0,060 0.055

0,230 0.068 0.090 0.163 0.090 0.238 0.110 0.174

0.400 0.058 0. | 20 0.215 0.120 -0.035 0.250 0.093

0.490 0.063 0.200 0.062 0.200 0.011 0.400 0.089

0.630 1.604"* 0.260 0,143 0.250 0.186 0.490 0.095

0.750 0.098 0.400 0.162 0.400 0.163 0.580 0.172

0.850 0.148 0.490 0,149 0.490 0.020 0.650 0.362

0.900 0.214 0.580 0.198 0.580 0.268 0.750 0.538

0.960 0.018 0.640 0.382 0.650 -0.029 0.830 0.631

0.750 0.278 0,750 -0.009 0,900 0.675

0.870 0.271 0.890 0.606 0.960 0.481

0.930 0.225 0.930 0.548

0.960 0.118 0.960 0.621

CN = 0.794 0.962 1.051 1.119

281
Table E-2. Continued.

Hight 216, Wing sweep = 26 °, Time = 11-6-47-000, MINF = 0.795, Camber = 10/6, ALPT = 3.02, BETA = -0,65, QINF = 296.8,

RNPU = 2.4E+06. CNWP = 0.3546

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.531 0,000 0.044 0.000 0,075** 0.010 0.399

0.060 0.081 0.020 0.370 0.020 0.542 0.020 0.280

0.110 -0.292 0.040 0.389 0.060 0.397** 0.060 -0.240

0.200 -0.303 0.060 -0.067 0.090 -0.303 0.110 -0.683

0.230 -0.316 0.090 -0.290 0.110 -0.584 0,140 - 1.134

0.400 -0.249 0.130 -0.571 0.130 -2.263 * * 0.190 -2.263 * *

0.490 -0.245 0.150 -0,903 0.150 - 1.019 0.250 -0.381

0.590 -0.321 0.200 -0,935 0.210 -0.965 0.400 -0.365

0.630 -0.362 0.250 -0.419 0,250 -0.351 0.490 -0.369

0,700 -0,379 0.260 -0.341 0.340 -0.385 0.580 -0.379

0.750 -0.801 0.280 -0.389 0.370 -0.397 0.650 -0.458

0.810 -0.732 0.290 -0.389 0.400 -0.388 0.700 -0,480

0.840 -0.700 0.310 -0.375 0.410 -2.001 ** 0.750 -0.573

0.900 -0.241 0.320 -0.366 0.430 -0.402 0.800 -0.636

0.960 -0.110 0.340 -0,372 0.440 -0.356 0.830 -0.508

0.350 -0.244'* 0.460 -0.387 0.900 -0.499

0.370 -0.341 0.490 -0.335 0.960 -0.535

0.380 -0.389 0.500 -0.406

0.400 -0.283 0.520 -0.375

0.410 -0.387 0.540 -0.397

0,430 -0.342 0.550 -0.377

0.440 -0.311 0.580 -0.395

0.460 -0.397 0.600 -0,401

0.470 -0.357 0.610 -0.409

0.490 -0.366 0,650 -0,887

0.500 -0.375 0.700 -0.645

0.520 -0,370 0.750 -0,698

0.530 -0.365 0.820 -0.422

0.550 -0.403 0.890 -0.388

0.560 -0.389 0.900 -0.411

0.580 -0.371 0.960 -0.345

0.590 -0.418

0.600 -0.432

0.640 -0634

0.700 -0.522

0.750 -0.125"*

0.820 -0.282

0.870 -0.325

0.930 -0.395

0.960 -0.423

Lower Surface

0.020 -0.965 0,020 -0,898 0.020 -0,749 0.020 - 1.080

0.110 -0.327 0.060 -0.384 0.060 -0,473 0.060 0.003

0.230 -0,063 0.090 -0.303 0.090 -0.262 0.110 -0.306

0.400 0.034 0.120 -0.115 0.120 -0.389 0.250 -0.142

0.490 0.046 0.200 -0.059 0.200 -0.116 0.400 -0.083

0.630 1.675** 0.260 -0.062 0.250 -0.001 0.490 -0.042

0.750 0.067 0.400 0.049 0,400 0.021 0.580 0.075

0.850 0.112 0.490 0.051 0.490 -0.088 0.650 0.302

0.900 0.193 0.580 0.127 0.580 0.187 0.750 0.466

0.960 0.127 0.640 0.254 0.650 -0.129 0.830 0.527

0.750 0.162 0,750 -0.007 0.900 0.607

0.870 0.140 0.890 0,467 0.960 0.461

0.930 0.150 0.930 0.412

0.960 0.072 0.960 0.527

CN = 0.313 0.434 0,488 0.578

282
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-6-59-500, MINF = 0.804, Camber = 10/6, ALPT = 5.94, BETA = -0.10, QINF = 304.5,

RNPU = 2.5E+06, CNWP = 0.5619

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.355 0.000 0.423 0.000 0.187"* 0,010 0.039

0,060 -0.105 0020 0.128 0.020 0.286 0.020 -0.066

O 110 -0.468 0.040 0.126 0.060 0.412" * 0.060 -0.697

0.200 -1.141 0.060 -0.299 0.090 -0.511 0.110 -0.989

0.230 - 1.080 0.090 -0.485 0.110 -0.764 0.140 - 1.358

0.400 -0.225 0.130 -0.752 0.130 -2.210"* 0.190 -2.210"*

0,490 -0.232 0.150 - 1.038 0.150 - 1.190 0.250 - 1.095

0.590 -0.329 0.200 - 1.129 0.210 - I. 186 0.400 -0.586

0.630 -0.385 0.250 - 1.197 0.250 - I. 159 0,490 -0.498

0.700 -0.407 0.260 - 1.105 0.340 - 1.151 0.580 -0.482

0.750 -0.855 0.280 - 1.166 0.370 - I. 141 0.650 -0.546

0.810 -0.802 0.290 - 1.141 0.400 - 1.116 0.700 -0.534

0.840 -0.811 0.310 -1.082 0,410 -I.955"* 0.750 -0.634

0.900 -0.338 0.320 - 1.093 0.430 -0.707 0.800 -0.644

0.960 -0208 0.340 - 1.083 0,440 -0.550 0.830 -0.543

0.350 -0.521 ** 0.460 -0.498 0.900 -0.512

0.370 - 1.050 0.490 -0.301 0.960 -0.528

0.380 - 1.143 0.500 -0.394

0.400 -0.309 0.520 -0.355

0.410 - 1.091 0.540 -0.349

0.430 -0.721 0,550 -0.357

0.440 -0.541 0.580 -0.340

0.460 -0.482 0.600 -0.354

0.470 -0.325 0,610 -0.375

0490 -0.323 0.650 -0.914

0.500 -0.301 0.700 -0.590

0.520 -0.290 0.750 -0,655

0.530 -0.261 0.820 -0.583

0.550 -0.293 0.890 -0,423

0.560 -0.265 0.900 -0.481

0.580 -0.279 0.960 -0.409

0.590 -0.327

0.600 -0.348

0.640 -0.481

0.700 -0.510

0.750 -0.098**

0.820 -0.346

0.870 -0.357

0.930 -0.433

0.960 -0.416

Lower Surface

0.020 -0.921 0,020 -0.396 0.020 -0.291 0.020 -0.144

0.110 -0.064 0.060 0.006 0.060 0.129 0.060 0.010

0.230 -0.007 0.090 . 0.036 0.090 0.101 0.110 0.011

0.400 0.036 0.120 0.103 0.120 -0.144 0.250 -0.008

0.490 0.040 0.200 0.007 0.200 -0.083 0.400 0.012

0.630 1.628** 0.260 0.078 0.250 0.092 0.490 0.028

0.750 0.057 0.400 0.099 0.400 0.094 0.580 0.132

0.850 0.100 0.490 0.097 0.490 -0.046 0.650 0.334

0.900 0.182 0.580 0.153 0.580 0.225 0.750 0.526

0.960 0.077 0.640 0.343 0.650 -0.102 0.830 0.596

0.750 0.217 0.750 0.004 0.900 0.644

0.870 0.219 0.890 0.594 0.960 0.471

0.930 0.181 0.930 0.525

0.960 0.092 0.960 0.642

CN = 0.511 0.702 0.798 0.874

283
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-7-3-000, MINF = 0.807, Camber = 10/7, ALPT = 8.29, BETA = -0.47, QINF = 309.3,

RNPU = 2.5E+06, CNWP = 0.7265

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.190 0.000 0.699 0.000 0.258** 0.010 -0.245

0.060 -0.255 0.020 -0.072 0.020 0.044 0.020 -0.267

0. 110 -0.557 0.040 -0.020 0.060 0.242** 0.060 -0.869

0.200 - 1.211 0.060 -0.494 0.090 -0.736 0.110 - 1.195

0.230 - 1.157 0.090 -0.629 0.110 -0.953 0.140 - 1.470

0.400 -0.946 0.130 -0.864 0.130 -2.193"* 0.190 -2.193"*

0.490 -0.703 0.150 -1.135 0.150 - 1.278 0.250 -1.467

0.590 -0.339 0.200 - 1.220 0.210 - 1.280 0.400 -0.954

0.630 -0.376 0.250 - 1.298 0.250 - 1.261 0.490 -0.733

0.700 -0.379 0.260 - 1.211 0.340 - 1.297 0.580 -0.687

0.750 -0.824 0.280 - 1.277 0.370 - 1.296 0.650 -0.694

0.810 -0.798 0.290 - 1.277 0.400 - 1.252 0.700 -0.696

0.840 -0.822 0.310 - 1.217 0.410 - 1.942"* 0.750 -0.724

0.900 -0.492 0.320 - 1.220 0.430 - 1.303 0.800 -0.547

0.960 -0.358 0.340 - 1.230 0.440 - 1.265 0.830 -0.445

0.350 -0.524** 0.460 -1.277 0.900 -0.376

0.370 - 1.188 0.490 - 1.250 0.960 -0.424

0.380 -1.288 0.500 -1.298

0.400 -0.306 0.520 - 1.256

0.410 - 1.243 0.540 - 1.280

0.430 - 1.197 0.550 - 1.239

0.440 -1.137 0.580 -1.228

0.460 - 1.264 0.600 - 1.207

0.470 - 1.228 0.610 - 1.086

0.490 - 1.186 0.650 -0.953

0.500 - 1.207 0.700 -0.572

0.520 - 1.178 0.750 -0.601

0.530 - 1.171 0.820 -0.318

0.550 - t .213 0.890 -0.298

0.560 - 1.193 0.900 -0.300

0.580 - 1.159 0.960 -0.270

0.590 - 1.202

0.600 -1.164

0.640 -0.466

0.700 -0.426

0.750 -0.053"*

0.820 -0.238

0.870 -0.244

0.930 -0.328

0.960 -0.337

Lower Surface

0.020 -0.284 0.020 0.030 0.020 0.026 0.020 0.232

0.110 0.021 0.060 0.221 0.060 0.269 0.060 0.054

0.230 0.064 0.090 0.178 0.090 0.251 0.110 0.159

0.400 0.057 0.120 0.231 0.120 -0.024 0.250 0.106

0.490 0.048 0.200 0.075 0.200 0.024 0.400 0.095

0.630 1.587" * 0.260 0.145 0.250 0.195 0.490 0.105

0.750 0.059 0.400 0.146 0.400 0.157 0.580 0.185

0.850 0.094 0.490 0.136 0.490 0.002 0.650 0.377

0.900 0.183 0.580 0.199 0.580 0.262 0.750 0.553

0.960 0.052 0.640 0.379 0.650 -0.053 0.830 0.607

0.750 0.232 0.750 0.030 0.900 0.680

0.870 0.215 0.890 0.625 0.960 0.493

0.930 0.223 0.930 0.554

0.960 0.134 0.960 0.680

CN = 0.727 0.939 1.048 1.104

284
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-8-20-000, MINF = 0.802, Camber = 10/4, ALPT = 3.09, BETA = -0.62, QINF = 302.2,

RNPU = 2.5E+06, CNWP = 0.3607

rl = 0.93 0.76 0.59 0_40

Upper Surface

x./c CP x/c CP x/c CP x./c CP

0,020 0.548 0.000 0.043 0.000 -0.057"* 0,010 0.411

0,060 0.076 0.020 0,350 0.020 0.558 0.020 0.262

0.110 -0.288 0,040 0,388 0.060 0.578** 0,060 -0.269

0.200 -0.311 0.060 -0.078 0,090 -0.300 0,110 -0.650

0,230 -0,323 0.090 -0.280 0.110 -0,569 0.140 -1,127

0.400 -0.257 0.130 -0.567 0.130 -2.220"* 0.190 -2,220"*

0,490 -0.217 0.150 -0.872 0,150 -1.014 0.250 -0.380

0,590 -0.324 0,200 -0.919 0.210 -0.960 0.400 -0.385

0,630 -0.335 0.250 -0.399 0.250 -0.343 0.490 -0,371

0,700 -0.329 0.260 -0.334 0.340 -0.391 0.580 -0.395

0.750 -0.448 0,280 -0.386 0,370 -0.403 0.650 -0,472

0.810 -0,419 0.290 -0,394 0.400 -0.379 0.700 -0.459

0,840 -0.402 0.310 -0.374 0.410 -1,963"* 0.750 -0.575

0,900 -0,235 0.320 -0.368 0.430 -0,400 0,800 -0,658

0.960 -0,113 0.340 -0.357 0,440 -0.372 0,830 -0.511

0.350 -0,253** 0.460 -0.387 0.900 -0.512

0.370 -0.340 0.490 -0,319 0.960 -0,539

0.380 -0,390 0.500 -0.402

0,400 -0.291 0.520 -0.364

0.410 -0,389 0,540 -0,388

0.430 -0,348 0.550 -0.383

0,440 -0.299 0.580 -0,383

0,460 -0.391 0.600 -0.392

0.470 -0.363 0,610 -0.401

0.490 -0.364 0.650 -0.981

0,500 -0,375 0.700 -0.654

0,520 -0.376 0.750 -0.698

0.530 -0.371 0,820 -044-4

0.550 -0.417 0,890 -0,425

0.560 -0.370 0.900 -0,424

0.580 -0,377 0.960 -0.376

0.590 -0.419

0.600 -0.432

0.640 -0.636

0.700 -0.587

0,750 -0.154"*

0.820 -0.315

0.870 -0,332

0.930 -0.397

0.960 -0,351

Lower Surface

0,020 - 1.045 0.020 -0.898 0.020 -0.764 0.020 - 1.073

0.110 -0.363 0.060 -0.423 0.060 -0.501 0.060 -0.013

0,230 -0.078 0.090 -0.333 0,090 -0.307 0.110 -0.273

0,400 0.002 0.120 -0.198 0,120 -0.421 0.250 -0.158

0.490 0.014 0.200 -0.070 0.200 -0,147 0.400 -0.094

0.630 1,647"* 0.260 -0,073 0.250 -0.017 0.490 -0.046

0.750 0.015 0,400 0.024 0.400 0.013 0.580 0.071

0.850 0.059 0.490 0.056 0.490 -0.106 0,650 0.299

0.900 0,126 0.580 0,116 0,580 0,178 0.750 0.459

0.960 0.079 0.640 0,233 0.650 -0.161 0,830 0.521

0.750 0,122 0,750 -0,019 0.900 0,596

0,870 0,1 l 5 0,890 0.475 0.960 0_463

0.930 0.142 0.930 0,414

0.960 0.069 0.960 0.580

CN = 0.224 0.416 0,484 0.579

285
Table E-2, Continued.

Flight 216, Wing sweep = 26 °, Time = 11-8-28-000, MINF = 0,810, Camber = 10/4, ALPT = 6.06, BETA = -0.44, QINF = 308.6,

RNPU = 2.5E+06, CNWP = 0.5489

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.371 0,000 0.423 0.000 0.176"* 0,010 0,044

0.060 -0.099 0,020 0.150 0.020 0.303 0.020 0.001

0.110 -0.434 0.040 0. ] 76 0.060 0,465 ** 0.060 -0.662

0.200 - 1.135 0,060 -0.305 0,090 -0.489 0.110 -0.951

0.230 - 1.096 0.090 -0.457 0. I 10 -0.758 0.140 - 1.301

0,400 -0,217 0,130 -0,717 0,130 -2,175"* 0.190 -2,175"*

0.490 -0.203 0.150 -1.007 0.150 -1.194 0.250 -1.117

0.590 -0.315 0.200 -1.104 0.210 -1.156 0,400 -0.607

0.630 -0.352 0.250 - 1.152 0,250 - 1.135 0.490 -0.505

0.700 -0.353 0,260 - 1.079 0.340 - 1.130 0.580 -0,476

0.750 -0.543 0.280 - 1.137 0.370 - 1.113 0.650 -0,534

0.810 -0.487 0,290 - 1.121 0.400 - 1.089 0,700 -0.532

0.840 -0.471 0.310 - 1.059 0.410 - 1.924"* 0,750 -0.649

0,900 -0.324 0.320 - 1.073 0,430 - 1.093 0.800 -0.630

0.960 -0.187 0.340 - 1.056 0.440 -0.728 0.830 -0.517

0.350 -0.514"* 0,460 -0.578 0.900 -0,500

0,370 - t .031 0.490 -0.409 0.960 -0.516

0,380 - 1.l 19 0.500 -0,429

0.400 -0.279 0.520 -0.362

0.410 - 1.071 0.540 -0,352

0.430 - 1.021 0.550 -0.348

0,440 -0.907 0,580 -0.348

0,460 -0.655 0.600 -0.333

0.470 -0.435 0.610 -0,352

0.490 -0.375 0.650 -0.893

0.500 -0,329 0.700 -0.555

0.520 -0,303 0.750 -0,624

0,530 -0.249 0,820 -0.509

0.550 -0.284 0,890 -0.404

0,560 -0,256 0.900 -0.434

0,580 -0.251 0.960 -0.361

0.590 -0.284

0.600 -0,309

0.640 -0.435

0.700 -0,494

0,750 -0.I 12"*

0.820 -0.431

0.870 -0.361

0.930 -0.311

0.960 -0.313

Lower Surface

0.020 -0.946 0.020 -0.410 0.020 -0.282 0.020 -0.137

0.110 -0.064 0,060 0,033 0.060 0.145 0.060 0.015

0.230 -0.001 0.090 0.030 0.090 0.107 0.110 0.016

0.400 0.029 0.120 0.103 0.120 -0.143 0.250 -0.003

0.490 0.030 0.200 0.001 0.200 -0.057 0,400 0.017

0.630 1.612"* 0,260 0.072 0.250 0.103 0.490 0,033

0.750 0,009 0,400 0.107 0,400 0,098 0,580 0.136

0,850 0,044 0.490 0.108 0,490 -0,048 0,650 0,342

0.900 0.132 0.580 0.156 0.580 0,227 0.750 0.519

0,960 0.061 0.640 0.340 0.650 -0.109 0.830 0.596

0.750 0.195 0.750 -0,005 0.900 0,658

0.870 0.176 0.890 0.605 0,960 0.476

0,930 0.191 0.930 0.545

0.960 0.106 0,960 0.677

CN = 0.435 0.697 0,794 0.872

286
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-8-31-000, MINF = 0.809, Camber = 10/4, ALPT = 8.00, BETA = -0.41, Q1NF = 307.0,

RNPU = 2.5E+06, CNWP = 0.7208

'fl = Q93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0,227 0.000 0.669 0.000 0.237"* 0,010 -0.188

0.060 -0,232 0,020 -0.053 0.020 0.074 0.020 -0.245

0.110 -0,527 0.040 0.028 0.060 0.220** 0.060 -0.837

0.200 - 1.183 0.060 -0.470 0.090 -0.703 0.110 - 1.153

0.230 - 1,156 0,090 -0.594 0.110 -0.887 0.140 - 1.449

0.400 -0.911 0.130 -0.835 0.130 -2.183" * 0.190 -2.183 **

0.490 -0.622 0.150 - I. 106 0.150 - 1.249 0,250 - 1.438

0.590 -0.314 0.200 - 1,198 0.210 - 1.261 0.400 -0,917

0.630 -0.351 0.250 - 1,261 0.250 - 1.245 0.490 -0,695

0.700 -0.347 0,260 - 1,190 0.340 - 1.265 0.580 -0,665

0.750 -0.497 0.280 - 1.247 0,370 - 1,255 0.650 -0.682

0.810 -0.457 0.290 - 1.242 0.400 - 1,235 0,700 -0.684

0.840 -0.448 0,310 -1,188 0,410 -1,930"* 0.750 -0.746

0.900 -0.432 0.320 - 1.193 0.430 - 1.272 0.800 -0.567

0.960 -0.224 0.340 - 1.202 0.440 - 1,237 0.830 -0,466

0,350 -0,529** 0.460 - 1,265 0.900 -0.417

0.370 - 1.160 0,490 - 1,174 0.960 -0.438

0,380 -1,275 0.500 -1,264

0.400 -0.283 0.520 - 1.235

0,410 -1.211 0.540 -1.252

0,430 - 1.174 0.550 - 1.215

0,440 -1.104 0.580 - 1.189

0,460 - 1.241 0.600 - 1.101

0,470 -1.182 0.610 -0.939

0.490 - 1,163 0.650 - 1.024

0.500 - 1.187 0.700 -0.640

0.520 -1.159 0.750 -0.619

0.530 -1,138 0.820 -0,314

0.550 -1,175 0.890 -0.306

0.560 - 1.170 0.900 -0.289

0.580 - 1.131 0.960 -0.255

0.590 -1.171

0.600 -1.161

0.640 -0.493

0.700 -0.453

0.750 -0.070"*

0.820 -0.367

0.870 -0.255

0.930 -0,258

0.960 -0.264

Lower Surface

0.020 -0.280 0.020 -0.027 0.020 -0.007 0.020 0,200

O. 110 0.027 0.060 0,224 0,060 0,254 0.060 0.051

0.230 0.061 0.090 0.165 0,090 0,222 0,110 0.148

0.400 0.030 0.120 0.208 0.120 -0.027 0.250 0.083

0.490 0.031 0.200 0.052 0,200 0,015 0,400 0.093

0.630 1.625"* 0.260 0.144 0.250 0.186 0.490 0.103

0.750 0.008 0.400 0.158 0.400 0.161 0.580 0.189

0.850 0,026 0.490 0.145 0.490 -0.015 0.650 0.377

0.900 0.118 0.580 0.190 0.580 0.261 0,750 0.540

0,960 0.035 0.640 0.364 0.650 -0.077 0.830 0.624

0.750 0.213 0.750 0.027 0.900 0.682

0.870 0.228 0,890 0.627 0.960 0.497

0.930 0.218 0,930 0.559

0.960 0.122 0.960 0.675

CN = 0,622 0.929 1,028 1.085

287
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-10-2-500, MINF = 0.806, Camber = 10/0, ALPT = 3.02, BETA = -0,24, QINF = 306.1,

RNPU = 2.5E+06, CNWP = 0.3578

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.526 0.000 0.044 0.000 -0.029"* 0,010 0,409

0.060 0.077 0,020 0.357 0.020 0.567 0,020 0.272

0.110 -0.292 0.040 0.390 0.060 0.541 ** 0.060 -0.273

0.200 -0.351 0.060 -0,069 0.090 -0.283 0.110 -0.629

0.230 -0.308 0.090 -0.284 0.110 -0.560 0.140 -1.120

0.400 -0,246 0.130 -0.560 0.130 -2.199 * * 0.190 -2.199 **

0.490 -0.196 0.150 -0.868 0.150 - 1.000 0.250 -0.389

0.590 -0.278 0.200 -0.931 0.210 -0.964 0.400 -0,373

0.630 -0.255 0.250 -0.388 0.250 -0.339 0.490 -0.368

0.700 -0.184 0.260 -0.310 0,340 -0.378 0.580 -0.387

0.750 -0.210 0.280 -0.375 0.370 -0.397 0.650 -0.463

0.810 -0.203 0.299 -0.371 0,400 -0.424 0.700 -0.455

0.840 -0.181 0.310 -0.364 0.410 -1.946"* 0.750 -0.575

0.900 -0.172 0.320 -0.361 0.430 -0.402 0.800 -0.657

0.960 -0.084 0.340 -0.353 0,440 -0.365 0,830 -0.530

0,350 -0.257** 0.460 -0.384 0.900 -0.521

0.370 -0.339 0.490 -0.322 0.960 -0.531

0.380 -0,388 0,500 -0.399

0.400 -0,294 0.520 -0.367

0.410 -0.382 0.540 -0.377

0.430 -0.351 0.550 -0.373

0.440 -0.291 0.580 -0.386

0.460 -0.393 0.600 -0.382

0.470 -0.359 0.610 -0.403

0.499 -0.359 0,650 -0.972

0.500 -0.372 0.700 -0.642

0.520 -0.364 0.750 -0.693

0.530 -0.363 0.820 -0.478

0,550 -0.410 0.890 -0.454

0.560 -0.378 0,900 -0,462

0.580 -0.367 0.960 -0.423

0.590 -0.412

0.600 -0.424

0.640 -0.628

0.700 -0.573

0.750 -0.177"*

0.820 -0,392

0.870 -0.367

0.930 -0.355

0.960 -0.383

Lower Surface

0.020 - 1.072 0,020 -0.884 0.020 -0.777 0.020 - 1.060

0.110 -0.340 0.060 -0.414 0.060 -0.508 0.060 -0.020

0.230 -0.066 0.090 -0.313 0.090 -0.305 0.110 -0.277

0.400 -0.013 0.120 -0.166 0.120 -0.431 0.250 -0.157

0.490 -0.012 0.200 -0.073 0.200 -0.139 0.400 -0.096

0.630 1.619"* 0.260 -0,086 0.250 -0.017 0.490 -0.049

0.750 -0.052 0.400 0.017 0.400 0.006 0.580 0.073

0.850 -0.017 0.490 0,040 0.490 -0.119 0.650 0.302

0.900 0.051 0.580 0.100 0.580 0.173 0.750 0.460

0.960 0.035 0.640 0.227 0.650 -0.180 0.830 0.516

0.750 0.073 0.750 -0.026 0.900 0.596

0.870 0.089 0.890 0.469 0.960 0.462

0.930 0.1 04 0.930 0.417

0.960 0.029 0.960 0.562

CN = 0.143 0.406 0.481 0.575

288
Table E-2. Continued.

Flight 216. Wing sweep = 26 °, Time = 11-10-12-000. MINF = 0.806, Camber = 10/0, ALPT = 5.83, BETA = -0.38, QINF = 306.9,

RNPU = 2.5E+06, CNWP = 0.5499

rl = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x,/c CP

0,020 0.393 0,000 0.398 0.000 0.159"* 0.010 0,074

0,060 -0,093 0,020 0.158 0.020 0,324 0.020 -0,031

0. I 10 -0,437 0.040 0.187 0.060 0.456"* 0,060 -0.647

0.200 - 1.14 l 0.060 -0.288 0.090 -0.483 0.110 -0,940

0,230 - 1.060 0.090 -0.454 0.110 -0.738 0.140 - 1.302

0,400 -0,193 0.130 -0.720 0.130 -2.199"* 0.190 -2.199"*

0,490 -0.233 0.150 -1.017 0.150 -1.163 0.250 -0.982

0.590 -0.287 0,200 - 1,105 0.210 - 1.156 0.400 -0,540

0.630 -0.268 0.250 - 1,170 0.250 - 1.136 0,490 -0,464

0.700 -0.200 0.260 - 1.064 0.340 - 1.119 0,580 -0,454

0.750 -0,239 0.280 - 1.121 0.370 -1.093 0,650 -0.513

0.810 -0,221 0,290 - 1,113 0.400 - 1.078 0.700 -0,506

0.840 -0,208 0.310 - 1.058 0.410 - 1.946"* 0.750 -0,628

0.900 -0.215 0.320 - 1.069 0.430 -0.612 0,800 -0.645

0.960 -0.130 0.340 - 1.061 0,440 -0.491 0,830 -0.531

0.350 -0.518"* 0,460 -0.441 0,900 -0,505

0.370 - 1.026 0.490 -0,312 0.960 -0,530

0.380 - 1.119 0.500 -0.361

0,400 -0,292 0.520 -0.326

0.410 -0.915 0.540 -0.326

0,430 -0.519 0,550 -0.325

0.440 -0,390 0.580 -0.344

0.460 -0.415 0.600 -0.346

0.470 -0.303 0.610 -0,353

0.499 -0.269 0.650 -0,921

0.500 -0.268 0.700 -0.584

0.520 -0.248 0,750 -0,646

0.530 -0.241 0.820 -0.531

0.550 -0,297 0.890 -0.434

0.560 -0.263 0.900 -0.469

0.580 -0.277 0.960 -0.388

0.590 -0.323

0.600 -0.342

0.640 -0.468

0,700 -0.498

0.750 -0.160**

0.820 -0.434

0.870 -0.357

0,930 -0,345

0.960 -0,351

Lower Surface

0.020 - 1.004 0.020 -0.44 1 0.020 -0.295 0,020 -0.187

0.110 -0.076 0.060 0.01 [ 0.060 0.109 0.060 0.004

0.230 -0.013 0.090 0.007 0,090 0.094 0.110 0,004

0.400 0.007 0.120 0.085 0.120 -0.155 0.250 -0.011

0.490 -0.014 0.200 -0.014 0.200 -0.082 0.400 0.009

0.630 1.610"* 0.260 0.061 0.250 0.099 0.490 0.029

0.750 -0.077 0.400 0.096 0,400 0,087 0.580 0.135

0.850 -0.045 0.490 0.082 0.490 -0.081 0.650 0.340

0.900 0,026 0.580 0.131 0.580 0.210 0.750 0.520

0.960 0.026 0.640 0.305 0.650 -0.149 0.830 0.588

0.750 0.128 0.750 -0.017 0.900 0.650

0.870 0.148 0.890 0.590 0.960 0,473

0.930 0.142 0.930 0.526

0.960 0.056 0.960 0.666

CN = 0.318 0,648 0.762 0,832

289
Table E-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 11-10-16-000, MINF = 0.803, Camber = 10/0, ALPT = 8.04. BETA = -0.30, QINF = 306.7,

RNPU = 2,5E+06, CNWP = 0.7191

1] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.157 0.000 0.707 0.000 0.222"* 0.010 -0.230

0.060 -0.279 0.020 -0.110 0.020 0.033 0.020 -0.288

0.110 -0.588 0.040 -0.052 0,060 0.249"* 0.060 -0.915

0.200 - 1.225 0.060 -0.531 0.090 -0,756 0.110 - 1.208

0.230 - 1.194 0.090 -0,636 0.110 -0.973 0.140 - 1.500

0.400 -0,987 0.130 -0.875 0.130 -2.215"* 0.190 -2.215"*

0.490 -0.449 0.150 - 1.148 0.150 - 1.307 0.250 - 1.483

0.590 -0.292 0.200 - 1.243 0.210 - 1.305 0.400 -0.967

0.630 -0.292 0.250 - 1,327 0.250 - 1.297 0.490 -0.729

0.700 -0.209 0.260 - 1.233 0.340 - 1.326 0.580 -0.681

0.750 -0.267 0.280 - 1.306 0.370 - 1.310 0.650 -0.718

0.810 -0.270 0.290 - 1.283 0.400 - 1.281 0.700 -0.710

0.840 -0.253 0.310 - 1.249 0.410 - 1.962"* 0.750 -0.756

0.900 -0.296 0.320 - 1.257 0.430 - 1.318 0.800 -0.528

0.960 -0.191 0.340 - 1.265 0.440 - 1.280 0.830 -0.450

0.350 -0.532** 0.460 -1.291 0.900 -0.380

0,370 - 1.206 0.490 - 1.220 0.960 -0.415

0.380 - 1.321 0.500 - 1.327

0.400 -0.306 0.520 -1.285

0.410 -1.278 0.540 -1.294

0.430 - 1.225 0,550 - 1,253

0.440 - 1.148 0.580 - 1.257

0.460 -1.293 0.600 -1.197

0.470 - 1.229 0.610 - 1.008

0.490 - 1.218 0.650 -0,926

0.500 - 1.246 0,700 -0,574

0.520 - 1.236 0.750 -0.614

0.530 -1.188 0.820 -0.334

0.550 - 1.236 0.890 -0.323

0.560 - 1.207 0.900 -0.310

0.580 - 1.194 0.960 -0.270

0.590 -1.208

0.600 -0.909

0.640 -0.467

0.700 -0,455

0.750 -0.152"*

0.820 -0.534

0.870 -0,439

0.930 -0.310

0.960 -0.333

Lower Surface

0.020 -0.253 0.020 0.051 0.020 0.053 0.020 0.249

0.110 0.039 0.060 0.253 0.060 0.292 0.060 0.032

0.230 0,057 0.090 0.190 0.090 0.263 0.110 0.172

0.400 0.018 0.120 0.214 0.120 -0.003 0.250 0.116

0.490 -0.003 0.200 0.058 0.200 0.021 0.400 0.099

0,630 1.596"* 0.260 0.142 0.250 0.207 0.490 0.102

0.750 -0.083 0.400 0.147 0.400 0.155 0.580 0.198

0.850 -0.058 0.490 0.130 0.490 -0.052 0.650 0.383

0.900 0.002 0.580 0.160 0.580 0.268 0.750 0.563

0.960 -0.011 0.640 0.345 0.650 -0.127 0.830 0.617

0.750 0.148 0.750 0.041 0.900 0.679

0,870 0.137 0.890 0.620 0.960 0.485

0.930 0.146 0.930 0.541

0.960 0.071 0.960 0.683

CN = 0.534 0,957 1,054 1.119

290
Table E-2. Continued.

Flight 192, Wing sweep = 26 °, Time = 11-25-33-000, MINF = 0.797, Camber = 5/15, ALPT = 7.00, BETA = -0.06, QINF = 233.9,

RNPU = 1.9E+06, CNWP = 0.5904

q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.200 0.000 0,896 0,000 -4.479** 0,010 - 1.028

0.060 -0.409 0.020 -0.804"* 0,020 -0,432 0.020 -0.868

0,1 I 0 -0.538 0,040 -0.363 0,060 -0.343 0.060 -0.929

0.200 -0,962 0.060 -0.694 0,090 -0.814 0.110 - 1.147

0.230 -0.848 0.090 -0.717 0.110 - 1.015 0.140 - 1.280

0,400 -0.224 0.130 -0.826 0.130 - 1.002 0.190 -5,825 **

0.490 -0.251 0.150 -1.018 0.150 -1.141 0.250 -1,232

0,590 -0.359 0.200 -0.966 0.210 - 1.170 0.400 -0,455

0.630 -0,395 0,250 - 1.165 0.250 - 1.107 0.490 -0,467

0.700 -0.406 0,260 - 1.006 0.340 - 1.122 0.580 -0,519

0.750 -0,694 0,280 - 1.129 0.370 - 1.090 0.650 -0.485

0.810 -0,740 0,290 - 1,1 04 0.400 -0.821 0.700 -0,512

0.840 -0.665 0.310 - 1.036 0.410 -0.539 0,750 -0,641

0.900 -0,531 0.320 -0.991 0.430 -0.505 0.800 -0.686

0.960 -0.626 0.340 - 1,040 0.440 -0.417 0.830 -0.515

0,350 -0,459"* 0.460 -0,091 ** 0.900 -0.476

0,370 - 1,000 0,490 -0.272 0,960 -0.478

0.380 -1.018 0.500 -0.388

0.400 -0.532 0.520 -0.266

0,410 -0,487 0.540 -0.302

0,430 -0.380 0.550 -0.319

0.440 -0.240 0.580 -0.390

0.460 -0.385 0.600 -0.381

0.470 -0.253 0.610 -0.282

0.499 -0.256 0.650 -2.331 **

0.500 -0.266 0.700 -0.630

0.520 -0.280 0.750 -0.677

0.530 -0.259 0.820 -0.646

0.550 -0,317 0.890 -0.417

0.560 -0,269 0,900 -0.497

0.580 -0,299 0,960 -0.457

0.590 -0.362

0,600 -0.454

0,640 -2.124"*

0700 -0.524

0,750 -0.659

0.820 -2.338**

0,870 -0.397

0,93O -0.369

0.960 -0,356

Lower Surface

0.020 -0,188 0,020 0.274 0.020 0,094 0,020 0.358

0.110 0.000 0.060 0,209 0.060 0,305 0.060 2.547**

0.230 0.130 0,090 0.122 0,090 0,181 0.110 0,052

0.400 0.107 0.120 0.159 0.120 -0,343 0.250 0.057

0.490 0.102 0.200 0.127 0,200 -0.013 0.400 0.065

0.630 2.503"* 0.260 0.054 0,250 0.140 0.490 0.026

0.750 0.270 0.400 -2.369** 0.400 0.103 0.580 0.092

0.850 0.337 0.490 0.139 0.490 0,096 0.650 0.306

0,900 0,386 0.580 0.259 0.580 0.214 0.750 0,515

0,960 0.129 0.640 0.642** 0.650 0.432 0.830 0,575

0,750 0.413 0.750 0,540 0,900 0,680

0.870 0.497 0.890 ******** 0,960 0,461

0,930 0.448 0.930 0.509

0.960 0.278 0.960 -2.199**

CN = 0.649 0.820 0,884 0.922

291
Table E-2. Continued.

Flight 192, Wing sweep -- 26 °, Time = I 1-25-40-000, MINF = 0.786, Camber = 5/15, ALPT = 8.08, BETA = 0.42, QINF = 224.2,

RNPU = 1.9E+06, CNWP = 0.6774

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.450 0.000 0.892 0.000 -4.641 ** 0.010 - 1,068

0.060 -0,592 0.020 - 1.126** 0.020 -0.650 0.020 - 1.099

0.110 -0.741 0.040 -0.513 0.060 -0.447 0.060 - 1.19 l

0.200 - 1.026 0,060 -0.836 0.090 -0,971 0.110 - 1.322

0,230 -0.902 0.090 -0.937 0.110 - 1.195 0.140 - 1.389

0.400 -0.281 0.130 - 1.030 0.130 - 1.162 0.190 -6.045" *

0.490 -0.268 0.150 - 1.174 0.150 - 1.258 0.250 - 1.407

0.590 -0.383 0.200 - 1.120 0.210 - 1.315 0.400 -0.628

0.630 -0.405 0.250 - 1.289 0.250 - 1,239 0.490 -0.525

0.700 -0.436 0.260 - 1.109 0,340 - 1.261 0.580 -0.516

0.750 -0.829 0.280 - 1.235 0.370 - 1.229 0.650 -0,463

0.810 -0.821 0.290 - 1.247 0.400 - 1.272 0.700 -0,521

0.840 -0,761 0.310 -1.150 0.410 -1.187 0.750 -0,646

0.900 -0.621 0.320 - 1.109 0.430 - 1,153 0.800 -0.683

0,960 -0.696 0.340 - 1.165 0.440 -0.752 0.830 -0,642

0.350 -0.446** 0.460 -0,356** 0.900 -0.329

0.370 - 1.108 0.490 -0.469 0.960 -0.368

0.380 -1.143 0.500 -0.552

0,400 - 1.031 0.520 -0.407

0.410 -1.175 0.540 -0.414

0.430 -1.030 0.550 -0,387

0.440 -0.627 0.580 -0.351

0.460 -0.659 0,600 -0.349

0,470 -0.475 0.610 -0,225

0.490 -0.397 0.650 -2,399**

0.500 -0.310 0.700 -0.515

0.520 -0.352 0.750 -0.640

0.530 -0.252 0.820 -0,664

0.550 -0.274 0,890 -0,312

0.560 -0.201 0.900 -0.370

0.580 -0.246 0,960 -0.366

0.590 -0.260

0,600 -0,389

0.640 -2.183"*

0.700 -0.514

0,750 -0,785

0,820 -2.406**

0,870 -0.353

0.930 -0.323

0.960 -0.310

Lower Surface

0.020 0.013 0,020 0.328 0.020 0,258 0.020 0.515

0.110 0,063 0.060 0.325 0.060 0.429 0.060 2.689**

0.230 0.179 0.090 0.211 0.090 0.275 0.110 0.141

0.400 0.144 0.120 0.219 0.120 -0,276 0.250 0.125

0,490 0.119 0,200 0.199 0.200 0.018 0,400 0.130

0,630 2.644** 0.260 0,098 0.250 0.199 0.490 0.070

0.750 0.279 0.400 -2.439** 0.400 0.160 0.580 0.116

0.850 0.329 0,490 0.163 0.490 0,142 0.650 0.312

0,900 0.391 0,580 0.292 0.580 0,246 0.750 0.518

0,960 0.129 0.640 0.691 ** 0.650 0.464 0.830 0.589

0.750 0.446 0.750 0.566 0.900 0.686

0.870 0.507 0.890 ******** 0.960 0.478

0,930 0.436 0,930 0.513

0.960 0,288 0.960 -2.261 **

CN = 0.741 0.952 1.001 1.034

292
Table E-2. Continued.

Flight 192, Wing sweep = 26 °, Time = 11-25-43-500. MINF = 0,784, Camber = 5/15, ALPT = 9.25, BETA = -0.08. QINF = 225.1,

RNPU = 1.9E+06, CNWP = 0.7521

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.920 0.000 0.788 0.000 -4,640** 0.010 -1.268

0.060 -0.741 0.020 - 1.443"* 0.020 - 1.048 0.020 - 1.272

0.110 -0.733 0.040 -0.834 0.060 -0.434 0.060 - 1.335

0.200 - 1.088 0.060 -0.998 0.090 - 1.115 0.110 - 1,402

0.230 -1.077 0.090 -1,029 0.110 -1,302 0.140 -1.500

0.400 -0.895 0.130 - I, 168 0.130 - 1.282 0.190 -6.037 * *

0.490 -0.311 0.150 - 1.298 0.150 - 1.388 0.250 - 1.534

0.590 -0.381 0.200 - 1,244 0.210 - 1.427 0,400 -0.910

0.630 -0,449 0.250 - 1.403 0.250 - 1.350 0.490 -0.742

0.700 -0.449 0.260 - 1.220 0.340 - 1,400 0,580 -0.557

0.750 -1.176 0.280 - 1.353 0,370 - 1.341 0.650 -0.484

0.810 -1.114 0.290 -1.354 0,400 -1,364 0,700 -0.527

0.840 - 1.007 0.310 - 1.264 0,410 - 1.298 0.750 -0.575

0.900 -0.709 0.320 - 1.229 0.430 - 1.374 0.800 -0.537

0.960 -0.794 0.340 - 1.298 0.440 - 1.309 0,830 -0,446

0.350 -0.445"* 0.460 - 1.027"* 0.900 -0.271

0.370 - 1.233 0.490 - 1.194 0,960 -0.325

0.380 -1.273 0.500 -1.003

0.400 - 1.166 0.520 -0.800

0.410 -1.305 0.540 -0.801

0.430 -1.258 0.550 -0.728

0.440 - I. 142 0.580 -0.715

0.460 - 1.405 0.600 -0.637

0.470 - 1.241 0,610 -0.521

0.490 - 1.229 0.650 -2.408 * *

0.500 - 1.159 0.700 -0.474

0.520 -0.941 0.750 -0.647

0,530 -0.649 0.820 -0,393

0,550 -0.623 0,890 -0,248

0.560 -0.521 0.900 -0.253

0.580 -0.489 0.960 -0.252

0.590 -0.471

0.600 -0.491

0.640 -2.193"*

0.700 -0.449

0.750 -1.010

0.820 -2.415"*

0,870 -0,303

0.930 -0.283

0.960 -0.264

Lower Surface

0.020 0.084 0,020 0.331 0.020 0.433 0.020 0.625

0.110 0.113 0.060 0.407 0.060 0.473 0.060 2.658 **

0.230 0.233 0.090 0.285 0.090 0.353 0.110 0.187

0.400 0.163 0.120 0.287 0.120 -0.209 0.250 0.180

0.490 0.148 0.200 0.251 0.200 0.082 0.400 0.159

0.630 2.613"* 0.260 0.147 0.250 0,247 0.490 0.109

0.750 0.272 0.400 -2.448 ** 0.400 0,206 0.580 0.149

0,850 0,321 0.490 0.196 0.490 0.161 0.650 0.350

0.900 0.380 0,580 0.301 0.580 0.274 0.750 0.535

0.960 0,104 0.640 0.696** 0.650 0.491 0.830 0.606

0.750 0.469 0.750 0.593 0,900 0.703

0.870 0.549 0.890 ******** 0.960 0.468

0.930 0.459 0.930 0.521

0.960 0.292 0.960 -2.271 **

CN = 0.939 1.145 1.134 1.138

293
Table E-2. Continued.

Flight 192, Wing sweep = 26 °, Time = 11-25-56-500, MINF = 0.795, Camber = 5/14, ALPT = 11.50, BETA = 0.86, QINF = 260.8,

RNPU = 2.2E+06, CNWP = 0.5738

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.105 0.000 0.690 0.000 -4.258** 0.010 - 1.401

0.060 - 1.081 0.020 - 1.619"* 0.020 - 1.206 0.020 - 1.392

0. I I 0 - 1.085 0.040 - 1.076 0.060 -0.603 0.060 - 1.507

0.200 - 1.206 0.060 - 1.165 0.090 - 1.279 0.110 - 1.557

0.230 -1.154 0.090 -1.240 0.110 -1.459 0.140 -1,569

0,400 - 1.096 0.130 - 1.323 0.130 - 1.407 0.190 -5.465 * *

0.490 -0.416 0.150 - 1.419 0.150 - 1.347 0.250 - 1.225

0.590 -0.357 0.200 - 1.379 0.210 - 1.231 0.400 -0.957

0.630 -0.394 0.250 - 1.552 0.250 -0.873 0.490 -0.912

0.700 -0,443 0.260 -1.382 0.340 -0.883 0.580 -0.848

0.750 - 1.242 0.280 - 1.471 0.370 -0.843 0.650 -0.562

0.810 - 1.329 0.290 - 1.487 0,400 -0.876 0.700 -0.641

0.840 - 1.288 0.310 - 1.355 0.410 -0.773 0.750 -0.606

0.900 -0.826 0.320 - 1.342 0.430 -0.817 0,800 -0.652

0.960 -0.860 0.340 - 1.377 0.440 -0.803 0.830 -0.604

0.350 -0.422** 0,460 -0.521 ** 0,900 -0.433

0,370 - 1.218 0.490 -0.727 0.960 -0.407

0.380 -1.216 0.500 -0.777

0.400 - 1.085 0.520 -0.697

0.410 - 1.186 0.540 -0.706

0.430 -0.992 0.550 -0.740

0.440 -0,806 0.580 -0.752

0.460 -0,958 0.600 -0.685

0.470 -0.754 0.610 -0.561

0.490 -0.726 0.650 -2.331 **

0.500 -0.642 0,700 -0.642

0.520 -0.665 0.750 -0.707

0.530 -0.471 0.820 -0.558

0.550 -0,555 0,890 -0.490

0.560 -0.380 0.900 -0.442

0.580 -0.396 0.960 -0.444

0.590 -0.320

0.600 -0.368

0,640 -2.146"*

0.700 -0.337

0.750 -0,476

0.820 -2.337**

0.870 -0.273

0.930 -0.295

0.960 -0.283

Lower Surface

0.020 0.205 0,020 0.348 0.020 0.587 0.020 0.801

0.110 0.193 0.060 0.543 0.060 0.610 0.060 2.043 * *

0.230 0.308 0.090 0.392 0.090 0.471 0.110 0.324

0.400 0.191 0.120 0.376 0.120 -0.037 0.250 0.265

0.490 O. 144 0.200 0.329 0.200 O.167 0.400 0.239

0.630 2.004"* 0.260 0.202 0.250 0.328 0.490 O. 158

0.750 0.294 0.400 -2.365** 0.400 0.247 0.580 0.202

0.850 0.328 0.490 0.216 0.490 O. 164 0.650 0.370

0.900 0.393 0.580 0.314 0.580 0.254 0.750 0.602

0.960 O.138 0.640 0.667"* 0.650 0.474 0.830 0.663

0.750 0.451 0.750 0.584 0.900 0.744

0.870 0.539 0.890 ******** 0.960 0.486

0.930 0.455 0,930 0.513

0.960 0.290 0.960 -2.213 **

CN = 1.094 1.108 1.095 1.265

294
Table E-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 9-15-28-000, MINF = 0.790, Camber = 5/15. ALPT = 3.97, BETA = -0.18, QINF = 266.4,

RNPU = 2.2E+06, CNWP = 0,4161

1"1= 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.260 0,000 0,657 0.000 1.408"* 0.010 -0.226

0.060 -0.060 0.020 0.139 0.020 0.136 0.020 -0.125**

0.110 -0.250 0.040 0.130 0.060 0,109"* 0,060 -0.486"*

0,200 -0.310 0,060 -0.252 0,090 -0.345 0.110 -0.709

0,230 -0.309 0.090 -0.357 0.110 -0.588 0.140 - 1.000

0.400 -0,395 0.130 -0.695 0.130 -0.761 0.190 -2.287 * *

0.490 -0.218 0.150 -0.654 0.150 -0.848 0.250 -0,409

0.590 -0.298 0.200 -0,531 0,210 -0.719 0.400 -0.376

0.630 -0.320 0.250 -0,403 0.250 -0.378 0.490 -0.365

0,700 -0.447 0.260 -0.348 0,340 -0.366 0.580 -0.375

0.750 -0.479 . 0,280 -0,380 0.370 -0.388 0.650 -0.425

0,810 -0.446 0.290 -0.380 0.400 -0.336 0.700 -0.54 t

0,840 -0.475 0.310 -0.362 0,410 -0,366 0.750 -0.567

0,900 -0.352 0,320 -0.354 0.430 -0.343 0.800 -0,686

0.960 -0.346 0.340 -0.351 0.440 -0.380 0.830 -0.502

0.350 -0.131 ** 0.460 -0.129 0.900 -0.446

0,370 -0,329 0.490 -0.301 0,960 -0,470**

0.380 -0.365 0.500 -0.352

0.400 -0,265 0.520 -0.354

0,410 -0,342 0.540 -0.380

0.430 -0,429 0.550 -0.343

0.440 -0.273 0.580 -0.338

0,460 -0.325 0.600 -0.394

0.470 -0.327 0.610 -0.408

0.490 -0.343 0.650 0.054**

0.500 -0.30 l 0.700 -0.606

0,520 -0.316 0.750 -0.611

0.530 -0.356 0.820 -0,271

0,550 -0,329 0,890 -0.427

0.560 -0,372 0.900 -0.514

0.580 -0.328 0.960 -0404

0.590 -0.393

0.600 -0.401

0.640 -0.647

0.700 -0.535

0,750 0.110"*

0,820 -0,501

0.870 -0.340

0.930 -0.343

0.960 -0.374

Lower Surface

0,020 -0.713 0,020 -0.476 0.020 -0.334 0.020 -0.099

0.110 -0.096 0.060 -0.064 0.060 0.036 0.060 0,050

0.230 0.040 0.090 -0.169 0.090 -0,014 0,110 -0.062

0.400 0.117 0.120 -0.007** 0,120 -0.325 0.250 -0.102

0.490 0,131 0,200 0.043 0.200 0.091 0,400 -0.074

0,630 5.117 * * 0.260 0,003 0.250 0.025 0.490 -0,017

0.750 0.307 0.400 0.088 0,400 0.037 0.580 0.019

0,850 0.339 0,490 0,111 0.490 0.121 0.650 0.307

0.900 0.431 0.580 0.176 0.580 0,166 0,750 0,442

0,960 0.201 0,640 0.393 0.650 0.095 0.830 0.548

0.750 0.467 0.750 -0.306"* 0.900 0.608

0,870 0.524 0.890 0.559 0.960 0.457

0.930 0.468 0,930 0.493

0.960 0.313 0.960 0.349

CN = 0.462 0.586 0,557 0.602

295
Table E-2. Continued.

Hight 204, Wing sweep = 26 °, Time = 9-15-38-500, MINF = 0.794, Camber = 5/15, ALPT = 4.99, BETA = -0.56, QINF = 267.9,

RNPU = 2.2E÷06, CNWP = 0.6139

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.080 0.000 0.683 0.000 1.312"* 0.010 -0.799

0.060 -0.214 0.020 -0.087 0.020 -0.155 0.020 -0.425"*

0.110 -0.436 0.040 -0.115 0.060 -0.023" * 0.060 -0.839"*

0.200 -0.387 0.060 -0.640 0.090 -0.604 0.110 -0.903

0.230 -0.421 0.090 -0.785 0. t 10 -0.778 0.140 - 1.126

0.400 -0.359 0.130 -0.712 0.130 -1.154 0.190 -2.265**

0.490 -0.347 0.150 -0,829 0,150 - 1.016 0.250 -0.943

0.590 -0.390 0.200 -0.922 0.210 - 1.065 0.400 -0.509

0.630 -0.481 0.250 -0.643 0.250 -0.943 0.490 -0.460

0.700 -0.697 0.260 -0.426 0.340 -0.714 0.580 -0.452

0.750 -0.623 0.280 -0.450 0.370 -0.458 0.650 -0.611

0.810 -0.794 0.290 -0.411 0.400 -0.422 0.700 -0.584

0.840 -0.561 0.310 -0.399 0.410 -0.449 0.750 -0.898

0.900 -0.530 0.320 -0.640 0.430 -0.724 0.800 -0.730

0.960 -0.529 0.340 -0.586 0.440 -0.438 0.830 -0.561

0.350 -0.387"* 0,460 -0.481 0.900 -0.547

0.370 -0.599 0.490 -0.397 0.960 -0.558**

0.380 -0.445 0.500 -0.458

0.400 -0.360 0.520 -0.703

0.410 -0.689 0.540 -0.448

0.430 -0.414 0.550 -0.572

0.440 -0.360 0.580 -0.418

0.460 -0.471 0.600 -0.445

0.470 -0.475 0.610 -0.493

0.490 -0.681 0.650 -0.035"*

0.500 -0.467 0.700 -0.695

0.520 -0.477 0.750 -0.769

0.530 -0.466 0.820 -0.361

0.550 -0.435 0.890 -0.546

0.560 -0.643 0.900 -0.848

0.580 -0.502 0.960 -0.518

0.590 -0.679

0.600 -0.482

0.640 -0.943

0.700 -0.653

0.750 0.066"*

0.820 -0.574

0.870 -0.402

0.930 -0.430

0.960 -0.420

Lower Surface

0.020 -0.396 0.020 -0.366 0.020 -0.313 0.020 -0.034

0.110 -0.318 0.060 -0.043 0.060 0.008 0.060 0.003

0.230 0.001 0.090 -0.113 0.090 -0.253 0.110 -0.054

0.400 -0.013 0.120 -0.022 ** 0.120 -0.288 0.250 -0.130

0.490 0.058 0.200 -0.013 0.200 -0.188 0.400 -0.375

0.630 5.098" * 0.260 -0.225 0.250 -0.076 0.490 -0.113

0.750 0.042 0.400 -0.029 0.400 -0,062 0.580 0.023

0.850 0.085 0.490 -0.010 0.490 -0.221 0.650 0.217

0.900 0.151 0.580 0.148 0.580 0.105 0,750 0.411

0.960 0.113 0.640 0.299 0.650 0.043 0.830 0.302

0.750 0.401 0.750 -0.295"* 0.900 0.317

0.870 0.230 0.890 0.549 0.960 0.383

0.930 0.389 0.930 0.169

0.960 0.047 0.960 0.289

CN = 0.434 0.648 0.662 0.668

296
Table E-2. Continued.

Flight 204, Wing sweep = 26", Time = 9-1547-500, MINF = 0.796, Camber = 5/15, ALPT = 6.01, BETA = -0.33, QINF = 270.1,

RNPU = 2.2E+06, CNWP = 0.4391

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.212 0.000 0.678 0.000 1.156"* 0.010 - 1,057

0.060 -0.485 0.020 -0.382 0.020 -0,677 0.020 -0.525**

0.110 -0.654 0.040 -0.345 0.060 -0.306"* 0.060 - 1.098"*

0.200 - 1.086 0.060 -0.685 0.090 -0.793 O. l 10 - 1.24 I

0.230 -0.885 0.090 -0.750 0.110 -0.949 O, 140 - 1.372

0.400 -0.333 0.130 -0,884 0.130 -1.027 0.190 -2,255"*

0.490 -0.324 0.150 - 1.250 0,150 - 1.168 0,250 - 1.235

0.590 -0.523 0.200 - 1.313 0.210 - 1.157 0.400 -0,609

0,630 -0.516 0.250 - 1.188 0.250 - 1.210 0.490 -0.529

0.700 -0.652 0,260 - 1.186 0.340 - 1.123 0.580 -0.601

0.750 -0.788 0.280 - 1.161 0.370 -0.682 0.650 -0,691

0.810 -0.733 0,290 - 1.190 0.400 -0.509 0.700 -0,672

0.840 -0.770 0.310 - 1,152 0.410 -0.547 0.750 -0.745

0.900 -0,627 0.320 -1,098 0.430 -0.434 0.800 -0.758

0.960 -0.669 0.340 - 1.098 0.440 -0.372 0.830 -0,683

0.350 -0.407** 0,460 -0.264 0.900 -0.644

0,370 -0.555 0,490 -0,516 0.960 -0,878"*

0.380 -0522 0.500 -0,481

0.400 -0.630 0,520 -0.736

0.410 -0,440 0.540 -0.471

0.430 -0,427 0.550 -0.757

0.440 -0.398 0.580 -0.738

0,460 -0.397 0.600 -0,794

0.470 -0.442 0.610 -0.449

0.490 -0.460 0.650 -0.044"*

0500 -0.467 0.700 -0.824

0,520 -0.439 0.750 -0,820

0.530 -0.488 0.820 -0.444

0.550 -0.518 0.890 -0.586

0.560 -0.535 0.900 -0.687

0.580 -0.508 0.960 -0.592

0.590 -0.594

0600 -0,590

0,640 -0.798

0,700 -0.754

0.750 0.008**

0,820 -0,700

0.870 -0,509

0.930 -0,4%

0,960 -0.539

Lower Surface

0.020 -0456 0,020 -0.228 0.020 -0.112 0.020 0,100

0.1 I 0 -0.206 0.060 -0.045 0.060 0.018 0.060 0.050

0,230 -0,080 0,090 -0092 0.090 0.039 0.110 -0.115

0,400 -0,070 0.120 -0,071 ** 0.120 -0.485 0.250 -0.038

0.490 -0.040 0.200 -0.075 0.200 0.026 0.400 -0.072

0.630 5.048** 0.260 -0.326 0.250 -0.040 0.490 -0.079

0.750 0.113 0.400 -0.065 0.400 -0.038 0,580 -0,310

0.850 0,193 0.490 0,010 0.490 0.039 0.650 0.126

0,900 0.271 0.580 0.159 0,580 0.063 0.750 0.452

0.960 -0.045 0.640 0,012 0.650 -0.007 0.830 0.391

0.750 0.301 0.750 -0,301 ** 0.900 0,514

0.870 0.138 0.890 0,479 0.960 0.274

0.930 0.276 0.930 0.370

0.960 0.119 0.960 0.207

CN = 0.577 0.740 0.784 0.836

297
Table E-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 9-15-50-500, MINF = 0.797, Camber = 5/15, ALPT = 7.18, BETA = -0.15, QINF = 272.2,

RNPU = 2.2E+06, CNWP = 0.7512

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.299 0.000 0.739 0.000 1.186** 0.010 - 1.047

0.060 -0.646 0.020 -0.681 0.020 -0.588 0.020 - 1.065"*

0.110 -0.634 0.040 -0,442 0.060 -0.367" * 0.060 - 1.106"*

0.200 - 1.078 0.060 -0.799 0.090 -0.961 0.110 - 1.244

0.230 -0.996 0.090 -0.788 0.1 l0 -1.013 0.140 -1.511

0.400 -0.366 0.130 -0.985 0.130 - 1.175 0.190 -2,249"*

0.490 -0.301 0.150 - 1.069 0.150 - 1,268 0.250 - 1.455

0.590 -0.470 0.200 -1.111 0.210 -1.287 0.400 -0.721

0.630 -0.524 0.250 - 1.176 0.250 - 1.267 0.490 -0.507

0.700 -0.514 0.260 - 1.220 0.340 - 1.310 0.580 -0.573

0.750 -0.913 0.280 - 1.272 0.370 - 1.280 0.650 -0.661

0.810 -0.804 0.290 - 1.253 0.400 - 1.257 0.700 -0.643

0.840 -0,841 0.310 - 1.193 0.410 - 1.263 0.750 -0,778

0.900 -0.761 0.320 - 1.206 0.430 - 1.236 0.800 -0,793

0.960 -0.751 0.340 -1.096 0.440 -0.892 0,830 -0.655

0.350 -0.491 ** 0.460 -0.489 0.900 -0.473

0,370 -1.199 0.490 -0.592 0.960 -0.567**

0,380 - 1.256 0.500 -0,576

0.400 - 1.168 0.520 -0,526

0.410 - 1.211 0.540 -0.493

0.430 - 1.135 0.550 -0.360

0.440 -0.802 0.580 -0.454

0.460 -0.638 0.600 -0.563

0.470 -0.536 0.610 -0,509

0.490 -0.465 0.650 0.079**

0.500 -0.428 0.700 -0.656

0.520 -0.397 0.750 -0.668

0.530 -0.365 0.820 -0.458

0.550 -0.361 0.890 -0.519

0.560 -0.366 0.900 -0.578

0.580 -0.306 0.960 -0.500

0.590 -0.439

0.600 -0,440

0.640 -0.466

0_700 -0.571

0.750 0.017"*

0.820 -0.542

0.870 -0,496

0.930 -0.480

0.960 -0.462

Lower Surface

0.020 -0.207 0.020 0.024 0.020 0.095 0.020 0.285

0.110 -0.115 0.060 0.092 0.060 0.223 0.060 -0.074

0.230 0.024 0.090 0.035 0.090 0.175 0.110 -0.016

0.400 -0.016 0.120 0.055" * 0.120 -0.146 0.250 -0.102

0,490 0.013 0.200 0.011 0.200 0.109 0.400 -0.075

0.630 4.999 ** 0.260 -0.013 0.250 0.006 0.490 -0.065

0.750 0.152 0.400 0.009 0.400 -0.011 0.580 -0.029

0.850 0.175 0.490 0.027 0.490 -0.004 0.650 0.178

0.900 0.239 0.580 0.091 0.580 0.059 0.750 0.395

0.960 0.009 0.640 0.303 0,650 0.066 0.830 0.563

0.750 0.329 0.750 -0.310"* 0.900 0.522

0.870 0.528 0.890 0.488 0.960 0.444

0.930 0.427 0.930 0.376

0.960 0.179 0.960 0.206

CN = 0.669 0.875 0.903 0.898

298
Table E-2, Concluded.

Flight 204, Wing sweep = 26 °, Time = 9-15-53-000, MINF = 0.795, Camber = 5/15, ALPT = 7,93, BETA = -0.24, QINF = 271.9,

RNPU = 22E+06. CNWP = 0,6265

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.591 0.000 0.753 0.000 1,161 ** 0,010 - 1.387

0.060 -0.734 0.020 -0,859 0,020 -0.713 0,020 - 1,208"*

0.110 -0.832 0.040 -0.835 0.060 -0.371 ** 0.060 - 1.263"*

0.200 - 1,424 0.060 -0.945 0,090 - 1.1 04 0.110 - 1.402

0,230 - 1.068 0.090 - 1.029 0.110 - 1.249 0.140 - 1.807

0 A00 -0.576 0.130 - 1.103 0.130 - 1.546 0.190 -2.262 * *

0,490 -0.646 0.150 - 1.198 0.150 - 1.372 0,250 - 1.553

0,590 -0,490 0.200 - 1,232 0.210 - 1.391 0.400 -0.92 I

0.630 -0.545 0,250 - 1.610 0,250 - 1.631 0,490 -0.670

0.700 -0.642 0.260 - 1,305 0,340 - 1.655 0,580 -0,636

0.750 - 1.101 0.280 - 1,354 0.370 - 1,397 0,650 -0.701

0.810 -0.918 0.290 - 1.603 0,400 - 1.366 0.700 -0.704

0.840 -0.959 0.310 - 1,300 0.410 - 1.312 0,750 -0.793

0.900 -0.839 0,320 - 1.564 0.430 - 1,380 0.800 -0.679

0,960 -0.840 0,340 -1.254 0.440 -1.377 0.830 -0.635

0,350 -0.515" * 0.460 - 1,113 0.900 -0.719

0.370 - 1,239 0.490 - 1.211 0.960 -0.480"*

0.380 -1.363 0.500 -1.191

0.400 - I. 187 0.520 -0,818

0,410 - 1.251 0.540 -0.709

0.430 - 1.283 0.550 -0.662

0,440 - 1.493 0.580 -0,64 1

0.460 - 1.334 0.600 -0.610

0.470 - 1.295 0.610 -0.577

0.490 - 1,195 0.650 -0.012"*

0.500 -0,825 0.700 -0.590

0.520 -0.957 0.750 -0.675

0.530 -0,583 0.820 -0.386

0.550 -0.477 0.890 -0.448

0,560 -0,507 0.900 -0.448

0.580 -0.446 0,960 -0.425

0.590 -0.453

0.600 -0.435

0640 -0.755

0.700 -0,557

0.750 0.006**

0.820 -0.545

0,870 -0.443

0.930 -0.458

0.960 -0.456

Lower Surface

0,020 -0.114 0.020 0.149 0.020 0.131 0.020 0.375

O. 110 -0.338 0.060 -0.103 0.060 0.208 0.060 0.028

0,230 0.038 0.090 -0,185 0.090 0.210 0.110 0.068

0,400 0,006 0.120 0,077"* 0.120 -0.352 0.250 -0.309

0,490 0,011 0.200 -0.213 0,200 0.137 0,400 -0.013

0,630 4.993"* 0.260 -0.036 0.250 0,084 0,490 -0.019

0.750 0.137 0.400 -0,239 0.400 0.011 0.580 0.004

0.850 -0.018 0,490 0.037 0,490 -0.257 0.650 0.188

0.900 0,232 0,580 0.237 0,580 0.121 0,750 0.390

0.960 -0.271 0.640 0.260 0.650 -0,170 0.830 0.468

0.750 0,073 0,750 -0,321 ** 0.900 0.528

0,870 0.432 0.890 0,491 0.960 0.324

0.930 0.309 0.930 0.382

0.960 0.221 0.960 0.221

CN = 0.750 0.913 0.983 1.003

299
APPENDIX F

Wing Pressure Coefficients for Nominal Dynamic Pressure

of 300 lb/ft 2 and Mach Number of 0.85.

Leading-edge wing sweep is 26 °. Table F-I contains a summary of the data listing in table F-2. The asterisks (*)

in table I=-2 indicate invalid values. Camber is _)LE/TE"Refer to Nomenclature for definitions.

Table F- 1. Summary of data.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

221 14-5-23-500 0.854 0/2 5.93 -0.47 300.0 2.4E+06 0.2288

221 14-5-24-000 0.854 0/2 5.80 0.05 300.0 2.4E+06 0.2409

221 14-4-17-500 0.854 0/2 5.99 -0.18 300.3 2.4E+06 0.2490

221 14-6-39-000 0.845 0/2 8.49 -0.44 290.2 2.3E+06 0.3880

221 14-10-6-500 0.845 0/2 10.13 -0.65 285.6 2.3E+06 0.3091

198 13-47-53-500 0.850 0/2 6.10 0.15 294.6 2.3E+06 0.3599

198 13-48-30-500 0.850 0/2 6.97 -0.01 295.0 2.3E+06 0.4476

198 13-48-42-000 0.855 0/2 8.05 0.15 299.2 2.3E+06 0.5304

198 13-48-48-500 0.857 0/2 8.60 0.47 301.2 2.4E+06 0.5761

198 13-48-54-000 0.857 0/2 9.06 0.26 301.0 2.4E+06 0.5635

198 13-48-56-500 0.855 0/2 9.93 0.23 299.4 2.3E+06 0.4326

198 13-49-9-500 0.853 0/2 10.94 0.65 298.5 2.3E+06 0.3605

198 13-44-5-000 0.864 0/2 7.04 0.47 306.9 2.4E+06 0.4640

198 13-44-36-000 0.844 0/2 8.20 0.31 297.1 2.4E+06 0.5278

198 13-44-48-000 0.839 0/2 8.62 0.26 294.4 2.3E+06 0.5279

198 13-44-56-000 0.846 0/2 9.00 0.10 299.8 2.4E+06 0.5776

198 13-45-6-000 0.847 0/2 10.00 0.07 301.5 2.4E+06 0.4444

221 13-17-25-000 0.852 0/2 5.08 -0.07 297.1 2.3E+06 0.2299

221 13-17-38-500 0.846 0/2 6.04 -0.18 291.6 2.3E+06 0.2906

221 13-17-42-500 0.853 0/2 7.07 -0.27 294.5 2.3E+06 0.3584

221 13-17-49-500 0.858 0/2 7.94 -0.18 296.8 2.3E+06 0.4297

221 13-17-51-500 0.861 0/2 8.68 -0.15 298.8 2.3E+06 0.4668

221 13-17-58-500 0.861 0/2 11.05 -0.33 306.5 2.4E+06 0.2951

221 13-18-1-500 0.854 0/2 12.24 0.60 307.6 2.4E+06 0.2915

221 14-6-7-500 0.855 0/2 5.48 -0.70 300.7 2.4E+06 0.2256

221 14-6-22-500 0.854 0/2 5.99 -0.36 300.3 2.4E+06 0.2446

221 14-6-28-000 0.849 0/2 7.11 -0.27 296.4 2.3E+06 0.3184

191 9-43-28-000 0.847 5/2 6.05 -0.03 289.2 2.3E+06 0.3660

191 9-43-34-500 0.850 5/2 7.07 0.10 292.9 2.3E+06 0.4629

191 9-43-39-000 0.852 5/2 7.95 -0.03 297.4 2.3E+06 0.5531

300
TableF-1.Continued.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

191 9-43-41-000 0.853 5/2 9.02 -0.01 300.3 2.4E+06 0.5452

195 10-44-14-000 0.851 5/2 6.08 0.18 288.6 2.3E+06 0.3727

195 10-44-36-000 0.855 5/2 7.04 0.18 290.3 2.3E+06 0.4688

195 10-45-4-500 0.851 5/2 7.91 -0.08 271.7 2.1E+06 0.5256

195 10-45-22-500 0.861 5/2 8.03 -0.14 286.9 2.2E+06 0.5330

195 10-45-27-500 0.861 5/2 9.21 -0.19 288.6 2.3E+06 0.5588

195 10-45-41-500 0.845 5/2 11.03 -0.06 281.2 2.2E+06 0.3657

195 10-45-49-500 0.847 5/2 12.01 0.02 294.4 2.3E+06 0.3023

200 8-25-10-500 0.857 5/2 12.20 0.25 309.8 2.4E+06 0.3799

216 10-44-12-000 0.850 5/2 3.99 -0.12 291.7 2.3E+06 0.2739

216 10-43-40-000 0.845 5/2 5.05 0.02 297.2 2.4E+06 0.3051

216 10-47-48-000 0.852 5/6 4.07 -0.04 304.1 2.4E+06 0.2578

195 10-47-55-500 0.840 5/6 5.04 0.10 287.3 2.3E+06 0.3877

195 10-48-15-500 0.845 5/6 7. I0 -0.24 287.1 2.3E+06 0.5438

195 10-48-31-500 0.847 5/6 8.17 0.52 278.1 2.2E+06 0.6261

195 10-49-27-500 0.855 5/6 8.02 0.05 290.0 2.3E+06 0.5841

195 10-49-47-000 0.860 5/6 11.79 0.15 305.2 2.4E+06 0.4523

195 10-49-52-500 0.852 5/6 11.09 -0.27 304.9 2.4E+06 0.4524

191 9-46-5-000 0.850 5/6 4.95 -0.16 286.4 2.3E+06 0.4005

191 9-46-15-500 0.852 5/6 7.04 -0.16 290.9 2.3E+06 0.5409

198 13-51-33-500 0.858 5/10 3.98 0.28 299.9 2.3E+06 0.3573

198 13-51-51-500 0.856 5/10 5.04 0.21 298.1 2.3E+06 0.4900

198 13-52-32-500 0.856 5/10 5.96 0.02 297.6 2.3E+06 0.4975

198 13-52-35-500 0.856 5/10 7.04 0.05 297.4 2.3E+06 0.5942

198 13-53-4-000 0.847 5/10 7.97 0.10 293.2 2.3E+06 0.6637

198 13-53-6-000 0.850 5/10 8.01 0.26 295.9 2.3E+06 0.6712

198 13-53-7-000 0.851 5/10 8.18 0.23 297.0 2.3E+06 0.6959

198 13-53-17-000 0.846 5/10 10.07 0.39 299.6 2.4E+06 0.7388

198 13-53-18-500 0.845 5/10 9.96 0.28 300.2 2.4E+06 0.7215

225 11-54-45-000 0.852 5/10 4.01 -0.44 296.8 2.3E+06 0.2698

225 11-55-6-500 0.848 5/11 5.03 -0.67 291.2 2.3E+06 0.3505

225 11-55-20-500 0.852 5/10 7.94 -0.15 296.1 2.3E+06 0.5658

225 11-55-22-000 0.854 5/10 7.95 -0.15 299.3 2.4E+06 0.5851

225 11-48-47-500 0.855 10/2 5.08 -0.04 299.0 2.3E+06 0.3061

225 11-49-11-500 0.857 10/2 5.99 -0.30 299.3 2.3E+06 0.3632

225 11-49-15-000 0.856 10/2 7.10 -0.56 297.6 2.3E+06 0.4462

225 11-49-22-500 0.842 10/2 8.03 -0.21 285.9 2.3E+06 0.4587

301
TableF-1.Concluded.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

225 11-49-26-500 0.845 10/2 8.07 -0.10 287.6 2.3E+06 0.4815

225 11-49-33-000 0.851 10/2 9.05 -0.10 295.0 2.3E+06 0.4381

225 11-51-4-500 0.853 10/2 9.10 -0.62 296.4 2.3E+06 0.4796

225 11-51-10-000 0.847 10/2 11.03 -0.41 292.0 2.3E+06 0.2847

225 11-51-17-500 0.844 10/2 12.22 0.17 301.6 2.4E+06 0.2170

216 10-50-51-000 0.853 10/2 6.04 -0.27 303.7 2.4E+06 0.3840

216 10-52-32-500 0.851 5/10 4.00 -0.18 301.0 2.4E+06 0.2904

216 10-53-13-500 0.849 5/10 4.01 -0.27 299.9 2.4E+06 0.2939

216 10-54-30-500 0.851 10/10 4.03 -0.01 301.2 2.4E+06 0.3363

216 10-54-43-000 0.850 10/10 4.08 -0.44 301.1 2.4E+06 0.3311

215 10-5-45-500 0.850 10/15 4.03 -0.33 255.6 2.0E+06 0.2065

302
Table F-2. Listing of data.

Flight 221, Wing sweep = 26 °, Time = 14-5-23-500, MINF = 0.854, Camber = 0/2. ALPT = 5.93, BETA = -0.47, QINF = 300.0,

RNPU = 2.4E+06, CNWP = 0.2288

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/r.- CP x/c CP

0.020 -0.665 0.000 0.840 0.000 1.093"* 0.010 -0.955

0.060 -0.626 0.020 -0_853 0.020 -0.768 0.020 -0.997

0.1 l0 -0.587 0,040 -0.684 0,060 -3,183** 0,060 -0,951

0,200 -0.320 0.060 -0.792 0,090 -0.824 0.110 -0.902

0,230 -0,486 0.090 -0.745 0,110 -0.840 0.140 -0.935

0.400 -0.223 0.130 -0.744 0.130 -0.748 0.190 - 1.957"*

0,499 -0,195 0.150 -0.757 0.150 -0.793 0,250 -0.940

0,590 -0.270 0,200 -0.640 0.210 -0.749 0.400 -0.727

0.630 -0.250 0,250 -0.748 0.250 -0.777 0490 -0,382

0.700 -0,178 0,260 -0.703 0.340 -0.787 0.580 -0,315

0.750 -0.266 0.280 -0,734 0.370 -0.782 0.650 -0,335

0.810 -0,275 0.290 -0.728 0.400 -0.834 0.700 -0.334

0.840 -0.224 0,310 -0,751 0.410 2,556"* 0,750 -0.393

0.900 -0.125 0.320 -0,739 0.430 -0,795 0.800 -0,371

0.960 -0,047 0,340 -0.703 0,440 -0,623 0.830 -0.274

0.350 -0.435** 0.460 -0,389 0.900 -0.128

0.370 -0.707 0.490 -0.187 0,960 0.008

0.380 -0.760 0.500 -0,240

0.400 -0.610 0.520 -0,171

0.410 -0,386 0,540 -0.163

0.430 -0.221 0.550 -0,185

0.440 -0.120 0,580 -0.208

0.460 -0.176 0_600 -0,180

0.470 -0.113 0,610 -0.207

0.490 -0.133 0_650 0.679**

0.500 -0.149 0,700 -0,371

0,520 -0.178 0.750 -0.407

0,530 -0.167 0.820 -0,323

0,550 -0.226 0.890 -0.089

0.560 -0.175 0.900 -0.077

0.580 -0,212 0.960 0.057

0.590 -0,263

0.600 -0.300

0.640 -0.345

0.700 -0.320

0,750 -0,032**

0,820 -0.256

0.870 -0,220

0.930 -0.088

0.960 -0.027

Lower Surface

0,020 -0.226 0.020 -0.006 0,020 0.085 0.020 0,422

0.110 -0.239 0.060 0.008 0.060 0.102 0,060 1,071 **

0.230 -0.073 0,090 -0.065 0.090 1.016"* 0.110 -0.044

0.400 -0.056 0. 120 -0,122 0.120 -0.327 0.250 -0.224

0.490 -0.074 0.200 -0,128 0.200 -0.200 0,400 -0.224

0.630 1,760"* 0.260 -0.228 0.250 -0.199 0.490 -0.317

0.750 0.030 0.400 -0.158 0.400 -0.187 0.580 -0.2%

0.850 0.116 0,490 -0.173 0,490 -0,051 0.650 -0,141

0.900 0,192 0.580 -0.149 0.580 -0.212 0.750 0.102

0.960 0.164 0,640 0.045 0.650 -0,044 0.830 0.282

0,750 0.173 0,750 -0.051 0.900 0,319

0.870 0,213 0.890 0.266 0,960 0.258

0.930 0.209 0.930 0,237

0.960 0.181 0.960 -2.060 **

CN = 0.254 0.394 0.382 0.477

303
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 14-5-24-000, MINF = 0.854, Camber = 0/2, ALPT = 5.80, BETA = 0.05, QINF = 300.0,

RNPU = 2.4E+06, CNWP = 0.2409

1"t= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x.,/c CP x./c CP x/c CP

0.020 -0.657 0.000 0.836 0.000 0.890** 0.010 -0.955

0.060 -0.641 0.020 -0.853 0.020 -0.768 0.020 -0.976

0.110 -0.495 0.040 -0.680 0.060 -2.988" * 0.060 -0.909

0.200 -0.320 0.060 -0.792 0.090 -0.834 0.110 -0.902

0.230 -0.449 0.090 -0.745 0.110 -0.849 0.140 -0.935

0.400 -0.223 0.130 -0.759 0.130 -0.748 0.190 -1.957"*

0.490 -0.199 0.150 -0.761 0.150 -0.793 0.250 -0.940

0.590 -0.273 0.200 -0.640 0.210 -0.749 0.400 -0.713

0.630 -0.261 0.250 -0.763 0.250 -0.785 0.490 -0.382

0.700 -0.178 0.260 -0.703 0.340 -0.787 0.580 -0.315

0.750 -0.266 0.280 -0.734 0.370 -0.790 0.650 -0.325

0.810 -0.282 0.290 -0.743 0.400 -0.834 0.700 -0.329

0.840 -0.239 0.310 -0.751 0.410 2.556"* 0.750 -0.397

0.900 -0.135 0.320 -0.739 0.430 -0.795 0.800 -0.368

0.960 -0.047 0.340 -0.703 0.440 -0.613 0.830 -0.279

0.350 -0.435"* 0.460 -0.378 0.900 -0.143

0.370 -0.711 0.490 -0.172 0.960 0.008

0.380 -0.764 0.500 -0.240

0.400 -0.610 0.520 -0.180

0.410 -0.373 0.540 -0.178

0.430 -0.209 0.550 -0.185

0.440 -0.132 0.580 -0.208

0.460 -0.176 0.600 -0.174

0.470 -0.126 0.610 -0.207

0.490 -0.129 0.650 0.625"*

0.500 -0.149 0.700 -0.397

0.520 -0.186 0.750 -0.415

0.530 -0.163 0.820 -0.328

0.550 -0.226 0.890 -0.103

0.560 -0.200 0.900 -0.077

0.580 -0.212 0.960 0.057

0.590 -0.263

0.600 -0.261

0.640 -0.349

0.700 -0.320

0.750 -0.032**

0.820 -0.256

0.870 -0.224

0.930 -0.092

0.960 -0.034

Lower Surface

0.020 -0.236 0.020 -0.003 0.020 0.077 0.020 0.422

0.110 -0.239 0.060 0.011 0.060 0.089 0.060 1.071 **

0.230 -0.073 0.090 -0.065 0.090 1.016** 0.110 -0.044

0.400 -0.056 0.120 -0.100 0.120 -0.319 0.250 -0.218

0.490 -0.081 0.200 -0.125 0.200 -0.200 0.400 -0.239

0.630 1.760** 0.260 -0.243 0.250 -0.195 0.490 -0.317

0.750 0.018 0.400 -0.158 0.400 -0.187 0.580 -0.296

0.850 0.116 0.490 -0.173 0.490 -0.059 0.650 -0.141

0.900 0.192 0.580 -0.141 0.580 -0.212 0,750 0.102

0.960 0.160 0.640 0.041 0.650 -0.052 0.830 0.282

0.750 0.178 0.750 -0.051 0.900 0.316

0.870 0.231 0.890 0.266 0.960 0.258

0.930 0.205 0.930 0.237

0.960 0.177 0.960 -2.004**

CN = 0.244 0.398 0.386 0.472

304
Table F-2. Continued.

Flight 22l, Wing sweep = 26 °, Time = 14-4-17-500, MINF = 0.854, Camber = 0/2, ALPT = 5.99, BETA = -0.18, QINF = 300.3,

RNPU = 2.4E+06, CNWP = 0.2490

r 1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.701 0.000 0.825 0.000 0.865"* 0.010 -0.964

0,060 -0.667 0.020 -0.898 0.020 -0,780 0.020 -0.964

0.110 -0.518 0.040 -0.701 0.060 -2,927** 0.060 - 1.001

0.200 -0.384 0.060 -0.811 0.090 -0,849 0.110 -0.910

0.230 -0.383 0.090 -0.773 0.110 -0.864 0.140 -0.941

0.400 -0.205 0.130 -0.780 0.130 -0.772 0.190 - 1.959 **

0.490 -0.159 0.150 -0.786 0.150 -0.781 0.250 -0.971

0.590 -0.270 0.200 -0.669 0.210 -0.765 0.400 -0.736

0.630 -0.247 0,250 -0,783 0.250 -0.802 0,490 -0.455

0.700 -0.178 0.260 -0.726 0.340 -0.820 0.580 -0.325

0.750 -0.266 0.280 -0.757 0.370 -0.810 0,650 -0.324

0.8 |0 -0.271 0,290 -0.757 0.400 -0.837 0.700 -0.317

0.840 -0.213 0.310 -0.768 0.410 2.550 * * 0.750 -0.375

0.900 -0.117 0.320 -0.754 0.430 -0.813 0,800 -0.343

0.960 -0.050 0.340 -0.741 0.440 -0,777 0,830 -0.272

0.350 -0.418"* 0.460 -0.770 0.900 -0.131

0,370 -0,740 0.490 -0.221 0,960 0.018

0,380 -0.789 0.500 -0.294

0.400 -0.686 0.520 -0.211

0.410 -0.751 0.540 -0.194

0.430 -0.406 0.550 -0,186

0.440 -0.227 0.580 -0.180

0.460 -0.224 0.600 -0.163

0.470 -0.134 0.6 l0 -0.183

0.490 -0.122 0.650 0.635"*

0.500 -0.132 0.700 -0.316

0.520 -0.136 0.750 -0.385

0.530 -0. 134 0.820 -0.304

0.550 -0.187 0.890 -0.097

0.560 -0.177 0.900 -0.072

0.580 -0.174 0.960 0.057

0.590 -0.226

0.600 -0.259

0.640 -0.31 I

0.700 -0.305

0.750 -0.017"*

0.820 -0.252

0.870 -0.224

0.930 -0.092

0.960 -0.023

Lower Surface

0.020 -0.195 0.020 -0,002 0.020 0.112 0.020 0.445

0.110 -0.228 0.060 0,030 0.060 0.145 0,060 1.073**

0.230 -0.070 0.090 -0.051 0.090 1.011 ** 0.110 -0.033

0.400 -0.038 0.120 -0.1 04 0.120 -0.308 0.250 -0.207

0.490 -0.070 0.200 -0.117 0.200 -0.182 0.400 -0.228

0.630 1.754"* 0.260 -0.232 0.250 -0.184 0.490 -0.306

0,750 0.014 0,400 -0.158 0.400 -0.176 0.580 -0.300

0.850 0.119 0.490 -0.170 0,490 -0.048 0.650 -0.137

0.900 0.192 0.580 -0.142 0.580 -0.208 0.750 0.103

0.960 0. | 59 0.640 0.048 0.650 -0.041 0.830 0.284

0.750 0.176 0.750 -0,040 0.900 0.320

0.870 0.224 0,890 0.269 0.960 0.257

0.930 0.212 0.930 0.241

0.960 0.177 0.960 - 1.959"*

CN = 0.240 0.415 0.407 0.493

305
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 14-6-39-000, MINF = 0.845, Camber = 0/2, ALPT = 8.49, BETA = -0.44, QINF = 290.2,

RNPU = 2.3E+06, CNWP = 0.3880

/'1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.993 0.000 0.689 0.000 0.821 ** 0.010 - 1.239

0.060 - 1.018 0.020 - 1.246 0.020 - 1.059 0.020 - 1.28 l

0.110 -0.953 0.040 - 1.000 0.060 -3.194 ** 0.060 - 1.273

0.200 -0.775 0.060 -1.098 0.090 -1.108 0.110 -1.213

0.230 -0.747 0.090 -1.083 0.110 -1.141 0.140 -1.253

0.400 -0.774 0.130 - 1.078 0.130 - 1,043 0.190 -2.000"*

0.490 -0.228 0.150 -1.073 0.150 -1.115 0.250 -1.241

0.590 -0.208 0.200 -0.973 0.2 l0 -1.019 0.400 -0.879

0.630 -0,223 0.250 - 1.056 0.250 - 1.064 0.490 -0.794

0.700 -0.176 0.260 -0.970 0.340 - 1.085 0.580 -0.738

0.750 -0.288 0.280 - 1.021 0.370 - 1.061 0.650 -0.564

0.810 -0.328 0.290 - 1.005 0.400 - 1.098 0.700 -0.513

0.840 -0.278 0.310 - 1.036 0.410 2.666"* 0.750 -0.308

0.900 -0.205 0.320 - 1.006 0.430 - 1.078 0. 800 -0,250

0.960 -0.120 0.340 -0.995 0.440 - 1.037 0.830 -0.138

0.350 -0.514** 0.460 - 1.075 0.900 -0.059

0.370 -0.999 0.490 - 1.019 0.960 -0.019

0.380 -1.065 0.500 -1.104

0.400 -0.925 0.520 - 1.033

0.410 -1.015 0.540 -1.046

0.430 -0.982 0.550 - 1.080

0.440 -0.953 0.580 -0.743

0.460 - 1.055 0.600 -0.517

0.470 -0.970 0.610 -0.455

0.490 - 1.028 0.650 0.647"*

0.500 - 1.031 0.700 -0.361

0.520 - 1.019 0.750 -0.401

0.530 -0.810 0.820 -0.124

0.550 -0.576 0.890 -0.037

0.560 -0,461 0.900 -0.028

0.580 -0.446 0.960 0.070

0.590 -0.432

0.600 -0.403

0.640 -0.210

0.700 -0.178

0.750 -0.010"*

0.820 -0.143

0.870 -0.144

0.930 -0.049

0.960 -0.004

Lower Surface

0.020 0.000 0.020 0.287 0.020 0.369 0.020 0.662

0.110 -0.100 0.060 0.210 0.060 0.276 0.060 1.130"*

0.230 -0.021 0.090 0.107 0.090 1.196** 0.110 0.124

0.400 -0.058 0.120 0.044 0.120 -0.147 0.250 -0.066

0.490 -0.084 0.200 -0.004 0.200 -0.030 0.400 -0.103

0.630 1.843"* 0.260 -0.124 0.250 -0.043 0.490 -0.196

0.750 -0.013 0.400 -0.074 0.400 -0.078 0.580 -0.225

0.850 0.076 0.490 -0.097 0.490 -0.022 0.650 -0.099

0.900 0.160 0.580 -0.122 0.580 -0.143 0.750 0.119

0.960 0.125 0.640 0.062 0.650 -0.038 0.830 0.297

0.750 0.168 0.750 -0.026 0.900 0.325

0.870 0.258 0.890 0.269 0.960 0.226

0.930 0.198 0.930 0.238

0.960 0.153 0.960 -2,081 **

CN = 0.450 0.674 0.683 0.749

306
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 14-10-6-500, MINF = 0.845, Camber = 0/2, ALPT = 10.13, BETA = -0.65, QINF = 285.6,

RNPU = 2.3E+06, CNWP = 0.3091

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x,/c CP

0.020 - 1.158 0.000 0,567 0.000 0.674"* 0.010 - 1.373

0.060 - 1.151 0.020 - 1.448 0.020 - 1.225 0.020 - 1.394

0.110 -0.979 0.040 - 1.174 0.060 -3.458" * 0.060 - 1.412

0.200 -0.946 0.060 - 1.213 0.090 - 1.245 0.110 - 1.355

0.230 -0,874 0,090 - 1.211 O. 110 - 1.261 O. 140 - 1.350

0.400 -0.730 O. 130 - 1.197 O.130 - 1.157 O. 190 -2.000 **

0.490 -0.149 O. 150 - 1.186 0.150 - 1.231 0.250 - 1.320

0.590 -0.266 0.200 -1.106 0.210 -1.151 0.400 -0.972

0.630 -0.274 0,250 -1.163 0.250 -1.163 0.490 -0,811

0.700 -0.201 0.260 - 1.070 0.340 -0.675 0.580 -0,569

0.750 -0.299 0.280 - 1.039 0.370 -0.640 0.650 -0.391

0.810 -0.339 0.290 -0.938 0.400 -0.688 0.700 -0.385

0.840 -0.308 0.310 -0.888 0,410 -3.045 * * 0.750 -0.365

0.900 -0.233 0.320 -0.891 0.430 -0.628 0.800 -0.303

0.960 -0.151 0,340 -0.794 0.440 -0.586 0.830 -0.282

0.350 -0.415"* 0.460 -0.616 0.900 -0.191

0.370 -0.695 0.490 -0.528 0.960 -0.094

0.380 -0.720 0.500 -0.610

0.400 -0.581 0.520 -0.570

0.410 -0.630 0.540 -0.561

0.430 -0.595 0.550 -0.581

0.440 -0.529 0,580 -0.589

0.460 -0.609 0.600 -0.512

0.470 -0.528 0.610 -0.489

0.490 -0.535 0.650 0563"*

0.500 -0.526 0.700 -0.496

0,520 -0.537 0.750 -0.580

0.530 -0.483 0.820 -0.367

0.550 -0.526 0.890 -0.285

0.560 -0432 0.900 -0.329

0.580 -0.471 0.960 -0.222

0.590 -0.461

0.600 -0.460

0.640 -0.348

0,700 -0.334

0.750 -0.020"*

0.820 -0.211

0,870 -0.202

0.930 -0.215

0,960 -0.203

Lower Surface

0.020 O.113 0.020 0.401 0.020 0.491 0.020 0,72 I

O, 110 -0.052 0.060 0.293 0.060 0.354 0.060 I. 150"*

0.230 0.008 0.090 0.171 0.090 1.249"* 0.110 0.212

0.400 -0,049 0.120 0.112 0.120 -0.103 0,250 -0.004

0.490 -0.076 0.200 0.066 0.200 0.024 0.400 -0.050

0.630 2.046"* 0.260 -0.071 0.250 0.019 0.490 -0.159

0,750 -0.032 0.400 -0.061 0.400 -0.046 0.580 -0.196

0.850 0.054 0.490 -0.117 0.490 -0.036 0.650 -0.107

0.900 0.133 0.580 -0.131 0.580 -0.151 0.750 0.103

0.960 0.098 0.640 0.029 0.650 -0,036 0.830 0.277

0.750 0.138 0.750 -0.021 0.900 0.300

0.870 0.162 0.890 0.199 0.960 0.198

0.930 0.123 0.930 0.143

0.960 0.065 0.960 -2.193"*

CN = 0.489 0.668 0.678 0.818

307
Table F-2, Continued.

Flight 198, Wing sweep = 26", Time = 13-47-53-500, MINF = 0.850, Camber -- 0/2, ALPT = 6.10, BETA = 0.15, QINF = 294.6,

RNPU = 2.3E+06, CNWP = 0.3599

rl = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.640 0.000 0.897 0.000 -5.744* * 0.010 -0.943 **

0.060 -0.666 0.020 -0.866"* 0.020 -0.750"* 0.020 -0.967"*

0.110 -0.606 0.040 -0.657 0.060 - 1.422" * 0.060 - 1.004

0.200 -0.306 0.060 -0.765 0.090 -0.826 0.110 -0.871

0.230 -0.448 0,090 -0.721 0.110 -0.866 0.140 1.917 **

0.400 -0.195 0.130 -0.757 0.130 -0.790 0.190 -5.609**

0.490 -0.210 0.150 -0,732 0.150 -0.735 0.250 -0.918

0.590 -0.237 0.200 -0.616 0.210 -0.812 0.400 -0.685

0.630 -0.255 0.250 -0.755 0.250 -0.809 0.490 -0.306

0.700 -0.216 0.260 -0.708 0.340 -0.837 0.580 -0.282

0.750 -0.218 0.280 -0.760 0.370 -0.825 0.650 -0.360

0.810 -0,246 0.290 -0,772 0.400 -0.834 0.700 -0.327

0.840 -0.206 0.310 -0.719 0.410 -0.763 0.750 -0.386

0.900 -0.101 0.320 -0.707 0.430 -0.505 0.800 -0.354

0.960 0.003 0.340 -0.753 0.440 -0.313 0.830 -0.298

0.350 -0.348** 0.460 -0.242 0.900 -0.129

0.370 -0.725 0.490 -0.159 0.960 0.049

0.380 -0.522 0.500 -0.169

0.400 -0.198 0.520 -0.165

0.410 -0.181 0.540 -0.169

0,430 -0.125 0.550 -0.177

0,440 -0.082 0.580 -0.172

0.460 -0.151 0.600 -0.207

0.470 -0.130 0.610 -0.151

0,490 -0.141 0.650 -2.835"*

0.500 -0.143 0,700 -0.436

0.520 -0.162 0,750 -0.352

0.530 -0.171 0.820 -0.309

0.550 -0.201 0.890 -0.081

0.560 -0.206 0.900 -0.051

0.580 -0.192 0.960 0.053

0.590 -0.242

0.600 -0.287

0.640 -2.670**

0.700 -0.312

0.750 -0.287

0.820 -2.847**

0.870 -0.188

0.930 -0.055

0.960 0.016

Lower Surface

0.020 -0.056 0.020 0.014 0.020 0.131 0.020 0.479

0.110 -0.199 0,060 0.076 0.060 0.166 0.060 3.240**

0.230 -0.057 0,090 -0.013 0.090 0.042 0.110 -0.021

0.400 -0.065 0.120 -0.085 0,120 -0.311 0.250 -0.170

0.490 -0.095 0.200 -0.058 0.200 -0.149 0.400 -0.190

0.630 3.284** 0.260 -0.187 0.250 -0.155 0.490 -0.264

0.750 0.038 0.400 -2.865"* 0.400 -0.160 0.580 -0.285

0.850 0.130 0.490 -0.133 0.490 0.004 0.650 -0.084

0.900 0.182 0.580 -0.074 0.580 -0.184 0.750 0.174

0.960 0.166 0.640 0.281 0.650 0.029 0.830 0.310

0.750 0.172 0.750 0.274 0.900 0.385

0.870 0.245 0.890 ******** 0.960 0.304

0.930 0.240 0.930 0.290

0.960 0.172 0.960 -2.864 * *

CN = 0.245 0,407 0.460 0.459

308
Table F-2. Continued.

Flight 198, Wing sweep = 26 °. Time = 13-48-30-500, MINF = 0,850, Camber = 0/2, ALPT = 6.97, BETA = -0.01, QINF = 295.0,

RNPU = 2.3E+06. CNWP = 0.4476

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.754 0.000 0.868 0.000 -5.737** 0.010 - 1.051 **

0.060 -0,799 0.020 - 1.000"* 0,020 -0.853** 0.020 - 1.054"*

0.110 -0.747 0.040 -0.724 0.060 - 1.538"* 0,060 - 1.102

0.200 -0.624 0.060 -0,845 0.090 -0.913 0.110 -0,973

0.230 -0.508 0.090 -0.860 0.110 -0.986 0.140 1.898**

0.400 -0.160 0.130 -0.878 0.130 -0,927 0.190 -5.603 * *

0.490 -0.172 0.150 -0.863 0.150 -0.855 0.250 -0.992

0.590 -0.205 0.200 -0.763 0.210 -0.919 0.400 -0.750

0,630 -0.238 0.250 -0.876 0.250 -0,907 0,490 -0.655

0,700 -0.212 0.260 -0.814 0.340 -0.948 0.580 -0.487

0.750 -0.225 0.280 -0.871 0.370 -0.931 0.650 -0.336

0.810 -0,257 0.290 -0.883 0.400 -0.932 0.700 -0.298

0.840 -0.224 0.310 -0.824 0.410 -0.883 0.750 -0.314

0.900 -0.128 0.320 -0.818 0.430 -0.944 0.800 -0.276

0.960 -0.036 0.340 -0.861 0.440 -0.918 0.830 -0.244

0.350 -0.381 ** 0.460 -0.922 0.900 -0.066

0.370 -0,830 0.490 -0.853 0.960 0.058

0.380 -0.851 0.500 -0.942

0,400 -0.775 0,520 -0,852

0.410 -0,870 0.540 -0.525

0.430 -0.851 0.550 -0.381

0.440 -0,805 0.580 -0.282

0,460 -0.887 0,600 -0.241

0.470 -0.865 0.610 -0.11 t

0.490 -0.504 0.650 -2.833 **

0.500 -0.315 0.700 -0.187

0.520 -0.243 0.750 -0.238

0.530 -0.163 0.820 -0.231

0.550 -0.131 0.890 -0.064

0.560 -0.101 0.900 -0.038

0.580 -0.081 0.960 0.043

0.590 -0.106

0.600 -0.132

0.640 -2.669"*

0.700 -0.203

0.750 -0.230

0.820 -2.846"*

0.870 -0,177

0.930 -0.050

0,960 0.024

Lower Surface

0.020 -0.010 0.020 0.145 0.020 0.239 0.020 0.562

0,110 -0.154 0.060 0.148 0.060 0.244 0.060 3.232"*

0.230 -0,048 0.090 0.056 0.090 0.115 0.110 0.039

0.400 -0.064 0.120 0.010 0.120 -0.252 0.250 -0.115

0.490 -0.075 0.200 -0.009 0.200 -0.055 0.400 -0.141

0.630 3.276** 0.260 -0.138 0.250 -0.094 0.490 -0.221

0.750 0,035 0.400 -2.863"* 0.400 -0.122 0.580 -0.257

0.850 0.115 0.490 -0.121 0.490 0.017 0.650 -0.079

0.900 0.173 0.580 -0.062 0.580 -0.164 0.750 0.181

0.960 0.150 0.640 0.287 0.650 0.040 0.830 0.316

0.750 0.169 0.750 0.286 0.900 0.390

0,870 0.251 0.890 ******** 0.960 0.304

0.930 0.252 0,930 0.290

0.960 0.173 0.960 -2.862 * *

CN = 0.285 0.520 0,585 0.552

309
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-48-42-000, MINF = 0.855, Camber = 0/2, ALPT = 8.05, BETA = 0.15, QINF = 299.2,

RNPU = 2.3E+06, CNWP = 0.5304

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.820 0.000 0.829 0.000 -5.662** 0.010 -1.090**

0.060 -0.906 0.020 -1.031 ** 0.020 -0.922"* 0.020 - 1.149"*

0.110 -0.828 0.040 -0.838 0.060 - 1.475 * * 0.060 - 1.161

0.200 -0.735 0.060 -0.931 0.090 -0.995 0.110 - 1.068

0.230 -0.612 0.090 -0.934 0.110 -1.043 0.140 1.889"*

0.400 -0.677 0.130 -0.934 0.130 -0.989 0.190 -5.530**

0.490 -0.357 0.150 -0.929 0.150 -0.933 0.250 - 1.097

0.590 -0.169 0.200 -0.847 0.210 -0.990 0.400 -0.805

0.630 -0.205 0.250 -0.932 0.250 -0.964 0.490 -0.749

0.700 -0.187 0.260 -0.888 0.340 - 1.041 0.580 -0.643

0.750 -0.227 0.280 -0.938 0.370 - 1.002 0.650 -0.604

0.810 -0.266 0.290 -0.960 0.400 -0.996 0.700 -0.659

0.840 -0.240 0.310 -0.897 0.410 -0.978 0.750 -0.505

0.900 -0.153 0.320 -0.888 0.430 - 1.029 0.800 -0.206

0.960 -0.061 0.340 -0.944 0.440 -0.999 0.830 -0.143

0.350 -0.392 ** 0.460 - 1.009 0.900 -0.009

0.370 -0.902 0.490 -0.934 0.960 0.034

0.380 -0.914 0.500 - 1.020

0.400 -0.852 0.520 - 1.003

0.410 -0.935 0.540 - 1.010

0.430 -0.936 0.550 -0.973

0.440 -0.863 0.580 -0.935

0.460 -0.985 0.600 -0.955

0.470 -0.960 0.610 -0.900

0.490 -0.912 0.650 -2.798"*

0.500 -0.913 0.700 -0.329

0.520 -0.902 0.750 -0.303

0.530 -0.889 0.820 -0.1 04

0.550 -0.906 0.890 0.009

0.560 -0.933 0.900 0.006

0.580 -0.737 0.960 0.082

0.590 -0.499

0.600 -0.417

0.640 -2.636**

0.700 -0.139

0.750 -0.094

0.820 -2.811"*

0.870 -0.110

0.930 -0.010

0.960 0.045

Lower Surface

0.020 0.058 0.020 0.251 0.020 0.324 0.020 0.648

0.110 -0.108 0.060 0.219 0.060 0.304 0.060 3.183"*

0.230 -0.030 0.090 0.119 0.090 0.181 0.110 0.089

0.400 -0.064 0.120 0.043 0.120 -0.186 0.250 -0.075

0.490 -0.086 0.200 0.030 0.200 0.003 0.400 -0.114

0.630 3.226** 0.260 -0.097 0.250 -0.042 0.490 -0.192

0.750 0.049 0.400 -2.828** 0.400 -0.079 0.580 -0.233

0.850 0.112 0.490 -0.101 0.490 0.034 0.650 -0.068

0.900 0.162 0.580 -0.047 0.580 -0.152 0.750 0.189

0.960 0.142 0.640 0.294 0.650 0.050 0.830 0.326

0.750 0.185 0.750 0.292 0.900 0.398

0.870 0.276 0.890 ******** 0.960 0.283

0.930 0.247 0.930 0.296

0.960 0.181 0.960 -2.827**

CN = 0.412 0.642 0.731 0.663

310
Table F-2 Continued.

Flight 198, Wing sweep = 26 °, Time = 13-48-48-500, MINF = 0.857, Camber = 0/2, ALPT = 8.60, BETA = 0.47, QINF = 301.2,

RNPU = 2AE+06, CNWP = 0.5761

rI= 0.93 0.76 0.59 0A0

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.865 0.000 0.803 0.000 -5.628** 0.010 - 1,150**

0.060 -0.949 0.020 - 1.100"* 0.020 -0.958"* 0,020 - 1.152"*

OA 10 -0,906 0.040 -0.885 0.060 -1.582"* 0.060 -1.199

0.200 -0,785 0.060 -0,944 0,090 - 1.034 0.110 - 1,104

0.230 -0,676 0.090 -0.966 0.110 - 1.093 0.140 1.854" *

0.400 -0,729 0,130 -0.965 0.130 - 1.034 0.190 -5,496 **

0.490 -0.667 0.150 -0.970 0.150 -0.981 0.250 - 1.150

0.590 -0.141 0.200 -0.884 0.210 - 1.035 0,400 -0.838

0.630 -0.196 0.250 -0.994 0.250 - 1.012 0.490 -0,776

0.700 -0.175 0.260 -0,913 0.340 - 1.084 0.580 -0.681

0.750 -0,218 0,280 -0,989 0.370 - 1.062 0.650 -0.633

0.810 -0,268 0.290 - 1,002 0,400 - 1,037 0,700 -0.675

0.840 -0.235 0,310 -0,935 0,410 -1.018 0,750 -0,520

0.900 -0.166 0.320 -0,929 0.430 - 1,087 0.800 -0.215

0.960 -0.072 0.340 -0.987 0.440 - 1,038 0,830 -0,140

0.350 -0.403** 0.460 - 1.052 0900 -0,040

0,370 -0,947 0,490 -0,968 0.960 0,006

0,380 -0.956 0.500 - 1.070

0.400 -0,882 0.520 - 1.052

0.410 -0.977 0,540 - 1.062

0.430 -0.969 0.550 - 1.032

0.440 -0.900 0.580 - 1.002

0.460 - 1.044 0.600 - 1.013

0.470 -0.977 0.610 -0.952

0.490 -0.952 0.650 -2.783**

0.500 -0,953 0,700 -0.377

0.520 -0.945 0,750 -0.394

0.530 -0.928 0.820 -0.191

0.550 -0.956 0890 -0.011

0.560 -0.961 0.900 -0,015

0.580 -0.677 0.960 0,04 1

0.590 -0.524

0,600 -0.471

0,640 -2.623**

0,700 -0,258

0.75O -0,101

0.820 -2,796**

0.870 -0,088

0.930 -0.006

0.960 0.034

Lower Surface

0.020 0.132 0.020 0.298 0,020 0.365 0.020 0,703

O. 110 -0.091 0.060 0.251 0.060 0.344 0.060 3.158**

0.230 -0.030 0.090 0.149 0.090 0.215 0.110 0.146

0.400 -0.086 O. 120 0.065 O. 120 -0.167 0.250 -0.030

0.490 -0.089 0.200 0.048 0.200 0.020 0.400 -0.095

0.630 3.201 ** 0.260 -0.078 0.250 -0.023 0.490 -0.180

0.750 0.018 0.400 -2.813 * * 0.400 -0.072 0.580 -0.235

0.850 0,100 0.490 -0.101 0.490 0.030 0.650 -0,064

0.900 0,149 0.580 -0.058 0.580 -0.154 0,750 0,169

0,960 0,137 0.640 0.282 0.650 0.031 0.830 0.320

0.750 0.163 0.750 0.279 0,900 0.386

0,870 0.239 0.890 ******** 0.960 0.286

0.930 0,224 0.930 0,275

0,960 0.158 0.960 -2,812**

CN = 0.455 0.673 0.782 0.708

311
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-48-54-000, MINF = 0.857, Camber = 0/2, ALPT = 9.06, BETA = 0.26, QINF = 301.0,

RNPU = 2.4E+06, CNWP = 0.5635

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.929 0.000 0.763 0.000 -5.632 ** 0.010 - 1.192"*

0.060 -0.996 0.020 -1.173"* 0.020 -1.004"* 0.020 - 1.216"*

0.110 -0.941 0,040 -0.939 0.060 - 1.539 * * 0.060 - 1.284

0.200 -0.851 0.060 -1.021 0.090 -1,087 0.110 -1.183

0.230 -0.714 0.090 -1.019 0.110 -1.147 0.140 1.892"*

0.400 -0.760 0.130 - 1.044 0.130 - 1.083 0.190 -5.500"*

0.490 -0.711 0.150 -1.019 0.150 -1.015 0.250 -1.180

0.590 -0. t 57 0.200 -0.934 0.210 - 1.073 0.400 -0.872

0.630 -0.196 0.250 - 1.047 0.250 - 1.056 0.490 -0.787

0.700 -0.179 0.260 -0.961 0.340 - 1.123 0.580 -0.718

0.750 -0.245 0.280 - 1.026 0.370 - 1.094 0.650 -0.638

0.810 -0.290 0,290 - 1.039 0.400 - 1.088 0.700 -0.686

0.840 -0.258 0.310 -0.974 0.410 - 1.070 0,750 -0.447

0.900 -0.180 0.320 -0.960 0.430 - 1.119 0.800 -0.243

0.960 -0,086 0.340 - 1.026 0.440 - 1.081 0.830 -0.159

0.350 -0.419 ** 0,460 - 1.093 0.900 -0.063

0.370 -0.987 0.490 - 1.019 0.960 -0.015

0.380 -0.997 0.500 - 1.099

0.400 -0.926 0.520 - 1.052

0.410 - 1.023 0.540 - 1.097

0.430 - 1,011 0.550 - 1,070

0.440 -0.938 0.580 -0.907

0.460 - 1.066 0.600 -0.637

0.470 - 1.030 0.610 -0.451

0.490 -0.910 0,650 -2.785"*

0.500 -0.740 0.700 -0.402

0.520 -0.658 0.750 -0.434

0.530 -0.512 0.820 -0.270

0.550 -0.479 0.890 -0.096

0.560 -0.440 0.900 -0.099

0.580 -0.415 0.960 -0.051

0.590 -0.432

0.600 -0,433

0.640 -2.624**

0.700 -0.327

0.750 -0.169

0.820 -2.798**

0.870 -0.127

0.930 -0.068

0.960 -0.050

Lower Surface

0.020 0.132 0.020 0.344 0.020 0.412 0,020 0.736

0.110 -0.071 0.060 0.277 0.060 0.364 0.060 3.160"*

0.230 -0.015 0.090 0.173 0.090 0,242 0.110 0.166

0.400 -0.049 0.120 0.095 0.120 -0.128 0.250 -0.010

0.490 -0,096 0.200 0.069 0.200 0.040 0.400 -0.066

0.630 3.204** 0.260 -0.064 0.250 -0.001 0.490 -0.165

0.750 0.007 0.400 -2.815"* 0,400 -0.052 0.580 -0,225

0.850 0.093 0.490 -0.101 0.490 0.027 0.650 -0.079

0.900 0.144 0.580 -0.061 0.580 -0.147 0.750 0.184

0.960 0.125 0.640 0.272 0.650 0.031 0.830 0.316

0.750 0.155 0.750 0.272 0.900 0.386

0.870 0.216 0.890 ******** 0,960 0.280

0.930 0.195 0.930 0.257

0.960 0.114 0.960 -2.814"*

CN = 0.486 0.681 0.798 0.744

312
TabLe F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-48-56-500, MINF = 0.855, Camber = 0/2, ALPT = 9.93, BETA = 0,23, QINF = 299,4,

RNPU = 2.3E+06. CNWP = 0.4326

r I = 0,93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0,020 -l.018 0.000 0.703 0.000 -5,659"* 0.010 -1.271"*

0.060 - 1,081 0.020 - 1.267"* 0,020 - 1.122"* 0.020 - 1.284"*

O. 110 - 1.040 0.040 - 1.048 0.060 - 1.615"* 0.060 - 1.353

0.200 -0.944 0.060 - 1.102 0.090 - 1,179 0.1 I0 - 1.247

0.230 -0,809 0.090 - 1.100 0.110 - 1.214 0,140 1.858**

0,400 -0.875 0.130 -1,088 0.130 -1,159 0.190 -5.527**

0.490 -0.425 0,150 - 1,082 0.150 - 1.101 0.250 - 1,242

0,590 -0.137 0.200 - 1,009 0.210 - 1.176 0.400 -0.930

0.630 -0.211 0.250 - 1.129 0.250 - 1.125 0,490 -0.808

0,700 -0.189 0,260 - 1,040 0.340 -0.833 0.580 -0.556

0.750 -0,252 0.280 - 1.110 0.370 -0.648 0.650 -0.476

0.810 -0,305 0.290 - 1,115 0.400 -0.625 0.700 -0,476

0,840 -0,280 0,310 - 1.037 0.410 -0.612 0.750 -0.418

0.900 -0.197 0.320 - 1.038 0.430 -0.645 0.800 -0.335

0.960 -0.106 0.340 - 1,008 0.440 -0.607 0.830 -0.363

0.350 -0,399** 0.460 -0.605 0.900 -0.241

0.370 -0.914 0.490 -0,537 0.960 -0.145

0.380 -0,848 0.500 -0.602

0,400 -0,712 0.520 -0.606

0.410 -0.758 0,540 -0.579

0.430 -0.723 0.550 -0,559

0.440 -0.618 0.580 -0.541

0.460 -0,661 0.600 -0.541

0.470 -0.57t 0,610 -0.417

0.490 -0.558 0.650 -2.798**

0.500 -0,512 0.700 -0.449

0.520 -0.507 0.750 -0.467

0.530 -0.461 0.820 -0.399

0.550 -0.453 0,890 -0.301

0.560 -0,441 0.900 -0.290

0.580 -0.422 0.960 -0,293

0.590 -0,437

0.600 -0.443

0.640 -2.636"*

0.700 -0.331

0.750 -0.215

0.820 -2,810"*

0.870 -0.205

0.930 -0.158

0.960 -0.137

Lower Surface

0.020 0.154 0,020 0.403 0.020 0.494 0.020 0.778

0.110 -0.022 0.060 0.332 0.060 0.434 0.060 3.178 **

0,230 -0.002 0.090 0.214 0,090 0.303 0.110 0.230

0A00 -0.085 0,120 0,131 0, 120 -0.090 0.250 0.031

0.490 -0,103 0.200 0.111 0,200 0.076 0.400 -0.028

0.630 3.222** 0.260 -0,026 0.250 0.037 0.490 -0.149

0.750 -0.006 0.400 -2,827"* 0.400 -0,041 0,580 -0.204

0.850 0.072 0.490 -0.096 0.490 0.010 0.650 -0.084

0.900 0,130 0,580 -0.071 0.580 -0.154 0.750 0.186

0.960 0.115 0.640 0.253 0.650 0.004 0,830 0.302

0.750 0.124 0.750 0.245 0.900 0.365

0.870 0.182 0.890 ******** 0.960 0.248

0.930 0.147 0.930 0.188

0,960 0.046 0.960 -2.826**

CN = 0.505 0.682 0.731 0.788

313
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-49-9-500, MINF = 0.853, Camber = 0/2, ALPT = 10.94, BETA = 0.65, QINF = 298.5,

RNPU = 2.3E+06, CNWP = 0.3605

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - I. 108 0.000 0.644 0.000 -5.683" * 0.010 - 1.383" *

0.060 - 1.168 0.020 - 1.369"* 0,020 - 1.180"* 0.020 -1.385**

0.110 - 1.172 0.040 - 1.135 0.060 - 1.693" * 0.060 - 1.454

0.200 -1.044 0.060 -1.190 0.090 -1.254 0.110 -1.341

0.230 -0.878 0.090 - 1.191 0. I 10 - 1.290 0.140 1.869"*

0.400 -0.612 0.130 -1.177 0.130 -1.239 0.190 -5.550**

0.490 -0.175 0.150 -1.163 0.150 -1,163 0.250 -1.093

0.590 -0.182 0.200 - 1,083 0.210 - 1.176 0.400 -0.752

0.630 -0.237 0.250 - 1.111 0,250 -0.799 0.490 -0.716

0.700 -0.222 0.260 -0.993 0.340 -0.673 0.580 -0.634

0.750 -0,275 0.280 - 1.006 0.370 -0.626 0.650 -0.546

0.8 ! 0 -0.298 0.290 -0.938 0.400 -0.619 0.700 -0.586

0.840 -0.272 0.310 -0.794 0.410 -0.590 0.750 -0.507

0.900 -0.226 0.320 -0.801 0.430 -0.623 0.800 -0.450

0.960 -0.105 0.340 -0.771 0.440 -0.600 0.830 -0.449

0.350 -0.272"* 0.460 -0.582 0.900 -0.345

0.370 -0.625 0.490 -0.530 0.960 -0.269

0.380 -0.604 0.500 -0.586

0.400 -0.542 0.520 -0.565

0.410 -0.616 0.540 -0.558

0.430 -0.527 0.550 -0.534

0.440 -0.522 0.580 -0.508

0.460 -0.546 0.600 -0.509

0.470 -0.493 0.610 -0.431

0.490 -0.458 0.650 -2.813"*

0.500 -0.451 0.700 -0.442

0.520 -0.423 0.750 -0.492

0.530 -0.437 0.820 -0.392

0.550 -0.401 0.890 -0.337

0.560 -0.421 0.900 -0.355

0.580 -0.355 0.960 -0.330

0.590 -0.400

0.600 -0.436

0.640 -2.651 **

0.700 -0.397

0.750 -0.298

0.820 -2.825**

0.870 -0.226

0.930 -0.294

0.960 -0.251

Lower Surface

0.020 0.252 0.020 0.487 0.020 0.567 0.020 0.801

0.110 0.006 0.060 0.387 0.060 0.477 0.060 3.182**

0.230 0.014 0.090 0.268 0.090 0.345 0.110 0.280

0.400 -0.069 0.120 0.184 0.120 -0.032 0.250 0.076

0.490 -0.094 0.200 0.145 0.200 0.115 0.400 0.002

0.630 3.225** 0.260 -0.003 0.250 0.076 0.490 -0.111

0.750 -0.013 0,400 -2,842"* 0.400 -0.022 0.580 -0.196

0.850 0.058 0.490 -0.099 0.490 0.018 0.650 -0.069

0.900 0.109 0.580 -0.092 0.580 -0.160 0.750 0.176

0.960 0.087 0.640 0.252 0.650 -0.016 0.830 0.294

0.750 0.125 0.750 0.225 0.900 0.330

0.870 0.173 0,890 ******** 0.960 0.203

0.930 0.134 0.930 0.151

0.960 0.044 0.960 -2.841 **

CN = 0.486 0.687 0.715 0.808

314
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-4-4-5-000, MINF = 0.864, Camber = 0/2, ALPT = 7.04, BETA = 0.47, QINF = 306.9,

RNPU = 2.4E+06, CNWP = 0.4640

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.687 0.000 0.866 0.000 -5,530"* 0,010 -0.991 **

0.060 -0.733 0.020 -0,889** 0,020 -0.783** 0.020 -1.014"*

0.110 -0.707 0,040 -0.669 0.060 - 1.455"* 0.060 - 1.040

0.200 -0.600 0.060 -0.783 0,090 -0,847 0. 110 -0.917

0,230 -0.489 0.090 -0,785 0.110 -0.905 0.140 1.836"*

0400 -0.568 0.130 -0.806 0.130 -0.868 0,190 -5,401"*

0,490 -0.180 0.150 -0.799 0.150 -0,799 0,250 -0,968

0.590 -0.172 0.200 -0.707 0.210 -0.861 0.400 -0.721

0.630 -0.211 0.250 -0.818 0.250 -0.865 0.490 -0.695

0.700 -0.186 0.260 -0.770 0.340 -0.912 0.580 -0.551

0.750 -0.209 0.280 -0.829 0.370 -0.903 0.650 -0.548

0.810 -0.233 0.290 -0.832 0.400 -0.896 0.700 -0.576

0.840 -0.208 0.310 -0.783 0.410 -0.865 0.750 -0.624

0.900 -0,117 0.320 -0.775 0.430 -0.909 0,800 -0.204

0.960 -0,021 0,340 -0.822 0.440 -0.883 0.830 -0,167

0,350 -0.357"* 0.460 -0.887 0.900 -0.019

0.370 -0.798 0.490 -0.827 0.960 0.063

0.380 -0.810 0.500 -0.915

0.400 -0.756 0.520 -0.887

0.410 -0.833 0.540 -0.906

0.430 -0.807 0.550 -0,875

0.440 -0.760 0.580 -0.837

0460 -0.853 0.600 -0.846

0.470 -0.833 0.610 -0.737

0.490 -0,794 0.650 -2.738 * *

0.500 -0806 0.700 -0.233

0.520 -0.793 0.750 -0.204

0.530 -0.786 0.820 -0.141

0,550 -0.807 0.890 -0.014

0.560 -0.822 0.900 0.004

0.580 -0.536 0.960 0.077

0.590 -0.360

0.600 -0.284

0.640 -2.581"*

0.700 -0.106

0.750 -0.145

0.820 -2.750**

0.870 -0.139

0.930 -0.024

0.960 0.037

Lower Surface

0.020 -0.057 0.020 0.104 0.020 0.198 0.020 0.552

0.110 -0.188 0.060 0.127 0.060 0.220 0.060 3.092**

0.230 -0.066 0,090 0.036 0,090 0.100 0.110 0.036

0.400 -0.084 0.120 -0.038 0.120 -0.217 0.250 -0.134

0.490 -0.094 0.200 -0.034 0.200 -0.087 0.400 -0.165

0.630 3.134"* 0.260 -0.162 0.250 -0.124 0.490 -0.249

0,750 0.022 0.400 -2.767** 0.400 -0.138 0.580 -0.297

0,850 0.110 0.490 -0.131 0.490 0.012 0.650 -0.091

0.900 0.163 0.580 -0.082 0.580 -0.187 0.750 0.183

0.960 0.152 0.640 0.269 0.650 0.024 0.830 0.311

0.750 0.170 0.750 0.281 0.900 0.389

0.870 0.250 0.890 ******** 0,960 0.303

0,930 0.241 0,930 0.293

0,960 0.176 0.960 -2.766"*

CN = 0.306 0.527 0,605 0.564

315
Table F-2.Continued.

Flight 198, Wing sweep = 26 °, Time --- 13-44-36-000, MINF = 0.844, Camber = 0/2, ALPT = 8.20, BETA = 0.31, QINF = 297.1,

RNPU = 2.4E+06, CNWP = 0.5278

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.902 0.000 0.771 0.000 -5.743 ** 0.010 - 1.202 * *

0.060 -0.984 0.020 -1.127"* 0.020 -I .003"* 0.020 - 1.183"*

O. 110 -0.924 0.040 -0.919 0.060 - 1.648 ** 0.060 - 1.210

0.200 -0.790 0.060 -0.982 0.090 - 1.063 O.110 - 1.133

0.230 -0.660 0.090 -0.999 O.1 lO -1.111 0.140 1.898"*

0.400 -0.710 0.130 -l.Ol I 0.130 -1.066 0.190 -5.610"*

0.490 -0.161 O.150 -0.993 O. 150 -0.988 0.250 - 1.160

0.590 -0.187 0.200 -0.917 0.210 -1,057 0.400 -0.857

0.630 -0.231 0.250 -1.015 0.250 -1.034 0.490 -0.771

0.700 -0.208 0.260 -0.947 0.340 - 1.100 0.580 -0.662

0.750 -0.234 0.280 - 1.023 0.370 - 1.086 0.650 -0.514

0.810 -0.280 0.290 - 1.019 0.400 - 1.081 0.700 -0.443

0.840 -0.240 0.310 -0.958 0.410 - 1.038 0.750 -0.254

0.900 -0.162 0.320 -0.949 0.430 - 1.096 0.800 -0.175

0.960 -0.059 0.340 - 1.012 0.440 - 1.057 0.830 -0.136

0.350 -0.413"* 0.460 -1.066 0.900 -0.016

0.370 -0.968 0.490 -0.989 0.960 0.033

0.380 -0.971 0.500 - 1.068

0.400 -0.888 0.520 - 1.060

0.410 -0.997 0.540 - 1.070

0.430 -0.988 0.550 - 1.040

0.440 -0.920 0.580 -0.621

0.460 - 1.037 0.600 -0.503

0.470 -0.997 0.610 -0.366

0.490 -0.966 0.650 -2.859**

0.500 -0.959 0.700 -0.253

0.520 -0.960 0.750 -0.234

0.530 -0.576 0.820 -0.110

0.550 -0.434 0.890 -0,005

0.560 -0.371 0.900 0.002

0.580 -0.314 0.960 0.063

0.590 -0.294

0.600 -0.275

0.640 -2.696**

0.700 -0.107

0.750 -0.132

0.820 -2.872**

0.870 -0.126

0.930 -0.026

0.960 0.030

Lower Surface

0.020 0.110 0.020 0.305 0.020 0.361 0.020 0.668

0.110 -0.086 0.060 0.242 0.060 0.308 0.060 3.1 64**

0.230 -0.005 0.090 0.146 0.090 0.205 0.110 0.133

0.400 -0.062 0.120 0.061 0.120 -0.132 0.250 -0.038

0.490 -0.084 0.200 0.047 0.200 0.033 0.400 -0.083

0.630 3.207** 0.260 -0.073 0.250 -0.025 0.490 -0.168

0.750 0.025 0.400 -2.889'* 0.400 -0.067 0.580 -0.211

0.850 0.096 0.490 -0.092 0.490 0.037 0.650 -0.058

0.900 0.147 0.580 -0.052 0.580 -0.143 0.750 0.192

0.960 0.129 0.640 0.282 0.650 0.038 0.830 0.326

0.750 0.164 0.750 0.289 0.900 0.391

0.870 0.244 0.890 ******** 0.960 0.297

0.930 0.233 0.930 0.293

0.960 0.166 0.960 -2.888 **

CN = 0.421 0.645 0.724 0.683

316
Table F-2, Continued.

Flight I98, Wing sweep = 26 °, Time = 13-44-48-000, MINF = 0,839, Camber = 0/2, ALPT = 8.62, BETA = 0.26, QINF = 294.4,

RNPU = 2.3E+06, CNWP = 0.5279

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,972 0.000 0.735 0.000 -5.800 * * 0.010 - 1.201 **

0.060 - 1.037 0.020 -1.200"* 0.020 - 1,055"* 0.020 - h247"*

0.110 -0.980 0,040 -0.970 0.060 - 1,626"* 0.060 - 1.295

0.200 -0.838 0.060 -1.058 0.090 -1,115 0.1 I0 -1,212

0.230 -0.712 0.090 -1.050 0.110 -1.173 0.140 1.921"*

0.400 -0.728 0.130 - 1.070 0.130 - 1.114 0.190 -5,664"*

0.490 -0.152 0.150 -1.044 0.150 -1.036 0,250 -1.218

0.590 -0.193 0.200 -0.965 0.210 -1.108 0,400 -0.881

0.630 -0.233 0.250 - 1.066 0.250 - 1.092 0.490 -0.791

0.700 -0.214 0.260 -0.993 0.340 - 1.146 0.580 -0.668

0.750 -0.240 0.280 - 1.058 0.370 - 1.133 0.650 -0.381

0.810 -0.294 0.290 - 1.072 0.400 - 1.110 0.700 -0.328

0.840 -0.261 0.310 - 1.004 0.410 - 1.084 0.750 -0.245

0.900 -0.177 0.320 -0.999 0.430 - 1.141 0.800 -0.180

0.960 -0,077 0,340 - 1.056 0.440 - 1.109 0.830 -0.126

0.350 -0.416"* 0.460 -1.117 0.900 -0.023

0.370 - 1.017 0.490 - 1.039 0.960 0.028

0.380 -1,033 0.500 -1.126

0.400 -0.951 0.520 -1.11 !

0.410 - 1.035 0.540 -0.856

0.430 - 1.034 0.550 -0.597

0.440 -0.963 0.580 -0.490

0.460 - 1.085 0.600 -0.472

0.470 -1.061 0.610 -0.358

0.490 -1.003 0.650 -2.889"*

0.500 -0.924 0.700 -0.295

0.520 -0.608 0.750 -0.269

0.530 -0.439 0.820 -0.109

0,550 -0.399 0.890 -0.002

0.560 -0.363 0.900 0.008

0.580 -0.319 0.960 0.063

0.590 -0.303

0.600 -0.296

0.640 -2.725**

0.700 -0.112

0.750 -0.130

0.820 -2,902**

0.870 -0.134

0.930 -0.026

0,960 0.022

Lower Surface

0,020 0,123 0.020 0.348 0.020 0.407 0.020 0.721

O. 110 -0.062 0.060 0.263 0.060 0.363 0.060 3.189"*

0.230 -0.001 0.090 O. 176 0.090 0.235 O.110 O. 167

0.400 -0.055 O. 120 0.088 O. 120 -0.105 0.250 -0.013

0.490 -0.066 0.200 0,074 0.200 0.052 0.400 -0.058

0.630 3.233** 0.260 -0.047 0,250 0.001 0.490 -0.143

0.750 0.025 0.400 -2.919"* 0.400 -0.046 0.580 -0.186

0.850 0,101 0.490 -0.074 0.490 0.04 1 0.650 -0.047

0.900 0.148 0.580 -0.034 0.580 -0.125 0.750 0.201

0.960 0.125 0.640 0.296 0.650 0.046 0.830 0.332

0.750 0.176 0.750 0.288 0.900 0.391

0.870 0.248 0.890 ******** 0.960 0.277

0.930 0.250 0.930 0.292

0.960 0.168 0.960 -2.918 * *

CN = 0.451 0.679 0.754 0.710

317
Table F-2, Continued.

Flight 198, Wing sweep = 26 °, Time = 13-44-56-000, MINF = 0.846, Camber = 0/2, ALPT = 9.00, BETA = 0.10, QINF = 299.8,

RNPU = 2.4E+06, CNWP = 0.5776

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.981 0.000 0.760 0.000 -5.698"* 0.010 -1.225"*

0.060 - 1.068 0.020 - 1.200'* 0.020 - 1.055"* 0.020 - 1.259"*

0.110 -0.988 0.040 -0.995 0.060 - 1.594 ** 0.060 - 1.275

0.200 -0.866 0,060 -1.073 0.090 -1.114 0.110 -1.213

0.230 -0.740 0.090 -1.060 0.110 -1.182 0.140 1.883"*

0,400 -0.787 0.130 - 1.077 0.130 - 1.133 0.190 -5.566 **

0.490 -0.357 0.150 - 1.053 0.150 - 1.054 0.250 - 1.228

0.590 -0.177 0.200 -0.973 0.210 - 1.110 0.400 -0.882

0.630 -0.217 0.250 - 1.076 0.250 - 1.097 0.490 -0.789

0.700 -0.206 0.260 - 1.005 0.340 - 1.159 0.580 -0.722

0.750 -0.247 0.280 - 1.069 0,370 - 1.139 0.650 -0.556

0.810 -0.285 0.290 - 1.074 0.400 - 1.107 0.700 -0.548

0.840 -0,260 0.310 - 1.011 0.410 - 1.107 0.750 -0.303

0.900 -0.182 0.320 -1.011 0.430 -1.163 0.800 -0.194

0.960 -0.086 0.340 - 1.065 0.440 - 1.124 0.830 -0.136

0.350 -0.417" * 0.460 - 1.129 0.900 -0.045

0.370 - 1.024 0.490 - 1.046 0.960 0.008

0.380 - 1.040 0.500 - 1.137

0.400 -0.948 0.520 - 1.129

0.410 -1.051 0.540 -1.136

0.430 - 1.042 0.550 - 1.060

0.440 -0.957 0.580 -0.590

0.460 - 1.1 04 0.600 -0.528

0.470 - 1.065 0.610 -0.439

0.490 - 1.012 0.650 -2.840* *

0.500 -0.954 0.700 -0.393

0.520 -0.768 0.750 -0.389

0.530 -0.569 0,820 -0.186

0.550 -0.493 0.890 -0.022

0.560 -0.453 0.900 -0.022

0.580 -0.415 0.960 0.029

0.590 -0.424

0.600 -0.41 l

0.640 -2.679**

0.700 -0.245

0.750 -0.112

0.820 -2,853**

0.870 -0.092

0.930 -0.010

0.960 0.026

Lower Surface

0,020 0.146 0.020 0.363 0.020 0.428 0,020 0.740

0.110 -0.050 0.060 0.289 0.060 0.380 0.060 3.128"*

0.230 -0.008 0.090 0.188 0.090 0.252 0. I 10 0.181

0.400 -0.057 0.120 0.105 0.120 -0.089 0.250 -0,003

0.490 -0.083 0.200 0.084 0.200 0.048 0.400 -0.052

0.630 3.172"* 0.260 -0.035 0.250 0.013 0.490 -0.137

0.750 0.017 0.400 -2.870* * 0.400 -0.038 0.580 -0.191

0.850 0.092 0.490 -0.079 0.490 0.04 1 0.650 -0.050

0.900 0.142 0.580 -0.044 0.580 -0.126 0.750 0.199

0.960 0.119 0.640 0.287 0.650 0.042 0.830 0.327

0.750 0.170 0.750 0.283 0.900 0.389

0.870 0.236 0.890 ******** 0.960 0.290

0.930 0.224 0.930 0.279

0.960 0.147 0.960 -2.869**

CN = 0.477 0.703 0,803 0.748

318
Table F-2. Continued.

Flight t98, Wing sweep = 26 °, Time = 13-45-6-000, MINF = 0.847, Camber = 0/2, ALPT = 10.00, BETA = 0.07, QINF = 301.5.

RNPU = 2.4E+06, CNWP = 0.4444

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1069 0.000 0.686 0.000 -5.674"* 0.010 - 1.316"*

0.060 -1.119 0.020 -1.219"* 0.020 -1.157"* 0.020 -1.319"*

O.110 - 1.094 0.040 - 1,1 O0 0,060 - 1,674 ** 0.060 - 1.391

0.200 -0.959 0,060 - l. 137 0.090 - 1,200 0.110 - 1.298

0,230 -0.855 0.090 - 1.140 0.110 - 1.245 0.140 1.846"*

0.400 -0.715 0,130 -1,149 0,130 -1.207 0.190 -5,542**

0.490 -0.141 0.150 -1.123 0.150 -l.131 0.250 -1.287

0,590 -0.177 0.200 - 1.048 0.210 - 1,196 0.400 -0.939

0.630 -0.247 0.250 - 1.168 0.250 - 1.091 0.490 -0.647

0.700 -0.242 0,260 - 1,089 0,340 -0,685 0.580 -0.548

0,750 -0.265 0.280 - 1,137 0.370 -0.663 0.650 -0.453

0.810 -0.32 [ 0.290 - 1.148 0.400 -0.638 0.700 -0.447

0.840 -0.296 0.3 l0 - 1.061 0.410 -0.603 0.750 -0.389

0.900 -0.198 0.320 - 1.061 0.430 -0,636 0.800 -0.322

0.960 -0.108 0.340 -0,983 0.440 -0,608 0.830 -0.337

0.350 -0.391 ** 0.460 -0,597 0.900 -0,235

0.370 -0,828 0.490 -0.551 0.960 -0.140

0.380 -0.771 0.500 -0.584

0.400 -0.659 0.520 -0.581

0.410 -0,678 0.540 -0.570

0.430 -0.632 0.550 -0.545

0.440 -0,562 0.580 -0.525

0.460 -0.604 0.600 -0.533

0.470 -0.537 0.610 -0.444

0.490 -0.508 0.650 -2.832**

0.500 -0.461 0.700 -0.477

0.520 -0.484 0.750 -0.484

0.530 -0.422 0.820 -0.416

0.550 -0.445 0.890 -0.342

0.560 -0.390 0.900 -0.319

0.580 -0,388 0,960 -0.290

0.590 -0.353

0.600 -0,368

0.640 -2.672"*

0.700 -0.273

0.750 -0.191

0,820 -2.845**

0.870 -0.214

0.930 -0.142

0.960 -0.124

Lower Surface

0.020 0.196 0.020 0,423 0,020 0.480 0.020 0.800

0.110 -0,025 0,060 0.331 0,060 0.437 0.060 3.103"*

0,230 -0.005 0.090 0.232 0,090 0.295 0 110 0.263

0.400 -0,091 0.120 0.119 0,120 -0.045 0.250 0,043

0.490 -0.105 0.200 0.118 0,200 0.093 0.400 -0.031

0,630 3.146' * 0.260 -0.021 0.250 0.034 0.490 -0.129

0.750 -0.009 0.400 -2.862** 0.400 -0.036 0.580 -0.198

0.850 0.061 0.490 -0.094 0.490 0,014 0.650 -0.072

0.900 0.128 0.580 -0.077 0,580 -0.148 0.750 0.180

0.960 0,098 0.640 0,242 0,650 0.009 0,830 0.296

0.750 0.120 0,750 0,233 0.900 0,355

0.870 0.176 0,890 ******** 0_960 0.253

0.930 0.132 0.930 0.183

0.960 0.039 0,960 -2.861 * *

CN = 0.473 0.667 0730 0.791

319
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-17-25-000, MINF = 0.852, Camber = 0/2, ALPT = 5.08, BETA = -0.07, QINF = 297.1,

RNPU = 2.3E+06, CNWP = 0.2299

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.358 0.000 0.853 0.000 1.000"* 0.010 -0.829

0.060 -0.439 0.020 -0.566 0.020 -0.550 0.020 -0.893

0.110 -0.387 0.040 -0.524 0.060 -2.938** 0.060 -0.867

0.200 -0.226 0.060 -0.603 0.090 -0.718 0.110 -0.823

0.230 -0.352 0.090 -0.622 0.110 -0.712 0.140 -0.864

0.400 -0.247 0.130 -0.626 0.130 -0.663 0.190 - 1.968"*

0.490 -0.181 0.150 -0.613 0.150 -0.673 0.250 -0.813

0.590 -0.283 0.200 -0.529 0.210 -0.663 0.400 -0.288

0.630 -0.290 0.250 -0.634 0.250 -0.681 0.490 -0.291

0.700 -0.198 0.260 -0.619 0.340 -0.558 0.580 -0.309

0.750 -0.256 0.280 -0.618 0.370 -0.251 0.650 -0.371

0.810 -0.269 0.290 -0.442 0.400 -0.223 0.700 -0.344

0.840 -0.225 0.310 -0.246 0.410 -2.973** 0.750 -0.418

0.900 -0.110 0.320 -0.232 0.430 -0.248 0.800 -0.440

0.960 -0.024 0.340 -0.201 0.440 -0.236 0.830 -0.406

0.350 -0.179** 0.460 -0.261 0.900 -0.153

0.370 -0.196 0.490 -0.218 0.960 0.004

0.380 -0.263 0.500 -0.290

0.400 -0.176 0.520 -0.275

0.410 -0.277 0.540 -0.267

0.430 -0.261 0.550 -0.277

0.440 -0.238 0.580 -0.290

0.460 -0.277 0.600 -0.271

0.470 -0.262 0.610 -0.296

0.490 -0.274 0.650 0.479'*

0.500 -0.285 0.700 -0.544

0.520 -0.328 0.750 -0.559

0.530 -0.289 0.820 -0.326

0.550 -0.338 0.890 -0.092

0.560 -0.300 0.900 -0.070

0.580 -0.293 0.960 0.059

0.590 -0.338

0.600 -0.339

0.640 -0.494

0.700 -0.451

0.750 -0.034**

0.820 -0.253

0.870 -0.218

0.930 -0.080

0.960 -0.022

Lower Surface

0.020 -0.308 0.020 -0. l I l 0.020 0.032 0.020 0.345

0.110 -0.266 0.060 -0.060 0.060 0.032 0.060 1.090 **

0.230 -0.084 0.090 -0.113 0.090 1.200** 0.110 -0.118

0.400 -0.071 0.120 -0.180 0.120 -0.283 0.250 -0.271

0.490 -0.081 0.200 -0.158 0.200 -0.220 0.400 -0.284

0.630 1.966** 0.260 -0.251 0.250 -0.255 0.490 -0.349

0.750 0.023 0.400 -0.174 0.400 -0.220 0.580 -0.330

0.850 0.122 0.490 -0.178 0.490 -0.065 0.650 -0.141

0.900 0.211 0.580 -0.149 0.580 -0.227 0.750 0.097

0.960 0.171 0.640 0.042 0.650 -0.050 0.830 0.268

0.750 0.175 0.750 -0.043 0.900 0.310

0.870 0.224 0.890 0.277 0.960 0.258

0.930 0.209 0.930 0.241

0.960 0.184 0.960 -2.019 * *

CN -- 0.205 0.322 0.313 0.363

320
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-17-38-500, MINF = 0.846, Camber = 0/2, ALPT = 6.04, BETA = -0.18, QINF = 291.6,

RNPU = 2.3E+06, CNWP = 0.2906

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.720 0.000 0.809 0.000 0.972** 0.010 -0.999

0.060 -0.693 0.020 -0.834 0.020 -0.826 0.020 -0.999

0.110 -0.659 0.040 -0.728 0.060 -3.038"* 0.060 -1.016

0.200 -0.382 0.060 -0.794 0.090 -0.886 O. 110 -0.923

0.230 -0.495 0.090 -0.773 O. 110 -0.868 O. 140 -0.976

0.400 -0.233 0.130 -0.803 0.130 -0.801 O. 190 - 1.994"*

0.490 -0.215 0.150 -0.799 0.150 -0.819 0.250 -0.977

0.590 -0.288 0.200 -0.685 0.210 -0.784 0,400 -0,735

0.630 -0.280 0.250 -0.793 0.250 -0.847 0.490 -0.334

0.700 -0.213 0.260 -0.781 0.340 -0.851 0.580 -0.308

0.750 -0.284 0.280 -0.777 0,370 -0.840 0.650 -0.329

0.810 -0.293 0.290 -0.786 0.400 -0.853 0.700 -0.333

0.840 -0.249 0.310 -0.775 0.410 -3.018"* 0.750 -0.377

0.900 -0.147 0.320 -0.772 0.430 -0.736 0.800 -0.345

0.960 -0.058 0.340 -0.754 0.440 -0.424 0.830 -0.287

0.350 -0.415"* 0.460 -0.327 0.900 -0.136

0.370 -0.753 0.490 -0.180 0.960 0.005

0.380 -0.786 0.500 -0.217

0.400 -0,374 0.520 -0.206

0.410 -0.282 0.540 -0.178

0.430 -0.199 0.550 -0.198

0.440 -0.147 0.580 -0.209

0.460 -0.164 0.600 -0.199

0.470 -0.138 0.610 -0.250

0.490 -0.129 0.650 0.644**

0.500 -0.198 0.700 -0.362

0.520 -0.163 0.750 -0.383

0,530 -0.185 0.820 -0.341

0.550 -0.221 0,890 -0.106

0.560 -0.226 0.900 -0.070

0.580 -0.227 0.960 0.049

0.590 -0.270

0.600 -0.283

0.640 -0.349

0.700 -0.339

0.750 -0.039**

0.820 -0,281

0.870 -0,237

0.930 -0.097

0,960 -0.030

Lower Surface

0.020 -0.136 0.020 0,024 0.020 0.125 0.020 0.446

0.110 -0.214 0.060 0.028 0.060 0.117 0.060 1.107 **

0,230 -0,070 0.090 -0.038 0.090 1.234"* 0,110 -0.020

0.400 -0.091 0.120 -0.120 0.120 -0.217 0.250 -0.206

0.490 -0.078 0.200 -0.105 0.200 -0.138 0.400 -0.226

0.630 2.015"* 0.260 -0.193 0.250 -0.181 0.490 -0.290

0.750 0.027 0.400 -0_ 142 0.400 -0.177 0.580 -0.279

0.850 0.1 04 0.490 -0.158 0.490 -0.055 0,650 -0.132

0.900 0.180 0.580 -0.125 0.580 -0.205 0.750 0.100

0,960 0.149 0.640 0.043 0.650 -0.055 0,830 0.293

0.750 0.175 0.750 -0.032 0.900 0.312

0.870 0.234 0.890 0.279 0.960 0.268

0.930 0.202 0.930 0.234

0.960 0.168 0.960 -2.065 * *

CN = 0.277 0.424 0.420 0.495

321
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-17-42-500, MINF = 0.853, Camber = 0/2, ALPT = 7.07, BETA = -0.27, QINF = 294.5,

RNPU = 2.3E+06, CNWP = 0.3584

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.794 0.000 0.789 0.000 0.942"* 0.010 - 1.017

0.060 -0.783 0.020 -0.932 0.020 -0.890 0.020 - 1.087

0.110 -0.772 0.040 -0.775 0.060 -3.006** 0.060 -1.040

0.200 -0.632 0.060 -0.887 0.090 -0.942 O. 110 - 1.005

0.230 -0.557 0.090 -0.886 O.110 -0.933 O. 140 - 1.008

0.400 -0.466 0.130 -0.886 0.130 -0.896 0.190 - 1.965 **

0.490 -0.167 0.150 -0.896 0.150 -0.913 0.250 - 1.073

0.590 -0.226 0.200 -0.812 0.210 -0.853 0.400 -0.783

0.630 -0.233 0.250 -0.854 0.250 -0.911 0.490 -0.711

0.700 -0.202 0.260 -0.848 0.340 -0.926 0.580 -0.615

0.750 -0.285 0.280 -0.849 0.370 -0.911 0.650 -0.545

0.810 -0.300 0.290 -0.849 0.400 -0.949 0.700 -0.447

0.840 -0.268 0.310 -0.872 0.410 -2.979"* 0.750 -0.290

0.900 -0.168 0.320 -0.861 0.430 -0.918 0.800 -0.305

0.960 -0.074 0.340 -0.839 0.440 -0.894 0.830 -0.201

0.350 -0.435"* 0.460 -0.912 0.900 -0.067

0.370 -0.845 0.490 -0.883 0.960 0.021

0.380 -0.900 0.500 -0.928

0.400 -0.809 0.520 -0.907

0.410 -0.871 0.540 -0.901

0.430 -0.847 0.550 -0.924

0.440 -0.831 0.580 -0.608

0.460 -0.868 0.600 -0.403

0.470 -0.833 0.610 -0.321

0.490 -0.855 0.650 0.825**

0.500 -0.865 0.700 -0.170

0.520 -0.824 0.750 -0.255

0.530 -0.475 0.820 -0.204

0.550 -0.364 0.890 -0.059

0.560 -0.253 0.900 -0.009

0.580 -0.209 0.960 0.071

0.590 -0.196

0.600 -0.177

0.640 -0.141

0.700 -0.177

0.750 -0.019"*

0.820 -0.239

0.870 -O.203

0.930 -0.091

0.960 -0.021

Lower Surface

0.020 -0.076 0.020 O. 136 0.020 0.212 0.020 0.560

0.110 -0.176 0.060 0.106 0.060 0.171 0.060 1.100"*

0.230 -0.061 0.090 0.025 0.090 1.230"* 0.110 0.010

0.400 -0.063 0.120 -0.036 0.120 -0.154 0.250 -0.141

0.490 -0.069 0.200 -0.054 0.200 -0.060 0.400 -0.193

0.630 2.004"* 0.260 -0.145 0.250 -0.126 0.490 -0.256

0.750 0.013 0.400 -0.113 0.400 -0.136 0.580 -0.262

0.850 0.100 0.490 -0.136 0.490 -0.039 0.650 -0.122

0.900 0.161 0.580 -0.122 0.580 -0.180 0.750 0.118

0.960 0.147 0.640 0.055 0.650 -0.047 0.830 0.292

0.750 0.182 0.750 -0.023 0.900 0.308

0.870 0.231 0.890 0.292 0.960 0.256

0.930 0.216 0.930 0.248

0.960 0.175 0.960 -2.089"*

CN = 0.339 0.545 0.544 0.609

322
Table F-2. Continued.

Fltght 221, Wing sweep = 26 °, Time = 13-17-49-500, MINF = 0.858, Camber = 0/2, ALPT = 7.94, BETA = -0.18, QINF = 296.8,

RNPU = 2.3E+06, CNWP = 0.4297

q = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x./c CP

0.020 -0.857 0.000 0.743 0.000 0.873** 0.010 - 1,126

0.060 -0.934 0.020 - 1.007 0.020 -0,945 0,020 - 1,168

0.110 -0,853 0.040 -0,887 0.060 -3.114"* 0,060 - I, 101

0.200 -0.722 0.060 -0,964 0.090 - 1.014 0.110 - 1.121

0.230 -0,689 0.090 -0.954 0.110 -I .004 0.140 - 1.117

0.400 -0.726 0.130 -0.950 0.130 -0.951 0.190 - 1.940**

0.490 -0,649 0,150 -0,953 0.150 -0.988 0.250 - 1.1 64

0,590 -0,210 0.200 -0.891 0.210 -0.927 0.400 -0,846

0.630 -0.210 0,250 -0.930 0,250 -0.975 0,490 -0,758

0.700 -0.149 0.260 -0.908 0,340 - 1.015 0.580 -0.690

0.750 -0.280 0.280 -0.919 0.370 -0,989 0,650 -0.659

0.810 -0.284 0,290 -0.919 0.400 - 1,014 0.700 -0.637

0.840 -0.271 0.310 -0.945 0.410 -2.946"* 0.750 -0.588

0.900 -0.200 0.320 -0,936 0.430 -0.993 0.800 -0.244

0.960 -0.104 0.340 -0.910 0.440 -0.966 0.830 -0_ 159

0.350 -0.453** 0.460 -0.983 0.900 -0.063

0.370 -0,910 0.490 -0.958 0.960 -0.025

0.380 -0,963 0.500 - 1.003

0,400 -0,874 0,520 -0,973

0,410 -0,935 0.540 -0.982

0.430 -0.916 0550 - 1.009

0.440 -0.907 0.580 -0.998

0.460 -0,938 0.600 -0.934

0.470 -0,911 0,610 -0.922

0.490 -&938 0.650 0.568**

0.500 -0.951 0.700 -0.386

0.520 -0.933 0.750 -0.426

0,530 -0.931 0.820 -0.153

0.550 -0.981 0,890 -0.015

0.560 -0.920 0.900 -0.011

0.580 -0.941 0.960 0.080

0.590 -0.984

0.600 -0,732

0.640 -0.280

0.700 -0.241

0,750 -0.017"*

0.820 -0.125

0.870 -0.130

0.930 -0.040

0.960 0.011

Lower Surface

0.020 -0.010 0.020 0.214 0.020 0.283 0.020 0.601

0.110 -0,146 0.060 0.164 0.060 0.231 0.060 1.090"*

0.230 -0.054 0.090 0.072 0.090 1.230"* O. 110 0.066

0,400 -0,071 0,120 0,003 0.120 -0.107 0.250 -0.099

0.490 -0.081 0. 200 -0.026 0.200 -0.020 0.400 -0.153

0,630 1,998"* 0.260 -0.121 0.250 -0,086 0.490 -0.229

0.750 -0.001 0.400 -0.102 0,400 -0,121 0.580 -0,265

0,850 0.082 0.490 -0.133 0,490 -0.040 0.650 -0.119

0.900 0,169 0,580 -0.127 0.580 -0.177 0.750 0.111

0.960 0.128 0,640 0.053 0.650 -0,037 0.830 0.284

0.750 0,175 0.750 -0.044 0.900 0.315

0.870 0,223 0.890 0.284 0.960 0,239

0,930 0.208 0.930 0.241

0.960 0.169 0.960 -2,050* *

CN = 0.448 0,645 0.666 0.702

323
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-17-51-500, MINF = 0.861, Camber = 0/2, ALP'I" = 8.68, BETA = -0.15, QINF = 298.8,

RNPU = 2.3E+06, CNWP = 0.4668

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 -0.901 0,000 0.707 0.000 0.837"* 0.010 -1.142

0,060 -0.939 0.020 - 1.059 0.020 -0.997 0.020 - 1.204

0.110 -0.930 0.040 -0.934 0.060 -3.119"* 0.060 -1.221

0.200 -0.769 0.060 -0.960 0.090 - 1.051 0.110 - 1,155

0.230 -0.723 0,090 -0.993 0.110 -1.044 0.140 -1.165

0.400 -0.776 0,130 -0.977 0.130 -0.982 0,190 - 1.929"*

0.490 -0.683 0.150 -0.985 0.150 - 1.026 0.250 - 1.165

0.590 -0.222 0.200 -0.927 0.210 -0,960 0.400 -0.856

0.630 -0.195 0.250 -0,964 0.250 - 1.014 0.490 -0.764

0,700 -0.146 0.260 -0.945 0.340 -1.025 0.580 -0.698

0.750 -0.276 0.280 -0.958 0.370 - 1.023 0.650 -0.682

0, 810 -0.299 0.290 -0.949 0.400 - 1.039 0,700 -0.666

0.840 -0.279 0.310 -0.972 0.410 -2.929"* 0.750 -0.571

0.900 -0.203 0.320 -0.980 0.430 - 1,033 0.800 -0.272

0.960 -0.105 0.340 -0.947 0.440 - 1.003 0.830 -0.187

0.350 -0.457"* 0.460 - 1.020 0.900 -0.101

0.370 -0.950 0.490 -0.976 0.960 -0.051

0.380 -0.995 0.500 - 1.036

0.400 -0.892 0.520 - 1.020

0.410 -0.963 0.540 - 1.005

0.430 -0.947 0.550 -1.041

0.440 -0.939 0.580 - 1.046

0.460 -0.970 0.600 -0.978

0.470 -0.926 0.610 -0,945

0.490 -0.977 0.650 0.596**

0.500 -0.991 0.700 -0.433

0.520 -0.990 0.750 -0.462

0.530 -0.962 0,820 -0.238

0,550 -0.876 0.890 -0.069

0.560 -0,592 0,900 -0.082

0,580 -0.501 0.960 0,000

0.590 -0.481

0.600 -0.443

0.640 -0.337

0,700 -0.322

0.750 -0.022**

0.820 -0.133

0,870 -0.116

0.930 -0.082

0.960 -0.054

Lower Surface

0.020 0,039 0.020 0.264 0.020 0.372 0.020 0.659

0.110 -0.121 0.060 0.195 0.060 0,267 0.060 1.082"*

0.230 -0.044 0.090 0.099 0.090 1.221 ** 0.110 0.134

0.400 -0.076 0.120 0.027 0.120 -0.073 0.250 -0.067

0,490 -0.053 0.200 -0.006 0,200 -0.002 0.400 -0.124

0.630 1.983"* 0.260 -0.100 0.250 -0.058 0.490 -0.215

0.750 -0.010 0.400 -0.095 0.400 -0.102 0.580 -0.255

0.850 0.076 0.490 -0.130 0.490 -0.045 0.650 -0.120

0.900 0.147 0.580 -0.117 0.580 -0.177 0.750 0.109

0.960 O. 126 0,640 0.044 0,650 -0.038 0.830 0.289

0.750 0.164 0.750 -0.045 0.900 0.311

0.870 0.211 0.890 0.281 0.960 0.230

0.930 0.176 0.930 0.223

0.960 0.133 0,960 -2.070'*

CN = 0.476 0.656 0.715 0.744

324
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-17-58-500, MINF = 0.861, Camber = 0/2, ALPT = 11.05, BETA = -0.33, QINF = 306.5,

RNPU = 2.4E+06, CNWP = 0.2951

rl = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0,020 - 1.170 0,000 0.503 0,000 0.662"* 0.010 - 1,368

0.060 - 1,176 0.020 - 1.388 0.020 - 1.240 0,020 - 1.36 I

0.110 - 1,125 0.040 - 1.203 0,060 -3,243"* 0,060 - 1.419

0.200 - 1.051 0.060 - 1.227 0,090 - 1.263 0.110 - 1,360

0.230 -0,980 0.090 - 1.216 0.110 - 1.248 0.140 - 1.410

0.400 -0,635 0.130 -1,149 0,130 -1,192 0.190 -1.928"*

0,490 -0,383 0.150 -0.976 0.150 - 1.209 0.250 - 1.320

0,590 -0.291 0.200 -0.896 0.210 - 1.057 0,400 -0.824

0,630 -0.265 0.250 -0.868 0.250 -0.907 0.490 -0.758

0.700 -0.231 0.260 -0.785 0,340 -0.731 0,580 -0,704

0,750 -0.303 0.280 -0.784 0.370 -0.694 0.650 -0.624

0.810 -0.365 0.290 -0.733 0.400 -0.698 0.700 -0.612

0.840 -0.349 0.310 -0,767 0.410 -2.902** 0.750 -0,568

0,900 -0,289 0,320 -0,764 0,430 -0.673 0.800 -0.460

0.960 -0.189 0.340 -0,640 0.440 -0.648 0,830 -0.479

0.350 -0.335** 0.460 -0.665 0.900 -0.375

0.370 -0,636 0.490 -0.616 0.960 -0.299

0.380 -0,660 0,500 -0.672

0.400 -0.562 0.520 -0.643

0.410 -0,583 0.540 -0.596

0.430 -0.621 0.550 -0.608

0.440 -0.523 0.580 -0.664

0.460 -0.623 0,600 -0.592

0,470 -0.520 0.610 -0,556

0,490 -0.543 0.650 0.422"*

0,500 -0548 0.700 -0.605

0,520 -0.567 0.750 -0.655

0.530 -0.492 0.820 -0.524

0.550 -0,565 0.890 -0.452

0.560 -0.460 0.900 -0.447

0.580 -0.512 0.960 -0.341

0.590 -0.489

0.600 -0.474

0.640 -0.377

0,700 -0.382

0.750 -0.053**

0.820 -0.351

0.870 -0.313

0.930 -0,351

0.960 -0.336

Lower Surface

0.020 0.215 0.020 0.503 0,020 0.557 0.020 0.775

0.110 -0.021 0.060 0.344 0.060 0.412 0.060 1.065"*

0,230 0.001 0.090 0.227 0,090 1,142"* 0.110 0.271

0.400 -0.071 0.120 0.169 0.120 0.067 0.250 0.053

0,490 -0.106 0.200 0.10t 0.200 0.110 0.400 -0.039

0,630 1.886"* 0.260 -0.013 0,250 0.040 0.490 -0.140

0.750 -0.077 0.400 -0.045 0.400 -0.045 0.580 -0.209

0.850 -0.016 0,490 -0.108 0.490 -0.069 0.650 -0.128

0.900 0.066 0.580 -0.143 0.580 -0,176 0.750 0.093

0.960 0.025 0.640 0,017 0.650 -0,069 0,830 0,254

0.750 0.100 0.750 -0.077 0.900 0.271

0.870 0.139 0.890 0.192 0,960 0.152

0.930 0.090 0.930 0.119

0.960 0,004 0.960 -2.093"*

CN = 0.513 0.662 0.726 0.892

325
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-18-1-500, MINF = 0.854. Camber = 0/2, ALPT = 12.24, BETA = 0.60, QINF = 307.6,

RNPU = 2.4E+06, CNWP = 0.2915

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -1.269 0.000 0.426 0.000 0.569"* 0.010 - 1.439

0.060 - 1.243 0.020 - 1.382 0.020 - 1.308 0.020 - 1.458

0.110 - 1.227 0.040 - 1.287 0.060 -3.187"* 0.060 - 1.496

0.200 -1.089 0.060 -1.322 0.090 -1.253 0.110 -1.431

0.230 - 1.025 0.090 - 1.307 0.110 -0.995 0.140 - 1.443

0.400 -0.741 0.130 -1.292 0.130 -1.061 0.190 -1.959"*

0.490 -0.376 0.150 - 1.235 0.150 -0.830 0.250 - 1.394

0.590 -0.338 0.200 - 1.153 0.210 -0.912 0.400 -0.884

0.630 -0.340 0.250 -0.810 0.250 -0.828 0.490 -0.731

0.700 -0.272 0.260 -0.883 0.340 -0.744 0.580 -0.528

0.750 -0.346 0.280 -0.759 0.370 -0.724 0.650 -0.457

0.810 -0.344 0.290 -0.725 0.400 -0.741 0.700 -0.438

0.840 -0.334 0.310 -0.734 0.410 -2.930"* 0.750 -0.425

0.900 -0.278 0.320 -0.726 0.430 -0.723 0.800 -0.438

0.960 -0.224 0.340 -0.779 0.440 -0.696 0.830 -0.437

0.350 -0.390* * 0.460 -0.727 0.900 -0.368

0.370 -0.675 0.490 -0.682 0.960 -0.300

0.380 -0.715 0.500 -0.738

0.400 -0.640 0.520 -0.726

0.410 -0.714 0.540 -0.696

0.430 -0.602 0.550 -0.716

0.440 -0.682 0.580 -0.724

0.460 -0.604 0.600 -0.655

0.470 -0.626 0.610 -0.627

0.490 -0.586 0.650 0.352 **

0_500 -0.647 0.700 -0.593

0.520 -0.589 0.750 -0.666

0.530 -0.605 0.820 -0.504

0.550 -0.584 0.890 -0.425

0.560 -0.555 0.900 -0.466

0.580 -0.517 0.960 -0.355

0.590 -0.590

0.600 -0.557

0.640 -0.513

0.700 -0.518

0.750 -0.044**

0.820 -0.395

0.870 -0.367

0.930 -0.359

0.960 -0.343

Lower Surface

0.020 0.281 0.020 0.596 0.020 0.607 0.020 0.808

0.110 0.021 0.060 0.363 0.060 0.455 0.060 1.052 **

0.230 0.025 0.090 0.269 0.090 1.1130"* 0. 110 0.320

0.400 -0.054 0.120 0.185 0.120 0.112 0.250 0.084

0.490 -0.100 0.200 0.135 0.200 0.167 0.400 -0.009

0.630 1.841 ** 0.260 0.018 0.250 0.088 0.490 -0.098

0.750 -0.083 0.400 -0.028 0.400 -0.025 0.580 -0.178

0.850 -0.010 0.490 -0.094 0.490 -0.056 0.650 -0.093

0.900 0.069 0.580 -0.141 0.580 -0.160 0.750 0.108

0.960 0.010 0.640 0.022 0.650 -0.062 0.830 0.258

0.750 0.121 0.750 -0.114 0.900 0.269

0.870 0.153 0.890 0.187 0.960 0.148

0.930 0.088 0.930 0.117

0.960 0.017 0.960 -2.124**

CN = 0.566 0.757 0.733 0.902

326
Table F-2. Continued.

Flight 221, Wing sweep = 26':, Time = 14-6-7-500, MINF = 0.855, Camber = 0/2, ALPT = 5.48, BETA = -0.70. QINF = 300.7,

RNPU = 2.4E÷06, CNWP = 0.2256

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0,537 0.000 0.838 0.000 0.930** 0.010 -0.807

0.060 -0.555 0.020 -0.700 0.020 -0.711 0.020 -0.953

0.110 -0.517 0.040 -0.642 0.060 -2.896** 0,060 -0,928

0.200 -0.219 0,060 -0.697 0.090 -0.780 0.110 -0.841

0,230 -0,338 0.090 -0.701 0.110 -0.793 0.140 -0.898

0.400 -0,230 0.130 -0.706 0.130 -0,699 0.190 - 1.953"*

0.490 -0.202 O.150 -0,699 0.150 -0.749 0.250 -0.896

0.590 -0,280 0,200 -0.599 0.210 -0.710 0.400 -0.642

0.630 -0.272 0.250 -0.711 0.250 -0.732 0,490 -0.315

0,700 -0.181 0.260 -0.661 0,340 -0.770 0,580 -0.314

0.750 -0.257 0.280 -0,698 0.370 -0.757 0.650 -0.355

0.810 -0.267 0.290 -0.698 0,400 -0.729 0.700 -0.343

0.840 -0.239 0.310 -0.698 0.410 2.551 ** 0,750 -0,407

0.900 -0.117 0.320 -0,689 0.430 -0.284 0.800 -0.402

0.960 -0,043 0,340 -0.662 0.440 -0.200 0,830 -0,328

0,350 -0,407"* 0.460 -0.217 0.900 -0.151

0,370 -0.312 0.490 -0.111 0,960 O000

0,380 -0,236 0,500 -0.221

0.400 -0,094 0,520 -0.179

0.410 -0.182 0,540 -0,205

0.430 -0.163 0.550 -0.206

0.440 -0.110 0.580 -0.243

0.460 -0.196 0.600 -0.210

0.470 -0.171 0.610 -0.247

0.490 -0,204 0.650 0.494"*

0.500 -0.230 0.700 -0.502

0.520 -0.248 0.750 -0.535

0.530 -0.234 0.820 -0.327

0.550 -0.298 0.890 -0.103

0.560 -0.255 0,900 -0,077

0.580 -0.265 0,960 0.057

0.590 -0.307

0.600 -0.338

0.640 -0.477

0,700 -0.410

0.750 -0.035**

0,820 -0.251

0.870 -0.223

0.930 -0,088

0.960 -0.023

Lower Surface

0.020 -0,274 0.020 -0.055 0,020 0,054 0.020 0.421

0,110 -0.265 0.060 -0.022 0.060 0.036 0.060 1.065**

0.230 -0.080 0.090 -0.097 0.090 1.014 ** 0.110 -0.105

0,400 -0,067 0.120 -0.143 0.120 -0.352 0.250 -0.243

0.490 -0,081 0,200 -0.150 0.200 -0,226 0,400 -0,260

0.630 1.756** 0,260 -0.256 0,250 -0,224 0.490 -0,338

0,750 0.014 0.400 -0.169 0,400 -0,196 0.580 -0,330

0.850 0. 123 0.490 -0.177 0.490 -0.051 0.650 -0.148

0.900 0.197 0.580 -0.149 0,580 -0.218 0.750 0.093

0.960 0.168 0,640 0.037 0,650 -0.051 0.830 0.273

0,750 0.173 0,750 -0.051 0,900 0.315

0.870 0.226 0,890 0.266 0,960 0.258

0,930 0.209 0.930 0.233

0,960 0.177 0.960 - 1,968"*

CN = 0.216 0.364 0.353 0.433

327
Table F-2. Continued.

Flight 22l, Wing sweep = 26 °, Time = 14-6-22-500, MINF = 0.854, Camber = 0/2, ALPT = 5.99, BETA = -0.36. QINF = 300.3,

RNPU = 2.4E+06, CNWP = 0.2446

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.697 0.000 0.821 0.000 0.896** 0.010 -0.976

0.060 -0.669 0.020 -0.910 0.020 -0.792 0.020 -0.976

0.110 -0.611 0.040 -0.698 0.060 -2.987" * 0.060 -0.993

0.200 -0.383 0.060 -0.807 0.090 -0.845 0.110 -0.922

0.230 -0.376 0.090 -0.772 0.110 -0.867 0.140 -0.936

0.400 -0.202 0.130 -0.779 0.130 -0.772 0.190 - 1.957**

0.490 -0.189 0.150 -0.781 0.150 -0.801 0.250 -0.940

0.590 -0.270 0.200 -0.664 0.210 -0.768 0.400 -0.727

0.630 -0.258 0.250 -0.789 0.250 -0.799 0.490 -0.439

0.700 -0.179 0.260 -0.731 0.340 -0.817 0.580 -0.321

0.750 -0.270 0.280 -0.767 0.370 -0.775 0.650 -0.315

0.810 -0.290 0.290 -0.752 0.400 -0.834 0.700 -0.319

0.840 -0.240 0.310 -0.764 0.410 2.553" * 0.750 -0.387

0.900 -0.129 0.320 -0.753 0.430 -0.810 0.800 -0.362

0.960 -0.048 0.340 -0.736 0.440 -0.768 0.830 -0.275

0.350 -0.441 ** 0.460 -0.649 0.900 -0.134

0.370 -0.730 0.490 -0.248 0.960 0.015

0.380 -0.787 0.500 -0.278

0.400 -0.676 0.520 -0.197

0.410 -0.708 0.540 -0.179

0.430 -0.303 0.550 -0.186

0.440 -0.183 0.580 -0.235

0.460 -0.200 0.600 -0.163

0.470 -0.127 0.610 -0.181

0.490 -0.122 0.650 0.669**

0.500 -0.155 0.700 -0.332

0.520 -0.148 0.750 -0.397

0.530 -0.139 0.820 -0.320

0.550 -0.199 0.890 -0.096

0.560 -0.189 0.900 -0.073

0.580 -0.186 0.960 0.059

0.590 -0.233

0.600 -0.261

0.640 -0.319

0.700 -0.309

0.750 -0.033**

0.820 -0.256

0.870 -0.214

0,930 -0.089

0.960 -0.024

Lower Surface

0.020 -0.158 0.020 0.017 0.020 0.115 0.020 0.440

0.1 l 0 -0.227 0.060 0.025 0.060 0. l 01 0.060 1.069**

0.230 -0.066 0.090 -0.054 0.090 1.014"* 0.110 -0.025

0.400 -0.057 0.120 -0.108 0.120 -0.311 0.250 -0.206

0.490 -0.067 0.200 -0. l 15 0.200 -0.187 0.400 -0.225

0.630 1.758" * 0.260 -0.229 0.250 -0.185 0.490 -0.310

0.750 0.017 0.400 -0.148 0.400 -0.178 0.580 -0.316

0.850 0.1 04 0.490 -0.163 0.490 -0.052 0.650 -0.138

0.900 0.199 0.580 -0.138 0.580 -0.198 0.750 0.101

0.960 0.159 0.640 0.051 0.650 -0.045 0.830 0.281

0.750 0.181 0.750 -0.052 0.900 0.32 l

0.870 0.230 0.890 0.272 0.960 0.257

0.930 0.208 0.930 0.236

0.960 0.176 0.960 - 1.999 **

CN = 0.251 0.417 0.402 0.487

328
Table F-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 14-6-28-000, MINF = 0.849, Camber = 0/2, ALPT = 7.11, BETA = -0.27, QINF = 296.4,

RNPU = 2.3E+06, CNWP = 0.3184

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.841 0.000 0,752 0.000 0.930"* 0.010 - 1.044

0.060 -0.805 0.020 - 1.069 0.020 -0.929 0.020 - 1.134

0.110 -0.795 0.040 -0,826 0.060 -3.046"* 0.060 - 1.145

0.200 -0.655 0.060 -0.940 0.090 -0.980 0.110 - 1.031

0.230 -0.506 0.090 -0.951 0.1 l0 -0.994 O. 140 - 1.105

0.400 -0.247 0.130 -0.941 0.130 -0.914 0.190 - 1.980 **

0.490 -0.170 0.150 -0.948 0.150 -0.994 0.250 - 1,065

0.590 -0.255 0.200 -0.830 0.210 -0.897 0.400 -0.813

0.630 -0.236 0.250 -0.914 0.250 -0.925 0,490 -0.714

0.700 -0.186 0.260 -0.848 0.340 -0.947 0.580 -0.613

0.750 -0.279 0.280 -0.883 0.370 -0.933 0.650 -0.327

0.810 -0.314 0.290 -0.893 0.400 -0,970 0.700 -0.310

0.840 -0,275 0,310 -0.903 0.410 2,589"* 0.750 -0.301

0.900 -0.169 0,320 -0.896 0.430 -0.955 0.800 -0.287

0.960 -0.104 0.340 -0.857 0.440 -0.911 0.830 -0.212

0.350 -0.502** 0.460 -0.930 0.900 -0,079

0.370 -0.855 0.490 -0.821 0.960 0.017

0.380 -0.920 0.500 -0.959

0.400 -0.820 0.520 -0.896

0.410 -0.898 0.540 -0.882

0.430 -0,866 0.550 -0.579

0.440 -0.841 0.580 -0.422

0.460 -0.937 0.600 -0.312

0.470 -0.860 0.610 -0.249

0.490 -0,885 0.650 0.776**

0.500 -0.567 0.700 -0.215

0,520 -0.430 0.750 -0.303

0.530 -0.294 0.820 -0.215

0.550 -0.264 0.890 -0.071

0.560 -0.191 0.900 -0.061

0.580 -0.159 0.960 0.054

0.590 -0.166

0.600 -0.183

0.640 -0.171

0.700 -0.211

0,750 -0.035"*

0.820 -0.215

0.870 -0.226

0.930 -0.103

0.960 -0.037

Lower Surface

0,020 -0.082 0.020 0.169 0.020 0.245 0.020 0.563

0.110 -0.173 0.060 0.097 0,060 0.156 0.060 1.085 **

0.230 -0.053 0.090 0.003 0.090 1.030** 0.110 0.038

0.400 -0.059 0.120 -0.048 0.120 -0,243 0.250 -0.154

0.490 -0.081 0.200 -0.070 0.200 -0.114 0.400 -0.167

0.630 1.783** 0.260 -0.186 0.250 -0_ 115 0.490 -0.259

0.750 0.008 0.400 -0.117 0.400 -0.128 0.580 -0.288

0.850 O. 103 0.490 -0.143 0.490 -0.058 0.650 -0.126

0.900 O. 159 0,580 -0.141 0.580 -0.176 0.750 0.099

0.960 O. 138 0.640 0.039 0,650 -0.059 0.830 0.287

0.750 O. 177 0.750 -0.065 0.900 0.327

0.870 0.226 0.890 0.263 0.960 0.257

0.930 0.206 0,930 0.242

0,960 0.158 0,960 - 2.050"*

CN = 0.311 0.541 0,529 0.606

329
Table F-2. Continued.

Flight 191, Wing sweep = 26 °, Time = 9-43-28-000, MINF = 0.847, Camber = 5/2. ALPT = 6.05, BETA = -0.03, QINF = 289.2,

RNPU = 2.3E+06, CNWP = 0.3660

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.162 0.000 0.756 0.000 -5.023 ** 0.010 -0.450

0.060 -0.126 0.020 -0.179 0.020 -0.001 0.020 -0.271

0.110 -0.343 0.040 -0.055 0.060 -0.220"* 0.060 -0.670

0.200 -0.836 0.060 -0.325 0.090 -0.378 0.110 -0.839

0.230 -0.813 0.090 -0.422 0.110 -0.655 0.140 -0.977

0.400 -0.114 0.130 -0.568 0.130 -0.722 0.190 -5.699"*

0.490 -0.131 0.150 -0.763 0.150 -0.817 0.250 - 1.003

0.590 -0.222 0.200 -0,757 0.210 -0.933 0.400 -0.555

0.630 -0.240 0.250 -0.924** 0.250 -0.885 0.490 -0,428

0,700 -0.179 0.260 -0.814 0.340 -0.909 0.580 -0.393

0.750 -0.227 0.280 -0.893 0.370 -0.905 0,650 -0.38 I

0.810 -0.279 0.290 -0.888 0.400 -0.933 0.700 -0.381

0.840 -0.199 0.310 -0.814 0.410 -0.859 0.750 -0.416

0.900 -0.098 0.320 -0,789 0.430 -0.921 0.800 -0.391

0.960 -0.019 0.340 -0.840 0.440 -0.857 0.830 -0.298

0.350 -0.416"* 0.460 -0.707 0.900 -0.144

0.370 -0.803 0.490 -0.339 0.960 0.039

0.380 -0.850 0.500 -0.314

0.400 -0.750 0.520 -0.239

0.410 -0.866 0.540 -0,222

0.430 -0.837 0.550 -0.225

0.440 -0.768 0.580 -0.202

0,460 -0.710 0.600 -0.211

0.470 -0.369 0.610 -0.155

0.490 -0.230 0.650 -2.865"*

0.500 -0.176 0,700 -0.334

0.520 -0.174 0.750 -0.393

0.530 -0.113 0,820 -0.295

0.550 -0.158 0.890 -0.080

0.560 -0.128 0.900 -0.071

0.580 -0.129 0.960 0.042

0.590 -0.156

0.600 -0.225

0.640 -2.697**

0.700 -0.266

0.750 -0.263

0.820 -2.878**

0,870 -0.200

0.930 -0,075

0.960 0.019

Lower Surface

0.020 -0.651 0.020 -0.678 0.020 -0.281 0.020 0.075

0.110 -0.204 0.060 -0.051 0.060 0.067 01060 3.062" *

0.230 -0.004 0.090 -0.135 0.090 -0,055 0.110 -01056

0.400 -0.059 0.120 -0.083 0.120 -0,433"* 0.250 -0.153

0.490 -0.093 0,200 0.023 0.200 -0.104 0.400 -0.187

0.630 3.088 * * 0.260 -0.157 0.250 -0.105 0.490 -0.277

0.750 0.035 0.400 -2.895 ** 0.400 -0.125 0.580 -0.293

0.850 0.104 0.490 -0. t 25 0.490 0.015 0.650 -0.121

0.900 0.191 0.580 -0.057 0.580 -0.184 0.750 0.149

0.960 0.156 0,640 0.281 0.650 0,040 0.830 0.299

0.750 0.191 0.750 0.278 0.900 0.374

0.870 0,232 0.890 ******** 0.960 0.286

0.930 0.240 0.930 0.271

0.960 0.171 0.960 -2.625 * *

CN = 0.242 0.432 0.488 0.478

330
Table F-2. Continued.

Flight 191, Wing sweep = 26 °, Time = 9-43-34-500, MINF = 0.850, Camber = 5/2, ALPT = 7.07, BETA = 0.10, Q1NF = 292,9,

RNPU = 2.3E+06, CNWP = 0.4629

r 1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP a/c CP

0.020 0.048 0.000 0.847 0.000 -4.974"* 0.010 -0.757

0.060 -0.208 0.020 -0.299 0.020 -0.141 0.020 -0.467

0.1 I0 -0.381 0.040 -0.155 0.060 -0.241 ** 0.060 -0.775

0.200 -0.856 0.060 -0.430 0.090 -0.597 0, ] 10 -0.929

0.230 -0.825 0,090 -0.472 0.110 -0.76 t 0.140 - 1.062

0.400 -0.684 0.130 -0.640 0.130 -0.811 0.190 -5.642"*

0.490 -0.147 0.150 -0.810 0.150 -0.902 0.250 - 1.061

0.590 -0.164 0,200 -0.803 0.210 -0.963 0.400 -0.758

0.630 -0.194 0,250 -0.992"* 0.250 -0.940 0.490 -0.620

0.700 -0.153 0.260 -0.851 0.340 -0.976 0.580 -0.490

0,750 -0.223 0.280 -0.949 0.370 -0.959 0,650 -0.481

0.810 -0.259 0.290 -0.948 0.400 -0.987 0,700 -0.506

0.840 -0.210 0.310 -0.877 0.410 -0.935 0.750 -0.343

0.900 -0. 123 0.320 -0.853 0430 - 1.003 0.800 -0.311

0.960 -0.047 0.340 -0.922 0.440 -0.951 0,830 -0.249

0.350 -0.410"* 0.460 -0.986 0.900 -0.094

0.370 -0.869 0.490 -0.923 0.960 0.057

0.380 -0.901 0.500 - 1.012

0.400 -0.814 0.520 -0.989

0.410 -0,931 0.540 - 1.003

0.430 -0.907 0.550 -0.968

0.440 -0.818 0.580 -0.578

0.460 -0.968 0.600 -0.431

0.470 -0.901 0.610 -0.287

0.490 -0.876 0.650 -2.843**

0,500 -0.877 0.700 -0.214

0.520 -0.874 0.750 -0.295

0.530 -0.855 0.820 -0.205

0.550 -0.870 0.890 -0.049

0.560 -0.480 0.900 -0.027

0.580 -0.327 0.960 0.054

0.590 -0.288

O.600 -0.276

0.640 -2.677**

0.700 -0.130

0.750 -0.147

0.820 -2.855**

0.870 -0.163

0.930 -0.039

0.960 0.024

Lower Surface

0.020 -0.533 0.020 -0.222 0.020 -0.101 0.020 0.241

0.110 -0.173 0.060 0.054 0.060 0.148 0.060 3.010"*

0.230 0.040 0.090 -0.032 0.090 0.032 O.110 0.029

0.400 -0.027 0.120 0.003 0.120 -0.331 ** 0.250 -0,096

0.490 -0.076 0.200 0,057 0.200 -0.052 0.400 -0.124

0,630 3.035** 0.260 -0.094 0.250 -0.027 0.490 -0.249

0.750 0.039 0.400 -2.873 ** 0.400 -0.081 0.580 -0.262

0.850 0.092 0.490 -0.103 0.490 0,009 0,650 -0.076

0.900 0.188 0,580 -0.048 0.580 -0.147 0.750 0.173

0.960 0.154 0.640 0,304 0.650 0.051 0.830 0.325

0.750 0.206 0.750 0.284 0.900 0.392

0.870 0,245 0,890 ******** 0.960 0.302

0.930 0.268 0.930 0.291

0.960 0.178 0.960 -2.606**

CN = 0.349 0.546 0.625 0.597

331
Table F-2. Continued.

Flight 191, Wing sweep -- 26 °, Time = 9-43-39-000, MINF = 0.852, Camber - 5/2, ALPT = 7.95, BETA -- -0.03, QINF = 297.4,

RNPU = 2.3E+06, CNWP = 0.5531

I1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.078 0.000 0.893 0.000 -4.920** 0.010 -0.826

0.060 -0.336 0.020 -0.479 0.020 -0.259 0.020 -0.686

O. 110 -0.424 0.040 -0.253 0.060 -0.379"* 0.060 -0.808

0.200 -0.882 0.060 -0.539 0.090 -0.717 0.110 - 1.025

0.230 -0.856 0.090 -0.610 0.110 -0.868 0.140 -1.136

0.400 -0.778 0.130 -0.710 0.130 -0.876 0.190 -5.577"*

0.490 -0.656 0.150 -0.861 0.150 -0.963 0.250 - 1.167

0.590 -0.172 0.200 -0.858 0.210 - 1.035 0.400 -0.822

0.630 -0.193 0.250 - 1.020"* 0.250 -0.990 0.490 -0.773

0.700 -0.152 0.260 -0.898 0.340 - 1.046 0.580 -0.638

0.750 -0.219 0.280 -0.989 0.370 - 1.015 0.650 -0.569

0.810 -0.254 0.290 - 1.017 0.400 - 1.030 0.700 -0.628

0.840 -0.206 0.310 -0.931 0.410 -0.999 0.750 -0.609

0.900 -0.157 0.320 -0.921 0.430 - 1.072 0.800 -0.247

0.960 -0.074 0.340 -0.962 0.440 - 1.023 0.830 -0.176

0.350 -0.415"* 0.460 - 1.067 0.900 -0.038

0.370 -0.924 0.490 -0.952 0.960 0.036

0.380 -0.946 0.500 - 1.080

0.400 -0.858 0.520 -1.017

0.410 -0.986 0.540 - 1.049

0.430 -0.974 0.550 - 1.032

0,440 -0.901 0.580 - 1.002

0,460 - 1.044 0.600 - 1.007

0.470 -0.957 0.610 -0.938

0.490 -0.939 0.650 -2.820**

0.500 -0.925 0.700 -0.408

0.520 -0.951 0.750 -0.455

0.530 -0.909 0.820 -0.148

0.550 -0.938 0.890 0.006

0.560 -0.956 0.900 0.014

0.580 -0.934 0.960 0.084

0.590 -0.935

0.600 - 1.006

0.640 -2.658**

0.700 -0.237

0.750 -0.071

0.820 -2.833**

0.870 -0.087

0.930 0.014

0.960 0.055

Lower Surface

0.020 -0.341 0.020 -0.036 0.020 0.035 0.020 0.362

0.110 -0.113 0.060 0.118 0.060 0.235 0.060 2.944**

0.230 0.067 0.090 0.033 0.090 0.099 0. 110 0.058

0.400 -0.033 0.120 0.049 0.120 -0.256** 0.250 -0.039

0.490 -0.088 0.200 0.079 0.200 -0.018 0.400 -0.091

0.630 2.969"* 0.260 -0.048 0.250 0.019 0.490 -0.192

0.750 0.021 0.400 -2.850** 0.400 -0.065 0.580 -0.214

0.850 0.099 0.490 -0.078 0.490 0.040 0.650 -0.070

0.900 0.183 0.580 -0.042 0.580 -0.136 0.750 0.179

0.960 0.133 0.640 0.308 0.650 0.052 0.830 0.322

0.750 0.204 0.750 0.281 0.900 0.386

0.870 0.260 0.890 ******** 0.960 0.300

0.930 0.255 0.930 0.300

0.960 0.184 0.960 -2.588**

CN = 0.430 0.662 0.750 0.702

332
Table F-2. Continued.

Flight 191, Wing sweep = 26 °, Time = 9-43-41-000, MINF = 0.853, Camber = 5/2, ALPT = 9.02, BETA = -0.01, QINF = 300.3,

RNPU = 2.4E+06, CNWP = 0.5452

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,203 0.000 0.913 0,000 -4.887"* 0.010 -0.782

0.060 -0.444 0,020 -0.627 0.020 -0.400 0.020 -0.848

0.110 -0.567 0.040 -0.325 0.060 -0.376** 0.060 -0.958

0.200 -0.939 0,060 -0.626 0.090 -0.799 0.110 - 1.094

0.230 -0,871 0.090 -0.730 0.1 l0 -0.959 0.140 -1.175

0.400 -0,832 0.130 -0.814 0.130 -0.964 0.190 -5.538**

0.490 -0.744 0.150 -0.948 0.150 - 1.029 0.250 - 1.242

0,590 -0.205 0.200 -0.929 0.210 - 1.105 0.400 -0.862

0.630 -0.183 0.250 - 1.116"* 0.250 - 1.060 0.490 -0.813

0.700 -0.144 0.260 -0,958 0,340 - 1.128 0.580 -0.712

0.750 -0.232 0,280 - 1.060 0.370 - 1.100 0.650 -0.631

0.810 -0.282 0.290 -1.073 0.400 -1.100 0.700 -0.711

0.840 -0,234 0.310 - 1.013 0.410 - 1.067 0.750 -0.538

0.900 -0.173 0,320 -0.976 0.430 - 1.131 0.800 -0.259

0.960 -0.091 0,340 - 1.036 0.440 - 1.086 0.830 -0.175

0.350 -0,407** 0.460 - 1.129 0.900 -0,055

0,370 -0.998 0.490 - 1.024 0.960 -0.002

0.380 -1.013 0.500 -1.132

0.400 -0.937 0.520 - 1.077

0.410 -1,051 0.540 -1.122

0.430 -1.030 0.550 -1.109

0.440 -0.963 0.580 - 1.010

0.460 - 1.1 04 0.600 -0.680

0.470 - 1.013 0.610 -0.467

0.490 -0.915 0.650 -2.808 * *

0.500 -0.954 0,700 -0.454

0.520 -0.837 0.750 -0.530

0.530 -0.742 0,820 -0.324

0.550 -0,530 0.899 -0.132

0.560 -0.491 0.900 -0.154

0.580 -0,449 0.960 -0.061

0.590 -0.467

0.600 -0.475

0.640 -2.647"*

0.700 -0.337

0,750 -0.200

0.820 -2.820**

0.870 -0.125

0,930 -0.085

0.960 -0.074

Lower Surface

0.020 -0.189 0.020 0.106 0,020 0.168 0.020 0.518

0.1 I 0 -0.080 0.060 0.205 0.060 0.297 0.060 2.901 **

0.230 0.112 0.090 0.109 0.090 0.182 0.110 0.139

0.400 -0.003 0.120 0.126 0,120 -0.194"* 0.250 0.029

0.490 -0.080 0.200 0.125 0.200 0.012 0.400 -0.039

0.630 2.925"* 0.260 -0.018 0.250 0,063 0.490 -0.160

0.750 0.012 0.400 -2.838** 0.400 -0.019 0.580 -0.202

0,850 0.079 0.490 -0.073 0.490 0.017 0.650 -0.062

0.900 0.148 0.580 -0.056 0.580 -0.120 0.750 0.173

0,960 0.130 0.640 0.292 0.650 0.052 0.830 0.334

0.750 0.185 0.750 0.263 0.900 0.397

0.870 0.220 0.890 ******** 0.960 0.276

0.930 0.190 0.930 0.262

0.960 0.105 0.960 -2.578* *

CN = 0.484 0.678 0.811 0.783

333
Table F-2. Continued.

Flight 195. Wing sweep = 26", Time = 10-44-14-000, MINF = 0.851, Camber = 5/2, ALPT = 6.08, BETA = 0.18, QINF = 288.6,

RNPU = 2.3E+06, CNWP = 0.3727

11 = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 0.145 0.000 0.778** 0.000 -4.690** 0.010 -0.504

0,060 -0.154 0.020 -0.193 0.020 -0.027 0.020 -0.265

0.110 -0.338 0.040 -0.063 0.060 -0.921 ** 0.060 -0.709

0.200 -0.852 0.060 -0.350 0.090 -0.496 0.110 -0.860

0,230 -0.808 0.090 -0.426 0.110 -0.669 0.140 1.949"*

0.400 -0,162 0.130 -0.592 0.130 -0.733 0.190 -4.552"*

0.490 -0.121 0.150 -0.778 0.150 -0.839 0.250 - 1.028

0.590 -0.193 0.200 -0.773 0.210 -0.929 0,400 -0.715

0.630 -0.218 0.250 -0,935 0.250 -0.896 0.490 -0.472

0.700 -0.184 0.260 -0.803 0.340 -0.952 0.580 -0.420

0.750 -0.229 0.280 -0.889 0.370 -0.942 0.650 -0.445

0.810 -0.261 0.290 -0.893 0.400 -0.936 0.700 -0.413

0.840 -0.204 0.310 -0.821 0.410 -0.902 0.750 -0.396

0.900 -0.107 0.320 -0.813 0.430 -0.948 0.800 -0.363

0,960 -0,036 0.340 -0.865 0,440 -0900 0.830 -0.297

0.350 -0.410"* 0.460 -0.918 0.900 -0.134

0.370 -0.824 0.490 -0.794 0,960 0.039

0.380 -0.855 0.500 -0,543

0.400 -0.768 0.520 -0.385

0.410 -0.878 0.540 -0.340

0.430 -0.832 0.550 -0.299

0,440 -0.726 0.580 -0.250

0.460 -0.962 0.600 -0.264

0.470 -0.877 0.610 -0.113

0.490 -0.759 0,650 - 1.720"*

0.500 -0.360 0.700 -0.276

0.520 -0.319 0.750 -0.350

0.530 -0.191 0.820 -0.270

0.550 -0.180 0.890 -0.085

0.560 -0.128 0.900 -0.059

0.580 -0.116 0.960 0,030

0.590 -0.156

0.600 -0.164

0640 - 1.553"*

0.700 -0.225

0.750 -0.234

0.820 -1.733"*

0.870 -0.194

0.930 -0.061

0.960 0.014

Lower Surface

0.020 -0.580 0.020 0,153 0.020 -0.259 0.020 0.092"*

O. 110 -0,205 0.060 -0.025 0.060 0.044 0.060 2.042**

0,230 0,003 0.090 -0.107 0,090 -0.053 O. 110 -0.065

0.400 -0.068 O. 120 -0,073 O. 120 -0.423 0.250 -0.147

0.490 -0.083 0.200 0.025 0.200 -0.098 0.400 -0.166

0.630 2.087** 0.260 -0.140 0.250 -0.091 0.490 -0.271

0,750 0.029 0.400 - 1.751 ** 0.400 -0.144 0.580 -0.293

0.850 0.119 0.490 -0.142 0,490 0.003 0.650 -0.119

0.900 0.187 0.580 -0.070 0.580 -0.182 0.750 0.156

0.960 0.150 0.640 0.288 0.650 0.020 0.830 0.297

0.750 0.165 0.750 0.270 0.900 0.378

0.870 0.229 0.890 ******** 0.960 0.287

0.930 0.243 0.930 0.282

0.960 0.163 0.960 - 1.750"*

CN = 0.250 0.450 0.500 0.510

334
Table F-2, Continued,

Flight 195, Wing sweep = 26 °, Time = 10-44-36-000, MINF = 0.855, Camber = 5/2, ALPT = 7.04, BETA = 0.18, QINF = 290.3,

RNPU = 2.3E+06. CNWP = 0.4688

rl = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.054 0.000 0.831 ** 0.000 -4.655** 0.010 -0,733

0.060 -0.212 0.020 -0.304 0.020 -0.136 0.020 -0.452

0.110 -0.387 0.040 -0.148 0,060 -0,895"* 0.060 -0.785

0.200 -0,866 0.060 -0.436 0.090 -0.605 O. 110 -0.940

0,230 -0.835 0,090 -0.470 0.110 -0.770 0.140 1,938"*

0.400 -0,700 0,130 -0.634 0.130 -0.808 0,190 -4.518 * *

0.490 -0.215 0,150 -0.811 0.150 -0.887 0,250 -1.059

0.590 -0.164 0,200 -0.801 0.210 -0.984 0,400 -0.782

0.630 -0.190 0,250 -0.976 0.250 -0,943 0.490 -0.686

0.700 -0.1 64 0,260 -0,854 0,340 - 1.003 0.580 -0.541

0.750 -0.220 0.280 -0,950 0,370 - 1,002 0,650 -0,515

0,810 -0.260 0.290 -0,950 0,400 -0.983 0,700 -0,534

0.840 -0,211 0.310 -0.867 0.410 -0,954 0,750 -0,567

0.900 -0.137 0.320 -0.863 0.430 - 1.015 0,800 -0,272

0.960 -0.058 0,340 -0,917 0.440 -0.957 0,830 -0.230

0.350 -0.411 * * 0.460 -0.982 0.900 -0.068

0.370 -0.872 0.490 -0903 0.960 0.046

0.380 -0,902 0.500 - 1.018

0,400 -0,835 0.520 -0.982

0.410 -0,939 0,540 - 1.028

0.430 -0.918 0.550 -0.979

0.440 -0.822 0.580 -0.948

0.460 - 1.017 0.600 -0_923

0.470 -0.898 0,610 -0.639

0,490 -0.890 0,650 - 1.703"*

0.500 -0.909 0.700 -0.252

0.520 -0,885 0.750 -0.300

0.530 -0,861 0.820 -0.174

0,550 -0,899 0.890 -0.043

0.560 -0,899 0.900 -0.019

0.580 -0.837 0.960 0.056

0.590 -0.603

0,600 -0.457

0,640 -1,536**

0,700 -0.130

0.750 -OA 14

0.820 -1.715"*

0.870 -0.145

0.930 -0.038

0.960 0.029

Lower Surface

0.020 -0,588 0.020 -0.180 0.020 -0.137 0,020 0,224**

0.1 I 0 -0,169 0,060 0,048 0.060 0.120 0.060 2,038"*

0.230 0.042 0,090 -0.032 0.090 0.017 0.110 0,006

0.400 -0.057 0,120 -0.019 0.120 -0.355 0,250 -0,098

0.490 -0,087 0.200 0.059 0,200 -0.055 0,400 -0.127

0.630 2.083** 0,260 -0.109 0,250 -0.045 0.490 -0,239

0.750 0,017 0.400 -1.733'* 0.400 -0.115 0,580 -0.263

0.850 0,114 0A90 -0.118 0.490 0.010 0.650 -0.103

0.900 0.177 0,580 -0.054 0,580 -0.155 0.750 0.152

0.960 0.140 0.640 0,298 0,650 0,035 0.830 0.303

0.750 0.171 0,750 0.276 0.900 0,390

0.870 0.245 0,890 ******** 0,960 0.290

0.930 0.257 0.930 0.288

0.960 0.173 0.960 -1.732"*

CN = 0.349 0,552 0,630 0.598

335
Table F-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-45-4-500, MINF = 0.851, Camber = 5/2, ALPT = 7.9l, BETA = -0.08, QINF = 271.7,

RNPU = 2.1E+06, CNWP = 0.5256

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.091 0.000 0.895"* 0.000 -4.860"* 0.010 -0,790

0.060 -0.344 0.020 -0.500 0.020 -0.280 0.020 -0.770

0.110 -0.435 0.040 -0.249 0.060 -0.975** 0.060 -0.822

0.200 -0.895 0.060 -0.586 0.090 -0.734 0.110 - 1.009

0.230 -0.834 0.090 -0.630 0.110 -0.876 0.140 2.087**

0.400 -0,769 0.130 -0.733 0.130 -0.888 0.190 -4.713"*

0.490 -0.561 0.150 -0.877 0.150 -0.977 0.250 - 1,178

0.590 -0.164 0.200 -0.852 0.210 - 1.051 0.400 -0.834

0.630 -0.178 0.250 - 1.034 0.250 - 1.016 0.490 -0.769

0.700 -0.151 0.260 -0.904 0.340 -1.072 0.580 -0.631

0.750 -0.215 0.280 - 1.009 0.370 - 1.055 0.650 -0.593

0.810 -0.262 0.290 - 1.003 0.400 -1.067 0.700 -0.637

0.840 -0.217 0.310 -0.928 0.410 - 1.029 0.750 -0.509

0.900 -0.152 0.320 -0.925 0.430 - 1.085 0.800 -0.235

0.960 -0.069 0.340 -0.987 0.440 - 1.029 0.830 -0.178

0.350 -0.412" * 0.460 - 1.052 0.900 -0.036

0.370 -0.931 0.490 -0.973 0.960 0.038

0.380 -0.957 0.500 - 1.082

0,400 -0.876 0.520 -1.052

0.410 - 1.001 0,540 - 1.082

0.430 -0.977 0.550 - 1.044

0.440 -0.871 0.580 - 1.035

0.460 - 1.097 0.600 - 1.037

0.470 -0,979 0.610 -0.930

0.490 -0.956 0.650 - 1.706**

0.500 -0.961 0.700 -0.336

0.520 -0.937 0.750 -0.391

0.530 -0.919 0.820 -0.123

0.550 -0.944 0.890 -0.012

0.560 -0,965 0.900 0.002

0.580 -0.929 0.960 0.068

0.590 -0.889

0.600 -0.660

0.640 -1.528"*

0.700 -0.203

0.750 -0.074

0.820 -1.720"*

0.870 -0.099

0.930 -0.009

0.960 0.048

Lower Surface

0.020 -0.339 0.020 -0.108 0.020 0.025 0.020 0.347**

0.110 -0.105 0.060 0.145 0.060 0.231 0.060 2.290**

0.230 0.081 0.090 0.047 0,090 0.101 0.110 0.034

0.400 -0.032 0.120 0.037 0.120 -0.305 0.250 -0.030

0.490 -0.072 0.200 0.107 0.200 -0.027 0.400 -0.071

0.630 2.338"* 0.260 -0.060 0.250 0.017 0.490 -0.189

0.750 0.026 0.400 - 1.739* * 0.400 -0.068 0.580 -0.219

0.850 0.108 0.490 -0.089 0.490 0.035 0.650 -0.077

0.900 0.172 0.580 -0.034 0.580 -0.121 0.750 0.179

0.960 0.134 0.640 0.323 0.650 0.045 0.830 0.321

0.750 0.181 0.750 0.287 0.900 0.399

0.870 0.227 0.890 ******** 0.960 0.290

0.930 0.250 0.930 0.290

0.960 0.164 0.960 - 1.737"*

CN = 0.427 0.633 0.730 0.693

336
Table F-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-45-22-500, MINF = 0.861, Camber = 5/2, ALPT = 8.03, BETA = -0.14, QINF = 286.9,

RNPU = 2.2E+06, CNWP = 0.5330

rI = 0.93 0.76 0.59 040

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.064 0.000 0,892* * 0.000 -4.660* * 0.010 -0.804

0.060 -0,308 0.020 -0.445 0,020 -0.252 0.020 -0.719

0.110 -0.424 0.040 -0.240 0.060 - 1,016"* 0,060 -0,812

0.200 -0.900 0,060 -0,534 0.090 -0.707 0.110 - 1.009

0.230 -0.821 0.090 -0.608 0,110 -0,860 0,140 1.959"*

0.400 -0.776 0,130 -0,706 0,130 -0.877 0.190 -4,521 **

0.490 -0.684 0.150 -0.859 0.150 -0,928 0,250 - I. 142

0.590 -0.270 0.200 -0,835 0,210 - 1.031 0.400 -0,823

0.630 -0.184 0.250 - 1,040 0.250 - 1.004 0.490 -0.770

0.700 -0.131 0.260 -0.896 0.340 - 1.059 0.580 -0.665

0.750 -0.207 0.280 -0.986 0.370 - 1.043 0.650 -0.615

0.810 -0.259 0.290 - 1.018 0.400 - 1.037 0.700 -0,648

0.840 -0.194 0.310 -0.920 0.410 - 1.018 0.750 -0,700

0.900 -0.153 0.320 -0.906 0.430 - 1.087 0,800 -0,320

0.960 -0.077 0.340 -0.968 0.440 - 1.019 0,830 -0.219

0.350 -0.412"* 0.460 - 1.050 0.900 -0,056

0,370 -0.920 0.490 -0.956 0.960 0.008

0.380 -0.951 0.500 - 1.057

0.400 -0.875 0.520 - 1.026

0.410 -0,990 0.540 - 1.066

0.430 -0.962 0.550 - 1.039

0,440 -0.862 0,580 -1.028

0,460 - 1.088 0,600 - 1.032

0,470 -0.979 0.610 -0.936

0.490 -0.949 0.650 -1.673"*

0.500 -0.944 0.700 -0.483

0.520 -0.955 0.750 -0.502

0.530 -0.918 0.820 -0.221

0.550 -0.952 0.890 -0.044

0.560 -0.958 0.900 -0.043

0.580 -0.919 0.960 -0.002

0.590 -0.955

0.600 -0.928

0.640 -1.504**

0.700 -0.323

0.750 -0.164

0.820 -1.686**

0.870 -0,094

0.930 -0.035

0.960 0.003

Lower Surface

0.020 -0.352 0.020 -0.045 0,020 0.013 0.020 0.354"*

0.110 -0.125 0.060 0.130 0.060 0.221 0.060 2.112"*

0.230 0.070 0.090 0.036 0.090 0.100 0.110 0.052

0.400 -0,050 0.120 0.039 0.120 -0.292 0.250 -0,036

0.490 -0.111 0,200 0.097 0,200 -0.023 0.400 -0.083

0.630 2.157"* 0,260 -0.069 0.250 0,004 0,490 -0.206

0.750 0.013 0.400 - 1.704" * 0,400 -0.081 0.580 -0.257

0.850 0.099 0,490 -0.104 0.490 0.014 0.650 -0.100

0.900 0.165 0.580 -0.055 0,580 -0.149 0.750 0.158

0.960 0.133 0.640 0.295 0,650 0.031 0.830 0.310

0,750 0.177 0.750 0.283 0.900 0.392

0.870 0,223 0,890 ******** 0.960 0.281

0,930 0.222 0,930 0.279

0.960 0.125 0.960 - 1,703"*

CN = 0.421 0.651 0.742 0,694

337
Table F-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-45-27-500, MINF = 0.861, Camber = 5/2, ALPT = 9.21, BETA = -0.19, QINF = 288.6,

RNPU = 2.3E+06, CNWP = 0.5588

"q -- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.217 0.000 0.897** 0.000 -4.645** 0.010 -0.753

0.060 -0.448 0.020 -0.657 0.020 -0.405 0.020 -0.843

0.110 -0.584 0.040 -0.343 0.060 - 1.007"* 0.060 -0.980

0.200 -0.946 0.060 -0.625 0.090 -0.820 0.110 - 1.062

0.230 -0.853 0,090 -0.729 0.110 -0.974 0.140 1.955"*

0.400 -0.847 0.130 -0.828 0.130 -0.970 0.190 -4.507 **

0.49t3 -0.730 0,150 -0.954 0.150 - 1.024 0.250 - 1.222

0,590 -0.179 0.200 -0,943 0.210 - 1.111 0.400 -0.887

0.630 -0.169 0.250 - 1.084 0.250 - 1.071 0.490 -0.812

0,700 -0.155 0.260 -0.966 0.340 - 1.147 0.580 -0.746

0,750 -0.255 0.280 - 1.061 0.370 - I. 108 0.650 -0.653

0.810 -0.287 0.290 - 1.075 0.400 - 1.119 0.700 -0.707

0.840 -0.253 0.310 -0.994 0.410 -1.083 0.750 -0.625

0.900 -0.198 0.320 -0.984 0.430 -1.158 0.800 -0.275

0.960 -0.111 0,340 - 1.047 0.440 - 1.097 0.830 -0.186

0.350 -0,402" * 0,460 - 1.125 0.900 -0.082

0,370 -0.995 0.490 - 1.040 0.960 -0.016

0.380 -1.036 0.500 -1.138

0.400 -0.935 0.520 - 1.123

0.410 -1.062 0.540 -1.144

0.430 -0.954 0.550 - 1.101

0.440 -0.811 0.580 -0.801

0.460 -0.917 0,600 -0,643

0.470 -0,634 0.610 -0,477

0.490 -0.621 0.650 - 1.676"*

0.500 -0.525 0.700 -0.459

0.520 -0.512 0.750 -0.541

0.530 -0.443 0.820 -0.373

0.550 -0.464 0.890 -0.206

0.560 -0.438 0.900 -0.219

0.580 -0.424 0,960 -0.160

0.590 -0.442

0.600 -0.484

0.640 - 1.508 **

0.700 -0.364

0,750 -0.269

0.820 -1,689**

0.870 -0.207

0.930 -0.234

0.960 -0.197

Lower Surface

0.020 -0.192 0.020 0.123 0.020 0.145 0.020 0.503 * *

0.110 -0.073 0.060 0.220 0.060 0.305 0.060 2.086**

0.230 0.115 0.090 0.109 0.090 0.179 0.110 0.097

0.4130 -0.043 0.120 0.111 0.120 -0.216 0.250 0.018

0.490 -0.096 0,200 0.129 0.200 0.001 0.400 -0.038

0,630 2.131 ** 0.260 -0.020 0.250 0.060 0.490 -0.1 64

0.750 -0.008 0.400 - 1.707"* 0.400 -0.047 0.580 -0.216

0.850 0.073 0.490 -0,097 0.490 0.016 0.650 -0.082

0.900 0.141 0.580 -0.04 1 0.580 -0.134 0.750 0.159

0.960 0.109 0.640 0.292 0.650 0.030 0.830 0, 311

0.750 0.135 0.750 0.268 0.900 0.392

0.870 0.176 0.890 ******** 0.960 0.276

0.930 0.155 0,930 0.240

0.960 0.046 0.960 - 1.705"*

CN = 0.475 0.647 0.803 0,767

338
Table F-2. Continued.

Flight 195, Wing sweep = 26", Time = 10-45-41-500, MINF = 0.845, Camber = 5/2, ALPT = 11.03, BETA = -0.06, QINF = 281.2,

RNPU = 2.2E+06, CNWP = 0.3657

h = 0.93 0,76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.691 0.000 0.838"* 0.000 -4.789"* 0.010 - 1.101

0.060 -0.696 0.020 - 1.083 0.020 -0.846 0.020 - 1.104

O. 110 -0.759 0.040 -0.690 0.060 - 1.189"* 0.060 - 1.200

0,200 - 1.060 0.060 -0.862 0.090 - 1.023 O. 1 I0 - 1.312

0.230 - 1.005 0.090 -0.924 0.110 - 1.182 0.140 2.029"*

0.400 -0.998 0.130 - 1.023 0.130 - 1.180 0.190 -4.648 * *

0.490 -0.386 0.150 - 1.137 0.150 - 1.220 0.250 -0.986

0.590 -0.219 0.200 -1.113 0.210 -1.191 0.400 -0.814

0.630 -0.233 0.250 - 1.256 0.250 -0.788 0.490 -0.784

0,700 -0.214 0.260 - 1.113 0,340 -0.740 0.580 -0.712

0.750 -0.269 0.280 - 1.219 0.370 -0.708 0.650 -0.582

0.810 -0.350 0.290 -1.258 0.400 -0.697 0.700 -0.616

0,840 -0.275 0.310 - 1.157 0.410 -0.665 0.750 -0.524

0.900 -0.205 0.320 - 1.136 0.430 -0.712 0.800 -0.463

0.960 -0.143 0.340 - 1.215 0.440 -0.642 0.830 -0.440

0.350 -0,431 ** 0,460 -0.656 0.900 -0.330

0.370 - 1.155 0,490 -0.580 0.960 -0.271

0.380 -1.183 0.500 -0.616

0.400 - 1.043 0.520 -0.584

0.410 - 1.040 0.540 -0.601

0.430 -0,869 0.550 -0.593

0.440 -0.735 0,580 -0.589

0.460 -0,868 0.600 -0,586

0.470 -0.697 0.610 -0,421

0.490 -0.653 0.650 - 1 742" *

0.500 -0,604 0,700 -0.481

0.520 -0.606 0.750 -0.551

0.530 -0.505 0.820 -0.431

0.550 -0.505 0.890 -0.403

0.560 -0.421 0.900 -0.354

0.580 -0.384 0.960 -0.363

0.590 -0.350

0.600 -0.342

0.640 -1.570"*

0.700 -0.185

0.750 -0.114

0.820 -1.755"*

0.870 -0.142

0.930 -0.126

0.960 -0.126

Lower Surface

0.020 0.024 0.020 0.206 0.020 0.341 0.020 0.621 **

0.110 0.013 0,060 0.338 0.060 0.421 0.060 2.119"*

0.230 0.159 0,090 0.215 0.090 0.287 0.110 0.217

0.400 -0.012 0.120 0.194 0.120 -0.129 0.250 0.091

0.490 -0.086 0.200 0.187 0.200 0.064 0,400 0.017

0.630 2.165"* 0.260 0.034 0.250 0.130 0.490 -0.112

0.750 -0.007 0.400 - 1.774"* 0.400 -0.006 0.580 -0.180

0.850 0.064 0.490 -0.075 0.490 0.018 0.650 -0.083

0.900 0.125 0.580 -0.041 0.580 -0.121 0.750 0.141

0.960 0.081 0.640 0.288 0.650 0,012 0.830 0.273

0.750 0.139 0.750 0.237 0.900 0.337

0.870 0.180 0.890 ******** 0.960 0.178

0.930 0.156 0.930 0.167

0.960 0.037 0.960 - 1.773"*

CN = 0.549 0.703 0.732 0.815

339
Table F-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-45-49-500, MINF = 0.847, Camber = 5/2, ALPT = 12.01, BETA = 0.02. QINF = 294.4,

RNPU = 2.3E+06, CNWP = 0.3023

rl = 0.93 0,76 0.59 0.40

Upper Surface

x,/c CP x/c CP x./c CP x,/c CP

0.020 -0.809 0.000 0.792"* 0.000 -4.653"* 0.010 - 1.143

0.060 -0.819 0.020 - 1.151 0.020 -0.937 0.020 - 1.167

0.110 -0.880 0.040 -0.772 0.060 -1.193"* 0.060 - 1.258

0.200 - 1.097 0.060 -0.954 0.090 - 1.106 0.110 - 1.379

0.230 - 1.079 0.090 - 1.029 0.110 - 1.270 0.140 1.921 **

0.400 -0.988 0.130 -1 .t 10 0.130 -1.033 0.190 -4.518"*

0.490 -0.400 0.150 - 1.206 0.150 -0.881 0.250 -0.976

0.590 -0.284 0.200 - 1.182 0.210 -0.854 0.400 -0.824

0.630 -0.259 0.250 - 1.324 0.250 -0.735 0.490 -0.783

0.700 -0.216 0.260 - 1.179 0.340 -0.743 0.580 -0.717

0.750 -0.246 0.280 - 1.283 0.370 -0.706 0.650 -0.601

0.810 -0.316 0.290 - 1.290 0.400 -0.708 0.700 -0.647

0.840 -0.275 0.310 - 1.194 0.410 -0.644 0.750 -0.572

0.900 -0.190 0.320 - 1.180 0.430 -0.693 0.800 -0.513

0.960 -0.156 0.340 - 1.179 0.440 -0.618 0.830 -0.520

0.350 -0.390** 0.460 -0.623 0.900 -0.390

0.370 - 1.060 0.490 -0.574 0.960 -0.330

0.380 - 1.039 0.500 -0.612

0.400 -0.891 0.520 -0.580

0.410 -0.909 0.540 -0.607

0.430 -0.810 0.550 -0.603

0.440 -0.695 0.580 -0.568

0.460 -0.858 0.600 -0.565

0.470 -0.743 0.610 -0.442

0.490 -0.660 0.650 - 1.743"*

0.500 -0.587 0.700 -0.504

0.520 -0.583 0.750 -0.589

0.530 -0.431 0.820 -0.476

0.550 -0.405 0.890 -0.414

0.560 -0.293 0.900 -0.376

0.580 -0.271 0.960 -0.351

0.590 -0.244

0.600 -0.247

0.640 -1.579**

0.700 -0.144

0.750 -0.102

0.820 - 1.756"*

0.870 -0.170

0.930 -0.200

0.960 -0.193

Lower Surface

0.020 0.126 0.020 0.195 0.020 0.449 0.020 0.725**

0.110 0.056 0.060 0.397 0.060 0.478 0.060 1.944**

0.230 0.197 0.090 0.279 0.090 0.346 0.110 0.285

0.400 -0.020 0.120 0.249 0.120 -0.043 0.250 0.149

0.490 -0.065 0.200 0.211 0.200 0.094 0.400 0.064

0.630 1.988"* 0.260 0.080 0.250 0.t83 0.490 -0.073

0.750 -0.035 0.400 -1.773"* 0.400 0.020 0.580 -0.141

0.850 0.045 0.490 -0.057 0.490 0.016 0.650 -0.073

0.900 0.109 0.580 -0.029 0.580 -0.102 0.750 0.150

0.960 0.052 0.640 0.283 0.650 0.007 0.830 0.278

0.750 0.119 0.750 0.237 0.900 0.338

0.870 0.158 0.890 ******** 0.960 0.165

0.930 0.122 0.930 0.154

0.960 0.008 0.960 - 1.772"*

CN = 0.586 0.720 0.728 0.872

340
Table F-2. Continued.

Flight 200, Wing sweep = 26 °, Time = 8-25-10-500, MINF = 0.857, Camber = 5/2, ALPT = 12.20, BETA = 0.25, QINF = 309.8,

RNPU = 2.4E+06, CNWP = 0.3799

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,800 0.000 0.789 0.000 0.780** O.OlO -1.067

0.060 -0,815 0.020 - 1.022 0.020 -0.915 0.020 - 1.107"*

O.110 -0.888 0.040 -0.752 0.060 O. 110"* 0.060 - I. 164**

0.200 - 1.068 0.060 -0.916 0.090 - 1.040 O. 110 - 1.306

0.230 - 1.019 0.090 -0.970 O.110 - 1.194 O. 140 - 1.397

0.400 - 1.007 O. 130 - 1.035 O.130 - 1.179 O. 190 - 1.947"*

0.490 -0,608 O. 150 - 1.166 O.150 - 1.073 0.250 - 1.069

0.590 -0.312 0,200 -1.174 0.210 -1.203 0.400 -0.912

0.630 -0.249 0.250 - 1.243 0.250 - 1.014 0.490 -0.819

0.700 -0.189 0.260 - 1.119 0.340 -0.803 0.580 -0.710

0.750 -0,239 0,280 - 1.173 0.370 -0,796 0.650 -0,657

0.810 -0.213 0,290 - 1.173 0,400 -0.755 0.700 -0.648

0.840 -0.222 0.310 - 1.152 0.410 -0,762 0.750 -0.574

0,900 -0.212 0,320 - 1.140 0,430 -0.768 0.800 -0.488

0.960 -0.129 0,340 - 1.070 0.440 -0.733 0.830 -0.513

0,350 -0.356** 0,460 -0.734 0,900 -0.392

0,370 -1.014 0,490 -0.683 0,960 -0.324"*

0,380 - 1.051 0.500 -0.708

0,400 -0.923 0.520 -0.668

0.410 -0.912 0.540 -0.678

0.430 -0.803 0.550 -0.653

0,440 -0.752 0,580 -0.582

0,460 -0.754 0,600 -0.609

0,470 -0.713 0.610 -0.570

0.490 -0.640 0.650 0.037"*

0.500 -0.664 0.700 -0.484

0.520 -0.593 0.750 -0.534

0.530 -0.593 0.820 -0.209

0.550 -0,545 0.890 -0.362

0.560 -0.559 0.900 -0.343

0,580 -0,507 0.960 -0.300

0.590 -0.572

0.600 -0544

0.640 -0,447

0.700 -0.437

0.750 0.015"*

0.820 -0.242

0,870 -0.160

0.930 -0.189

0.960 -0.154

Lower Surface

0.020 0.131 0.020 0.434 0.020 0.459 0.020 0.739

0.110 0.060 0.060 0,377 0.060 0.491 0.060 0.312

0.230 0.187 0.090 0,280 0.090 0.366 0.110 0.331

0.400 -0.001 0.120 0.253"* 0.120 0,066 0.250 0.155

0.490 -0.033 0.200 0.200 0.200 0.140 0.400 0.051

0,630 1.824"* 0.260 0.105 0.250 0,179 0.490 -0.044

0.750 -0.015 0.400 0.017 0.400 0.033 0.580 -0.1 44

0,850 0.024 0.490 -0.04 1 0.490 -0.004 0.650 -0.054

0.900 0.120 0.580 -0.095 0.580 -0.110 0.750 0.168

0.960 0.075 0,640 0.034 0.650 0.017 0.830 0,297

0.750 0.180 0.750 0,004"* 0,900 0.331

0.870 0.142 0.890 0.241 0,960 0.191

0,930 0,143 0.930 0.151

0.960 0.069 0.960 0,576

CN = 0.608 0.776 0.783 0.888

341
Table F-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 1044-12-000, MINF = 0,850, Camber = 5/2, ALPT = 3.99, BETA = -0.12, QINF = 291.7,

RNPU = 2.3E+06, CNWP = 0.2739

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.324 0.000 0.579 0.000 0.271 ** 0.010 -0.126

0,060 -0.032 0.020 0.080 0.020 0.196 0.020 -0.122

0. 110 -0.266 0.040 0.176 0.060 0.312"* 0.060 -0.502

0.200 -0.744 0,060 -0.206 0.090 -0.325 0.110 -0.607

0.230 -0.254 0.090 -0.296 0.110 -0.538 0.140 -0.904

0.400 -0.227 0.130 -0.454 0.130 - 1.979"* 0.190 - 1.979 * *

0.490 -0.171 0.150 -0.668 0.150 -0.795 0.250 -0.666

0.590 -0.259 0.200 -0.708 0.210 -0.771 0.400 -0.363

0.630 -0.266 0.250 -0.753 0.250 -0.751 0.490 -0.341

0,700 -0.223 0.260 -0.684 0.340 -0.295 0.580 -0,338

0.750 -0.251 0.280 -0.734 0.370 -0.294 0.650 -0.399

0.810 -0.235 0.290 -0.495 0.400 -0.285 0.700 -0.373

0.840 -0.204 0.310 -0.296 0.410 -3.003** 0.750 -0,439

0.900 -0.116 0.320 -0.283 0.430 -0.305 0.800 -0.583

0.960 -0.008 0,340 -0.223 0.440 -0.299 0.830 -0.502

0.350 -0.189** 0.460 -0.302 0.900 -0.170

0.370 -0.224 0.490 -0.236 0.960 -0.006

0.380 -0.272 0.500 -0.315

0.400 -0.203 0.520 -0.288

0.410 -0.289 0.540 -0.306

0.430 -0.272 0.550 -0.300

0.440 -0.204 0.580 -0.322

0.460 -0.312 0,600 -0.312

0.470 -0.291 0.610 -0.305

0.490 -0.286 0.650 -0.764

0.500 -0.303 0.700 -0.541

0.520 -0.309 0.750 -0.574

0.530 -0.292 0.820 -0.338

0.550 -0,350 0.890 -0.1 04

0.560 -0.315 0.900 -0.082

0.580 -0.304 0.960 0.062

0.590 -0.334

0.600 -0.35 I

0.640 -0.522

0.700 -0.446

0.750 -0.025"*

0.820 -0.279

0.870 -0.219

0.930 -0.099

0,960 -0.032

Lower Surface

0.020 - 1.403 0.020 - 1.265 0,020 - 1.093 0.020 -0.232

0.110 -0.180 0.060 -0,460 0.060 -0.159 0.060 -0.028

0.230 -0.091 0.090 -0.279 0.090 -0.222 0.110 -0.235

0.400 -0.085 0.120 -0.219 0.120 -0.512 0.250 -0.287

0.490 -0.088 0.200 -0.076 0.200 -0.147 0.400 -0.302

0.630 4.526** 0.260 -0.231 0,250 -0.235 0.490 -0.369

0.750 0.022 0.400 -0.163 0.400 -0,250 0.580 -0.352

0.850 0.087 0.490 -0.176 0.490 -0,057 0.650 -0.157

0.900 0.191 0.580 -0.170 0.580 -0.222 0.750 0.1 04

0.960 0.154 0.640 0.018 0.650 -0.034 0.830 0.256

0.750 0.171 0.750 -0.030 0.900 0.297

0.870 0,209 0.890 0.277 0.960 0.260

0.930 0.215 0.930 0.248

0.960 0.182 0.960 0.451

CN = 0.185 0.269 0.294 0.309

342
Table F-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-43-40-000, MINF = 0.845, Camber = 5/2, ALPT = 5.05, BETA = 0.02, QINF = 297.2,

RNPU = 2,4E+06. CNWP = 0.3051

r1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.209 0.000 0.679 0.000 0.333"* 0.010 -0.347

0.060 -0.105 0,020 0.077 0.020 0.098 0.020 -0.229

0.110 -0.351 0.040 0.054 0,060 0.175 * * 0.060 -0.638

0.200 -0.825 0.060 -0.309 0.090 -0.426 0.110 -0.771

0.230 -0.685 0.090 -0.375 0.110 -0.599 0.140 - 1,013

0.400 -0.174 0.130 -0.535 0.130 -2.000"* 0.190 -2.000"*

0.490 -0.199 0,150 -0.735 0.150 -0.864 0.250 -0.744

0.590 -0.251 0.200 -0.757 0.210 -0.862 0.400 -0.439

0.630 -0.266 0.250 -0.852 0.250 -0.844 0.490 -0.365

0.700 -0.224 0.260 -0.799 0.340 -0.895 0.580 -0.339

0.750 -0.267 0.280 -0.826 0.370 -0.872 0.650 -0.399

0.810 -0.235 0.290 -0.817 0,400 -0.486 0.700 -0.374

0.840 -0.213 0.310 -0.786 0.410 -3.005** 0.750 -0.428

0.900 -0.136 0.320 -0,792 0.430 -0.342 0.800 -0.436

0.960 -0.023 0.340 -0.802 0.440 -0.280 0.830 -0.335

0.350 -0.417"* 0,460 -0.281 0.900 -0.169

0.370 -0.775 0.490 -0.183 0.960 0.012

0.380 -0.681 0.500 -0.269

0.400 -0.322 0.520 -0.212

0.410 -0.274 0.540 -0.255

0.430 -0.191 0.550 -0.268

0.440 -0.134 0.580 -0.260

0.460 -0.199 0.600 -0.280

0.470 -0.178 0.6 t0 -0.284

0.490 -0.209 0.650 -0.735

0.500 -0.217 0.700 -0.521

0.520 -0.229 0.750 -0.472

0.530 -0.219 0.820 -0.335

0.550 -0.280 0.890 -0,108

0.560 -0.256 0.900 -0.073

0.580 -0.255 0.960 0.060

0.590 -0.290

0600 -0.332

0.640 -0.365

0.700 -0.354

0.750 -0.019"*

0.820 -0.271

0,870 -0.224

0,930 -0.087

0.960 -0,032

Lower Surface

0.020 -0.844 0.020 -0.950 0.020 -0.662 0.020 -0.050

O I 10 -0.222 0.060 -0.142 0.060 -0.063 0.060 -0.036

0,230 -0.045 0.090 -0.186 0.090 -0.122 0.110 -0.106

0.400 -0.074 0.120 -0.154 0.120 -0.428 0,250 -0.227

0.490 -0.076 0.200 -0.039 0.200 -0.099 0.400 -0.231

0.630 4.385"* 0.260 -0.166 0.250 -0.154 0.490 -0.307

0.750 0.035 0.400 -0.135 0.400 -0.203 0.580 -0.303

0,850 0.095 0.490 -0.154 0.490 -0.046 0.650 -0.1 44

0.900 0.187 0.580 -0.160 0.580 -0.215 0.750 0.119

0.960 0.134 0.640 0.043 0.650 -0.046 0.830 0.271

0.750 0.183 0.750 -0,046 0.900 0.328

0.870 0.226 0.890 0,293 0.960 0.249

0.930 0.232 0.930 0.246

0.960 0.170 0.960 0.454

CN = 0,243 0.358 0.391 0.383

343
Table F-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-47-48-000, MINF = 0.852, Camber = 5/6, ALPT -- 4.07, BETA = -0.04, QINF = 304.1,

RNPU = 2.4E+06, CNWP = 0.2578

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.290 0.000 0.569 0.000 0.298"* 0.010 -0.160

0.060 -0.048 0.020 0.131 0.020 0.189 0.020 -0.107

0.110 -0.310 0.040 0.171 0.060 0.340** 0.060 -0.506

0.200 -0.755 0.060 -0.196 0.090 -0.326 0.110 -0,599

0.230 -0.300 0.090 -0.293 0,110 -0.532 0.140 -0.903

0.400 -0.230 0.130 -0.465 0.130 - 1.970"* 0.190 - 1.970"*

0.490 -0.224 0.150 -0.679 0.150 -0.770 0.250 -0.672

0.590 -0.299 0.200 -0.696 0.210 -0.783 0.400 -0.366

0.630 -0.337 0.250 -0.770 0.250 -0.761 0.490 -0.348

0.700 -0.376 0.260 -0.707 0.340 -0.356 0.580 -0.363

0.750 -0.745 0.280 -0,739 0.370 -0.304 0.650 -0.431

0.810 -0.689 0.290 -0.707 0.400 -0.301 0.700 -0.392

0.840 -0.715 0.310 -0.582 0.410 -2.952** 0.750 -0.483

0.900 -0.143 0.320 -0.473 0.430 -0.335 0.800 -0.926

0.960 -0.033 0.340 -0.266 0.440 -0.305 0.830 -0.872

0.350 -0.195"* 0.460 -0.320 0.900 -0.266

0.370 -0,223 0,490 -0.254 0.960 -0.220

0.380 -0.268 0.500 -0.337

0.400 -0.200 0.520 -0.290

0,410 -0.284 0.540 -0.302

0.430 -0.255 0.550 -0.308

0.440 -0.221 0.580 -0.324

0.460 -0.291 0.600 -0.304

0.470 -0.283 0.610 -0.324

0.490 -0.296 0.650 -0.817

0.500 -0.326 0.700 -0.560

0.520 -0.309 0.750 -0.592

0.530 -0.313 0.820 -0.896

0.550 -0.349 0.890 -0.229

0.560 -0.330 0.900 -0.214

0.580 -0.321 0.960 -0.125

0.590 -0.343

0.600 -0.368

0.640 -0.543

0.700 -0.520

0.750 -0.011 **

0.820 -0.488

0.870 -0.453

0.930 -0.198

0.960 -0.183

Lower Surface

0.020 - 1.217 0.020 - 1.260 0.020 - 1.047 0.020 -0.211

0.110 -0.196 0.060 -0.321 0.060 -0.164 0.060 -0.021

0.230 -0.060 0.090 -0.242 0.090 -0,202 0.110 -0,243

0.400 -0.043 O. 120 -0.157 O. 120 -0.497 0.250 -0.270

0.490 -0.002 0.200 -0.067 0.200 -0.144 0.400 -0.244

0.630 4.269** 0.260 -0.177 O. 250 -0.202 0.490 -0.278

0.750 0.095 0.400 -0.110 0.400 -0.174 0.580 -0.237

O.850 O. 175 0.490 -0,110 0.490 -0.038 0.650 -0.024

0.900 0.249 0.580 -0.059 0,580 -0.103 0.750 0.210

0.960 O. 158 0.640 O. 149 0.650 -0.045 0.830 0.323

0.750 0.264 0.750 -0.031 0.900 0.385

0.870 0.266 0.890 0.361 0.960 0.257

0.930 0.230 0.930 0.291

0.960 0.155 0.960 0.450

CN = 0.335 0.396 0.399 0.426

344
Table F-2, Continued.

Flight 195, Wing sweep = 26", Time = 10-47-55-500, MINF = 0.840, Camber = 5/6, ALPT = 5.04, BETA = 0.10, Q1NF = 287.3,

RNPU = 2.3E+06, CNWP = 0.3877

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.247 0.000 0,689** 0.000 -4.752** 0.010 -0.333

0.060 -0.078 0.020 -0,094 0.020 0.119 0.020 -0.181

0.110 -0,344 0.040 0,038 0.060 -0.832** 0.060 -0,583

0.200 -0.810 0.060 -0.252 0.090 -0.403 0.1 |0 -0.773

0.230 -0.637 0,090 -0.364 0.110 -0.625 0.140 1.989 **

0.400 -0,191 0.130 -0.528 0.130 -0.704 0.190 -4.613"*

0.490 -0,214 0,150 -0.738 0.150 -0.806 0.250 -0,630

0.590 -0.282 0.200 -0.717 0.210 -0.894 0.400 -0,381

0.630 -0.323 0.250 -0.866 0.250 -0.835 0.490 -0,385

0.700 -0.340 0.260 -0.752 0.340 -0.841 0.580 -0.370

0.750 -0,717 0.280 -0,799 0,370 -0.417 0.650 -0.436

0,810 -0.743 0.290 -0.826 0.400 -0.336 0,700 -0.418

0,840 -0.710 0.310 -0.740 0,410 -0,277 0,750 -0.493

0.900 -0.140 0.320 -0.730 0.430 -0.308 0.800 -0.952

0.960 -0.054 0.340 -0.769 0.440 -0,260 0,830 -0.930

0.350 -0.323** 0.460 -0.278 0.900 -0.221

0,370 -0.281 0.490 -0.231 0.960 -0.148

0,380 -0.241 0.500 -0.296

0.400 -0.141 0,520 -0.278

0.410 -0.229 0.540 -0.301

0.430 -0.198 0.550 -0.281

0.440 -0.134 0.580 -0.287

0.460 -0.301 0.600 -0.335

0.470 -0.184 0.610 -0.226

0.490 -0.246 0.650 - 1.769"*

0.500 -0.253 0.700 -0.549

0.520 -0.269 0,750 -0,591

0.530 -0.250 0.820 -0.891

0.550 -0.311 0.890 -0.193

0,560 -0.285 0.900 -0.177

0,580 -0.269 0.960 -0.133

0.590 -0.337

0.600 -0.364

0.640 -1.601 **

0.700 -0,501

0.750 -0.622

0.820 -1.782"*

0.870 -0,426

0,930 -0,180

0.960 -0.127

Lower Surface

0.020 -0.791 0.020 0.147 0.020 -0.797 0,020 -0.062"*

0.110 -0.180 0.060 -0.099 0.060 -0,019 0.060 2.009"*

0.230 -0.014 0.090 -0.156 0.090 -0.129 0.110 -0.153

0.400 -0.003 0,120 -0,116 0.120 -0.482 0.250 -0.178

0.490 -0.019 0.200 0,018 0,200 -0.093 0.400 -0.163

0.630 2.054"* 0.260 -0.137 0.250 -0.103 0.490 -0.230

0.750 0.116 0.400 - 1.800"* 0.400 -0.115 0.580 -0.190

0.850 0.206 0.490 -0.069 0.490 0.022 0.650 -0.003

0,900 0,272 0,580 0,037 0,580 -0,072 0.750 0.247

0,960 0,183 0.640 0,397 0.650 0.160 0.830 0.37 I

0.750 0.245 0.750 0.352 0.900 0.462

0.870 0.307 0.890 ******** 0.960 0.301

0.930 0.290 0.930 0,334

0,960 0,163 0,960 - 1.799 **

CN = 0.379 0.486 0.522 0.486

345
Table F-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-48-15-500, MINF = 0.845, Camber = 5/6, ALPT = 7.10, BETA = -0.24, QINF = 287.1,

RNPU = 2.3E+06, CNWP = 0.5438

1] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.024 0.000 0.845"* 0.000 -4.733"* 0.010 -0.773

0.060 -0.248 0.020 -0.353 0.020 -0.179 0.020 -0,566

0.110 -0.357 0.040 -0.197 0.060 -0,931 ** 0.060 -0,825

0,200 -0.896 0.060 -0.471 0.090 -0.654 0.110 -0.977

0.230 -0.809 0.090 -0.504 0.110 -0.801 0,140 1,994"*

0.400 -0.681 0.130 -0.682 0.130 -0.846 0.190 -4,594**

0.490 -0.321 0.150 -0.844 0.150 -0.923 0.250 - 1.096

0.590 -0.239 0.200 -0.833 0.210 - 1.009 0,400 -0.785

0.630 -0.276 0.250 - 1.007 0.250 -0.972 0.490 -0.600

0.700 -0.294 0.260 -0.879 0.340 - 1.028 0.580 -0.518

0.750 -0.674 0.280 -0.973 0.370 - 1.012 0.650 -0.518

0.810 -0.740 0.290 -0.968 0.400 - 1.006 0.700 -0.550

0.840 -0.665 0.310 -0.889 0.410 -0.979 0,750 -0.623

0.900 -0.209 0.320 -0.888 0.430 - 1.040 0.800 -0,665

0.960 -0.128 0,340 -0.944 0.440 -0.976 0.830 -0.499

0.350 -0.392"* 0.460 - 1.007 0,900 -0.179

0.370 -0.892 0.490 -0.933 0,960 -0.125

0.380 -0.919 0.500 - 1.040

0.400 -0.855 0.520 - 1.004

0.410 -0.962 0.540 - 1.034

0.430 -0.918 0.550 -0.982

0.440 -0.827 0.580 -0,777

0.460 - 1.056 0,600 -0.644

0.470 -0.955 0.610 -0,480

0,490 -0.902 0,650 -1.748"*

0.500 -0.902 0.700 -0.586

0.520 -0.908 0.750 -0.568

0.530 -0.872 0.820 -0.347

0.550 -0.884 0.890 -0.090

0.560 -0.926 0.900 -0.072

0.580 -0.874 0.960 -0.052

0.590 -0.884

0,600 -0.968

0.640 -1.580"*

0.700 -0.261

0.750 -0.464

0.820 -1.761"*

0.870 -0.306

0.930 -0.085

0.960 -0.024

Lower Surface

0.020 -0.464 0.020 0.196 0.020 -0.088 0.020 0.254**

0.110 -0.122 0.060 0.102 0,060 0.169 0.060 2.034**

0.230 0.069 0.090 0.008 0.090 0.052 0.110 0.019

0.400 0.012 0.120 0.031 0.120 -0.315 0.250 -0.058

0.490 0.012 0.200 0.094 0.200 -0.028 0.400 -0.064

0.630 2.079** 0.260 -0.053 0.250 0.012 0.490 -0.152

0.750 0.115 0.400 - 1.779 ** 0.400 -0,039 0.580 -0.135

0.850 0.197 0,490 -0.022 0,490 0.060 0.650 0.032

0.900 0.261 0.580 0.067 0.580 -0.019 0.750 0.270

0.960 0.150 0.640 0.426 0,650 0.190 0.830 0.399

0,750 0.269 0.750 0.376 0.900 0.486

0.870 0.330 0.890 ******** 0.960 0.318

0.930 0.328 0.930 0.357

0.960 0.209 0.960 - 1.778* *

CN = 0.517 0.741 0.769 0.723

346
Table F-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-48-31-500, MINF = 0,847, Camber = 5/6, ALPT = 8,t7, BETA = 0.52, QINF = 278.1,

RNPU = 2.2E+06, CNWP = 0.6261

q = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.117 0,000 0.910"* 0,000 -4.812"* 0.010 -0.855

0.060 -0,395 0.020 -0.540 0,020 -0,329 0,020 -0.790

0.110 -0,504 0.040 -0.274 0.060 -1,005"* 0.060 -0.864

0.200 -0.916 0.060 -0.592 0.090 -0.777 0,110 - 1.062

0,230 -0.825 0.090 -0.669 0.110 -0,894 O. 140 2,069**

0,400 -0.778 0.130 -0.770 0.130 -0.943 0.190 -4,669"*

0.490 -0,666 0,150 -0.903 0.150 - 1.005 0,250 - 1.197

0.590 -0,464 0,200 -0.885 0.210 - 1,098 0,400 -0.866

0.630 -0,270 0,250 - 1.072 0.250 - 1.048 0,490 -0.792

0,700 -0.269 0.260 -0.933 0,340 - 1.116 0.580 -0.677

0.750 -0,607 0,280 - 1.042 0.370 - 1.068 0,650 -0.628

0.810 -0,667 0,290 - 1.042 0.400 - 1.066 0,700 -0.687

0.840 -0,631 0,310 -0.954 0.410 - 1.042 0.750 -0,735

0.900 -0,268 0,320 -0.944 0.430 - 1.129 0.800 -0.483

0,960 -0.168 0,340 - 1,001 0.440 - 1.064 0,830 -0.364

0,350 -0.394"* 0.460 - 1.084 0.900 -0.219

0,370 -0.953 0.490 - 1.015 0.960 -0.145

0,380 -0.991 0.500 -1.110

0.400 -0.907 0.520 - 1.072

0.410 -1.039 0.540 -1.117

0.430 - 1.017 0.550 - 1.069

0.440 -0.894 0.580 - 1.094

0.460 - 1.118 0.600 - 1.075

0.470 - 1.003 0.610 -0.983

0.490 -0,982 0.650 - 1.730**

0.500 - 1,001 0.700 -0.57 I

0.520 -0,967 0.750 -0.568

0.530 -0,941 0.820 -0.280

0.550 -0,978 0,890 -0.156

0.560 -0.995 0,900 -0.171

0.580 -0.941 0.960 -0.142

0,590 -0.984

0.600 - 1.030

0.640 -1,557"*

0700 -0.365

0.750 -0.224

0,820 -1.744**

0.870 -0,159

0,930 -0.163

0.960 -0.156

Lower Surface

0.020 -0,240 0.020 0,224 0.020 0.072 0.020 0.382**

0,110 -0.065 0.060 0.192 0.060 0.271 0.060 2.173"*

0,230 0.102 0.090 0,083 0.090 0.145 0,110 0,081

0.400 0,023 0.120 0.099 0,120 -0,249 0.250 0.009

0,490 -0.016 0.200 0.143 0.200 0.011 0.400 -0,015

0.630 2.220"* 0.260 -0.009 0.250 0,063 0,490 -0.130

0,750 0.117 0.400 -1.763"* 0.400 -0,013 0,580 -0.122

0.850 0.170 0,490 -0.012 0,490 0,136 0.650 0.044

0,900 0.254 0.580 0.073 0.580 -0.024 0.750 0.300

0.960 0.153 0,640 0.425 0.650 0.176 0.830 0.4 l 3

0.750 0.261 0.750 0.383 0.900 0.490

0,870 0,322 0,890 ******** 0,960 0.333

0.930 0.291 0.930 0.347

0.960 0.156 0.960 -1.761"*

CN = 0.604 0.789 0.885 0.834

347
Table F-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-49-27-500, MINF = 0.855, Camber = 5/6, ALPT = 8.02, BETA = 0.05, QINF = 290.0,

RNPU = 2.3E+06, CNWP = 0.5841

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP affc CP

0.020 -0.085 0.000 0.889** 0.000 -4.657** 0.010 -0.833

0.060 -0.363 0.020 -0.49l 0.020 -0.271 0.020 -0.749

0.110 -0.427 0,040 -0.250 0.060 -0.951 ** 0.060 -0.820

0.200 -0.876 0.060 -0.565 0.090 -0.737 0.110 - 1.031

0.230 -0,785 0.090 -0.619 0.110 -0.870 0,140 1.971 **

0.400 -0.767 0.130 -0.731 0.130 -0,890 0.190 -4.520**

0.490 -0.667 0.150 -0.871 0.150 -0.959 0.250 - 1.162

0.590 -0.582 0.200 -0.856 0.210 - 1.051 0.400 -0.837

0.630 -0.269 0.250 - 1.026 0.250 - 1.014 0.490 -0.773

0.700 -0.252 0,260 -0.901 0.340 - 1.084 0.580 -0.652

0.750 -0.548 0.280 -0.994 0.370 - 1.053 0.650 -0.607

0.810 -0.613 0.290 - 1.007 0.400 - 1.028 0,700 -0.646

0.840 -0.583 0.310 -0,925 0.410 - 1.028 0.750 -0.718

0.900 -0.267 0.320 -0.923 0.430 - 1.080 0.800 -0.558

0.960 -0.145 0.340 -0.974 0.440 - 1.023 0.830 -0.401

0.350 -0.396** 0.460 - 1.065 0.900 -0.256

0,370 -0.927 0.490 -0.972 0,960 -0.199

0.380 -0.955 0,500 - 1.077

0.400 -0.883 0.520 - 1.041

0.410 -0.998 0.540 - 1.070

0.430 -0.973 0.550 - 1.051

0,440 -0.870 0.580 - 1.017

0.460 - 1.098 0.600 - 1.044

0.470 -0,968 0.610 -0.941

0.490 -0.951 0.650 - 1.703"*

0.500 -0.956 0.700 -0.701

0.520 -0.941 0.750 -0.580

0.530 -0.920 0.820 -0.234

0,550 -0.951 0.890 -0.159

0.560 -0,965 0.900 -0.161

0.580 -0.929 0.960 -0.153

0.590 -0.961

0.600 - 1.007

0.640 -1.536"*

0.700 -0.348

0.750 -0.209

0.820 -1.716"*

0.870 -0.184

0.930 -0.162

0.960 -0.152

Lower Surface

0.020 -0.291 0.020 0.202 0.020 0.040 0.020 0.368"*

0.1 I 0 -0.089 0.060 0.156 0.060 0.247 0.060 2.040"*

0.230 0.096 0.090 0.060 0.090 0.121 0.110 0.079

0.400 0.001 0.120 0.074 0.120 -0.261 0.250 -0.012

0.490 -0.029 0.200 0.124 0.200 0.005 0.400 -0.036

0,630 2.085** 0.260 -0.025 0.250 0,039 0.490 -0.138

0.750 0.099 0.400 - 1.734** 0,400 -0.021 0.580 -0.126

0.850 0.173 0.490 -0.025 0.490 0.04 1 0.650 0.037

0.900 0.239 0.580 0.049 0.580 -0.022 0.750 0.284

0.960 0.159 0,640 0.403 0.650 0.178 0.830 0.405

0.750 0.237 0.750 0.369 0.900 0.490

0.870 0,295 0,890 ******** 0.960 0.318

0.930 0.292 0.930 0.327

0.960 0.143 0.960 - 1.732"*

CN = 0.572 0,749 0.850 0.810

348
Table F-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-49-47-000, MINF = 0.860, Camber = 5/6, ALPT = 11.79, BETA = 0.15, QINF = 305.2,

RNPU = 2.4E+06. CNWP = 0.4523

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0,741 0.000 0.808** 0.000 -4,502** 0.010 -1,086

0.060 -0.729 0.020 - 1.076 0.020 -0.836 0.020 - 1.109

0.110 -0.799 0.040 -0.669 0.060 - 1.159 ** 0.060 - 1.183

0.200 - 1.042 0,060 -0.874 0.090 - 1.030 0.110 - 1.299

0.230 - 1.006 0.090 -0.960 0.110 - 1.159 0.140 1.857"*

0.400 -0.990 0.130 -1.035 0.130 -1.168 0.190 -4.372**

0.490 -0.902 0.150 -1.135 0.150 -1.177 0,250 -0,995

0.590 -0.825 0.200 - 1.099 0.210 - 1.040 0.400 -0,853

0.630 -0.539 0.250 - 1.261 0.250 -0.850 0.490 -0.804

0.700 -0.283 0.260 - 1.121 0.340 -0,852 0.580 -0.748

0.750 -0.379 0.280 - 1.204 0.370 -0.797 0.650 -0.615

0.810 -0.460 0,290 - 1.224 0.400 -0.774 0.700 -0.691

0.840 -0.455 0.310 - I. 123 0.410 -0.743 0.750 -0.643

0.900 -0,260 0.320 - 1.100 0.430 -0.788 0.800 -0.625

0.960 -0.305 0.340 - 1.169 0.440 -0.732 0.830 -0.604

0.350 -0.401 ** 0.460 -0.723 0.900 -0.563

0.370 - 1.081 0.490 -0.660 0.960 -0.496

0.380 -1.114 0,500 -0.716

0.400 - 1.035 0.520 -0.688

0.410 - 1.159 0.540 -0.665

0.430 - 1.080 0.550 -0.699

0.440 -0.964 0.580 -0.634

0.460 - 1,083 0.600 -0.624

0.470 -0.886 0.610 -0.486

0.490 -0.753 0.650 -1.694"*

0.500 -0.787 0.700 -0.561

0.520 -0.682 0.750 -0.612

0,530 -0.705 0.820 -0.528

0.550 -0.655 0.890 -0.495

0.560 -0.670 0.900 -0.463

0.580 -0.615 0.960 -0.462

0.590 -0.660

0.600 -0.639

0.640 -I.536"*

0.700 -0.456

0.750 -0.313

0.820 -1.706"*

0.870 , -0,256

0.930 -0.295

0,960 -0.278

Lower Surface

0.020 0.100 0.020 0.201 0.020 0.434 0.020 0.697"*

0.110 0.058 0.060 0.385 0.060 0.452 0.060 1.864**

0.230 0.192 0.090 0.277 0.090 0.346 0.1 I0 0.266

0.400 0.019 0.120 0.227 0.120 -0.056 0.250 0.138

0.490 -0.039 0.200 0.220 0.200 0.101 0.400 0.071

0.630 1.906** 0.260 0.086 0.250 0.193 0.490 -0.040

0.750 0.042 0.400 - 1.723 ** 0.400 0.060 0.580 -0.063

0.850 0.1 04 0,490 0.013 0.490 0.032 0.650 0,067

0.900 0.172 0.580 0.236 0.580 0.004 0.750 0.286

0.960 0.038 0.640 0.382 0.650 0.173 0.830 0.390

0.750 0.236 0,750 0.354 0.900 0.468

0.870 0.277 0.890 ******** 0.960 0.272

0.930 0.231 0,930 0.262

0.960 0.071 0.960 - 1.722"*

CN = 0.733 0.882 0.867 0.957

349
Table F-2. Continued.

Flight 195, Wing sweep = 26 °, Time = 10-49-52-500, MINF = 0.852, Camber = 5/6, ALPT = 11.09, BETA = -0.27, QINF = 304.9,

RNPU = 2.4E+06, CNWP = 0.4524

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.716 0.000 0.820* * 0.000 -4.539"* 0.010 - 1.035

0.060 -0.710 0.020 - 1.067 0.020 -0.840 0.020 - 1.079

0.110 -0.745 0.040 -0.684 0.060 -1.112"* 0.060 -1.188

0.200 - 1.032 0.060 -0.849 0.090 - 1.004 O. 110 - 1.295

0.230 -0.997 0.090 -0.924 O. 110 - 1.164 O. 140 1.870"*

0.400 -0.987 O. 130 - 1.012 O.130 - 1.173 O. 190 -4.409"*

0.490 -0.760 O. 150 - 1.126 O.150 - 1.209 0.250 - 1.056

0.590 -0.269 0.200 - 1.104 0.210 - 1.280 0.400 -0.836

0.630 -0.230 0.250 - 1.238 0.250 - 1.125 0.490 -0.813

0.700 -0.262 0.260 - 1.112 0.340 -0.797 0.580 -0.728

0.750 -0.500 0.280 - 1.221 0.370 -0.740 0.650 -0.614

0.810 -0.577 0.290 -1.219 0.400 -0.735 0.700 -0.670

0.840 -0.556 0.310 - 1.145 0.410 -0.703 0.750 -0.619

0.900 -0.269 0.320 - 1.! 21 0.430 -0.733 0.800 -0.587

0.960 -0.215 0.340 - 1.187 0.440 -0.681 0.830 -0.585

0.350 -0.395** 0.460 -0.686 0.900 -0.489

0.370 - 1.103 0.490 -0.621 0.960 -0.405

0.380 - 1,113 0.500 -0.687

0.400 - 1.004 0.520 -0.669

0.410 - 1.067 0.540 -0.669

0.430 -0.919 0.550 -0.616

0.440 -0.821 0.580 -0.624

0.460 -0.943 0.600 -0.626

0.470 -0.774 0.610 -0.517

0.490 -0.697 0.650 -1.728**

0.500 -0.672 0.700 -0.509

0.520 -0.664 0.750 -0.613

0.530 -0.614 0.820 -0.473

0.550 -0.636 0.890 -0.403

0.560 -0.580 0.900 -0.409

0.580 -0.579 0.960 -0.377

0.590 -0.575

0.600 -0.585

0.640 - 1.570"*

0.700 -0.446

0.750 -0.316

0.820 -1.740"*

0.870 -0.242

0.930 -0.267

0.960 -0.286

Lower Surface

0.020 0.063 0.020 0.212 0.020 0.368 0.020 0.671 **

0.110 0.034 0.060 0.360 0.060 0.437 0.060 1.833"*

0.230 O. 188 0.090 0.247 0.090 0.315 O. 110 0.242

0.400 0.023 O. 120 0.224 O. 120 -0.071 0.250 O. I 19

0.490 -0.032 0.200 0.217 0.200 0.098 0.400 0.059

0.630 1.876"* 0.260 0.076 0.250 O. 168 0.490 -0.051

0.750 0.045 0.400 -1.757"* 0.400 0.047 0.580 -0.068

0.850 0.115 0.490 0.002 0.490 0.046 0.650 0.056

0.900 0.178 0.580 0.215 0.580 0.001 0.750 0.287

0.960 0.061 0.640 0.394 0.650 O. 162 0.830 0.392

0.750 0.233 0.750 0.343 0.900 0.467

0.870 0.288 0.890 ******** 0.960 0.266

0.930 0.227 0.930 0.273

0.960 0.078 0.960 - 1.756**

CN -- 0.670 0.856 0.857 0.938

350
Table F-2. Continued.

Flight 191, Wing sweep = 26 °, Time = 9-46-5-000, MINF = 0.850, Camber = 5/6, ALPT = 4.95, BETA = -0,16, QINF = 286.4,

RNPU = 2.3E+06, CNWP = 0,4005

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.289 0.000 0.662 0.000 -5.039"* 0.010 -0.253

0.060 -0.036 0.020 -0.040 0.020 O. 164 0.020 -0.145

0.110 -0.304 0.040 0.069 0.060 -0.102"* 0.060 -0.570

0.200 -0.772 0.060 -0.212 0.090 -0.345 0.110 -0.685

0.230 -0.666 0,090 -0,335 0. l 10 -0.586 0.140 -0,862

0,400 -0,175 0.130 -0.489 0.130 -0.648 0.190 -5.721 "*

0,490 -0.198 0.150 -0.705 0.150 -0.781 0.250 -0.595

0.590 -0.274 0.200 -0.692 0.210 -0.829 0.400 -0.330

0.630 -0.311 0.250 -0.833** 0.250 -0.776 0.490 -0.364

0.700 -0.364 0.260 -0.689 0.340 -0.818 0.580 -0.356

0.750 -0.711 0.280 -0.771 0.370 -0.673 0.650 -0.407

0.810 -0,772 0.290 -0.769 0.400 -0.420 0.700 -0.415

0,840 -0.716 0.310 -0.720 0.410 -0.276 0.750 -0.509

0,900 -0.116 0.320 -0.694 0.430 -0.299 0.800 -0.928

0.960 -0,050 0.340 -0,728 0.440 -0,251 0,830 -0.892

0,350 -0,374** 0,460 -0.274 0,900 -0.248

0.370 -0.656 0.490 -0.207 0.960 -0.184

0,380 -0,381 0,500 -0.289

0.400 -0.171 0,520 -0,250

0.410 -0.234 0,540 -0,235

0.430 -0.181 0.550 -0.263

0.440 -0.135 0.580 -0.259

0.460 -0.231 0.600 -0.273

0.470 -0.191 0,610 -0.219

0,490 -0.205 0.650 -2.859**

0.500 -0.195 0.700 -0.535

0.520 -0.229 0.750 -0.600

0.530 -0.221 0.820 -0.875

0.550 -0.257 0,890 -0,209

0.560 -0.248 0.900 -0.217

0.580 -0.243 0.960 -0.17 I

0.590 -0,292

0,600 -0.352

0.640 -2.690**

0.700 -0.479

0.750 -0.578

0.820 -2.872**

0.870 -0.438

0.930 -0.188

0.960 -0.150

Lower Surface

0.020 -0.943 0.020 - 1,093 0.020 -0.954 0.020 -0.097

0.110 -0.172 0.060 -0.122 0.060 -0.054 0,060 3.126"*

0.230 -0.017 0.090 -0.194 0.090 -0,162 0,110 -0.150

0.400 -0.030 0.120 -0.112 0.120 -0.513"* 0.250 -0.202

0.490 -0.030 0,200 -0.004 0.200 -0.122 0.400 -0.186

0.630 3.152"* 0.260 -0.155 0.250 -0.130 0.490 -0.276

0.750 0.121 0.400 -2.890** 0.400 -0.112 0.580 -0.193

0. 850 0.192 0.490 -0,072 0.490 0.034 0.650 -0.002

0.900 0.277 0.580 0.030 0.580 -0,080 0.750 0.240

0,960 0,185 0.640 0.400 0,650 0.168 0.830 0.394

0.750 0,239 0.750 0.347 0,900 0.469

0.870 0,310 0.890 ******** 0.960 0.313

0,930 0,280 0.930 0.328

0.960 0.172 0.960 -2.617**

CN = 0.370 0.468 0.524 0.458

351
Table F-2. Continued.

Flight 191, Wing sweep = 26 °, Time = 9-46-15-500, MINF = 0.852, Camber = 5/6, ALPT = 7.04, BETA = -0.16, QINF = 290.9,

RNPU = 2.3E+06, CNWP -- 0.5409

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0,020 0.063 0.000 0,846 0.000 -4.985"* 0.010 -0.728

0,060 -0.187 0.020 -0,338 0.020 -0.136 0.020 -0.427

0.110 -0,373 0.040 -0.145 0.060 -0.280"* 0.060 -0.769

0.200 -0846 0.060 -0.411 0.090 -0.590 0.110 -0.933

0.230 -0.846 0.090 -0.462 0.110 -0.762 0.140 - 1.060

0.400 -0.681 0.130 -0.621 0.130 -0,794 0.190 -5.657" *

0.490 -0.555 0.150 -0.805 0.150 -0.894 0.250 - 1.061

0.590 -0.249 0.200 -0.797 0.2 l0 -0.957 0.400 -0.741

0.630 -0.266 0.250 -0.976"* 0.250 -0.916 0.490 -0.631

0.700 -0.258 0,260 -0.841 0.340 -0.976 0.580 -0.504

0.750 -0.647 0.280 -0,933 0.370 -0.951 0.650 -0.485

0.810 -0.693 0.290 -0.936 0.400 -0,979 0.700 -0.530

0.840 -0.630 0.310 -0.867 0.410 -0.927 0.750 -0,605

0.900 -0.205 0.320 -0.846 0.430 -0.988 0,800 -0.857

0.960 -0.114 0.340 -0.898 0.440 -0.950 0.830 -0.512

0.350 -0,396** 0.460 -0.979 0.900 -0.209

0.370 -0,860 0,490 -0.922 0.960 -0.184

0.380 -0.884 0.500 - 1.006

0.400 -0.797 0.520 -0.937

0.410 -0.925 0.540 -0.972

0.430 -0.891 0.550 -0.965

0.440 -0.810 0.580 -0.912

0.460 -0.965 0.600 -0,789

0,470 -0.878 0.610 -0.591

0.490 -0.863 0.650 -2,839**

0.500 -0.871 0.700 -0,609

0.520 -0.866 0.750 -0.707

0.530 -0.841 0.820 -0.257

0.550 -0.872 0.890 -0.110

0.560 -0.865 0,900 -0.102

0_580 -0.844 0.960 -0.083

0.590 -0.877

0.600 -0.939

0.640 -2,673**

0.700 -0.436

0.750 -0.326

0.820 -2.852**

0.870 -0.267

0.930 -0.063

0.960 0.001

Lower Surface

0.020 -0.458 0.020 -0.194 0.020 -0.096 0.020 0.245

0.110 -0.130 0.060 0.073 0.060 0.178 0.060 3.053"*

0.230 0.062 0.090 -0.010 0.090 0.047 0.110 0.031

0.400 0.010 0.120 0.025 0.120 -0.320"* 0.250 -0.059

0.490 -0.013 0.200 0.061 0.200 -0.040 0.400 -0.087

0.630 3.078"* 0,260 -0.050 0.250 0.003 0.490 -0.175

0.750 0.132 0.400 -2.870** 0,400 -0.027 0.580 -0.137

0,850 0.193 0.490 -0.019 0.490 0.016 0.650 0.034

0.900 0.279 0.580 0.069 0,580 -0.028 0.750 0.282

0.960 0.177 0.640 0.427 0.650 0.201 0.830 0.420

0.750 0,290 0.750 0.385 0.900 0.489

0.870 0.354 0.890 ******** 0.960 0.326

0.930 0.341 0.930 0.355

0.960 0.231 0.960 -2.602**

CN = 0.527 0,715 0.775 0,724

352
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-51-33-500, MINF = 0.858, Camber = 5/10, ALPT = 3.98, BETA = 0.28, QINF = 299.9,

RNPU = 2.3E+06, CNWP = 0.3573

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 0.382 0.000 0.609 0.000 -5.643** 0.010 -0.034**

0.060 0.020 0,020 0.174"* 0.020 0.311 ** 0.020 0.006**

0.110 -0,262 0.040 0.177 0.060 -0.992"* 0.060 -0.400

0.200 -0.726 0.060 -0.077 0.090 -0.239 0.110 -0.513

0,230 -0.227 0.090 -0.225 0.110 -0.466 0.140 1.920**

0.400 -0.184 0.130 -0.418 0.130 -0.594 0.190 -5.511 * *

0.490 -0.194 0.150 -0.616 0.150 -0.678 0.250 -0.607

0.590 -0.248 0.200 -0.611 0.210 -0.742 0.400 -0.299

0.630 -0,295 0.250 -0,689 0.250 -0.687 0.490 -0.302

0.700 -0.396 0.260 -0.635 0.340 -0,286 0.580 -0.334

0.750 -0.527 0.280 -0,666 0.370 -0.271 0.650 -0.384

0.810 -0.552 0.290 -0,650 0.400 -0.297 0.700 -0.379

0.840 -0.513 0.310 -0.425 0.410 -0.254 0.750 -0.498

0.900 -0.226 0.320 -0,321 0.430 -0.299 0.800 - 1,062

0.960 -0.248 0.340 -0.210 0.440 -0.284 0,830 -0,666

0.350 -0.138** 0,460 -0.287 0.900 -0.394

0.370 -0.186 0.490 -0,225 0,960 -0.394

0.380 -0.198 0.500 -0.283

0.400 -0.135 0.520 -0,256

0.410 -0.235 0.540 -0.264

0.430 -0.241 0,550 -0.258

0.440 -0,170 0.580 -0.247

0,460 -0,290 0.600 -0.274

0.470 -0.282 0.610 -0.219

0.490 -0.244 0.650 -2,786**

0.500 -0.248 0.700 -0.512

0.520 -0,263 0.750 -0.534

0.530 -0.257 0.820 -0.732

0.550 -0.302 0.890 -0.394

0.560 -0.275 0.900 -0.456

0.580 -0.254 0.960 -0.431

0.590 -0,302

0.600 -0.328

0.640 -2.625**

0.700 -0.480

0.750 -0.581

0.820 -2.799**

0.870 -0.280

0.930 -0.294

0.960 -0.291

Lower Surface

0.020 - 1.392 0.020 - 1.208 0.020 - 1.097 0.020 -0.274

0. I 10 -0.108 0.060 -0.454 0.060 -0.193 0.060 3.181 **

0.230 -0.033 0.090 -0.183 0.090 -0.230 0.110 -0.237

0.400 0.007 0.120 -0.130 0.120 -0.495 0.250 -0.232

0.490 0.015 0.200 -0.030 0.200 -0.092 0.400 -0.196

0.630 3.224"* 0.260 -0.113 0.250 -0.147 0,490 -0,202

0.750 0.194 0.400 -2.816"* 0.400 -0.090 0.580 -0.110

0.850 0.255 0.490 -0.017 0.490 0.032 0,650 0.117

0.900 0.307 0.580 0.115 0,580 0.014 0,750 0.364

0.960 0.141 0.640 0.465 0.650 0.280 0,830 0.446

0.750 0.321 0,750 0.423 0.900 0.551

0.870 0.369 0,890 ******** 0,960 0.350

0.930 0.314 0.930 0.384

0.960 0.171 0.960 -2.815"*

CN = 0.346 0.422 0.488 0.453

353
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-51-51-500, MINF = 0.856, Camber = 5/10, ALPT = 5.04. BETA = 0.21, QINF = 298.1,

RNPU = 2.3E+06, CNWP = 0.4900

rl = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.303 0.000 0.698 0.000 -5.672 * * 0.010 -0.240 * *

0,060 -0.057 0.020 0.084** 0.020 0.I 73"* 0.020 -0.136"*

0.110 -0,245 0,040 0.083 0.060 - 1.024"* 0,060 -0.566

0.200 -0,789 0.060 -0.179 0.090 -0.318 0.110 -0.648

0,230 -0.616 0,090 -0.289 0.110 -0.530 0.140 1.929"*

0.400 -0,121 0.130 -0.471 0.130 -0.649 0.190 -5.538**

0.490 -0.166 0.150 -0.658 0.150 -0.751 0.250 -0.661

0.590 -0.242 0.200 -0,669 0.210 -0.816 0.400 -0.377

0,630 -0,290 0.250 -0.791 0.250 -0,780 0,490 -0,373

0,700 -0.388 0.260 -0.714 0.340 -0.816 0.580 -0.360

0.750 -0.792 0,280 -0,762 0.370 -0.805 0,650 -0.419

0.810 -0.760 0.290 -0.765 0,400 -0,797 0.700 -0.407

0.840 -0.705 0.310 -0.702 0.410 -0.665 0.750 -0.502

0.900 -0.260 0.320 -0,690 0,430 -0.496 0.800 -0,933

0.960 -0.293 0.340 -0.731 0.440 -0.381 0,830 -0.542

0.350 -0.320** 0,460 -0,330 0,900 -0.371

0.370 -0.693 0.490 -0,257 0,960 -0,374

0.380 -0,702 0,500 -0.268

0.400 -0.621 0.520 -0.250

0.410 -0.713 0.540 -0,245

0,430 -0,603 0.550 -0,228

0,440 -0,369 0.580 -0.224

0,460 -0.273 0.600 -0.244

0.470 -0. 127 0.610 -0.200

0.490 -0.149 0.650 -2.797 * *

0.500 -0.134 0.700 -0,476

0,520 -0.142 0.750 -0.505

0.530 -0.142 0.820 -0,925

0.550 -0,165 0,890 -0,386

0,560 -0.170 0.900 -0,444

0.580 -0.163 0,960 -0.423

0,590 -0.222

0.600 -0,265

0,640 -2.634**

0,700 -0,425

0,750 -0.679

0,820 -2.809"*

0,870 -0.275

0.930 -0.285

0,960 -0.293

Lower Surface

0.020 -0.882 0,020 -0.989 0.020 -0,877 0,020 -0.058

0.110 -0.149 0.060 -0.108 0,060 -0.014 0.060 3,207 **

0,230 0,012 0.090 -0,121 0.090 -0.101 0.110 -0.109

0,400 0.007 0.120 -0.065 0.120 -0.413 0,250 -0.160

0.490 0.029 0,200 0,024 0.200 -0,052 0,400 -0.139

0.630 3.251 ** 0.260 -0,070 0,250 -0.089 0,490 -0.166

0,750 0.198 0.400 -2.827** 0.400 -0.053 0.580 -0,083

0,850 0.270 0.490 0.016 0.490 0.050 0,650 0.136

0,900 0.315 0.580 0.126 0.580 0,032 0.750 0.373

0.960 0.140 0.640 0,480 0.650 0,299 0,830 0.470

0.750 0,338 0.750 0,447 0.900 0.555

0.870 0.433 0,890 ******** 0.960 0,368

0,930 0,359 0.930 0.416

0.960 0,201 0,960 -2.825**

CN = 0.418 0.549 0,625 0.533

354
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-52-32-500, MINF = 0.856, Camber = 5/t0, ALFrT = 5.96, BETA = 0.02, QINF = 297.6,

RNPU = 2.3E+06, CNWP = 0.4975

1"}= 093 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.218 0.000 0.755 0.000 -5.679" * 0.010 -0.366"*

0.060 -0.065 0.020 -0.032"* 0.020 0.045"* 0.020 -0.198"*

0.110 -0.336 0.040 0.005 0,060 - 1,082* * 0,060 -0.660

0.200 -0.828 0.060 -0.255 0.090 -0.380 0.110 -0.767

0.230 -0.690 0.090 -0.358 0.110 -0.593 0.140 1.927"*

0.400 -0.523 0.130 -0,529 O. 130 -0.703 0.190 -5.545**

0.490 -0.168 0.150 -0,713 0.150 -0,801 0.250 -0.959

0.590 -0.218 0.200 -0.723 0.210 -0.872 0.400 -0.663

0.630 -0.273 0.250 -0.856 0.250 -0,846 0.490 -0.439

0.700 -0.298 0.260 -0,782 0.340 -0.901 0.580 -0.423

0.750 -0.907 0.280 -0.833 0.370 -0,884 0.650 -0.449

0.810 -0.961 0.290 -0.846 0.400 -0.870 0.700 -0.464

0.840 -0.922 0.310 -0.774 0.410 -0,837 0,750 -0.560

0.900 -0.302 0.320 -0.768 0.430 -0.882 0.800 -0.630

0.960 -0.341 0.340 -0.808 0.440 -0.861 0,830 -0.475

0,350 -0.344** 0.460 -0.870 0.900 -0.360

0,370 -0.776 0,490 -0.784 0,960 -0.364

0.380 -0.795 0,500 -0.720

0.400 -0.707 0.520 -0.510

0.410 -0.800 0.540 -0.439

0.430 -0.781 0.550 -0,389

0.440 -0.714 0.580 -0.346

0,460 -0.852 0.600 -0.353

0.470 -0.793 0.610 -0.283

0.490 -0,764 0,650 -2.799**

0.500 -0.738 0.700 -0.507

0.520 -0.756 0.750 -0.519

0.530 -0.740 0.820 -0.596

0.550 -0,757 0,890 -0.296

0.560 -0,614 0,900 -0,328

0.580 -0,320 0,960 -0,341

0,590 -0.251

0.600 -0.229

0,640 -2.637* *

0.700 -0.302

0.750 -0.689

0.820 -2,812"*

0.870 -0.363

0.930 -0,258

0.960 -0.262

Lower Surface

0,020 -0.589 0.020 -0.560 0.020 -0,276 0,020 0.072

0.110 -0.144 0.060 -0.009 0.060 0,067 0.060 3,214"*

0.230 0.029 0,090 -0,048 0,090 -0.021 O. 110 -0.046

0400 0.016 0, 120 -0.025 0.120 -0.341 0,250 -0.112

0.490 0.024 0.200 0.041 0.200 -0,023 0,400 -0,10 l

0.630 3,258"* 0.260 -0,046 0.250 -0.043 0.490 -0.134

0.750 O. 196 0.400 -2.829"* 0.400 -0.020 0.580 -0.071

0.850 0.265 0.490 0.018 0.490 0.056 0,650 0.142

0.900 0.310 0.580 0.125 0.580 0,038 0.750 0.381

0.960 0.126 0.640 0.486 0,650 0.302 0,830 0.482

0.750 0.341 0.750 0,450 0,900 0,579

0.870 0.455 0,890 ******** 0.960 0.370

0.930 0,351 0.930 0.419

0.960 0.207 0.960 -2,828**

CN = 0.517 0,667 0.707 0.660

355
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-52-35-500, MINF = 0.856, Camber = 5/10, ALPT = 7.04, BETA = 0.05, QINF = 297.4,

RNPU = 2.3E+06, CNWP = 0.5942

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.106 0.000 0.844 0.000 -5.683 * * 0.010 -0.649 * *

0.060 -0.190 0,020 -0.213** 0.020 -0.104"* 0.020 -0.290**

0.110 -0.355 0.040 -0.110 0.060 -1.139"* 0.060 -0,763

0.200 -0.866 0.060 -0.365 0.090 -0.556 0.110 -0.892

0.230 -0.751 0,090 -0.431 0.110 -0.688 0.140 1.931 **

0.400 -0.653 0.130 -0.607 0.130 -0.768 0.190 -5.549**

0.490 -0.544 0.150 -0.759 0.150 -0.854 0.250 - 1.031

0.590 -0.371 0.200 -0.770 0.210 -0,925 0.400 -0.732

0.630 -0.312 0.250 -0.921 0.250 -0.912 0.490 -0.586

0.700 -0.369 0.260 -0.836 0.340 -0.949 0.580 -0.504

0.750 -0.854 0.280 -0.909 0.370 -0.957 0.650 -0.488

0.810 -0.923 0,290 -0.904 0.400 -0.944 0.700 -0.519

0.840 -0.885 0.310 -0.833 0.410 -0.917 0.750 -0.597

0.900 -0.341 0.320 -0.819 0.430 -0.976 0.800 -0.587

0.960 -0.383 0.340 -0.878 0.440 -0.931 0.830 -0.442

0.350 -0.340* * 0.460 -0.951 0.900 -0.355

0.370 -0.842 0.490 -0.881 0.960 -0.358

0.380 -0,858 0.500 -0.978

0.400 -0.770 0.520 -0.966

0.410 -0.874 0.540 -0.965

0.430 -0.862 0.550 -0.936

0.440 -0.792 0.580 -0.897

0.460 -0.923 0.600 -0.825

0.470 -0,864 0.610 -0,635

0.490 -0.835 0.650 -2.801 **

0.500 -0.837 0.700 -0.572

0.520 -0.857 0.750 -0.646

0.530 -0.816 0.820 -0.318

0.550 -0.841 0.890 -0.245

0.560 -0,844 0.900 -0,262

0.580 -0.812 0.960 -0.272

0.590 -0.833

0,600 -0.893

0.640 -2.638**

0.700 -0.904

0.750 -0.356

0.820 -2.814"*

0.870 -0.194

0.930 -0.206

0,960 -0.196

Lower Surface

0.020 -0.362 0.020 -0.203 0.020 -0.088 0.020 0.251

0.110 -0.106 0.060 0,084 0.060 0.175 0.060 3,216"*

0.230 0.074 0,090 0.032 0.090 0.077 0.110 0.051

0.400 0.031 0.120 0.042 0.120 -0.257 0.250 -0.037

0.490 0.024 0.200 0.092 0.200 -0.001 0.400 -0.049

0.630 3.260** 0.260 0.005 0.250 0.024 0.490 -0.097

0.750 0.203 0.400 -2.831 ** 0.400 0.025 0.580 -0.041

0.850 0.272 0.490 0.044 0.490 0.078 0.650 0.156

0.900 0.316 0.580 0.143 0.580 0,068 0.750 0.405

0.960 0.128 0.640 0.506 0.650 0.313 0.830 0.497

0.750 0.347 0.750 0,465 0.900 0.585

0.870 0.442 0.890 ******** 0.960 0.385

0.930 0.373 0.930 0.434

0.960 0.229 0.960 -2.830**

CN = 0.622 0.791 0.829 0.761

356
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-53-4-000, MINF = 0.847, Camber = 5/10, ALPT = 7.97, BETA = 0.10, QINF = 293.2,

RNPU = 2,3E+06, CNWP = 0.6637

rl = 0,93 0,76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.060 0,000 0.891 0.000 -5.777** 0.010 -0.819"*

0,060 -0.372 0.020 -0.397** 0.020 -0.309** 0.020 -0.731 **

O. 110 -0,426 0.040 -0.250 0,060 - 1.278 ** 0.060 -0,823

0.200 -0.903 0.060 -0.543 0.090 -0.713 0.110 - 1.015

0.230 -0.856 0.090 -0.605 0,110 -0,836 0.140 1.974"*

0,400 -0.732 0.130 -0.713 0.130 -0,887 0.190 -5.642"*

0,490 -0.618 0.150 -0,850 0.150 -0,952 0.250 -1.177

0.590 -0.537 0.200 -0.850 0.210 - 1.043 0.400 -0.818

0.630 -0.351 0.250 -0.998 0.250 - 1.013 0,490 -0,734

0,700 -0,317 0,260 -0.938 0.340 - 1.057 0.580 -0.629

0.750 -0.873 0.280 -0.998 0,370 -1.050 0,650 -0.578

0.810 -0.928 0.290 - 1.013 0.400 - 1.039 0.700 -0.630

0.840 -0.927 0.310 -0.930 0.410 - 1.010 0.750 -0.701

0,900 -0.457 0.320 -0.932 0.430 - 1.084 0.800 -0.536

0.960 -0.474 0.340 -0.986 0.440 - 1.035 0.830 -0.438

0.350 -0.365** 0.460 - 1.052 0.900 -0.350

0.370 -0.938 0.490 -0.998 0.960 -0.320

0.380 -0.960 0.500 - 1.070

0.400 -0.880 0.520 - 1.034

0,410 -0.988 0.540 - 1.056

0,430 -0.983 0,550 - 1.034

0.440 -0.908 0.580 - 1.002

0.460 - 1,031 0.600 - t .029

0.470 -0.988 0.610 -0.958

0.490 -0.945 0.650 -2.855"*

0,500 -0.946 0.700 -0.845

0.520 -0.930 0.750 -0.731

0.530 -0.915 0.820 -0.305

0,550 -0.937 0.890 -0.256

0.560 -0.936 0.900 -0.260

0.580 -0.902 0,960 -0.263

0.590 -0.944

0.600 -0.980

0,640 -2.690**

0.700 -0.410

0,750 -0.254

0,820 -2.868**

0.870 -0.229

0.930 -0,257

0,960 -0.251

Lower Surface

0.020 -0.272 0.020 -0.011 0.020 0,070 0.020 0.366

0.110 -0.044 0.060 0.166 0.060 0.261 0.060 3.248 * *

0.230 0.118 0,090 0,108 0.090 0.151 0.110 0.109

0,400 0,017 O. 120 0.096 0.120 -0.183 0.250 0.026

0.490 0.032 0.200 0.138 0.200 0.055 0.400 0.003

0,630 3,292** 0.260 0.050 0.250 0.062 0.490 -0.067

0,750 0.176 0.400 -2.885"* 0.400 0.036 0.580 -0.015

0.850 0.260 0.490 0.049 0.490 0.080 0.650 O.167

0.900 0.303 0.580 0.142 0.580 0.073 0.750 0.397

0.960 0,116 0,640 0.497 0,650 0.326 0.830 0.511

0.750 0,355 0.750 0.457 0.900 0.582

0.870 0.411 0,890 ******** 0,960 0.373

0,930 0.342 0.930 0.417

0,960 0.195 0.960 -2.884**

CN = 0.699 0.834 0.952 0.873

357
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-53-6-000, MINF = 0.850, Camber = 5/10, ALPT = 8.01, BETA = 0.26, QINF = 295.9,

RNPU = 2.3E+06, CNWP = 0.6712

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.033 0.000 0.906 0.000 -5.729 * * 0.010 -0.790* *

0.060 -0.348 0.020 -0.358** 0.020 -0.255** 0.020 -0.686**

0.110 -0.449 0.040 -0.225 0.060 - 1.262 * * 0.060 -0.819

0.200 -0.898 0.060 -0.527 0,090 -0.696 0.110 -0.994

0.230 -0.809 0.090 -0.580 0.110 -0.817 0.140 1.959**

0.400 -0.737 0,130 -0.704 0.130 -0.883 0.190 -5.595 **

0.490 -0.635 0.150 -0.827 0.150 -0.922 0.250 - 1.156

0.590 -0.559 0.200 -0.840 0,210 - 1.022 0.400 -0.807

0.630 -0.379 0.250 -0.992 0.250 - 1.000 0.490 -0.731

0.700 -0.318 0.260 -0.912 0.340 - 1.052 0.580 -0.612

0.750 -0.835 0.280 -0.984 0.370 - 1.030 0.650 -0.576

0.810 -0.916 0.290 -0.988 0.400 - 1.026 0.700 -0.628

0.840 -0.885 0.310 -0.919 0.410 -0.997 0,750 -0.699

0.900 -0.451 0.320 -0.909 0.430 - 1.063 0.800 -0.542

0.960 -0.473 0.340 -0.963 0.440 - 1.029 0.830 -0.451

0,350 -0.346** 0.460 -1.041 0.900 -0.345

0.370 -0.915 0.490 -0.955 0.960 -0.323

0.380 -0.936 0.500 -1.059

0.400 -0.861 0.520 - 1.029

0.410 -0.965 0.540 - 1.050

0.430 -0.957 0.550 - 1.023

0.440 -0.880 0.580 -0.961

0.460 - 1.013 0.600 - 1.009

0.470 -0.948 0.610 -0.939

0.490 -0.925 0.650 -2,833"*

0.500 -0.927 0.700 -0.867

0.520 -0.918 0.750 -0.732

0.530 -0.896 0.820 -0.300

0.550 -0.923 0.890 -0.25 l

0.560 -0,944 0.900 -0,257

0.580 -0.897 0.960 -0.272

0.590 -0.924

0.600 -0.975

0.640 -2.670**

0.700 -0.366

0,750 -0.255

0.820 -2.846"*

0.870 -0.244

0.930 -0.251

0.960 -0.248

Lower Surface

0.020 -0.231 0.020 -0,022 0.020 0.066 0.020 0.381

0.110 -0.054 0.060 0.180 0.060 0.269 0.060 3.215" *

0.230 0.110 0.090 0.107 0.090 0.161 0.110 0.104

0.400 0.039 0.120 0.114 0.120 -0,168 0.250 0.022

0.490 0.028 0.200 0.133 0.200 0,045 0.400 -0.001

0.630 3.259** 0.260 0.046 0.250 0.069 0.490 -0.056

0.750 0.189 0.400 -2.863 ** 0.400 0.047 0.580 -0.014

0.850 0.258 0.490 0.060 0.490 0.090 0.650 0.177

0.900 0.299 0.580 0.149 0.580 0.084 0.750 0.419

0.960 0.112 0.640 0.498 0.650 0,327 0.830 0.511

0.750 0.352 0.750 0.471 0.900 0.594

0.870 0,437 0.890 ******** 0.960 0.387

0.930 0.357 0.930 0.432

0.960 0.216 0.960 -2.862**

CN = 0.697 0.827 0.950 0.868

358
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-53-7-000, MINF = 0.851, Camber = 5/10, ALPT = 8,18, BETA = 0.23. QINF = 297.0,

RNPU = 2.3E+06, CNWP = 0.6959

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP xYc CP xYc CP xYc CP

0.020 -0.075 0,000 0.908 0,000 -5.711 ** 0.010 -0.811 **

0.060 -0.349 0.020 -0.437"* 0,020 -0.313"* 0.020 -O761 **

0.110 -0.450 0.040 -0.249 0.060 - 1.248 * * 0.060 -0, 841

0,200 -0.898 0.060 -0.528 0.090 -0.717 0,110 - 1.023

0.230 -0.818 0,090 -0.625 0.1 I 0 -0,862 0.140 1.943"*

0.400 -0.760 0,130 -0.724 0.130 -0.895 0.190 -5.577"*

0.490 -0,665 0,150 -0.855 0.150 -0.955 0.250 - 1,183

0.590 -0.605 0.200 -0.862 0.210 - 1.041 0.400 -0,835

0,630 -0.434 0.250 - 1.018 0.250 - 1.022 0,490 -0,750

0.700 -0.312 0.260 -0.932 0.340 - 1,082 0.580 -0.645

0250 -0,812 0.280 -0.992 0.370 - 1,045 0.650 -0.586

0.810 -0,884 0.290 - 1,006 0.400 - 1.047 0.700 -0.661

0.840 -0.862 0.310 -0.937 0.410 - 1.020 0.750 -0,721

0.900 -0.477 0,320 -0.930 0.430 - 1.077 0,800 -0.543

0.960 -0.510 0,340 -0.976 0.440 - 1.039 0,830 -0.424

0.350 -0.353** 0.460 -1.063 0,900 -0.356

0.370 -0,933 0.490 -0,977 0.960 -0.341

0.380 -0.954 0.500 - 1.077

0.400 -0.882 0.520 - 1.054

0.410 -0.987 0.540 - 1.077

0.430 -0,974 0.550 - 1.040

0.440 -0.916 0.580 -1.031

0.460 - 1,037 0.600 - 1.033

0.470 -0.928 0.610 -0.966

0.490 -0.944 0.650 -2.825**

0.500 -0,948 0.700 -0.990

0.520 -0.933 0.750 -0.641

0.530 -0.916 0.820 -0.335

0.550 -0.941 0.890 -0.289

0.560 -0.937 0,900 -0.300

0.580 -0.917 0,960 -0.315

0.590 -0.941

0.600 -0,989

0.640 -2.662**

0.700 -0.364

0.750 -0.268

0.820 -2.838**

0.870 -0.254

0.930 -0,272

0.960 -0,258

Lower Surface

0,020 -0.195 0.020 0,017 0.020 0,102 0.020 0.409

0,110 -0.043 0.060 0,198 0.060 0.278 0.060 3.200"*

0.230 0.122 0.090 0.121 0,090 0.180 0,110 0.122

0.400 0,040 0.120 0.118 0.120 -0.170 0.250 0.032

0,490 0.055 0.200 0,137 0.200 0.049 0,400 0.004

0.630 3.244** 0.260 0.043 0.250 0.081 0.490 -0.051

0.750 0.182 0.400 -2.855"* 0.400 0.054 0,580 -0,006

0,850 0.250 0.490 0.057 0.490 0,087 0.650 0.177

0.900 0.295 0,580 0.149 0.580 0.084 0.750 0.415

0.960 0,112 0,640 0.505 0.650 0.322 0.830 0.511

0.750 0.357 0.750 0.467 0.900 0.595

0,870 0.428 0.890 ******** 0.960 0.388

0.930 0.350 0.930 0.428

0.960 0.201 0.960 -2.854**

CN = 0.715 0.843 0.982 0.893

359
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-53-17-000, MINF = 0.846, Camber = 5/10, ALPT = 10.07, BETA = 0.39, QINF = 299.6,

RNPU = 2.4E+06, CNWP = 0.7388

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.324 0.000 0.883 0.000 -5.702"* 0.010 -0.913"*

0.060 -0.495 0.020 -0.714"* 0.020 -0.644"* 0.020 -0.951 **

0,110 -0.624 0.040 -0.378 0.060 - 1.295"* 0.060 - 1.048

0,200 - 1.004 0.060 -0.674 0.090 -0.850 0.110 - 1.149

0.230 -0.886 0.090 -0.790 0.110 -0.999 0.140 1.923"*

0.400 -0,878 0.130 -0.917 0.130 - 1.038 0.190 -5.569 **

0.490 -0.772 0.150 -0.986 0.150 - 1.087 0.250 - 1.315

0.590 -0.390 0.200 - 1.007 0.210 - 1.164 0.400 -0.899

0.630 -0.238 0.250 - I. 149 0.250 - 1.147 0.490 -0,835

0.700 -0.280 0.260 - 1,057 0.340 - 1.208 0.580 -0.759

0.750 -0.825 0,280 - 1.127 0.370 - 1.190 0.650 -0.708

0.810 -0.913 0.290 -1.142 0,400 -1.107 0.700 -0.768

0.840 -0.889 0.310 -1.054 0.410 -1.119 0.750 -0.748

0.900 -0.465 0.320 - 1.044 0.430 - 1.203 0.800 -0.528

0.960 -0.396 0,340 - 1.118 0.440 - 1.177 0.830 -0.431

0.350 -0.337"* 0.460 -1.176 0.900 -0.322

0,370 - 1.048 0.490 - 1.082 0.960 -0.312

0.380 -1.081 0.500 -1.185

0.400 -1.012 0.520 -1.171

0.410 -1,108 0.540 -1.190

0.430 - 1.090 0.550 - 1.1 64

0.440 -1.005 0.580 -1.142

0.460 -1.130 0.600 -1.091

0.470 -0.818 0.610 -0.758

0,490 -0.610 0.650 -2.841 * *

0.500 -0.558 0.700 -0.555

0.520 -0.526 0.750 -0.600

0.530 -0.511 0,820 -0.484

0.550 -0.461 0.890 -0.439

0.560 -0.483 0,900 -0.442

0.580 -0.455 0.960 -0.440

0.590 -0.481

0.600 -0.483

0,640 -2.680**

0.700 -0.419

0.750 -0.356

0.820 -2.854**

0.870 -0.362

0.930 -0.343

0.960 -0.322

Lower Surface

0,020 0,032 0.020 0.260 0.020 0.307 0.020 0.562

0.110 0.028 0.060 0.304 0.060 0.385 0.060 3.132"*

0.230 0.188 0.090 0.230 0.090 0.283 0.110 0.230

0.400 0.057 0.120 0.217 0.120 -0.079 0.250 0.110

0.490 0.043 0.200 0.204 0.200 0.114 0.400 0.058

0.630 3.175"* 0.260 0.1 04 0.250 0.161 0.490 0.012

0.750 0.157 0.400 -2.871 ** 0.400 0.087 0.580 0.028

0.850 0.239 0.490 0.093 0.490 0.089 0.650 0.197

0.900 0.269 0.580 0.158 0.580 0.116 0,750 0.449

0.960 0.086 0.640 0.501 0.650 0.330 0,830 0.514

0.750 0.342 0.750 0.484 0.900 0.593

0.870 0.428 0.890 ******** 0.960 0.397

0.930 0.331 0.930 0.412

0.960 0.191 0.960 -2.870**

CN = 0.753 0.882 1.067 1.011

360
Table F-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-53-18-500, MINF = 0.845, Camber = 5/10, ALPT = 9.96, BETA = 0,28. QINF = 300.2,

RNPU = 2.4E+06, CNWP = 0.7215

rl = 0,93 0,76 0,59 040

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.418 0.000 0.875 0.000 -5.698 ** 0.010 -0.898 * *

0.060 -0.566 0.020 -0.706"* 0.020 -0,720 ** 0.020 -0.943 **

0,1 I 0 -0.685 0.040 -0.548 0,060 - 1.301 ** 0.060 - 1,117

0.200 - 1.022 0.060 -0,697 0.090 -0,888 0,110 - I. 180

0.230 -0.911 0.090 -0,791 0.110 -1.040 0.140 1,919"*

0.400 -0,900 0.130 -0.926 0.130 - 1,081 0. 190 -5.566"*

0,490 -0,807 0.150 -1.024 0.150 -1.110 0.250 -1.349

0,590 -0,308 0,200 - 1.027 0,210 - 1.189 0.400 -0.939

0.630 -0.272 0.250 - 1.166 0,250 - 1.167 0.490 -0,856

0.700 -0.310 0.260 - 1,076 0.340 - 1.230 0,580 -0.797

0.750 -0.820 0.280 - 1,151 0.370 - 1.221 0.650 -0.737

0.810 -0.919 0.290 - 1.161 0.400 - 1.193 0.700 -0.776

0.840 -0,903 0.310 - 1.089 0.410 - 1.160 0.750 -0.733

0.900 -0,404 0,320 - 1.073 0.430 - 1.225 0.800 -0.506

0.960 -0.432 0.340 -1.138 0.440 -1.190 0.830 -0,410

0.350 -0.360"* 0.460 - 1.217 0.900 -0,297

0.370 -1.083 0,490 -1.110 0.960 -0.311

0,380 -1,100 0.500 -1.210

0,400 - 1.026 0.520 - 1,197

0.410 - 1.083 0,540 - 1.195

0.430 -0,812 0,550 -1.168

0.440 -0.621 0,580 - 1,063

0,460 -0,704 0.600 -0.792

0470 -0.604 0.610 -0.61 I

0.490 -0,536 0.650 -2.844**

0.500 -0.543 0.700 -0.548

0,520 -0.526 0,750 -0,628

0.530 -0.514 0.820 -0,520

0.550 -0,504 0.890 -0.454

0.560 -0,501 0.900 -0.454

0.580 -0.462 0.960 -0.444

0.590 -0.490

0.600 -0.515

0.640 -2.683**

0.700 -0.434

0.750 -0.363

0,820 -2,856**

0.87O -0.355

0.930 -0,332

0,960 -0.333

Lower Surface

0,020 0.043 0.020 0.301 0.020 0.338 0,020 0.624

0.110 0.044 0,060 0.328 0,060 0.417 0.060 3,117"*

0.230 0.183 0.090 0.239 0,090 0.308 0.110 0.211

0.400 0.053 0.120 0.216 0.120 -0,063 0.250 0.12 I

0.490 0,027 0.200 0.203 0,200 0.112 0.400 0.072

0,630 3,160"* 0.260 0.118 0.250 0,167 0.490 0.012

0.750 0,156 0.400 -2,873 * * 0.400 0,104 0.580 0.044

0.850 0.219 0.490 0,084 0.490 0.092 0.650 0.203

0,900 0.267 0.580 0,161 0.580 0.107 0.750 0.445

0,960 0.080 0.640 0.500 0.650 0.329 0.830 0.519

0.750 0.354 0.750 0.471 0.900 0.604

0.870 0.410 0.890 ******** 0.960 0.388

0.930 0.323 0.930 0.410

0.960 0,172 0.960 -2.872**

CN = 0.766 0.881 1.076 1.031

361
Table F-2. Continued.

Flight 225, Wing sweep = 26 °. Time = 11-54-45-000, MINF = 0.852, Camber = 5/10, ALPT = 4.01, BETA = -0.44, QINF = 296.8,

RNPU = 2.3E+06, CNWP = 0.2698

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.277 0.000 0,590 0.000 3.750"* 0.010 -0.081

0,060 0.047 0.020 -0.114 0.020 0.213 0.020 -0.042

0.110 -0.135 0.040 0.084 0,060 -3.793"* 0,060 -0.414

0.200 -0.703 0.060 -0.166 0.090 -0.319 0.110 -0.535

0.230 -0.153 0.090 -0.293 0.110 -0.544 0.140 -0,834

0.400 -0.201 0.130 -0.431 0.130 -0.585 0.190 - 1.969* *

0.490 -0.221 0.150 -0.680 0.150 -0.787 0.250 -0.612

0.590 -0.283 0.200 -0,653 0.210 -0.754 0.400 -0.335

0.630 -0.317 0.250 -0.770 0.250 -0,673 0.490 -0.318

0.700 -0.365 0.260 -0.650 0.340 -0.330 0.580 -0.367

0.750 -0.641 0.280 -0.720 0.370 -0.299 0.650 -0.406

0.810 -0.593 0.290 -0.702 0.400 -0.304 0.700 -0.386

0.840 -0.578 0.310 -0.593 0,410 - 1.662** 0.750 -0,490

0.900 -0,277 0.320 -0.465 0.430 -0.324 0.800 - 1,114

0.960 -0,262 0.340 -0.242 0.440 -0.282 0.830 -0.586

0.350 -0.207** 0.460 -0.324 0.900 -0.429

0.370 -0.173 0.490 -0.195 0.960 -0.425

0.380 -0.264 0.500 -0.335

0.400 -0.145 0.520 -0.278

0,410 -0.285 0.540 -0.291

0.430 -0.254 0.550 -0.274

0,440 -0.172 0.580 -0.295

0.460 -0.357 0.600 -0.297

0.470 -0,271 0.610 -0.321

0,490 -0.287 0.650 2,291 **

0,500 -0,325 0.700 -0.547

0.520 -0.313 0.750 -0.640

0.530 -0,280 0,820 -0,724

0.550 -0,298 0.890 -0.393

0,560 -0,328 0.900 -0.462

0.580 -0,303 0,960 -0.372

0,590 -0,347

0,600 -0.378

0.640 -0,507

0.700 -0.513

0.750 0,000**

0,820 -0.526

0.870 -0.305

0,930 -0.325

0.960 -0.321

Lower Surface

0.020 - t .074 0,020 - 1.172 0.020 -0,975 0.020 -0.192

0.110 -0.170 0,060 -0.249 0.060 -0.082 0.060 1.998"*

0.230 -0.038 0.090 -0.202 0.090 1.516"* 0.110 -0.107

0.400 0.028 0.120 -0.102 0.120 -0.477 0.250 -0.210

0.490 0.070 0.200 -0.054 0.200 -0.128 0.400 -0.158

0.630 2.298"* 0.260 -0.129 0.250 -0.106 0.490 -0.213

0.750 0.175 0.400 -0.032 0.400 -0.089 0.580 -0.113

0.850 0.269 0.490 -0.024 0.490 -0.013 0.650 0.101

0.900 0.310 0.580 0.060 0.580 0.039 0.750 0.306

0.960 0.151 0.640 0.287 0.650 -0.027 0.830 0.470

0,750 0.357 0.750 0.115 0.900 0.517

0.870 0.394 0.890 0.425 0.960 0.342

0,930 0.314 0.930 0,347

0,960 0.208 0.960 -1.915"*

CN = 0.352 0.478 0.443 0.500

362
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-55-6-500, M1NF = 0.848, Camber = 5/11, ALPT = 5.03, BETA = -0.67, QINF = 291.2.

RNPU = 2,3E+06. CNWP = 0.3505

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.164 0.000 0.681 0.000 3.843"* 0.010 -0.309

0.060 -0.147 0.020 -0.010 0.020 0.034 0.020 -0.204

0.110 -0.492 0.040 -0.023 0.060 -3.847 ** 0.060 -0.584

0.200 -0.777 0.060 -0.292 0.090 -0,385 0.110 -0.738

0.230 -0.643 0.090 -0.374 0. I 10 -0.640 0.140 -0.953

0.400 -0.154 0.130 -0.516 0.130 -0.677 0.190 - 1.987"*

0,490 -0.198 0.150 -0.767 0.150 -0.891 0.250 -0,663

0.590 -0.339 0.200 -0,759 0.210 -0.841 0.400 -0.416

0.630 -0.323 0.250 -0.887 0.250 -0.794 0.490 -0.397

0.700 -0.364 0.260 -0.750 0.340 -0.874 0.580 -0.409

0.750 -0.977 0.280 -0.834 0.370 -0.842 0.650 -0.457

0.810 -0.800 0.290 -0.816 0.400 -0.853 0.700 -0.432

0.840 -0.738 0.310 -0.785 0.410 - 1.675"* 0.750 -0.526

0.900 -0.319 0.320 -0.773 0.430 -0.496 0.800 - 1.030

0.960 -0.347 0.340 -0.758 0.440 °0.368 0.830 -0.590

0.350 -0.484"* 0.460 -0.350 0,900 -0.433

0,370 -0.741 0.490 -0.225 0,960 -0.454

0.380 -0.832 0.500 -0.333

0.400 -0.723 0.520 -0.260

0.410 -0.806 0.540 -0.271

0.430 -0.397 0.550 -0.234

0,440 -0.244 0.580 -0.242

0.460 -0.323 0.600 -0.286

0.470 -0.213 0.610 -0.295

0.490 -0.197 0.650 2.355 **

0.500 -0.163 0.700 -0.549

0.520 -0,178 0.750 -0.637

0.530 -0.186 0.820 -0.684

0.550 -0.306 0.890 -0.391

0.560 -0.247 0.900 -0.471

0.580 -0.237 0.960 -0.364

0.590 -0.306

0.600 -0.340

0.640 -0.497

0.700 -0.469

0.750 -0.003"*

0.820 -0.524

0.870 -0.370

0.930 -O.343

0.960 -0.341

Lower Surface

0.020 -0.726 0.020 -0.615 0.020 -0.299 0.020 -0.001

0.110 -0.162 0.060 -0.086 0.060 0.013 0.060 2.057"*

0.230 -0.022 0.090 -0.130 0.090 1.565"* 0.110 -0.078

0.400 0.022 O. 120 -0.066 O. 120 -0.431 0.250 -0.139

0.490 0.068 0.200 -0.008 0.200 -0.114 0.400 -0.123

0.630 2.363** 0.260 -0.086 0.250 -0.059 0.490 -0.159

0.750 O. 167 0.400 -0.013 0.400 -0.046 0.580 -0.090

0.850 0.275 0,490 -0.005 0.490 0.014 0.650 O. 130

0.900 0.317 0.580 0.077 0.580 0.066 0.750 0.326

0.960 O. 118 0.640 0.301 0.650 -0.015 0.830 0.483

0.750 0.378 0.750 0.099 0.900 0,525

0.870 0.410 0.890 0.445 0.960 0.348

0.930 0.313 0.930 0.389

0.960 0.220 0.960 -1.932**

CN = 0.477 0.584 0.559 0.594

363
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-55-20-500, MINF = 0.852, Camber = 5/10, ALPT = 7.94, BETA = -0.15, QINF = 296.1,

RNPU = 2.3E+06, CNWP = 0.5658

11 = 0.93 0.76 0.59 0.40

Upper S ur face

x/c CP x/c CP x/c CP x/c CP

0.020 -0.157 0.000 0.862 0.000 3.582** 0.010 -0.783

0.060 -0.392 0.020 -0.461 0.020 -0.349 0.020 -0.741

0.110 -0.619 0.040 -0.293 0.060 -3.799** 0.060 -0.784

0.200 -0.853 0,060 -0.619 0.090 -0.682 0.110 -0.975

0.230 -0.757 0.090 -0,636 0,110 -0.902 0.140 - 1.160

0.400 -0,758 0.130 -0.738 0.130 -0.879 0.199 - 1.970**

0.490 -0.631 0.150 -0.902 0.150 - 1.028 0.250 - 1.182

0.590 -0.639 0.200 -0.884 0.210 -1.015 0.400 -0.868

0.630 -0.448 0.250 - 1.036 0.250 -0.971 0,490 -0.710

0.700 -0.341 0,260 -0.923 0.340 - 1.059 0.580 -0.663

0.750 -0,849 0.280 -0.997 0.370 - 1.036 0.650 -0.662

0.810 -0.830 0.290 - 1.003 0.400 - 1.049 0.700 -0.673

0.840 -0.824 0.310 -0.978 0.410 -2.008** 0.750 -0.716

0.900 -0.549 0.320 -0.956 0.430 -1.082 0.800 -0,561

0.960 -0.550 0.340 -0.959 0.440 - 1.023 0,830 -0,450

0.350 -0.480** 0.460 - 1.065 0.900 -0.369

0.370 -0,922 0,490 -0.949 0.960 -0.369

0.380 - 1.049 0.500 - 1.089

0.400 -0.893 0.520 - 1.028

0.410 - 1.028 0.540 - 1.059

0.430 -0.971 0,550 -1.011

0.440 -0.887 0.580 - 1.004

0.460 - 1.096 0.600 - 1.005

0.470 -0.994 0.610 -1.011

0.490 -0,974 0,650 2.299**

0.500 -0.976 0.700 -0.994

0.520 -0.979 0.750 -0,769

0.530 -0,936 0.820 -0.351

0.550 - 1.035 0.890 -0.307

0.560 -0.973 0.900 -0.305

0.580 -0,967 0.960 -0,273

0.590 -I .013

0.600 - 1.027

0.640 -0.429

0.700 -0.400

0.750 0.033**

0.820 -0.258

0,870 -0.265

0.930 -0.308

0.960 -0,288

Lower Surface

0.020 -0.279 0.020 0.009 0.020 0.113 0.020 0.382

0.110 -0.049 0,060 0.141 0.060 0.254 0.060 1.901 **

0.230 0.083 0.090 0.060 0,090 1.522** 0.110 0.136

0.400 0.027 0.120 0.097 0.120 -0.204 0.250 0.012

0.490 0.058 0.200 0.086 0.200 0.002 0.400 0.007

0.630 1.962"* 0.260 0.002 0.250 0.067 0.490 -0.082

0.750 0.135 0.400 0.035 0.400 0.034 0.580 -0.044

0.850 0.237 0.490 0.017 0.490 0.032 0.650 0.157

0.900 0.315 0.580 0.086 0.580 0.093 0.750 0.369

0.960 0.119 0.640 0.298 0.650 0.021 0.830 0.515

0.750 0.376 0.750 0.133 0.900 0.554

0.870 0.423 0.890 0.466 0.960 0.358

0.930 0.325 0.930 0.381

0.960 0.215 0.960 -2.097**

CN = 0.712 0.822 0.885 0.908

364
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-55-22-000. MINF = 0.854, Camber = 5/10, ALPT = 7.95, BETA = -0.15, QINF = 299.3,

RNPU = 2.4E+06, CNWP = 0.5851

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.110 0.000 0.847 0.000 3.534** 0.010 -0.763

0.060 -0.269 0.020 -0.527 0.020 -0.324 0.020 -0.743

0.110 -0.483 0.040 -0.277 0.060 -3.768"* 0.060 -0.765

0.200 -0.853 0.060 -0.606 0.090 -0.752 0.110 -0.974

0.230 -0.740 0.090 -0.635 0.110 -0.869 0.140 - 1.193

0.400 -0.756 0.130 -0.733 0.130 -0.853 0.190 - 1.959"*

0.490 -0.670 0.150 -0.902 0.150 -1.033 0.250 - 1.115

0.590 -0.627 0.200 -0.863 0.210 -1.019 0.400 -0.869

0.630 -0.465 0.250 - 1.007 0.250 -0.956 0.490 -0.726

0.700 -0.437 0.260 -0.922 0.340 - 1.043 0.580 -0.660

0.750 -0.846 0.280 - 1.011 0.370 - 1.035 0.650 -0.650

0.810 -0.816 0.290 -0.979 0.400 - 1.055 0.700 -0.665

0.840 -0.810 0.310 -0.971 0.410 - 1.997 ** 0.750 -0.703

0.900 -0.563 0.320 -0.960 0.430 - 1.065 0.800 -0.578

0.960 -0.568 0.340 -0.944 0.440 - 1.007 0.830 -0.431

0.350 -0.484** 0.460 -1.043 0.900 -0.369

0.370 -0.922 0.490 -0.926 0.960 -0.375

0.380 - 1.028 0.500 - 1.097

0.400 -0.879 0.520 - 1.012

0.410 - 1.027 0.540 - 1.057

0.430 -0.979 0.550 -0.995

0.440 -0.890 0.580 -0.985

0.460 - 1.067 0.600 - 1.004

0.470 -0.967 0.610 -0.982

0.490 -0.954 0.650 2.265"*

0.500 -0.991 0.700 - 1.008

0.520 -0.964 0.750 -0.767

0.530 -0.947 0.820 -0.357

0.550 -0.997 0.890 -0.329

0.560 -0.972 0.900 -0.322

0.580 -0.967 0.960 -0.283

0.590 - 1.007

0.600 - 1.021

0.640 -0.408

0.700 -0.387

0.750 0.04 1* *

0.820 -0.280

0.870 -0.298

0.930 -0.311

0.960 -0.299

Lower Surface

0.020 -0.305 0.020 -0.004 0.020 0.102 0.020 0.384

O. 110 -0.058 0.060 O. 130 0.060 0.255 0.060 1.871 **

O. 230 0.099 0.090 0.050 0.090 1.497"* O. 110 O. 115

0.400 0.040 0.120 0.101 0.120 -0.233 0.250 -0.016

0.490 0.033 0.200 0.091 0.200 -0.004 0.400 -0.002

0.630 1.931 ** 0.260 0.007 0.250 0.064 0.490 -0.076

0.750 0.162 0.400 0.025 0.400 0.024 0.580 -0.053

0.850 0.233 0.490 0.026 0.490 0.040 0.650 0.160

0.900 0.312 0.580 0.075 0.580 0.079 0.750 0.345

0.960 0.096 0.640 0.315 0.650 0.011 0.830 0.514

0.750 0.354 0.750 0.137 0.900 0.545

0.870 0.437 0.890 0.452 0.960 0.363

0.930 0.312 0.930 0.389

0.960 0.210 0.960 -2.084 * *

CN = 0.702 0.819 0.882 0.889

365
Table F-2. Continued.

Flight 225, Wing sweep = 26", Time = I I..48-47-500, MINF = 0.855, Camber = 10/2, ALPT = 5.08, BETA = -0.04, QINF = 299.0,

RNPU = 2.3E+06, CNWP = 0.3061

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.485 0.000 0.213 0.000 3.887** 0.010 0.351

0.060 0.049 0.020 0.165 0.020 0.527 0.020 0.238

0.110 -0.363 0.040 0.281 0.060 -3.588** 0.060 -0.309

0.200 -0.971 0.060 -0.101 0.090 -0.257 0.110 -0.576

0.230 -0.882 0.090 -0.277 0.110 -0.570 0.140 -1.033

0.400 -0.146 O. 130 -0.512 0.130 -0.755 O. 190 - 1.954"*

0.490 -0.094 0.150 -0.823 0.150 -0.994 0.250 -0.779

0.590 -0.214 0.200 -0.881 0.210 -0.947 0.400 -0.664

0.630 -0.206 0.250 -0.962 0.250 -0.865 0.490 -0.402

0.700 -0.161 0.260 -0.861 0.340 -0.900 0.580 -0.405

0.750 -0.241 0.280 -0.910 0.370 -0.893 0.650 -0.408

0.810 -0.238 0.290 -0.899 0.400 -0.901 0.700 -0.413

0.840 -0.178 0.310 -0.871 0.410 - 1.650"* 0.750 -0.444

0.900 -0.123 0.320 -0.838 0.430 -0.893 0.800 -0.409

0.960 -0.038 0.340 -0.834 0.440 -0.848 0.830 -0.298

0.350 -0.521 ** 0.460 -0.863 0.900 -0.166

0.370 -0.792 0.490 -0.427 0.960 -0.001

0.380 -0.904 0.500 -0.405

0.400 -0.815 0.520 -0.304

0.410 -0.890 0.540 -0.279

0.430 -0.830 0.550 -0.240

0.440 -0.749 0.580 -0.199

0.460 -0.906 0.600 -0.228

0.470 -0.781 0,610 -0.227

0.490 -0.600 0.650 2.453"*

0.500 -0.356 0.700 -0.330

0.520 -0.286 0.750 -0.425

0.530 -0.190 0.820 -0,321

0.550 -0.204 0.890 -0.094

0.560 -0.1 44 0.900 -0.067

0.580 -0.144 0.960 0.074

0.590 -0.167

0.600 -0.188

0.640 -0.231

0.700 -0.259

0.750 -0.033**

0.820 -0.224

0.870 -0.211

0.930 -0.097

0.960 -0.028

Lower Surface

0.020 -0.822 0.020 -0.187 0.020 -0.802 0.020 -0.758

0.110 -0.556 0.060 -0.611 0.060 -0.453 0.060 2.208**

0.230 -0.097 0.090 -0.491 0.090 ! .506** 0.110 -0.090

0.400 -0.005 0.120 -0.193 0,120 -0.479 0.250 -0.176

0.490 -0.001 0.200 -0.083 0.200 -0.192 0.400 -0.215

0.630 2.282** 0.260 -0.133 0.250 -0.076 0.490 -0.330

0.750 0.017 0.400 -0.111 0.400 -0.168 0.580 -0.322

0.850 0,134 0.490 -0.137 0.490 -0.042 0,650 -0.146

0.900 0.169 0.580 -0.093 0.580 -0.163 0.750 0.098

0.960 0.135 0.640 0.051 0.650 -0.057 0.830 0.295

0.750 0.177 0.750 0.077 0.900 0.336

0.870 0.264 0.890 0.248 0.960 0.287

0.930 0.187 0.930 0.226

0.960 0.173 0.960 - 1.738"*

CN = 0.212 0.375 0.378 0.398

366
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-49-11-500, MINF = 0.857, Camber = 10/L ALPT = 5.99, BETA -- -0.30, QINF = 299.3,

RNPU = 2.3E+06, CNWP = 0.3632

"q = 0.93 0.76 0.59 0.40

Upper Surtace

x/c CP x/c CP x/c CP x/c CP

0.020 0.442 0,000 0.289 0_000 3.888"* 0.010 0.257

0,060 -0,002 0.020 0.341 0.020 0.460 0.020 O. 149

O. 110 -0.392 0.040 0.264 0.060 -3.579** 0.060 -0.440

0.200 - 1.015 0.060 -0.157 0.090 -0.304 O. 110 -0.708

0.230 -0.793 0,090 -0.315 0.110 -0.624 O. 140 -1.063

0.400 -0.721 0,130 -0.545 0.130 -0.797 O. 190 - 1.947"*

0.490 -0.070 O. 150 -0.860 O.150 - 1.0 ! 3 0.250 - 1.027

0.590 -0,174 0.200 -0.903 0.210 -0.983 0.400 -0.777

0.630 -0.181 0.250 - 1.000 0.250 -0.910 0.490 -0.505

0.700 -0.137 0.260 -0.895 0.340 -0.969 0.580 -0.493

0.750 -0.255 0.280 -0.963 0.370 -0.957 0.650 -0.519

0.810 -0.240 0.290 -0.945 0.400 -0.984 0.700 -0.516

0.840 -0.195 0.310 -0.916 0.410 - 1.643 * * 0.750 -0.562

0.900 -0.146 0.320 -0.901 0.430 -0.977 0.800 -0.327

0.960 -0,047 0.340 -0.897 0.440 -0.914 0.830 -0.229

0.350 -0.516"* 0.460 -0.950 0.900 -0.111

0.370 -0.852 0.490 -0.852 0.960 0.016

0.380 -0.967 0.500 -0.974

0.400 -0.765 0.520 -0.923

0.410 -0.942 0.540 -0.921

0.430 -0.894 0.550 -0.726

0.440 -0.822 0.580 -0.507

0.460 -0.986 0.600 -0,446

0.470 -0.892 0.610 -0.397

0.490 -0.891 0.650 2.456'*

0.500 -0.826 0.700 -0.284

0.520 -0.886 0.750 -0.375

0.530 -0.857 0.820 -0.256

0.550 -0.927 0.890 -0.079

0.560 -0.808 0.900 -0.035

0.580 -0.473 0.960 0.071

0.590 -0.379

0.600 -0.320

0.640 -0,129

0,700 -0.155

0.750 -0.025**

0.820 -0.173

0.87O -0,184

0.930 -0.073

0.960 -0.012

Lower Surface

0.020 -0.744 0,020 -0.171 0.020 -0.881 0.020 -0.503

O.110 -0.512 0.060 -0.493 0.060 -0.160 0.060 2.210'*

0.230 -0.077 0.090 -0.357 0.090 1.509** 0.110 -0.004

0.400 0.000 0.120 -0.085 0.120 -0.354 0.250 -0.133

0.490 -0.010 0.200 -0.070 0.200 -0.139 0.400 -0.181

0.630 2.285** 0.260 -0.098 0.250 -0.057 0.490 -0.288

0.750 0.022 0.400 -0.090 0.400 -0.147 0.580 -0.321

0.850 0.120 0.490 -0.128 0.490 -0.029 0.650 -0.119

0.900 0.168 0.580 -0.088 0.580 -0.147 0.750 0.107

0.960 0.136 0.640 0.067 0.650 -0.044 0.830 0.308

0.750 0.199 0.750 0.067 0.900 0.344

0.870 0.186 0.890 0.267 0.960 0.271

0.930 0.206 0.930 0.242

0.960 0.174 0.960 - 1.731 * *

CN = 0.287 0.449 0,495 0.516

367
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-49-15-000, MINF = 0.856, Camber = 10/2, ALPT = 7,10, BETA = -0.56, QINF = 297.6,

RNPU = 2.3E+06, CNWP = 0.4462

rl = 0.93 0,76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.395 0.000 0.397 0.000 3.916"* 0.010 0.118

0.060 -0.024 0.020 0.121 0.020 0.373 0,020 0.031

0. | 10 -0.353 0.040 0.176 0.060 -3.592"* 0.060 -0,509

0.200 -1.052 0.060 -0.198 0.090 -0,372 0.110 -0.823

0,230 -0.911 0.090 -0.353 0.110 -0.666 0.140 -1.151

0.400 -0.778 0.130 -0.594 0.130 -0.830 0.190 - 1.951 **

0.490 -0.516 0.150 -0.903 0.150 - 1.054 0.250 - 1.069

0.590 -0.168 0.200 -0.953 0.210 - 1.028 0.400 -0,803

0.630 -0.160 0,250 - 1.063 0.250 -0,973 0,490 -0,624

0.700 -0.115 0.260 -0.941 0.340 - 1.029 0,580 -0.558

0.750 -0.241 0.280 - 1.005 0.370 - 1.034 0,650 -0.566

0.810 -0.270 0.290 - 1.005 0.400 - 1.049 0.700 -0,574

0.840 -0.178 0.310 -0.982 0.410 - 1.646"* 0.750 -0.602

0,900 -0.162 0,320 -0.957 0.430 - 1,036 0.800 -0.322

0,960 -0,062 0.340 -0.957 0.440 -0.985 0,830 -0.205

0.350 -0.544** 0,460 - 1.027 0.900 -0.064

0.370 -0.912 0.490 -0.926 0.960 0.015

0.380 - 1.030 0.500 - 1.049

0.400 -0.884 0.520 -0.989

0,410 -1.009 0,540 -1.015

0.430 -0.961 0.550 -0.958

0,440 -0.875 0,580 -0,926

0,460 - 1.057 0.600 -0,945

0.470 -0,962 0.610 -0.894

0.490 -0.952 0,650 2.476**

0.500 -0.988 0.700 -0.342

0.520 -0.955 0.750 -0.392

0,530 -0.926 0.820 -0.183

0.550 -0.998 0.890 -0.037

0.560 -0.943 0.900 -0,002

0.580 -0,939 0,960 0.096

0.590 - 1.005

0.600 -0.984

0.640 -0.257

0.700 -0.226

0.750 -0.011 **

0,820 -0.088

0.870 -0.123

0,930 -0.045

0.960 0.013

Lower Surface

0.020 -0.669 0.020 -0.169 0.020 -0.613 0.020 -0.241

0.110 -0.327 0.060 -0.292 0.060 0.057 0.060 2,229**

0.230 -0.051 0.090 -0.1 64 0.090 1.524"* 0.110 0.064

0.400 -0.012 0,120 0.031 0.120 -0,288 0.250 -0.074

0.490 -0.004 0.200 -0,045 0.200 -0,133 0.400 -0.124

0.630 2.305"* 0,260 -0.041 0.250 -0.010 0.490 -0,245

0.750 0.021 0.400 -0.061 0.400 -0.111 0.580 -0.276

0.850 0.120 0.490 -0.110 0.490 -0.016 0.650 -0.112

0,900 0.162 0.580 -0,089 0.580 -0.133 0,750 0.120

0.960 0.135 0,640 0.078 0.650 -0.038 0.830 0.317

0.750 0.190 0.750 0.075 0,900 0.350

0.870 0.240 0.890 0.290 0.960 0.273

0,930 0.225 0.930 0.261

0,960 0.182 0.960 - 1.733" *

CN = 0.382 0.558 0.609 0.596

368
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-49-22-500, M1NF = 0.842, Camber = 10/2, ALPT = 8.03, BETA = -0.21, QINF = 285.9,

RNPU = 2,3E+06, CNWP = 0,4587

r I = 0.93 026 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.327 0.000 0.508 0.000 4.094"* 0.010 -0.057

0.060 -0.116 0.020 0.043 0.020 0.221 0.020 0.027

0.110 -0.520 0.040 0.070 0,060 -3.722** 0.060 -0.655

0.200 - 1.092 0.060 -0.319 0.090 -0,436 0.1 I0 -0.963

0.230 -0.990 0.090 -0.460 0.110 -0.781 O. 140 - 1.275

0.400 -0.856 0.130 -0.684 0.130 -0.934 0.190 -2.014"*

0.490 -0.474 0.150 -0.995 0.150 - 1.169 0.250 - 1.230

0.590 -0.198 0.200 - 1.052 0.2 l0 - 1.121 0.400 -0.899

0.630 -0.190 0.250 - 1.162 0.250 - 1.064 0.490 -0.732

0.700 -0.139 0.260 - 1.034 0.340 - 1.149 0.580 -0.662

0.750 -0.259 0.280 - I. 121 0.370 - 1.126 0.650 -0.610

0.810 -0,302 0.290 - 1.121 0.400 - 1.052 0.700 -0.592

0.840 -0.223 0.310 - 1.089 0.410 - 1.696"* 0.750 -0.343

0.900 -0.194 0.320 - 1.063 0.430 - 1.156 0.800 -0.289

0.960 -0,099 0,340 - 1.065 0.440 - 1.100 0.830 -0.187

0.350 -0,566"* 0.460 - 1.145 0.900 -0.069

0.370 - 1.017 0.490 - 1.050 0.960 0,005

0.380 -1.146 0,500 -1.164

0,400 -0,984 0.520 -1.101

0.410 -1.117 0.540 -1.132

0.430 - 1.053 0.550 - 1.083

0.440 -0.983 0.580 - 1.094

0.460 -1.170 0.600 -0.790

0.470 - 1 _086 0.610 -0.575

0,490 - 1.061 0.650 2.594"*

0.500 - 1.058 0.700 -0.415

0.520 - 1.066 0.750 -0.484

0.530 - 1.036 0.820 -0.169

0.550 - 1.117 0.890 -0,034

0.560 - 1.049 0.900 -0.007

0.580 -0.688 0.960 0.084

0.590 -0.615

0.600 -0.543

0.640 -0.310

0.700 -0.288

0.750 -0.005**

0.820 -0.094

0.870 -0.111

0,930 -0.045

0.960 -0.004

Lower Surface

0.020 -0.679 0.020 -0.151 0.020 -0.213 0.020 -0,033

0.110 -0.074 0.060 -0.011 0.060 0,172 0.060 2.337**

0.230 -0.021 0.090 -0.019 0.090 1.603"* 0.110 0.147

0.400 -0.023 0.120 0.088 0.120 -0.247 0.250 -0.018

0.490 0.001 0,200 -0.023 0.200 -0.101 0.400 -0.074

0.630 2.416** 0.260 -0.011 0.250 0.04 1 0.490 -0.191

0.750 0.011 0.400 -0,047 0.400 -0.058 0.580 -0.213

0.850 0,093 0.490 -0.094 0.490 0.001 0.650 -0.084

0.900 0.155 0.580 -0.088 0.580 -0.107 0.750 0.121

0.960 0.118 0.640 0.079 0.650 -0.022 0.830 0.320

0.750 0.197 0.750 0.102 0.900 0,349

0.870 0.248 0.890 0.281 0.960 0.258

0.930 0.205 0.930 0.250

0,960 0.175 0.960 - 1.787"*

CN = 0A62 0.638 0.682 0.695

369
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-49-26-500, MINF = 0.845, Camber = 10/2, ALPT = 8.07, BETA = -0.10, QINF = 287.6,

RNPU = 2.3E+06, CNWP = 0.4815

"q -- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.311 0.000 0.507 0.000 4.071 ** 0.010 -0.056

0,060 -0.105 0.020 0.044 0.020 0.229 0.020 -0.037

0.110 -0.359 0.040 0.052 0.060 -3.699"* 0.060 -0.596

0.200 - 1.097 0.060 -0.316 0.090 -0.465 0,110 -0.977

0.230 -0.809 0.090 -0,456 0.110 -0.766 0.140 -1.248

0.400 -0.873 0.130 -0.685 0.130 -0.927 0.190 -2.001 **

0.490 -0.722 0.150 -0.992 0.150 - 1.152 0.250 - 1.251

0.590 -0.200 0.200 - 1.045 0.210 - 1.114 0.400 -0.900

0.630 -0.183 0.250 - 1.154 0.250 - 1.057 0.490 -0.736

0.700 -0.133 0.260 - 1.027 0.340 - 1.141 0.580 -0.662

0.750 -0.256 0.280 - 1.122 0.370 - 1.142 0.650 -0.653

0.810 -0.284 0.290 - 1.095 0.400 - 1.091 0.700 -0.630

0.840 -0.209 0.310 - 1.085 0.410 - 1.685 * * 0.750 -0.400

0.900 -0.189 0.320 -1.055 0.430 - 1.148 0.800 -0.286

0.960 -0.097 0.340 - 1.058 0.440 - 1.109 0.830 -0.176

0.350 -0.561"* 0.460 -1.142 0.900 -0.067

0.370 - 1.010 0.490 - 1.059 0.960 -0.009

0.380 -1.143 0.500 -1.166

0.400 -0.977 0,520 - 1.102

0.410 -1.110 0.540 -1.124

0,430 - 1.061 0,550 - 1.075

0.440 -0.976 0.580 - 1.050

0.460 - 1.162 0.600 - 1.072

0.470 - 1.058 0.610 -0.710

0.490 -1.062 0.650 2.581 **

0.500 - 1.107 0.700 -0.458

0.520 - 1.067 0.750 -0.518

0.530 -1.036 0.820 -0.180

0.550 - 1.090 0.890 -0.032

0.560 - 1.036 0.900 -0.011

0.580 -0.710 0.960 0.095

0.590 -0.629

0.600 -0.569

0.640 -0.352

0.700 -0.339

0,750 0.003**

0.820 -0.120

0.870 -0.094

0.930 -0.044

0.960 -0.006

Lower Surface

0.020 -0.702 0.020 -0.149 0.020 -0.194 0.020 -0.025

0.1 t 0 -0.065 0.060 -0.002 0.060 0.173 0.060 2.325 **

0.230 -0.011 0.090 -0.012 0.090 1.596"* 0.110 0.127

0.400 -0.026 0.120 0.096 0.120 -0.236 0.250 -0.017

0.490 -0.013 0.200 -0.014 0.200 -0.113 0.400 -0.072

0.630 2.403'* 0.260 -0.010 0.250 0.050 0.490 -0.189

0.750 0.008 0.400 -0.033 0.400 -0.061 0.580 -0.226

0.850 0.106 0.490 -0.1 (30 0.490 -0.005 0.650 -0.090

0.900 0.161 0.580 -0.094 0.580 -0.112 0.750 0.127

0.960 0.128 0.640 0.076 0.650 -0.021 0.830 0.328

0.750 0.223 0.750 0.095 0.900 0.349

0.870 0.238 0.890 0.280 0.960 0.264

0.930 0.206 0,930 0.250

0.960 0.168 0.960 - 1.776**

CN = 0,453 0.649 0.698 0,704

370
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-49-33-000, M1NF = 0.851, Camber = 10/2, ALPT = 9.05, BETA = -0.10, QINF = 295.0,

RNPU = 2.3E+06, CNWP = 0.4381

rl = 0,93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.256 0,000 0.638 0,000 3.948"* 0.010 -0.067

0.060 -0.169 0.020 -0.063 0.020 0,152 0.020 -0,127

0.110 -0.473 0.040 -0,008 0.060 -3.628 * * 0,060 -0,715

0.200 - 1.127 0060 -0,346 0.090 -0.592 0,1 I 0 - 1,038

0,230 -0.968 0.090 -0,503 0.110 -0.839 0.140 -1.295

0.400 -0,621 0,130 -0.672 0.130 -0.982 0.190 - 1.972"*

0.490 -0.274 0.150 - 1,023 0.150 - 1.174 0,250 - 1.254

0.590 -0.240 0,200 - 1.065 0.210 - 1.148 0.400 -0.975

0.630 -0,236 0,250 - 1.183 0.250 - 1.084 0.490 -0.795

0.700 -0.178 0,260 - 1.069 0.340 - 1,195 0,580 -0.769

0.750 -0,303 0,280 - 1.153 0.370 - 1.169 0,650 -0.524

0.810 -0.275 0.290 - 1.112 0.400 - 1.167 0.700 -0.490

0.840 -0,232 0.310 -1.009 0.410 -1.664"* 0,750 -0.315

0.900 -0,173 0,320 -0.979 0.430 -0.958 0.800 -0,284

0.960 -0,122 0.340 - 1.036 0.440 -0.705 0,830 -0.242

0.350 -0.527** 0.460 -0.681 0.900 -0.120

0,370 -0.682 0.490 -0.555 0.960 -0,04 1

0.380 -0.725 0.500 -0.649

0.400 -0.576 0.520 -0.627

0.410 -0.673 0.540 -0.617

0.430 -0.594 0.550 -0.578

0,440 -0.521 0.580 -0,567

0,460 -0.656 0.600 -0.535

0,470 -0.557 0.610 -0.519

0.490 -0.529 0.650 2.495 **

0,500 -0.544 0.700 -0.482

0.520 -0,542 0.750 -0.575

0.530 -0.476 0.820 -0.368

0,550 -0.537 0.890 -0.288

0,560 -0,478 0.900 -0.290

0,580 -0.487 0.960 -0.198

0.590 -0.482

0.600 -0.496

0.640 -0.371

0200 -0.381

0.750 -0.013"*

0,820 -0.253

0.870 -0.343

0.930 -0.247

O,96O -0.224

Lower Surface

0.020 -0,804 0.020 -0.136 0.020 -0.054 0,020 0.205

0.1 l0 -0.043 0,060 0.114 0.060 0.204 0.060 2.246**

0.230 0,006 0,090 0.048 0.090 1.535"* 0.110 0.277

0.400 -0,005 0.120 0.158 0.120 -0.160 0.250 0.039

0.490 -0.041 0.200 0.003 0.200 -0.075 0.400 -0,040

0,630 2.322** 0,260 0.007 0.250 0.099 0,490 -0.160

0.750 -0,053 0,400 -0.039 0.400 -0.051 0.580 -0.226

0.850 0.062 0,490 -0.119 0.490 -0.011 0.650 -0.087

0.900 0.130 0,580 -0.118 0.580 -0.115 0.750 0.138

0.960 0,079 0.640 0,033 0.650 -0.033 0.830 0.314

0.750 0.161 0.750 0.110 0,900 0,349

0.870 0.204 0.890 0.238 0.960 0,255

0.930 0.124 0.930 0.185

0,960 0,057 0.960 - 1.753"*

CN = 0.400 0,583 0.694 0.765

371
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-51-4-500, MINF = 0.853, Camber = 10/2, ALPT = 9.10, BETA = -0.62, QINF = 296.4,

RNPU = 2.3E+06, CNWP = 0.4796

13 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.273 0.000 0.600 0.000 3.766** 0.010 -0.017

0.060 -0.154 0.020 -0.019 0.020 0.161 0.020 -0.125

0.110 -0.260 0.040 0.020 0.060 -3.788** 0.060 -0.689

0.200 - 1. t08 0.060 -0.374 0.090 -0.572 0.110 -0.992

0.230 - 1.071 0.090 -0.490 0.110 -0.821 0.140 - 1.269

0.400 -0.867 0.130 -0.709 0.130 -0.946 0.190 - 1.961 **

0.490 -0.319 0.150 - 1.004 0.150 - 1.148 0.250 - 1.276

0.590 -0.245 0.200 - 1.041 0.210 - 1.127 0.400 -0.934

0.630 -0.222 0.250 - 1.163 0.250 - 1.074 0.490 -0.766

0.700 -0.183 0.260 - 1.049 0.340 - 1.157 0.580 -0.732

0.750 -0.296 0.280 - 1.129 0.370 - 1.161 0.650 -0.700

0.810 -0.295 0.290 -1.129 0.400 -1.116 0.700 -0.679

0.840 -0.230 0.310 - 1.099 0.410 - 1.655" * 0,750 -0.415

0.900 -0.211 0.320 - 1.078 0.430 - 1.180 0.800 -0.289

0.960 -0.121 0.340 - 1.079 0.440 - 1.122 0.830 -0.193

0.350 -0.555** 0.460 - 1.164 0.900 -0.106

0.370 - 1.029 0.490 - 1.032 0.960 -0.030

0.380 -1.155 0.500 -0.897

0.400 - 1.064 0.520 -0.690

0.410 -0.974 0.540 -0.649

0.430 -0.719 0.550 -0.589

0.440 -0.561 0.580 -0.563

0.460 -0.675 0.600 -0.558

0.470 -0.533 0.610 -0.544

0.490 -0.532 0.650 2.304**

0.500 -0.528 0.700 -0.538

0.520 -0.530 0.750 -0.620

0.530 -0.484 0.820 -0.418

0.550 -0.521 0.890 -0.280

0.560 -0.490 0.900 -0.289

0.580 -0,478 0,960 -0.179

0.590 -0.507

0.600 -0.517

0.640 -0.373

0,700 -0.385

0.750 -0.016"*

0.820 -0.216

0.870 -0.277

0.930 -0.215

0.960 -0.207

Lower Surface

0.020 -0.732 0.020 -0.146 0.020 -0.099 0.020 0.170

0.110 -0.04 1 0.060 0.081 0.060 0.229 0.060 2.012 **

0.230 0.003 0,090 0.037 0.090 1.528"* 0.110 0.180

0.400 -0.037 0.120 0.192 0.120 -0.190 0.250 0.025

0.490 -0.047 0.200 0.000 0.200 -0.101 0.400 -0.042

0.630 2.312"* 0.260 0.008 0.250 0.073 0.490 -0.165

0.750 -0.024 0.400 -0.04 1 0.400 -0.049 0.580 -0.224

0.850 0.075 0,490 -0.110 0.490 -0.014 0.650 -0.085

0.900 0.148 0.580 -0.119 0.580 -0.121 0.750 0.123

0.960 0.098 0.640 0.050 0.650 -0.039 0.830 0.322

0.750 0.187 0.750 0.095 0.900 0.346

0.870 0.193 0.890 0.253 0.960 0.251

0.930 0.125 0.930 0.200

0.960 0.051 0.960 -1.907"*

CN -- 0.440 0.607 0.727 0.757

372
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-51-10-000, MINF = 0.847, Camber = 10/2, ALPT = 11.03. BETA = -0.41, QINF = 292.0,

RNPU = 2.3E+06, CNWP = 0.2847

= 0,93 0.76 0.59 0,40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.095 0.000 0.789 0.000 3.821 * * 0.010 -0.519

0.060 -0.287 0.020 -0.240 0,020 -0.044 0.020 -0.274

O. 110 -0.724 0.040 -0.150 0.060 -3.847 * * 0.060 -0.851

0.200 - 1.072 0.060 -0.525 0.090 -0.759 O. 110 - 1.135

0.230 -0.827 0.090 -0.712 O. 110 -0.995 O. 140 - 1.385

0.400 -0.535 O. 130 -0.867 O. 130 - 1.099 O. 190 - 1.993"*

0,490 -0,379 0.150 -1.114 0.150 -1.298 0.250 - 1.064

0.590 -0.346 0.200 - 1.125 0.210 - 1.275 0.400 -0.892

0.630 -0.278 0.250 -0.829 0,250 -0.787 0.490 -0.774

0.700 -0.227 0.260 -0.668 0,340 -0.744 0.580 -0.708

0.750 -0.279 0,280 -0.730 0.370 -0.738 0,650 -0.571

0.810 -0.264 0.290 -0.712 0.400 -0.717 0.700 -0.559

0,840 -0.228 0.310 -0.692 0.410 - 1.681 ** 0,750 -0,468

0.900 -0.227 0.320 -0.673 0.430 -0.675 0.800 -0.452

0,960 -0.205 0,340 -0,634 0.440 -0.628 0.830 -0,435

0.350 -0.391 ** 0.460 -0,665 0.900 -0.307

0.370 -0.592 0.490 -0.554 0.960 -0.233

0,380 -0.695 0.500 -0,656

0.400 -0.649 0,520 -0.601

0.410 -0.654 0,540 -0.610

0,430 -0,621 0.550 -0,559

0,440 -0.486 0,580 -0,540

0,460 -0.660 0.600 -0,544

0.470 -0.548 0.610 -0.518

0.490 -0,555 0.650 2.337 **

0.500 -0.544 0.700 -0.472

0,520 -0.588 0,750 -0.631

0,530 -0.507 0,820 -0,389

0.550 -0,599 0.890 -0,340

0.560 -0.541 0.900 -0.324

0,580 -0.540 0,960 -0.266

0,590 -0,560

0,600 -0.577

0.640 -0,433

0,700 -0.445

0.750 -0.025"*

0.820 -0,291

0.870 -0.283

0.930 -0,322

0,960 -0.295

Lower Surface

0,020 -0.238 0.020 -0.139 0.020 0.122 0.020 0.380

0.110 0.019 0.060 0.230 0,060 0,355 0,060 2.040"*

0.230 0,044 0,090 0.131 0.090 1.549"* 0,110 0.279

0.400 -0,009 0.120 0.186 0.120 -0,070 0,250 0.107

0,490 -0,034 0.200 0,040 0.200 -0.026 0,400 0,020

0,630 2.345"* 0.260 0.066 0.250 0.156 0,490 -0.116

0,750 -0.070 0,400 -0.009 0,400 -0.001 0.580 -0.183

0,850 0.022 0,490 -0.082 0.490 -0.019 0.650 -0.080

0.900 0.106 0.580 -0. 123 0.580 -0.117 0.750 0.104

0.960 0.028 0.640 0.048 0,650 -0.064 0,830 0,297

0.750 0.169 0.750 0.091 0.900 0.315

0,870 0.205 0.890 0,203 0.960 0.175

0.930 0,099 0,930 0.141

0.960 0.024 0.960 -1.938"*

CN = 0,434 0,614 0.673 0.811

373
Table F-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 11-51-17-500, MINF = 0.844, Camber = 10/2, ALPT = 12.22, BETA = 0.17, QINF = 301.6,

RNPU = 2.4E+06, CNWP = 0.2170

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.016 0.000 0.872 0.000 3.621 ** 0.010 -0.708

0.060 -0.394 0.020 -0.406 0.020 -0.229 0.020 -0.688

0.110 -0.731 0.040 -0.254 0.060 -3.803 ** 0.060 -0.917

0.200 -0.652 0.060 -0.651 0.090 -0.853 0.110 - 1.200

0.230 -0.382 0.090 -0.831 0.110 -1.101 0.140 -1.221

0.400 -0.433 0.130 -0.973 0.130 - 1.185 0.190 -2.007 **

0.490 -0.393 0.150 - 1.131 0.150 -0.977 0.250 - 1.005

0.590 -0.404 0.200 -0.710 0.210 -0.855 0.400 -0.915

0.630 -0.350 0.250 -0.718 0.250 -0.716 0.490 -0.800

0.700 -0.295 0.260 -0.590 0.340 -0.709 0.580 -0.742

0.750 -0.333 0.280 -0.641 0.370 -0.695 0.650 -0.668

0.810 -0.352 0.290 -0.624 0.400 -0.691 0.700 -0.668

0.840 -0.306 0.310 -0.610 0.410 - 1.706"* 0.750 -0.573

0.900 -0.286 0.320 -0.598 0.430 -0.687 0.800 -0.573

0.960 -0.272 0.340 -0.578 0.440 -0.637 0.830 -0.534

0.350 -0.351 ** 0.460 -0.650 0.900 -0.445

0.370 -0.519 0.490 -0.555 0.960 -0.390

0.380 -0.622 0.500 -0.639

0.400 -0.506 0.520 -0.586

0.410 -0.611 0.540 -0.595

0.430 -0.559 0.550 -0.546

0.440 -0.469 0.580 -0.544

0.460 -0.619 0.600 -0.540

0.470 -0.515 0.610 -0.541

0.490 -0.518 0.650 2.185**

0.500 -0.520 0.700 -0.574

0.520 -0.535 0.750 -0.637

0.530 -0.488 0.820 -0.515

0.550 -0.539 0.890 -0.437

0.560 -0.491 0.900 -0.418

0.580 -0.487 0.960 -0.356

0.590 -0.520

0.600 -0.524

0.640 -0.414

0.700 -0.439

0.750 -0.032**

0,820 -0.308

0.870 -0.310

0.930 -0,357

0,960 -0.341

Lower Surface

0.020 -0.098 0.020 -0.113 0.020 0.330 0.020 0.528

0.110 0.074 0.060 0.331 0.060 0.431 0.060 1.897**

0.230 0.065 0.090 0.231 0.090 1.422** 0.110 0.367

0.400 0.021 0.120 0.300 0.120 -0.016 0.250 0.178

0.490 -0.015 0.200 0.060 0.200 -0.043 0.400 0.073

0.630 2.192"* 0.260 0.124 0.250 0.205 0.490 -0.057

0.750 -0.037 0.400 0.044 0.400 0.025 0.580 -0.166

0.850 0.018 0.490 -0.068 0.490 -0.037 0.650 -0.082

0.900 0.082 0.580 -0.101 0.580 -0.095 0.750 0.130

0.960 -0.015 0.640 0.043 0.650 -0.051 0.830 0.286

0.750 0.156 0.750 0.073 0.900 0.307

0.870 0.163 0.890 0.193 0.960 0.162

0.930 0.077 0.930 0.125

0.960 -0.018 0.960 - 1.954 **

CN = 0.411 0.610 0.680 0.895

374
Table F-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-50-51-000, MINF = 0,853, Camber = 10/2, ALl:q" = 6.04, BETA = -0,27, QINF = 303.7,

RNPU = 2.4E÷06, CNWP = 0,3840

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.450 0.000 0.319 0.000 0,258"* 0.010 O. 185

0.060 -0.007 0,020 0.275 0.020 0.436 0.020 0.058

0.110 -0.350 0.040 0.296 0.060 0,389** 0.060 -0.533

0.200 -1.049 0.060 -0.156 0.090 -0.357 0.110 -0.819

0,230 -0,940 0.090 -0,339 0. 110 -0,610 0,140 - 1.138

0.400 -0,740 0,130 -0.594 0,130 - 1.963"* 0.190 - 1.963"*

0.490 -0.135 0,150 -0.869 0,150 - 1.026 0.250 - 1.096

0.590 -0.157 0.200 -0,954 0.210 - 1,000 0.400 -0.807

0.630 -0.191 0.250 -1.015 0.250 -0.989 0.490 -0.539

0.700 -0.154 0.260 -0.948 0.340 - 1.001 0,580 -0.503

0.750 -0.237 0.280 -0.986 0.370 -0,975 0.650 -0.537

0,8 L0 -0.208 0.290 -0,978 0.400 -0,970 0.700 -0.514

0,840 -0, 215 0.310 -0.933 0.410 -2.947 * * 0.750 -0,561

0,900 -0,149 0.320 -0.939 0.430 -0,993 0.800 -0.315

0.960 -0.046 0,340 -0.931 0.440 -0.958 0.830 -0.248

0,350 -0.473** 0.460 -0.977 0.900 -0.109

0.370 -0,912 0.490 -0.900 0.960 0.030

0.380 -0,989 0.500 - 1.002

0.400 -0.892 0,520 -0.962

0.410 -0.962 0,540 -0.954

0.430 -0.912 0.550 -0.689

0.440 -0853 0,580 -0.485

0.460 -0.981 0,600 -0.384

0.470 -0,929 0.610 -0.310

0.490 -0.918 0.650 -0.522

0.500 -0.923 0,700 -0.219

0.520 -0905 0.750 -0.319

0.530 -0.893 0.820 -0.243

0.550 -0.720 0,890 -0.076

0.560 -0.434 0.900 -0,047

0.580 -0.340 0,960 0.084

0.590 -0.307

0.600 -0.263

0.640 -0.136

0.700 -0.153

0.750 -0.021 **

0.820 -0190

0,870 -0.182

0.930 -0.073

0.960 -0,009

Lower Surface

0.020 -0.666 0.020 -0.828 0.020 -0.870 0.020 -0.400

0.110 -0.457 0.060 -0.356 0.060 -0.118 0.060 -0.030

0.230 -0.062 0.090 -0,182 0.090 -0,051 0. I 10 -0.109

0.400 -0,019 0.120 -0.066 0.120 -0.309 0.250 -0.130

0.490 -0.022 0,200 -0.062 0.200 -0.117 0,400 -0.179

0.630 4,284** 0,260 -0.083 0.250 -0.064 0.490 -0,262

0.750 0.017 0.400 -0.086 0.400 -0.141 0.580 -0,293

0.850 0,075 0.490 -0.116 0.490 -0,044 0.650 -0,139

0.900 0,153 0.580 -0,106 0.580 -0.166 0.750 0,125

0.960 0.123 0.640 0.055 0,650 -0.029 0.830 0.276

0.750 0,169 0.750 -0.036 0.900 0.326

0,870 0.207 0,890 0.284 0.960 0.261

0.930 0.210 0.930 0,256

0.960 0.178 0,960 0,438

CN = 0.311 0.468 0.522 0.539

375
Table F-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-52-32-500, MINF = 0.851, Camber = 5/10, ALPT = 4.00, BETA = -0.18, QINF = 301.0,

RNPU = 2.4E+06, CNWP = 0.2904

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.309 0.000 0.587 0.000 0.219"* 0.010 -0.156

0.060 -0.041 0.020 0.092 0,020 0,191 0.020 -0.127

0.110 -0,308 0,040 0.163 0.060 0.344"* 0.060 -0.495

0.200 -0.747 0.060 -0,213 0.090 -0.328 0.110 -0.629

0.230 -0.394 0.090 -0.303 0.110 -0.531 0,140 -0.896

0.400 -0.232 0.130 -0.467 0.130 - 1.974** 0.190 - 1.974"*

0.490 -0.240 0.150 -0.682 0.150 -0.796 0.250 -0.663

0.590 -0.298 0.200 -0.698 0.210 -0.775 0.400 -0.389

0.630 -0.328 0.250 -0.775 0.250 -0.753 0.490 -0.354

0.700 -0.409 0.260 -0.699 0.340 -0.388 0.580 -0.372

0.750 -0.624 0.280 -0.722 0.370 -0.322 0.650 -0.425

0.810 -0.606 0.290 -0.722 0.400 -0.310 0.700 -0.405

0.840 -0,625 0.310 -0.678 0.410 -2.967"* 0.750 -0.523

0.900 -0.294 0.320 -0,656 0.430 -0.323 0.800 - 1.104

0,960 -0.293 0,340 -0.300 0,440 -0.298 0.830 -0.591

0.350 -0.191 ** 0.460 -0.319 0.900 -0,411

0,370 -0.217 0,490 -0.256 0.960 -0.424

0.380 -0.255 0.500 -0.334

0.400 -0.201 0.520 -0.311

0,410 -0.274 0,540 -0.317

0,430 -0.242 0.550 -0.307

0,440 -0,210 0.580 -0.311

0.460 -0,305 0.600 -0.3 ] 8

0.470 -0.283 0.610 -0.332

0.490 -0.291 0.650 -0.806

0.500 -0.308 0.700 -0.521

0.520 -0.312 0.750 -0,616

0,530 -0,308 0.820 -0.750

0.550 -0,388 0,890 -0.415

0.560 -0.330 0.900 -0.485

0.580 -0.315 0.960 -0.402

0.590 -0.368

0.600 -0.371

0,640 -0,542

0.700 -0.524

0,750 -0.014"*

0.820 -0.560

0.870 -0,347

0.930 -0.324

0.960 -0.327

Lower Surface

0.020 - 1.045 0.020 - 1.170 0.020 - 1.027 0.020 -0,197

0.110 -0.183 0.060 -0.211 0,060 -0.136 0,060 -0.009

0,230 °0.037 0.090 -0.209 0.090 -0.160 0.110 -0.190

0.400 -0.002 0.120 -0,129 0.120 -0.461 0.250 -0.234

0,490 0.036 0.200 -0.048 0.200 -0.106 0.400 -0.195

0.630 4.330"* 0.260 -0.127 0.250 -0.144 0.490 -0.198

0.750 0.158 0,400 -0.046 0.400 -0.101 0.580 -0.119

0.850 0.209 0.490 -0.027 0.490 -0.030 0.650 0,081

0.900 0.292 0.580 0.037 0.580 -0.001 0.750 0.318

0.960 0.105 0.640 0.261 0.650 -0.030 0.830 0.418

0,750 0.340 0.750 -0.015 0.900 0.488

0.870 0.358 0.890 0.438 0.960 0.323

0.930 0.302 0.930 0.361

0.960 0.194 0.960 0,479

CN = 0.385 0.484 0.469 0.515

376
Table F-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-53-13-500, MINF = 0.849, Camber = 5/10, ALPT = 4.01, BETA = -0.27, QINF = 299.9,

RNPU = 2.4E+06, CNWP = 0.2939

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.302 0.000 0.581 0.000 0,213'* O.OlO -0.146

0.060 -0.042 0.020 0.054 0.020 0.192 0.020 -0.128

0.1 I 0 -0.321 0.040 0.160 0,060 0.400** 0.060 -0.497

0.200 -0.750 0.060 -0.199 0.090 -0.335 0.110 -0.631

0.230 -0.303 0.090 -0.305 0.110 -0.533 0.140 -0.900

0.400 -0.225 0.130 -0.469 0.130 - 1,981 ** 0.190 - 1.981 **

0.490 -0.222 0.150 -0.685 0.150 -0.799 0.250 -0.665

0.590 -0.284 0.200 -0.707 0.210 -0.778 0.400 -0,384

0.630 -0.333 0.250 -0.772 0.250 -0.756 0.490 -0.355

0.700 -0.410 0.260 -0.701 0.340 -0.360 0.580 -0.373

0.750 -0.689 0.280 -0.733 0370 -0.323 0,650 -0.431

0.810 -0,590 0.290 -0.716 0.400 -0.267 0.700 -0.417

0.840 -0.576 0.310 -0.613 0.410 -2.977** 0.750 -0.525

0.900 -0.290 0.320 -0.522 0.430 -0,324 0.800 - 1.077

0.960 -0.295 0.340 -0.267 0.440 -0,299 0.830 -0.602

0.350 -0.171 ** 0.460 -0.325 0.900 -0.431

0.370 -0222 0.490 -0.257 0.960 -0.426

0.380 -0.270 0,500 -0.345

0.400 -0.212 0.520 -0.312

0.410 -0.289 0.540 -0.319

0.430 -0.255 0.550 -0.321

0.440 -0.214 0.580 -0.312

0.460 -0.306 0,600 -0.319

0.470 -0.304 0.610 -0.333

0.490 -0.304 0.650 -0.813

0.500 -0.314 0.700 -0.563

0.520 -0.321 0.750 -0.622

0.530 -0,316 0.820 -0.740

0.550 -0.371 0.890 -0.436

0.560 -0.344 0.900 -0.497

0.580 -0.316 0.960 -0.421

0.590 -0.356

0.600 -0.377

0.640 -0.544

0.700 -0.529

0.750 -0.010"*

0.820 -0.558

0.870 -0.371

O.930 -0,322

0.960 -0.328

Lower Surface

0.020 - 1.041 0.020 - I. 167 0.020 - 1.031 0.020 -0.198

O. 110 -0.177 0.060 -0.216 0.060 -0.137 0.060 -0.009

0.230 -0.049 0.090 -0.210 0.090 -0.161 O. 110 -0.150

0.400 -0.005 O. 120 -0.130 O. 120 -0.454 0.250 -0.235

0.490 0.033 0,200 -0.045 0.200 -0.103 0.400 -0.196

0.630 4.345 ** 0.260 -0.127 0.250 -0.138 0.490 -0.184

0.750 O. 158 0.400 -0.043 0.400 -0.101 0.580 -0.115

0.850 0.213 0,490 -0.027 0.490 -0.030 0.650 0.089

0.900 0.290 0.580 0.037 0.580 -0.002 0.750 0.319

0.960 O. l 13 0.640 0.250 0.650 -0,030 0.830 0.419

0.750 0.325 0,750 -0.015 0.900 0.484

0.870 0.369 0.890 0.432 0.960 0.324

0.930 0.303 0.930 0.362

0.960 0.195 0.960 0.481

CN = 0.375 0.483 0.472 0.523

377
Table F-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-54-30-500, MINF = 0.851, Camber = 10/10, ALPT = 4.03, BETA = -0.01, QINF = 301.2,

RNPU = 2.4E+06, CNWP = 0.3363

q = 0.93 0.76 0.59 0.40

Upper S urface

x/c CP x/c C P x/c C P x/c C P

0.020 0.531 0.000 0.151 0.000 0.073** 0.010 0.376

0.060 0.076 0.020 0.300 0.020 0.550 0.020 0.247

0.110 -0.273 0.040 0.413 0.060 0.509** 0.060 -0.306

0.200 -0.934 0.060 -0.057 0.090 -0.244 0.110 -0.608

0.230 -0.834 0.090 -0.233 0.110 -0.520 0.140 - 1.037

0.400 -0.126 0.130 -0.486 0.130 - 1.972"* 0.190 - 1.972"*

0.490 -0.172 0.150 -0.790 0.150 -0.937 0.250 -0.773

0.590 -0.274 0.200 -0.876 0.210 -0.918 0.400 -0.388

0.630 -0.331 0.250 -0.915 0.250 -0.867 0.490 -0.353

0.700 -0.355 0.260 -0.841 0.340 -0.837 0.580 -0.370

0.750 -0.774 0.280 -0.859 0.370 -0.813 0.650 -0.418

0.810 -0.672 0.290 -0.839 0.400 -0.419 0.700 -0.404

0.840 -0.683 0.310 -0.787 0.410 -2.009"* 0.750 -0.522

0.900 -0.248 0.320 -0.807 0.430 -0.351 0.800 - 1.085

0.960 -0.250 0.340 -0.795 0.440 -0.301 0.830 -0.589

0.350 -0.423** 0.460 -0.295 0.900 -0.392

0.370 -0.762 0.490 -0.232 0.960 -0.413

0.380 -0.829 0.500 -0.305

0.400 -0.603 0.520 -0.276

0.410 -0.395 0.540 -0.282

0.430 -0.241 0.550 -0.282

0.440 -0.196 0.580 -0.292

0.460 -0.233 0.600 -0.307

0.470 -0.191 0.610 -0.290

0.490 -0.202 0.650 -0.825

0.500 -0.209 0.700 -0.534

0.520 -0.218 0.750 -0.589

0.530 -0.221 0.820 -0.690

0.550 -0.260 0.890 -0.374

0.560 -0.249 0.900 -0.426

0.580 -0.262 0.960 -0.355

0.590 -0.309

0.600 -0.316

0.640 -0.516

0.700 -0.493

0.750 -0.031 **

0.820 -0.521

0.870 -0.372

0.930 -0.286

0.960 -0.289

Lower Surface

0.020 -0.774 0.020 -0.976 0.020 - 1.041 0.020 -0.892

0.110 -0.612 0.060 -0.490 0.060 -0.549 0.060 -0.004

0.230 -0.058 0.090 -0.376 0.090 -0.372 0.110 -0.304

0.400 0.066 0.120 -0.251 0.120 -0.485 0.250 -0.193

0.490 0.078 0.200 -0.065 0.200- -0.129 0.400 -0.187

0.630 1.909"* 0.260 -0.140 0.250 -0.071 0.490 -0.190

0.750 0.139 0.400 -0.019 0.400 -0.070 0.580 -0.113

0.850 0.175 0.490 0.004 0.490 -0.040 0.650 0.075

0.900 0.216 0.580 0.064 0.580 0.007 0.750 0.304

0.960 0.093 0.640 0.209 0.650 -0.057 0.830 0.427

0.750 0.244 0.750 -0.029 0.900 0.468

0.870 0.245 0.890 0.381 0.960 0.329

0.930 0.238 0.930 0.303

0.960 0.148 0.960 0.452

CN = 0.358 0.461 0.478 0.511

378
Table F-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 10-54-43-000, MINF = 0.850, Camber = 10/10, ALP'I" = 4.08, BETA = -0.44, QINF = 301.1,

RNPU = 2.4E+06. CNWP = 0.331 l

!q = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0,526 0,000 0.150 0.000 0.013"* 0.010 0.350

0.060 0.067 0.020 0.371 0.020 0.544 0.020 0.242

O, 110 -0.289 0,040 0.397 0.060 0,542"* 0.060 -0.312

0.200 -0.952 0.060 -0.063 0.090 -0.260 0.110 -0.633

0,230 -0,858 0,090 -0.256 O.110 -0.535 0.140 - 1.078

0,400 -0.131 0,130 -0.504 0.130 - 1.978"* 0.190 - 1.978"*

0,490 -0,181 0, 150 -0.803 0.150 -0.942 0.250 -0.779

0,590 -0.294 0.200 -0.877 0.210 -0.917 0.400 -0.393

0,630 -0.332 0,250 -0.918 0.250 -0.872 0.490 -0.358

0,700 -0.356 0.260 -0.838 0,340 -0,857 0,580 -0.386

0,750 -0.783 0.280 -0,864 0,370 -0.834 0,650 -0.434

0.810 -0.756 0.290 -0.847 0.400 -0,439 0.700 -0.414

0.840 -0.769 0.310 -0.806 0.410 -2.015"* 0,750 -0.534

0.900 -0.253 0.320 -0.810 0.430 -0,349 0.800 - 1.049

0,960 -0.248 0.340 -0.799 0,440 -0,291 0.830 -0,558

0.350 -0.439** 0,460 -0.306 0.900 -0,406

0.370 -0.779 0.490 -0,230 0.960 -0.404

0.380 -0.848 0.500 -0,301

0.400 -0.598 0.520 -0.281

0.410 -0.400 0.540 -0.294

0.430 -0.269 0.550 -0.293

0.440 -0.193 0.580 -0.298

0.460 -0.250 0.600 -0.298

0.470 -0.229 0.6 lO -0.309

0.490 -0.2 t5 0.650 -0.801

0.500 -0.230 0.700 -0.539

0.520 -0,231 0.750 -0.598

0.530 -0.230 0,820 -0.754

0.550 -0,283 0,890 -0.351

0.560 -0,266 0.900 -0.415

0.580 -0.259 0.960 -0,325

0.590 -0.306

0.600 -0.331

0.640 -0.510

0.700 -0.484

0.750 -0.025"*

0.820 -0.537

0.870 -0.362

0.930 -0.299

0.960 -0.301

Lower Surface

0.020 -0.780 0.020 -0,971 0.020 -0.891 0,020 -0.89 I

0.110 -0.583 0.060 -0.462 0,060 -0.542 0.060 -0.013

0.230 -0.075 0,090 -0.358 0.090 -0.354 O,110 -0.274

0.400 0.039 O.120 -0,227 O. 120 -0.465 0.250 -0.192

0.490 0.069 0,200 -0.067 0.200 -0.127 0,400 -0.184

0,630 1.904"* 0.260 -0.138 0,250 -0.068 0.490 -0,195

0,750 O.123 0.400 -0.024 0,400 -0.075 0.580 -0,118

0.850 0.166 0,490 -0.001 0.490 -0.04 1 0.650 0.085

0,900 0.231 0.580 0.059 0.580 0.024 0.750 0.304

0.960 0.096 0.640 0.200 0.650 -0.04 1 O.830 0.414

0.750 0.254 0.750 -0.019 0.900 0.481

0.870 0.272 0,890 0.383 0.960 0.324

0.930 0.237 0.930 0.320

0.960 0.157 0,960 0.443

CN = 0,367 0.472 0.491 0.520

379
Table F-2. Concluded.

Flight 215, Wing sweep = 26", Time = 10-5-45-500, MINF = 0.850, Camber = 10/15, ALPT = 4.03, BETA = -0.33, QINF = 255.6,

RNPU = 2.0E+06, CNWP = 0.2065

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.214 0.000 -0.517 0,000 -0.739"* 0.010 -0.399

0,060 -0.656 0.020 -0.410 0.020 -0.184 0.020 0.032

0.110 - 1.027 0.040 -0.336 0.060 0.017 ** 0,060 - 1.055

0.200 - 1.686 0.060 -0.842 0.090 -0.994 0.110 -0.856

0.230 -1.615 0.090 -1.004 0A 10 -1.279 0.140 -1.752

0.400 -0.867 0.130 - 1.245 0.130 - 1.484 0.190 - 1.976 **

0.490 -0.896 0.150 - 1.554 0.150 - 1.685 0.250 -0.982

0.590 -1.014 0,200 -1,620 0.210 -1.119 0.400 -1.151

0.630 - 1.045 0,250 - 1.660 0.250 - 1.613 0.490 - 1.101

0,700 - 1.119 0.260 - 1.580 0.340 - 1.599 0.580 - 1.131

0.750 - 1.279 0.280 - 1.086 0.370 - 1.603 0.650 - 1.188

0.810 - 1.242 0.290 - 1.588 0.400 - 1.395 0,700 - I. 170

0,840 -1.219 0.310 -1.553 0,410 -3.143"* 0.750 -0.758

0.900 - 1,155 0,320 - 1.553 0.430 - 1.168 0.800 - 1.40 l

0.960 - 1.180 0.340 - 1.550 0.440 - 1.092 0.830 - 1.264

0.350 - 1.149"* 0,460 - 1.080 0.900 - 1.212

0.370 -0,998 0,490 -0.992 0.960 - 1.236

0,380 - 1.599 0.500 - 1.045

0.400 - 1.649 0.520 - 1.035

0.410 - 1.544 0.540 - 1.044

0.430 - 1.193 0.550 - 1.036

0,440 - 1.04 1 0.580 - 1.043

0.460 -0,502 0.600 -0.502

0.470 -0.952 0.610 - 1.045

0.490 -0,953 0.650 - 1.647

0.500 -0.946 0.700 - 1.270

0.520 -0.939 0.750 - 1.348

0.530 -0.938 0.820 - 1.331

0,550 -0.993 0.890 -1.211

0.560 -0.968 0.900 - 1.295

0.580 -0.956 0.960 - 1.219

0.590 -0.483

0.600 -1.039

0.640 -1.217

0.700 -1.210

0.750 -0,738**

0.820 -1,280

0.870 - 1.135

0.930 -1.121

0.960 -1.124

Lower Surface

0.020 - 1.968 0.020 - 1.483 0.020 - 1.488 0.020 - 1,087

0. l 10 -0.964 0,060 - 1.059 0.060 - 1.169 0.060 -0.728

0,230 -0,783 0.090 - 1.032 0,090 -0.971 0.110 -0,440

0.400 -0.671 0.120 -0.951 0.120 - 1.170 0.250 -0,885

0.490 -0,609 0.200 -0,779 0.200 -0.839 0.400 -0.321

0.630 3,698** 0,260 -0,825 0.250 -0.209 0.490 -0,820

0.750 -0.537 0.400 -0.688 0.400 -0.732 0.580 -0.711

0.850 -0.513 0.490 -0.651 0.490 -0.753 0.650 -0.491

0,900 -0,440 0.580 -0,580 0.580 -0,591 0.750 -0.304

0.960 -0.638 0.640 -0.437 0.650 -0.769 0,830 -0.216

0.750 -0,394 0.750 -0.735 0,900 -0.150

0.870 -0.328 0.890 -0.253 0.960 -0.310

0.930 -0.387 0.930 -0,327

0.960 -0,506 0.960 -0.172

CN = 0.449 0.554 0.592 0.596

380
APPENDIX G

Wing Pressure Coefficients for Nominal Dynamic Pressure

of 300 lb/ft 2 and Mach Number of 0.90.

Leading-edge wing sweep is 26 °. Table G-1 contains a summary of the data listing in table G-2. The asterisks

(*) in table G-2 indicate invalid values. Camber is 5LE.,TE.Refer to Nomenclature for definitions.

Table G-1. Summary of data.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

198 13-56-25-000 0.905 0/2 5.09 0.42 297.8 2.3E+06 0.2701

198 13-56-41-000 0.895 0/2 6.00 0.34 291.2 2.2E+06 0.3247

198 13-56-52-000 0.905 0/2 7.02 -0.22 298.2 2.3E+06 0.3702

198 13-57-6-000 0.899 0/2 8.02 0.55 295.7 2.2E+06 0.4302

198 13-57-20-000 0.901 0/2 8.05 0.26 301.2 2.3E+06 0.4293

198 13-57-40-500 0.901 0/2 9.05 0.42 303.2 2.3E+06 0.4417

198 13-57-45-000 0.898 0/2 9.99 0.36 301.3 2.3E+06 0.4834

226 10-9-29-000 0.900 0/2 6.02 -0.04 292.3 2.2E+06 0.3283

226 10-9-35-000 0.898 0/2 6.02 -0.41 290.1 2.2E+06 0.3213

226 10-9-58-500 0.896 0/2 11.93 -0.70 290.6 2.2E+06 0.3468

211 11-33-56-000 0.896 0/2 5.02 0.02 298.7 2.3E+06 0.3176

211 11-34-26-500 0.896 0/2 7.96 0.45 301.0 2.3E+06 0.4324

211 11-34-41-500 0.923 0/2 9.09 -0.33 339.7 2.5E+06 0.4651

211 11-34-52-500 0.900 0/2 9.87 -0.07 335.9 2.6E+06 0.4729

198 14-1-12-000 0.901 5/2 8.27 0.52 296.5 2.2E+06 0.4358

198 14-1-22-500 0.905 5/2 8.99 0.55 298.5 2.3E+06 0.4474

198 14-1-33-000 0.900 5/2 10.15 0.39 296. i 2.2E+06 0.4739

226 10-7-8-500 0.904 5/2 6.15 -0.38 297.9 2.3E+06 0.3388

226 10-7-21-500 0.902 5/2 7.05 -0.44 297.5 2.3E+06 0.3831

226 10-7-24-000 0.901 5/2 7.03 -0.85 296.4 2.2E+06 0.3873

226 10-7-30-500 0.904 5/2 7.99 -0.67 298.4 2.3E+06 0.4302

226 10-7-40-000 0.903 5/2 12.02 -0.70 304.2 2.3E+06 0.3996

226 10-7-43-000 0.898 5/2 12.15 -0.10 305.7 2.3E+06 0.3509

200 8-21-10-000 0.898 5/6 5.01 0.45 294.2 2.2E+06 0.3343

200 8-21-25-000 0.907 5/6 6.11 0.14 298.6 2.3E+06 0.3882

200 8-21-28-500 0.908 5/6 6.99 0.08 299.1 2.3E+06 0.4526

200 8-21-32-500 0.903 5/6 8.15 0.17 296.9 2.2E+06 0.5111

200 8-21-41-000 0.889 5/6 9.11 0.25 289.3 2.2E+06 0.5676

204 9-33-24-000 0.892 5/6 8.25 -0.36 269.2 2.1E+06 0.5367

204 9-35-23-500 0.901 5/6 9.27 -0.21 275.9 2.1E+06 0.5518

381
TableG-1.Continued.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

204 9-35-34-500 0.894 5/6 12.19 0.51 292.8 2.2E+06 0.4976

198 14-4-42-500 0.898 10/2 5.99 0.05 292.9 2.2E+06 0.3341

198 14-4-46-000 0.898 10/2 6.04 -0.16 293.1 2.2E+06 0.3421

198 14-5-4-500 0.903 10/2 6.92 0.23 294.5 2.2E+06 0.3829

198 14-5-13-500 0.902 10/2 7.95 0.57 294.6 2.2E+06 0.4405

198 14-5-20-500 0.898 10/2 7.99 0.52 293.8 2.2E+06 0.4551

198 14-5-35-500 0.900 10/2 9.05 0.76 297.3 2.3E+06 0.4444

198 14-5-41-000 0.901 10/2 10.08 0.21 301.9 2.3E+06 0.4682

198 14-5-53-500 0.896 10/2 11.04 0.26 307.8 2.3E+06 0.3301

211 11-28-12-500 0.899 10/2 6.00 0.05 300.1 2.3E+06 0.3627

211 11-29-4-500 0.903 10/2 8.06 -0.41 297.1 2.3E+06 0.4635

211 11-29-11-000 0.907 10/2 8.96 0.37 301.9 2.3E+06 0.4647

226 9-38-4-500 0.906 10/2 5.96 0.19 295.9 2.2E+06 0.3462

226 9-38-25-500 0.907 10/2 7.09 0.25 295.8 2.2E+06 0.3933

226 9-38-41-500 0.894 10/2 12.06 0.19 297.7 2.3E+06 0.2948

211 11-25-20-500 0.898 5/10 4.04 0.14 299.5 2.3E+06 0.3072

211 11-25-28-000 0.900 5/11 5.00 -0.36 300.8 2.3E+06 0.3527

211 11-25-34-500 0.897 5/10 6.01 0.19 298.2 2.3E+06 0.4057

211 11-25-39-500 0.898 5/10 7.09 -0.21 299.0 2.3E+06 0.4689

211 11-25-44-500 0.894 5/10 8.16 -0.01 297.7 2.3E+06 0.5649

211 11-26-1-500 0.889 5/11 10.22 0.54 311.0 2.4E+06 0.5362

211 11-26-8-000 0.895 5/10 9.92 0.37 332.3 2.5E+06 0.5767

226 10-11-10-000 0.906 5/10 5.05 -0.24 303.6 2.3E+06 0.3583

226 10-11-33-500 0.897 5/10 7.08 -0.27 295.4 2.2E+06 0.4828

201 9-30-23-000 0.893 5/10 4.09 0.57 291.1 2.2E+06 0.4156

201 9-30-39-500 0.899 5/10 6.15 0.14 290.3 2.2E+06 0.5217

201 9-30-47-000 0.888 5/10 8.98 0.31 285.9 2.2E+06 0.6378

201 8-40-10-000 0.902 10/10 4.04 0.45 387.2 2.9E+06 0.3596

226 10-2-12-500 0.899 10/10 5.09 0.02 299.1 2.3E+06 0.3417

226 10-2-36-500 0.899 10/10 5.99 -0.21 301.3 2.3E+06 0.4245

226 10-2-57-500 0.902 10/10 7.98 -0.15 308.0 2.3E+06 0.5400

226 10-3-6-500 0.899 10/10 10.23 -0.15 316.8 2.4E+06 0.5804

215 10-6-14-500 0.899 10/15 3.98 -0.24 301.8 2.3E+06 0.2946

215 10-7-7-500 0.898 10/15 4.05 -0.07 298.5 2.3E+06 0.3422

215 10-7-21-000 0.904 10/15 4.07 0.02 302.5 2.3E+06 0.2596

198 14-8-15-000 0.905 0/11 4.07 -0.03 295.2 2.2E+06 0.3235

198 14-8-25-500 0.909 0/10 5.16 0.15 296.5 2.2E+06 0.3633

382
TableG-1.Concluded.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

198 14-8-31-000 0.909 0/10 6.15 0.47 296.0 2.2E+06 0.4054

198 14-8-42-500 0.889 0/10 7.06 0.47 283.6 2.2E+06 0.5175

198 14-9-15-000 0.891 0/10 7.95 0.26 293.2 2.2E+06 0.5712

198 14-9-25-000 0.892 0/10 9.21 0.55 303.2 2.3E+06 0.5879

198 14-9-29-000 0.887 0/10 10.01 -0.06 304.7 2.3E+06 0.6142

383
Table G-2. Listing of data.

Flight 198, Wing sweep = 26 °, Time = 13-56-25-000, MINF = 0.905, Camber = 0/2, ALPT = 5.09, BETA = 0.42, QINF = 297.8,

RNPU = 2.3E+06, CNWP = 0.2701

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0.129 0.000 0.915 0.000 -5.473"* 0.010 -0.683"*

0.060 -0.314 0.020 -0.503 * * 0.020 -0.310* * 0.020 -0.717"*

0.110 -0.318 0.040 -0.245 0.060 - 1.195" * 0.060 -0.648

0.200 -0.407 0.060 -0.473 0.090 -0.569 0.110 -0.660

0.230 -0.357 0.090 -0.459 0.I 10 -0.618 0.140 1.864"*

0.400 -0.471 0.130 -0.470 0.130 -0.540 0.190 -5.339"*

0.490 -0.404 0.150 -0.484 0.150 -0.527 0.250 -0.722

0.590 -0.322 0.200 -0.409 0.210 -0.601 0.400 -0.571

0.630 -0.167 0.250 -0.577 0.250 -0.584 0.490 -0.463

0.700 -0.117 0.260 -0.507 0.340 -0.668 0.580 -0.421

0.750 -0.169 0.280 -0.571 0.370 -0.660 0.650 -0.440

0.810 -0.202 0.290 -0.573 0.400 -0.661 0.700 -0.425

0.840 -0.154 0.310 -0.523 0.410 -0.616 0.750 -0.489

0.900 -0.046 0.320 -0.512 0.430 -0.650 0.800 -0.671

0.960 0.035 0.340 -0.546 0.440 -0.642 0.830 -0.640

0.350 -0.355"* 0.460 -0.663 0.900 -0.061

0.370 -0.543 0.490 -0.564 0.960 0.005

0.380 -0.565 0.500 -0.579

0.400 -0.474 0.520 -0.537

0.410 -0.576 0.540 -0.558

0.430 -0.568 0.550 -0.538

0.440 -0.512 0.580 -0.532

0.460 -0.660 0.600 -0.514

0.470 -0.587 0.610 -0.402

0.490 -0.581 0.650 -2.595"*

0.500 -0.584 0.700 -0.504

0.520 -0.580 0.750 -0.548

0.530 -0.565 0.820 -0.395

0.550 -0.577 0.890 -0.009

0.560 -0.588 0.900 0.019

0.580 -0.569 0.960 0.064

0.590 -0.607

0.600 -0.654

0.640 -2.432**

0.700 -0.559

0.750 -0.096

0.820 -2.607**

0.870 -0.075

0.930 0.012

0.960 0.074

Lower Surface

0.020 -0.467 0.020 -0.266 0.020 -0.071 0.020 0.347

0.110 -0.459 0.060 -0.060 0.060 0.058 0.060 3.415" *

0.230 -0.434 0.090 -0.161 0.090 -0.061 0.110 -0.088

0.400 -0.091 0.120 -0.259 0.120 -0.447 0.250 -0.221

0.490 -0.127 0.200 -0.229 0.200 -0.291 0.400 -0.288

0.630 3.459"* 0.260 -0.343 0.250 -0.327 0.490 -0.415

0.750 0.053 0.400 -2.625** 0.400 -0.328 0.580 -0.534

0.850 0.167 0.490 -0.440 0.490 -0.030 0.650 -0.238

0.900 0.220 0.580 -0.048 0.580 -0.516 0.750 0.028

0.960 0.196 0.640 0.284 0.650 0.049 0,830 0.169

0.750 0.186 0.750 -0.009 0.900 0.311

0.870 0.262 0.890 ******** 0.960 0.271

0.930 0.266 0.930 0.287

0.960 0.200 0.960 -2.624**

CN = 0.153 0.302 0.339 0.349

384
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-56-41-000, MINF = 0895, Camber = 0/2, ALPT = 6.00, BETA = 0.34, QINF = 291.2,

RNPU = 2.2E+06, CNWP = 0.3247

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.294 0.000 0.903 0.000 -5.595 * * 0.010 -0.741 * *

0.060 -0.396 0.020 -0.611 ** 0.020 -0.530** 0.020 -0.830**

O. 110 -0.441 0.040 -0,484 0,060 -1,287"* 0.060 -0,836

0.200 -0.506 0.060 -0.578 0.090 -0.645 O. 110 -0,765

0.230 -0.422 0.090 -0.572 0.110 -0.753 0.140 1.919"*

0.400 -0.504 0.130 -0.610 0.130 -0.651 0.190 -5.458 * *

0.490 -0.468 0.150 -0.592 0.150 -0.632 0.250 -0.817

0.590 -0.293 0.200 -0.519 0.210 -0.711 0.400 -0.612

0.630 -0.159 0.250 -0.654 0.250 -0.672 0.490 -0.560

0.700 -0.126 0.260 -0.580 0.340 -0.746 0.580 -0.479

0.750 -0.176 0.280 -0.666 0,370 -0,732 0.650 -0.498

0.810 -0.213 0.290 -0.696 0,400 -0.787 0.700 -0.499

0.840 -0.164 0.310 -0.640 0.410 -0.709 0.750 -0.560

0.900 -0.074 0.320 -0.605 0,430 -0.743 0.800 -0.736

0.960 0.000 0.340 -0.650 0.440 -0.730 0.830 -0.702

0.350 -0.362"* 0.460 -0.753 0.900 -0.062

0.370 -0.644 0.490 -0.675 0.960 -0.007

0.380 -0.660 0.500 -0.779

0.400 -0.569 0.520 -0.744

0.410 -0.688 0.540 -0.741

0.430 -0.678 0.550 -0.649

0.440 -0.609 0.580 -0,597

0.460 -0.761 0,600 -0.575

0.470 -0.679 0.610 -0.510

0.490 -0.646 0.650 -2.652 * *

0.500 -0.668 0.700 -0.581

0.520 -0.655 0.750 -0.622

0.530 -0.648 0.820 -0.194

0.550 -0,672 0.890 -0.012

0.560 -0.649 0.900 0.010

0.580 -0.635 0.960 0.043

0.590 -0.663

0.600 -0.713

0.640 -2.486**

0.700 -0.563

0,750 -0.063

0.820 -2.665**

0.870 -0.072

0.930 0.006

0,960 0.062

Lower Surface

0.020 -0.276 0.020 °0.079 0.020 0.042 0.020 0.450

0.110 -0.407 0.060 0.001 0.060 0.142 0.060 3.493"*

0.230 -0.072 0.090 -0.082 0.090 0.001 0.110 -0.047

0.400 -0.115 0.120 -0.173 0.120 -0.403 0,250 -0.218

0.490 -0.107 0.200 -0.110 0.200 -0.226 0.400 -0.24 I

0.630 3.537** 0.260 -0,320 0.250 -0.243 0.490 -0.385

0.750 0.044 0.400 -2.683** 0.400 -0.271 0.580 -0.503

0.850 0.145 0.490 -0.180 0.490 -0.021 0.650 -0.111

0.900 0.195 0.580 -0.101 0.580 -0.212 0.750 0.140

0.960 0.171 0.640 0.281 0.650 0.033 0,830 0.286

0.750 0.182 0.750 -0.012 0,900 0.363

0.870 0.241 0.890 ******** 0.960 0.272

0.930 0.273 0.930 0.302

0.960 0.190 0.960 -2.681 * *

CN = 0.244 0.435 0.456 0.462

385
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-56-52-000, MINF = 0.905, Camber = 0/2, ALPT = 7.02, BETA = -0.22, QINF = 298.2,

RNPU = 2.3E+06, CNWP = 0.3702

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.470 0.000 0.889 0.000 -5,466** 0.010 -0.868**

0.060 -0.571 0.020 -0.748** 0.020 -0.628** 0.020 -0.828**

0.110 -0.494 0.040 -0.543 0.060 - 1.364** 0.060 -0.918

0.200 -0.631 0.060 -0.659 0.090 -0.737 0.110 -0.814

0.230 -0.533 0.090 -0.641 0.110 -0.807 0.140 1.844**

0.400 -0.555 0.130 -0,672 0.130 -0.711 0.190 -5.333**

0.490 -0.530 0.150 -0.678 0.150 -0.694 0.250 -0.851

0.590 -0.517 0.200 -0.579 0.210 -0.759 0.400 -0.650

0.630 -0.470 0,250 -0.722 0.250 -0.747 0,490 -0.640

0.700 -0.450 0.260 -0,653 0.340 -0.808 0.580 -0.532

0.750 -0.104 0,280 -0.721 0.370 -0,794 0.650 -0.527

0.810 -0.142 0,290 -0,742 0.400 -0.852 0.700 -0.526

0.840 -0.102 0.310 -0.684 0.410 -0.765 0.750 -0.601

0.900 -0.065 0.320 -0.667 0.430 -0.820 0.800 -0.765

0.960 -0.003 0.340 -0.716 0.440 -0.782 0.830 -0,740

0.350 -0.365"* 0.460 -0.792 0.900 -0.161

0.370 -0.701 0.490 -0.735 0.960 -0.128

0.380 -0.715 0.500 -0.836

0.400 -0.643 0.520 -0.813

0.410 -0.741 0.540 -0.81 I

0.430 -0.727 0.550 -0,790

0.440 -0.654 0.580 -0.777

0,460 -0.784 0.600 -0.775

0.470 -0.752 0.610 -0.671

0.490 -0.721 0.650 -2.592"*

0.500 -0.713 0.700 -0.681

0.520 -0.733 0.750 -0.744

0.530 -0.706 0.820 -0.277

0.550 -0.736 0.890 -0.099

0.560 -0.735 0.900 -0.088

0.580 -0.710 0.960 -0.057

0.590 -0,716

0.600 -0.792

0.640 -2.430**

0.700 -0.586

0.750 -0.195

0.820 -2,605**

0.870 -0.099

0,930 -0.067

0.960 -0.049

Lower Surface

0.020 -0.203 0.020 -0.005 0.020 0.165 0,020 0.516

0.110 -0.354 0.060 0.065 0.060 0.188 0.060 3.408 **

0.230 -0.244 0.090 -0.032 0.090 0.064 0.110 -0.002

0.400 -0.129 0.120 -0.112 0.120 -0.333 0.250 -0.164

0.490 -0.144 0.200 -0.071 0.200 -0.177 0.400 -0.202

0.630 3.451 ** 0.260 -0.279 0.250 -0.181 0.490 -0.356

0.750 0.010 0.400 -2.622** 0.400 -0.242 0.580 -0.478

0.850 0.120 0.490 -0.159 0.490 -0.038 0.650 -0,329

0.900 0.186 0.580 -0.123 0,580 -0.444 0.750 0.110

0,960 0.158 0.640 0.254 0.650 0.014 0.830 0.255

0.750 0.152 0.750 -0.029 0,900 0.346

0.870 0.255 0.890 ******** 0.960 0.257

0.930 0.213 0.930 0.247

0.960 0.135 0.960 -2.621 * *

CN = 0.298 0.510 0,526 0.510

386
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-57-6-000, MINF = 0.899, Camber = 0/2, ALPT = 8,02, BETA = 0.55, QINF = 295.7,

RNPU = 2.2E+06, CNWP = 0.4302

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP xA" CP

0.020 -0.635 0.000 0.865 0.000 -5.521 ** 0.010 -0.955"*

0.060 -0.700 0.020 -0.956"* 0.020 -0.745"* 0.020 -0.978"*

0,110 -0.641 0,040 -0.638 0.060 - 1.440"* 0,060 - 1.027

0.200 -0.735 0.060 -0.767 0.090 -0,838 0.110 -0.935

0.230 -0,502 0,090 -0.777 0,110 -0.917 0.140 1,879"*

0.400 -0.653 0.130 -0,790 0.130 -0.848 0,190 -5.387"*

0.490 -0.602 0,150 -0.802 0.150 -0, 837 0.250 - 1.002

0.590 -0.587 0.200 -0.717 0.210 -0.874 0.400 -0.719

0,630 -0,537 0,250 -0,842 0.250 -0,843 0,490 -0.687

0,700 -0,485 0.260 -0,749 0.340 -0,917 0.580 -0.605

0,750 -0.110 0.280 -0.816 0.370 -0.898 0.650 -0.571

0.810 -0.167 0.290 -0.842 0.400 -0.904 0,700 -0.599

0.840 -0.119 0,310 -0.782 0,410 -0.868 0.750 -0.651

0,900 -0.109 0.320 -0.767 0.430 -0.929 0.800 -0.794

0.960 -0,041 0.340 -0.815 0,440 -0.887 0.830 -0.721

0,350 -0.388"* 0.460 -0.902 0.900 -0.193

0.370 -0.788 0,490 -0.832 0,960 -0.168

0.380 -0.810 0.500 -0.925

0.400 -0,730 0.520 -0.866

0.410 -0.846 0.540 -0.910

0.430 -0.835 0.550 -0.891

0.440 -0259 0.580 -0.866

0.460 -0,906 0.600 -0,849

0,470 -0, 871 0.610 -0.798

0.490 -0.815 0,650 -2.623**

0.500 -0,810 0.700 -0.894

0.520 -0.779 0.750 -0.752

0,530 -0,797 0.820 -0.264

0,550 -0.817 0.890 -0,163

0.560 -0.823 0.900 -0.172

0.580 -0.804 0.960 -0.152

0.590 -0.831

0.600 -0,882

0.640 -2.459**

0,700 -0.262

0.750 -0,209

0,820 -2,636**

0.870 -0.184

0.930 -0.188

0.960 -0.170

Lower Surface

0.020 -0.005 0,020 0.160 0.020 0,252 0.020 0.618

0.110 -0_215 0.060 0.163 0,060 0.276 0.060 3.429"*

0.230 -0.082 0.090 0,058 0.090 0.149 0.110 0.067

0,400 -0.131 0.120 -0.038 0.120 -0,276 0.250 -0.091

0.490 -0.161 0.200 -0,021 0.200 -0,048 0.400 -0.138

0.630 3.473** 0,260 -0.208 0.250 -0.102 0.490 -0.307

0.750 -0,022 0.400 -2.653** 0,400 -0.176 0.580 -0.404

0,850 0.085 0.490 -0,196 0.490 -0.032 0.650 -0,143

0,900 0.139 0.580 -0.147 0.580 -0,249 0.750 0.137

0.960 0.137 0,640 0.237 0,650 -0.016 0,830 0.281

0,750 0.126 0.750 -0.019 0,900 0.353

0.870 0.170 0.890 ******** 0.960 0.239

0.930 0.158 0.930 0.225

0,960 0.072 0,960 -2.652 * *

CN = 0.379 0.567 0.659 0.638

387
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-57-20-000, MINF = 0.901, Camber = 0/2, ALPT = 8.05, BETA = 0.26. QINF = 301.2,

RNPU = 2.3E+06, CNWP = 0.4293

rl = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.626 0,000 0.879 0.000 -5.445"* 0.010 -0,953**

0.060 -0.682 0.020 -0.952"* 0.020 -0.726** 0.020 -0.976**

0.110 -0.658 0.040 -0,628 0.060 - 1.428" * 0.060 - 1.013

0.200 -0,729 0.060 -0.748 0.090 -0.839 0.110 -0.922

0.230 -0.581 0.090 -0.767 0.110 -0.919 0.140 1.850**

0,400 -0.651 0.130 -0.777 0.130 -0,840 0.190 -5,313"*

0.490 -0.597 0.150 -0,795 0,150 -0.800 0,250 -0.979

0,590 -0.579 0.200 -0.710 0.210 -0.862 0,400 -0.714

0.630 -0.533 0.250 -0,822 0,250 -0.851 0.490 -0.679

0.700 -0,592 0.260 -0.744 0.340 -0.911 0.580 -0.610

0.750 -0.099 0.280 -0.828 0.370 -0.885 0.650 -0.571

0.810 -0.133 0.290 -0.831 0.400 -0.897 0.700 -0.583

0.840 -0.097 0.310 -0.772 0.410 -0.858 0.750 -0.649

0.900 -0.102 0.320 -0,761 0.430 -0.915 0.800 -0.796

0.960 -0.035 0.340 -0,824 0.440 -0.876 0.830 -0.768

0,350 -0.381 * * 0.460 -0.898 0.900 -0.194

0.370 -0.780 0.490 -0.819 0.960 -0.172

0.380 -0.804 0.500 -0.912

0.400 -0.733 0.520 -0.897

0.410 -0.835 0.540 -0.917

0.430 -0.826 0.550 -0.882

0.440 -0.752 0,580 -0.863

0,460 -0.897 0.600 -0.853

0.470 -0.837 0.610 -0,785

0.490 -0.806 0,650 -2.599 * *

0.500 -0.806 0,700 -0,934

0.520 -0.798 0.750 -0.797

0.530 -0.784 0.820 -0,267

0.550 -0.806 0.890 -0.175

0,560 -0.816 0.900 -0.190

0.580 -0.790 0.960 -0.152

0.590 -0.802

0.600 -0.875

0.640 -2.439**

0.700 -0.263

0.750 -0.178

0.820 -2.612"*

0.870 -0.204

0,930 -0.183

0.960 -0.161

Lower Surface

0.020 -0,066 0,020 0,180 0.020 0.299 0.020 0.631

0,110 -0.212 0.060 0.169 0.060 0.290 0.060 3.342"*

0.230 -0,091 0.090 0.062 0.090 0.156 0.110 0.091

0.400 -0.135 0.120 0.012 0.120 -0.249 0.250 -0.085

0,490 -0.160 0,200 -0.016 0.200 -0.055 0.400 -0.137

0.630 3.385"* 0.260 -0.206 0.250 -0.102 0.490 -0.304

0.750 -0.027 0.400 -2,629"* 0,400 -0.172 0.580 -0,406

0.850 0.081 0.490 -0,195 0.490 -0.056 0.650 -0,180

0.900 O. 153 0.580 -0.147 0.580 -0.327 0.750 O. 139

0.960 O. 135 0.640 0.238 0.650 -0,007 0.830 0,267

0.750 0. | 45 0.750 -0.018 0.900 0.360

0,870 0.191 0.890 ******** 0.960 0.243

0.930 0.164 0.930 0.226

0.960 0.064 0.960 -2.628 * *

CN = 0.386 0.568 0.659 0,634

388
Table G-2, Continued.

Flight 198, Wing sweep = 26 °, Time = 13-57-40-500, MINF = 0.901, Camber = 0/2, ALPT = 9.05, BETA = 0.42, QINF = 303.2,

RNPU = 2.3E÷06, CNWP = 0.4417

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP .r,/c CP x/c CP x/c CP

0,020 -0,699 0,000 0.842 0.000 -5.422** 0.010 -1.050**

0,060 -0,786 0,020 - 1.054"* 0.020 -0.826"* 0.020 - 1,053"*

0.110 -0,709 0_040 -0.738 0.060 -1.380"* 0,060 -1.100

0.200 -0.801 0,060 -0,849 0.090 -0.926 0.110 - 1.023

0,230 -0,632 0,090 -0.847 0.110 -0.995 0.140 1.832'*

0.400 -0.691 0.130 -0.855 0.130 -0.917 0.190 -5.291"*

0.490 -0.668 0.150 -0.859 0,150 -0.876 0,250 - 1.049

0.590 -0.641 0.200 -0.775 0.210 -0.940 0.400 -0,784

0,630 -0.585 0.250 -0.905 0.250 -0.910 0.490 -0.711

0.700 -0.638 0.260 -0.806 0.340 -0.980 0.580 -0.657

0.750 -0.128 0,280 -0,883 0,370 -0.956 0.650 -0,605

0.810 -0.172 0.290 -0.895 0.400 -0.962 0.700 °0.641

0.840 -0.103 0.310 -0,838 0.410 -0.925 0.750 -0.687

0.900 -0.152 0.320 -0.828 0.430 -0,992 0.800 -0.818

0.960 -0.076 0.340 -0.886 0.440 -0.962 0.830 -0.707

0.350 -0.388** 0.460 -0.964 0.900 -0.264

0.370 -0.845 0,490 -0.878 0.960 -0.219

0.380 -0,868 0.500 -0.982

0.400 -0.792 0.520 -0.959

0.410 -0.892 0.540 -0.965

0.430 -0.890 0.550 -0.949

0.440 -0.810 0.580 -0.960

0.460 -0.961 0.600 -0.931

0.470 -0,921 0.610 -0.869

0.490 -0.865 0.650 -2.596**

0.500 -0.874 0.700 -0.602

0.520 -0.867 0.750 -0.521

0.530 -0.853 0.820 -0.388

0.550 -0.878 0.890 -0.289

0.560 -0.766 0.900 -0.306

0.580 -0.660 0.960 -0,270

0,590 -0.429

0.600 -0.410

0.640 -2.436**

0.700 -0,286

0.750 -0.248

0,820 -2.608**

0.870 -0.259

0.930 -0.250

0.960 -0.228

Lower Surface

0.020 -0.008 0.020 0.269 0,020 0.360 0.020 0.697

0.110 -0.150 0.060 0.231 0.060 0.348 0.060 3.306"*

0.230 -0.063 0.090 0.127 0.090 0,216 0.110 0A72

0.400 -0,133 0.120 0,042 0.120 -0,204 0.250 -0.031

0.490 -0.176 0.200 0.028 0,200 0.006 0.400 -0.099

0.630 3.349** 0.260 -0,147 0.250 -0.042 0.490 -0.249

0.750 -0.060 0.400 -2.625** 0.400 -0.135 0.580 -0.378

0,850 0.036 0.490 -0.185 0.490 -0.026 0.650 -0.126

0.900 0.109 0.580 -0.152 0.580 -0.266 0.750 0.144

0.960 0.103 0.640 0.224 0.650 -0.017 0.830 0.289

0.750 0.129 0.750 -0.017 0.900 0.359

0.870 0.167 0.890 ******** 0.960 0.233

0.930 0.120 0.930 0.210

0.960 0.028 0.960 -2.624**

CN = 0.433 0.602 0,713 0.723

389
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 13-57-45-000, MINF = 0.898, Camber = 0/2, ALPT = 9.99, BETA = 0.36, QINF = 301.3,

RNPU = 2.3E+06, CNWP = 0.4834

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.811 0.000 0.775 0.000 -5.456** 0.010 - 1.077"*

0,060 -0.881 0.020 - 1.096"* 0.020 -0.914"* 0.020 - 1.132 **

0.110 -0.847 0.040 -0.837 0,060 - 1.520"* 0.060 - 1.189

0.200 -0.882 0.060 -0,945 0.090 -0.993 0.110 - 1.116

0,230 -0.653 0.090 -0.920 0.110 - 1.072 0.140 1.821 **

0.400 -0.754 0.130 -0,944 0.130 -0.994 0.190 -5,324"*

0.490 -0.689 0.150 -0.939 0.150 -0.980 0.250 - 1.111

0.590 -0.688 0.200 -0.850 0.210 - 1.001 0.400 -0.836

0.630 -0.633 0.250 -0.988 0.250 -0,979 0.490 -0,762

0.700 -0.314 0.260 -0.877 0.340 - 1.047 0.580 -0,702

0,750 -0.204 0.280 -0.941 0.370 - 1.031 0,650 -0.644

0.810 -0.247 0,290 -0.963 0.400 - 1.025 0,700 -0.707

0.840 -0.192 0.310 -0.905 0.410 - 1.000 0,750 -0.726

0.900 -0.205 0.320 -0.892 0.430 - 1.073 0,800 -0,843

0.960 -0.140 0.340 -0.946 0.440 - 1.029 0.830 -0.599

0.350 -0.415"* 0_460 - 1.038 0.900 -0.292

0,370 -0.918 0.490 -0.956 0,960 -0.228

0,380 -0.939 0.500 - 1.044

0,400 -0.860 0,520 - 1.015

0.410 -0.967 0.540 - 1.025

0.430 -0,954 0.550 - 1.003

0.440 -0.870 0.580 -0.982

0.460 -0.954 0.600 -0.996

0.470 -0,731 0.610 -0.817

0,490 -0.612 0.650 -2.611 **

0.500 -0.473 0.700 -0.476

0.520 -0.469 0.750 -0.552

0,530 -0.409 0,820 -0,468

0.550 -0.404 0.890 -0,373

0,560 -0.392 0.900 -0.384

0.580 -0.381 0,960 -0.369

0,590 -0.401

0.600 -0.397

0,640 -2.450**

0.700 -0,341

0,750 -0.302

0.820 -2.623**

0.870 -0.309

0.930 -0.308

0.960 -0.291

Lower Surface

0.020 0.109 0.020 0.349 0.020 0.426 0.020 0,766

0.110 -0,096 0.060 0.289 0.060 0.397 0,060 3,329**

0.230 -0.043 0.090 0.182 0.090 0.267 0.110 0.194

0,400 -0.118 0.120 0.088 0.120 -0.152 0.250 0.010

0.490 -0.158 0.200 0.073 0.200 0.055 0.400 -0.062

0.630 3.372** 0.260 -0.096 0.250 -0.004 0.490 -0.205

0.750 -0.070 0.400 -2.641 * * 0.400 -0.095 0.580 -0.338

0.850 0.000 0.490 -0.170 0.490 -0.024 0.650 -0.111

0.900 0.074 0.580 -0.145 0.580 -0.248 0.750 O. 146

0,960 0,060 0.640 0,227 0,650 -0.015 0.830 0.292

0.750 0.106 0.750 -0.0 l2 0.900 0.359

0.870 0.133 0.890 ******** 0,960 0,236

0.930 0,101 0.930 0,190

0.960 0.001 0.960 -2.639 * *

CN = 0.477 0.623 0.774 0,788

390
Table G-2. Continued,

Flight 226, Wing sweep = 26 °, Time = 10-9-29-000, MINF = 0.900, Camber = 0/2, ALPT = 6,02, BETA = -0.04, QINF = 292.3,

RNPU = 2.2E+06, CNWP = 0.3283

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.466 0.000 0.861 0.000 3,648"* 0.010 -0.694

0.060 -0.421 0,020 -0,636 0.020 -0.646 0.020 -0.780

0.110 -0.522 0,040 -0.551 0,060 -4.781 ** 0.060 -0.775

0.200 -0.444 0,060 -0.682 0,090 -0.677 0, 110 -0.738

0.230 -0.228 0.090 -0.602 0.110 -0,718 0.140 -0.772

0.400 -0.520 0.130 -0,619 0.130 -0.602 0.190 -1.762**

0,490 -0.470 0.150 -0,657 0.150 -0.706 0.250 -0.790

0.590 -0.487 0,200 -0.531 0.210 -0.629 0.400 -0.645

0.630 -0,254 0.250 -0.627 0.250 -0.655 0.490 -0.569

0.700 -0.091 0.260 -0,609 0.340 -0.682 0.580 -0.486

0.750 -0.190 0.280 -0.624 0,370 -0,696 0.650 -0.461

0.8 l0 -0,200 0.290 -0.633 0,400 -0.665 0.700 -0.462

0.840 -0.136 0.310 -0.676 0,410 -2.784** 0.750 -0.559

0.900 -0.096 0.320 -0.649 0.430 -0.691 0.800 -0,698

0,960 -0.011 0.340 -0.611 0,440 -0.653 0.830 -0.631

0.350 -0.433** 0.460 -0.702 0,900 -0.109

0.370 -0,634 0.490 -0.662 0.960 -0.087

0.380 -0,671 0.500 -0.750

0,400 -0.516 0.520 -0.664

0.410 -0.664 0.540 -0.684

0.430 -0,620 0,550 -0.669

0.440 -0.602 0,580 -0.586

0.460 -0.709 0.600 -0.513

0.470 -0.647 0.610 -0.509

0.490 -0.691 0.650 2,242**

0.500 -0.708 0.700 -0.654

0.520 -0.698 0.750 -0.700

0.530 -0.685 0,820 -0.276

0.550 -0.729 0.890 -0.062

0,560 -0.632 0.900 -0,032

0.580 -0.689 0.960 0.030

0.590 -0.725

0.600 -0.755

0.640 -0.734

0.700 -0.683

0.750 -0.039**

0.820 -0.071

0,870 -0.067

0.930 -0.025

0.960 0.034

Lower Surface

0.020 -0.305 0.020 -0.174 0.020 0.106 0.020 0.485

0.110 -0.403 0.060 -0,002 0.060 0.125 0.060 1.946"*

0.230 -0.267 0.090 -0.110 0.090 1.228"* 0.110 -0.007

0,400 -0.117 0.120 -0.168 0,120 -0.362 0,250 -0.213

0.490 -0.036 0,200 -0.194 0.200 -0,232 0.400 -0,244

0.630 2,007** 0.260 -0.329 0.250 -0.236 0.490 -0.392

0,750 -0.010 0.400 -0,338 0.400 -0,266 0.580 -0,455

0.850 0.141 0.490 -0,203 0.490 -0.062 0.650 -0.204

0.900 0,209 0.580 -0.182 0.580 -0,231 0.750 0.053

0.960 0.177 0.640 0,036 0,650 -0.059 0.830 0.267

0.750 0.215 0.750 0,299 0.900 0.323

0.870 0.271 0.890 0.237 0,960 0.246

0.930 0.212 0.930 0.208

0.960 0.180 0.960 -2.873**

CN = 0.225 0.438 0.468 0.474

391
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-9-35-000, MINF = 0.898, Camber = 0/2, ALPT = 6.02, BETA = -0.41, QINF = 290.1,

RNPU = 2.2E+06, CNWP = 0.3213

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.459 0.000 0.855 0.000 3,680** 0.010 -0.695

0.060 -0.478 0.020 -0.637 0.020 -0,647 0.020 -0.782

0.110 -0.569 0.040 -0.555 0.060 -4.813 ** 0.060 -0,776

0.200 -0.444 0.060 -0.652 0.090 -0.678 0.110 -0.739

0.230 -0.474 0.090 -0.611 0.110 -0.719 0.140 -0.829

0.400 -0.528 0.130 -0,619 0.130 -0.587 0.190 -1.771"*

0.490 -0.462 0,150 -0.654 0.150 -0.707 0.250 -0.792

0.590 -0.463 0.200 -0.552 0.210 -0.620 0.400 -0.645

0.630 -0.180 0.250 -0.628 0.250 -0,648 0.490 -0.540

0.700 -0.095 0.260 -0.610 0.340 -0.683 0.580 -0.486

0.750 -0.216 0.280 -0.640 0.370 -0.672 0.650 -0.461

0.810 -0.212 0.290 -0.633 0.400 -0.742 0.700 -0.456

0.840 -0.156 0.310 -0.677 0.410 -2.801"* 0,750 -0.559

0.900 -0.100 0.320 -0.650 0,430 -0.692 0.800 -0.699

0.960 0.001 0.340 -0.627 0.440 -0,654 0.830 -0.647

0.350 -0.432 * * 0.460 -0.697 0.900 -0.101

0.370 -0.627 0.490 -0.561 0.960 -0,052

0.380 -0.672 0.500 -0.742

0.400 -0.640 0.520 -0.648

0.410 -0.661 0.540 -0.657

0.430 -0.620 0,550 -0.619

0.440 -0,609 0.580 -0.586

0.460 -0.695 0.600 -0.528

0.470 -0.64 1 0.610 -0.531

0.490 -0.692 0.650 2.263"*

0.500 -0.704 0.700 -0.617

0.520 -0.699 0,750 -0,689

0.530 -0,667 0.820 -0,257

0.550 -0.731 0.890 -0.054

0.560 -0,626 0.900 -0.013

0.580 -0.683 0.960 0.038

0,590 -0.731

0.600 -0.741

0.640 -0.728

0,700 -0.681

0.750 -0.020**

0.820 -0.071

0.870 -0,086

0.930 -0.017

0.960 0.042

Lower Surface

0.020 -0.303 0.020 -0.171 0.020 0.111 0.020 0.479

0.110 -0.387 0,060 -0.025 0.060 0.137 0.060 1.964* *

0.230 -0.175 0.090 -0.112 0,090 1.241 ** 0.110 0.008

0.400 -0.094 0.120 -0.158 0.120 -0.374 0.250 -0,230

0.490 -0.070 0.200 -0.195 0.200 -0.237 0.400 -0.241

0.630 2.026** 0.260 -0.343 0.250 -0.249 0.490 -0.391

0.750 0.018 0.400 -0.297 0.400 -0.264 0.580 -0.470

0.850 0.154 0,490 -0.193 0.490 -0.055 0.650 -0.163

0,900 0.217 0.580 -0.155 0.580 -0.168 0.750 0.067

0.960 0.182 0.640 0.048 0.650 -0.055 0.830 0.282

0.750 0.221 0.750 0.267 0.900 0.324

0.870 0.278 0.890 0.235 0.960 0.252

0.930 0.203 0.930 0.221

0.960 0.185 0.960 -2.891 **

CN = 0.272 0.448 0.461 0.479

392
Table G-2 Continued,

Flight 226, Wing sweep = 26 °, Time = 10-9-58-500, MINF = 0.896, Camber = 0/2, ALPT = 11.93, BETA = -0.70, QINF = 290.6,

RNPU = 2.2E+06, CNWP = 0.3468

TI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 - 1.094 0.000 0.535 0.000 3.662"* 0.010 - 1.250

0.060 - 1.093 0.020 - 1.492 0.020 - I. 152 0.020 - 1.250

0.110 -1.277 0.040 -1.113 0.060 -4.816"* 0.060 -1.304

0.200 -0.894 0.060 - 1.158 0.090 - 1.157 O. 110 - 1.240

0.230 - 1.022 0.090 - 1,122 O. 110 - 1.168 O. 140 - 1.265

0.400 -0.895 0,130 -1.119 0.130 -1.033 0.190 -1.780"*

0.490 -0.605 0,150 -1.137 0.150 -1.188 0.250 -1.209

0.590 -0.490 0.200 - 1.047 0.210 - 1.037 0.400 -0.870

0.630 -0.438 0.250 -0.819 0.250 - 1.099 0.490 -0.739

0.700 -0.361 0.260 -0.668 0.340 -0.771 0,580 -0.697

0.750 -0.392 0,280 -0.664 0.370 -0.683 0.650 -0.629

0.810 -0,400 0.290 -0.628 0.400 -0,744 0.700 -0.605

0.840 -0.360 0.310 -0.665 0.410 -2.808** 0,750 -0.607

0.900 -0.326 0.320 -0.640 0.430 -0.655 0.800 -0.601

0.960 -0.259 0.340 -0,578 0.440 -0.601 0.830 -0.538

0.350 -0.372** 0.460 -0.624 0.900 -0.450

0.370 -0.566 0.490 -0.533 0.960 -0.382

0.380 -0.600 0.500 -0,630

0.400 -0.522 0.520 -0.573

0.410 -0.576 0.540 -0.568

0.430 -0.532 0.550 -0.601

0.440 -0.524 0.580 -0.636

0.460 -0.585 0.600 -0.533

0.470 -0.509 0.6 l0 -0.525

0.490 -0.548 0.650 2.248 * *

0.500 -0.575 0.700 -0.627

0,520 -0,526 0.750 -0.684

0.530 -0.530 0.820 -0.491

0.550 -0.613 0.890 -0.476

0.560 -0.461 0,900 -0.512

0.580 -0.513 0.960 -0.400

0.590 -0.561

0.600 -0.553

0.640 -0.433

0.700 -0,419

0.750 -0.057 **

0.820 -0.385

0.870 -0.474

0.93O -0.405

0.960 -0.388

Lower Surface

0.020 0.176 0.020 0.494 0.020 0.613 0.020 0.816

0.110 -0.006 0.060 0.367 0.060 0.481 0.060 1.950"*

0.230 -0.026 0.090 0.216 0.090 1.228"* 0.110 0.283

0.400 -0.094 O. 120 O. 185 O. 120 -0.043 0.250 0.088

0.490 -0.120 0.200 O. 106 0.200 0.080 0.400 0.007

0.630 2.012"* 0.260 -0.032 0.250 0.087 0.490 -0.140

0.750 -0.129 0.400 -0.067 0.400 -0.060 0.580 -0.254

0,850 -0.072 0,490 -0.149 0.490 -0.074 0.650 -0,097

0.900 -0.005 0.580 -0.187 0.580 -0.186 0.750 0,075

0.960 -0.037 0.640 -0.006 0.650 -0.096 0.830 0.279

0.750 0.148 0.750 0.294 0.900 0302

0.870 0.123 0.890 0.165 0.960 0.161

0.930 0.045 0.930 0.110

0.960 -0.015 0.960 -2.897 **

CN = 0.590 0.673 0.764 0.892

393
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-33-56-000, MINF = 0.896, Camber = 0/2, ALPT = 5.02, BETA = 0.02, QINF = 298.7,

RNPU = 2.3E+06, CNWP = 0.3176

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x,/c CP

0.020 -0.163 0.000 0.871 0.000 0.494"* 0.010 -0.714

0.060 -0.386 0.020 -0.521 0.020 -0.346 0.020 -0.793

0.110 -0.449 0.040 -0.362 0.060 1.251 ** 0.060 -0.709

0.200 -0.466 0.060 -0.522 0.090 -0.625 0.110 -0.735

0.230 -0.417 0.090 -0.554 0. l 10 -0.668 0.140 -0.767

0.400 -0.502 0.130 -0.546 0.130 - 1.778 ** 0.190 - 1.778 **

0.490 -0.417 0.150 -0.559 0.150 -0.617 0.250 -0.809

0.590 -0.180 0.200 -0.445 0.210 -0.643 0.400 -0.645

0.630 -0.211 0.250 -0.635 0.250 -0.649 0.490 -0.494

0.700 -0.147 0.260 -0.583 0.340 -0.721 0.580 -0.454

0.750 -0.223 0.280 -0.630 0.370 -0.729 0.650 -0.501

0.810 -0.226 0.290 -0.621 0.400 -0.711 0.700 -0.461

0.840 -0.194 0.310 -0.603 0.410 0.653"* 0.750 -0.533

0.900 -0.100 0.320 -0.621 0.430 -0.714 0.800 -0.711

0.960 -0.004 0.340 -0.627 0.440 -0.710 0.830 -0.671

0.350 -0.369"* 0.460 -0.714 0.900 -0.083

0.370 -0.633 0.490 -0.641 0.960 0.009

0.380 -0.673 0.500 -0.713

0.400 -0.586 0.520 -0.627

0.410 -0.649 0.540 -0.601

0.430 -0.600 0.550 -0.601

0.440 -0.576 0.580 -0.585

0.460 -0.649 0.600 -0.556

0.470 -0.646 0.610 -0.539

0.490 -0.634 0.650 -0.712

0.500 -0.663 0.700 -0.556

0.520 -0.637 0.750 -0.612

0.530 -0.624 0.820 -0.225

0.550 -0.661 0.890 -0.041

0.560 -0.661 0.900 0.001

0.580 -0.635 0.960 0.103

0.590 -0.681

0.600 -0.688

0.640 -0.678

0.700 -0.272

0.750 -0.031 **

0.820 -0.138

0.870 -0.140

0.930 -0.032

0.960 0.029

Lower Surface

0.020 -0.340 0.020 -0.200 0.020 -0.030 0.020 0.360

0.110 -0.439 0.060 -0.025 0.060 0.037 0.060 -0.052

0.230 -0.311 0.090 -0.165 0.090 -0.067 0.110 -0.025

0.400 -0.119 0.120 -0.246 0.120 -0.324 0.250 -0.278

0.490 -0.073 0.200 -0.201 0.200 -0.269 0.400 -0.319

0.630 4.043** 0.260 -0.359 0.250 -0.319 0.490 -0.422

0.750 0.027 0.400 -0.377 0,400 -0.328 0.580 -0.519

0.850 0.091 0.490 -0.169 0.490 -0.087 0.650 -0.193

0.900 0.185 0.580 -0.190 0.580 -0.201 0.750 0.077

0.960 0.167 0.640 0.038 0.650 -0.051 0.830 0.211

0.750 0.184 0.750 -0.073 0.900 0.284

0.870 0.239 0.890 0.282 0.960 0.253

0.930 0.255 0.930 0.269

0.960 0.197 0.960 0.392

CN --- 0.201 0.358 0.398 0.428

394
Table G-2. Continued.

Flight 211, Wing sweep = 26", Time = 11-34-26-500, MINF = 0,896, Camber = 0/2, ALPT = 7.96, BETA = 0.45, QINF = 301.0.

RNPU = 2,3E+06, CNWP = 0.4324

"q = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.678 0.000 0.816 0.000 0.286** 0.010 -1.017

0.060 -0.740 0.020 -0.896 0.020 -0.820 0,020 - 1.023

0.110 -0.769 0,040 -0.643 0.060 0,899"* 0.060 - 1.012

0.200 -0.740 0.060 -0.827 0,090 -0,901 0.110 -0.990

0.230 -0,637 0.090 -0.835 0,110 -0.949 0.140 -1.017

0.400 -0.687 0.130 -0.817 0.130 -1.781"* 0.190 -1.781"*

0.490 -0.631 0.150 -0.846 0.150 -0.880 0.250 - 1.044

0.590 -0.618 0.200 -0.726 0.210 -0.871 0.400 -0.803

0.630 -0.574 0.250 -0.859 0.250 -0.891 0.490 -0.704

0.700 -0.535 0.260 -0.812 0.340 -0.957 0.580 -0.649

0.750 -0.149 0.280 -0.859 0,370 -0.951 0.650 -0.640

0.810 -0.169 0.290 -0.853 0.400 -0.943 0.700 -0.614

0.840 -0.164 0.310 -0.841 0.4 I0 0.631 ** 0.750 -0.683

0,900 -0.170 0.320 -0.843 0.430 -0.950 0.800 -0.792

0.960 -0.062 0.340 -0.839 0.440 -0.942 0.830 -0.613

0.350 -0.405** 0.460 -0,931 0.900 -0.219

0,370 -0.826 0.490 -0.886 0.960 -0.185

0.380 -0.912 0.500 -0.968

0.400 -0.791 0.520 -0.941

0.410 -0,892 0.540 -0.959

0.430 -0.851 0.550 -0.928

0.440 -0.805 0.580 -0.928

0,460 -0.909 0,600 -0.916

0.470 -0,863 0.610 -0.887

0.490 -0.877 0,650 - 1.115

0.500 -0.855 0.700 -0,967

0.520 -0.858 0.750 -0.649

0,530 -0.839 0.820 -0.324

0.550 -0.884 0.890 -0.195

0.560 -0.882 0.900 -0.207

0.580 -0.865 0.960 -0.137

0.590 -0.913

0.600 -0,861

0.640 -0.301

0.700 -0.298

0.750 -0.062**

0.820 -0.248

0.870 -0.239

0.930 -0.236

0.960 -0.217

Lower Surface

0,020 -0.060 0.020 0.173 0.020 0.278 0.020 0.593

0.110 -0.213 0.060 0.179 0.060 0.236 0.060 -0.068

0.230 -0.107 0.090 0.043 0.090 0.120 0. | 10 0.205

0.400 -0.190 0, | 20 -0,035 0.120 -0.138 0.250 -0.122

0.490 -0.156 0.200 -0.082 0.200 -0.046 0.400 -0.185

0.630 3.995** 0.260 -0.214 0.250 -0.138 0.490 -0.309

0.750 -0.055 0,400 -0.222 0.400 -0.209 0.580 -0.407

0,850 0.016 0.490 -0,222 0.490 -0.096 0.650 -0.171

0,900 0.131 0,580 -0.221 0.580 -0.277 0.750 0.098

0,960 0.123 0.640 -0.024 0.650 -0.081 0,830 0.241

0.750 0.121 0.750 -0.074 0.900 0.307

0.870 0.171 0.890 0.249 0.960 0.199

0,930 0.142 0.930 0,206

0.960 0.073 0.960 0,288

CN = 0.410 0.564 0.684 0.686

395
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-34-41-500, MINF = 0.923, Camber = 0/2, ALPT = 9.09, BETA = -0.33, QINF = 339.7,

RNPU = 2.5E+06, CNWP = 0.4651

'11= 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 -0,668 0.000 0,785 0,000 0,215"* 0.010 -0.970

0.060 -0.718 0.020 -0.889 0.020 -0.801 0.020 -0.988

0.110 -0.744 0.040 -0.675 0.060 0.751 ** 0.060 - 1.058

0.200 -0.779 0.060 -0.820 0.090 -0,900 0.110 - 1.005

0.230 -0.678 0.090 -0.825 0.110 -0.937 0.140 - 1.051

0.400 -0.687 0.130 -0.827 0.130 - 1.676** 0.190 - 1.676"*

0.490 -0.659 0. t 50 -0.828 0.150 -0.871 0.250 - 1.032

0.590 -0.674 0.200 -0.733 0.210 -0.861 0.400 -0.799

0.630 -0.619 0.250 -0.849 0,250 -0.886 0.490 -0.672

0,700 -0.672 0.260 -0.805 0.340 -0.946 0.580 -0.616

0.750 -0.658 0.280 -0,847 0.370 -0.951 0.650 -0.635

0.810 -0.744 0.290 -0.854 0.400 -0.913 0.700 -0.625

0.840 -0.756 0.310 -0,826 0.410 0.461 ** 0.750 -0.663

0.900 -0,223 0.320 -0.830 0.430 -0.953 0.800 -0,789

0.960 -0.175 0.340 -0.849 0.440 -0.931 0.830 -0.752

0,350 -0.418"* 0.460 -0.938 0.900 -0.500

0.370 -0.835 0.490 -0.877 0.960 -0.403

0.380 -0.897 0.500 -0.961

0.400 -0.775 0.520 -0.947

0.410 -0.879 0,540 -0.942

0.430 -0.850 0.550 -0.930

0.440 -0.806 0.580 -0.916

0.460 -0.900 0.600 -0.918

0.470 -0.901 0.610 -0.901

0.490 -0.861 0.650 - 1,087

0.500 -0.876 0.700 -0.934

0.520 -0.867 0.750 - 1.008

0.530 -0.851 0,820 -0.453

0.550 -0.893 0.890 -0.367

0.560 -0.879 0,900 -0.383

0.580 -0.852 0.960 -0.310

0.590 -0,904

0.600 -0.907

0.640 -0.518

0.700 -0.406

0,750 -0.096**

0.820 -0.341

0.870 -0.327

0.930 -0.319

0.960 -0.312

Lower Surface

0.020 -0.005 0.020 0.282 0.020 0.353 0.020 0.683

0.110 -0.199 0.060 0.236 0.060 0.282 0.060 -0.092

0.230 -0,230 0.090 0.088 0.090 0.185 0,110 0.248

0.400 -0.237 0.120 -0.012 0.120 -0.077 0.250 -0.068

0.490 -0.268 0.200 -0,037 0.200 -0.015 0.400 -0.148

0,630 3.442"* 0.260 -0.184 0.250 -0.103 0.490 -0.266

0.750 -0.125 0.400 -0.232 0.400 -0.165 0.580 -0.384

0.850 -0.099 0.490 -0.353 0.490 -0.130 0.650 -0.624

0.900 0.007 0.580 -0,427 0,580 -0.400 0.750 0,038

0.960 -0.017 0.640 -0.013 0.650 -0.117 0.830 0.204

0.750 0. I 01 0.750 -0.137 0.900 0.274

0.870 0.136 0.890 0.230 0.960 0.165

0.930 0.091 0.930 0.164

0.960 0.020 0.960 0.228

CN = 0.442 0.580 0.723 0.688

396
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-34-52-500, MINF = 0.900, Camber = 0/2, ALPI" = 9.87, BETA = -0.07, QINF = 335.9,

RNPU = 2.6E+06, CNWP = 0.4729

r I = 0,93 0.76 0.59 0.40

Upper Surface

.Jc CP x/c CP x/c CP x/c CP

0.020 -0.831 0.000 0,711 0.000 0.254"* 0.010 - 1,112

0.060 -0.899 0,020 - 1.049 0.020 -0.973 0,020 -1.149

0.110 -0.911 0.040 -0.827 0.060 0.726** 0.060 -1,183

0,200 -0.893 0.060 -0.972 0,090 - 1.031 0,1 I0 - 1,128

0.230 -0.764 0.090 -0.952 0.110 - 1.076 0.140 °1.122

0.400 -0.786 0.130 -0.957 0.130 -1.765"* 0.190 -1.765**

0,490 -0.724 0,150 -0,963 0.150 - 1.002 0.250 - 1.134

0.590 -0.76 t 0.200 -0.872 0.210 -0,992 0,400 -0,876

0.630 -0.682 0.250 -0.981 0.250 - 1,00l 0,490 -0.744

0.700 -0.482 0.260 -0,923 0,340 - 1.068 0.580 -0.689

0,750 -0.212 0.280 -0.975 0.370 - 1.051 0.650 -0.728

0.810 -0.195 0.290 -0.968 0.400 °0.985 0.700 -0.707

0.840 -0.197 0.310 -0,935 0.410 0.397** 0.750 -0.738

0,900 -0.229 0.320 -0.949 0,430 - 1.075 0.800 -0.861

0,960 -0.166 0.340 -0.962 0.440 - 1.052 0.830 -0.740

0.350 -0.433** 0.460 -1.061 0.900 -0.337

0.370 -0.942 0.490 -0.992 0.960 -0.255

0.380 -1.021 0.500 -1,061

0.400 -0.904 0.520 - 1.049

0,410 -0.994 0.540 - 1.063

0.430 -0.967 0.550 - 1.035

0.440 -0.898 0.580 - 1,031

0.460 -0.991 0.600 - 1.021

0.470 -0.811 0.610 -0.839

0.490 -0.694 0.650 -0.685

0.500 -0,665 0.700 -0.531

0.520 -0.543 0,750 -0.581

0.530 -0.477 0,820 -0.489

0.550 -0.485 0.890 -0.424

0.560 -0466 0,900 -0.426

0.580 -0.444 0,960 -0.346

0.590 -0.465

0.600 -0.451

0.640 -0.375

0.700 -0.381

0.750 -0.064"*

0.820 -0.345

0,870 -0.321

0,930 -0.326

0.960 -0.312

Lower Surface

0.020 0.095 0.020 0.422 0.020 0.435 0,020 0,733

0.110 -0.123 0.060 0,312 0.060 0.351 0.060 -0.070

0.230 -0.078 0.090 0.149 0.090 0,238 0,110 0.287

0.400 -0.150 0.120 0.057 0.120 -0,026 0.250 -0.023

0.490 -0.162 0.200 0.015 0,200 0.033 0.400 -0,100

0.630 3.411 * * 0.260 -0.104 0.250 -0.035 0.490 -0.213

0.750 -0.131 0,400 -0,151 0.400 -0.121 0.580 -0.348

0.850 -0.074 0.490 -0,195 0.490 -0.095 0.650 -0.142

0.900 0.039 0.580 -0.242 0,580 -0.277 0,750 0.109

0.960 0.027 0.640 -0.034 0.650 -0.082 0.830 0.254

0.750 0.102 0.750 -0.102 0,900 0.300

0.870 0.124 0.890 0.228 0.960 0.193

0.930 0.079 0.930 0.153

0.960 0,004 0.960 O. 178

CN = 0.491 0,634 0.774 0.820

397
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-1-12-000, MINF = 0.901, Camber = 5/2, ALPT = 8.27, BETA = 0.52, QINF = 296.5,

RNPU = 2.2E+06, CNWP = 0.4358

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.101 0.000 0.873 0.000 -5.504"* O.OlO -0.657"*

0.060 -0.214 0.020 -0.224** 0.020 -0.125** 0.020 -0.574"*

0.110 -0.357 0.040 -0.090 0.060 -1.102"* 0.060 -0.707

0.200 -0.833 0.060 -0.374 0.090 -0.542 O. 110 -0.864

0.230 -0.691 0.090 -0.441 O. 110 -0.687 O. 140 1.880"*

0.400 -0.710 O. 130 -0.566 O. 130 -0.743 O. 190 -5.370 **

0.490 -0.649 O. 150 -0.718 O. 150 -0.825 0.250 - 1.032

0.590 -0.621 0.200 -0.720 0.210 -0.892 0.400 -0.734

0.630 -0.567 0.250 -0.875 0.250 -0.867 0.490 -0.706

0.700 -0.626 0.260 -0.764 0.340 -0.928 0.580 -0.618

0,750 -0.119 0.280 -0.864 0.370 -0.910 0.650 -0.567

0.810 -0.149 0.290 -0.877 0.400 -0.928 0.700 -0.590

0,840 -0.093 0.310 -0.810 0.410 -0.887 0.750 -0.654

0.900 -0.121 0.320 -0.795 0.430 -0.956 0.800 -0.810

0.960 -0.044 0.340 -0.838 0.440 -0.919 0.830 -0.786

0.350 -0.343"* 0.460 -0.934 0,900 -0.231

0.370 -0.809 0.490 -0.857 0.960 -0.179

0.380 -0.835 0.500 -0.963

0.400 -0.743 0.520 -0.899

0.410 -0.865 0.540 -0.946

0.430 -0.851 0.550 -0.921

0.440 -0.775 0.580 -0.899

0,460 -0.935 0.600 -0.916

0.470 -0.851 0.610 -0.849

0.490 -0.834 0.650 -2.613"*

0.500 -0.834 0.700 -0,958

0,520 -0.837 0.750 -0.677

0.530 -0.815 0.820 -0,377

0.550 -0.851 0.890 -0.247

0,560 -0.841 0.900 -0.265

0.580 -0.810 0.960 -0.220

0.590 -0.734

0.600 -0.664

0.640 -2.450**

0.700 -0.281

0.750 -0.223

0.820 -2.626**

0.870 -0.242

0.930 -0.221

0.960 -0.211

Lower Surface

0.020 -0.618 0.020 -0.218 0.020 -0.047 0.020 0.337

0.110 -0.196 0.060 0.071 0.060 0.186 0.060 3.423" *

0.230 0.043 0,090 -0.011 0.090 0.094 0.110 0.043

0.400 -0.117 0,120 -0.028 0.120 -0.293 0.250 -0.046

0.490 -0.165 0,200 0.062 0.200 -0.037 0.400 -0.123

0.630 3.467** 0.260 -0.120 0.250 -0.046 0.490 -0.288

0.750 -0.038 0.400 -2.643** 0.400 -0.157 0.580 -0.395

0.850 0.064 0,490 -0, l 81 0.490 -0.022 0.650 -0.140

0.900 0.135 0.580 -0.144 0.580 -0,253 0.750 0.135

0.960 0.121 0.640 0.238 0.650 -0.012 0.830 0.281

0.750 0.118 0.750 -0.005 0.900 0.360

0.870 0.169 0,890 ******** 0.960 0.244

0.930 0.135 0.930 0,219

0.960 0.034 0.960 -2.642**

CN = 0.394 0.529 0.667 0.651

398
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-1-22-500, MINF = 0.905, Camber = 5/2, ALPT = 8.99, BETA = 0.55, QINF = 298.5,

RNPU = 2.3E+06, CNWP = 0,4474

q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.022 0.000 0.891 0.000 -5.464"* 0.010 -0.708"*

0.060 -0,253 0,020 -0,352** 0.020 -0.218** 0.020 -0.625**

O. 110 -0,425 0,040 -0,152 0,060 - 1.133 ** 0.060 -0.821

0.200 -0,865 0,060 -0.431 0.090 -0,625 O.110 -0.897

0.230 -0.783 0.090 -0.515 O. 110 -0,744 O.140 1.476"*

0.400 -0.734 0.130 -0.641 0.130 -0.799 O. 190 -5.331"*

0.490 -0.694 O.150 -0.759 O, 150 -0.866 0,250 - 1.081

0.590 -0.671 0,200 -0,752 0.210 -0.947 0.400 -0.783

0.630 -0,622 0,250 -0.934 0.250 -0.896 0.490 -0.724

0.700 -0.635 0.260 -0.826 0.340 -0.967 0.580 -0.690

0.750 -0.152 0.280 -0.894 0.370 -0,956 0.650 -0.585

0.810 -0.195 0.290 -0.929 0.400 -0,942 0.700 -0.642

0,840 -0.122 0.310 -0.852 0.410 -0.919 0.750 -0.684

0.900 -0.156 0.320 -0.827 0.430 -0.994 0.800 -0.817

0.960 -0.100 0.340 -0.872 0.440 -0.968 0.830 -0,798

0.350 -0.364"* 0.460 -0.972 0.900 -0.316

0,370 -0.856 0.490 -0.908 0.960 -0.234

0,380 -0.868 0.500 -0.984

0.400 -0.805 0.520 -0.984

0.410 -0.893 0.540 -0.981

0.430 -0.894 0,550 -0.965

0.440 -0.821 0.580 -0.950

0.460 -0.975 0.600 -0.944

0.470 -0.910 0.610 -0.884

0.490 -0.865 0.650 -2.593**

0.500 -0,884 0.700 -0.756

0.520 -0.890 0.750 -0.592

0.530 -0.868 0.820 -0.462

0.550 -0.885 0.890 -0.363

0.560 -0.871 0.900 -0.369

0.580 -0.818 0.960 -0.324

0.590 -0.64 l

0.600 -0.506

0.640 -2.431 **

0.700 -0.321

0.750 -0.271

0.820 -2.606"*

0.870 -0.272

0.930 -0.281

0.96O -0,274

Lower Surface

0.020 -0,388 0.020 -0.109 0.020 0.050 0.020 0.420

O. 110 -0.174 0.060 O_128 0.060 O.265 0.060 3.401 * *

O,230 0.067 0.090 0.047 0.090 O. 150 O, 110 0,091

0.400 -0.126 O. 120 0.026 O. 120 -0.256 0.250 -0.005

0.490 -0.162 0.200 0.085 0.200 -0.032 0.400 -0.088

0.630 3.444** 0.260 -0,085 0.250 -0.007 0.490 -0.262

0.750 -0.078 0.400 -2.623** 0.400 -0.124 0.580 -0.381

0.850 0.023 0.490 -0.182 0.490 -0.020 0.650 -0.152

0.900 0.085 0.580 -0.160 0.580 -0.257 0.750 0,130

0,960 0.085 0.640 0.220 0.650 -0.033 0.830 0.289

0.750 0.119 0.750 -0.015 0.900 0.354

0.870 0.155 0.890 ******** 0.960 0.238

0.930 0.121 0.930 0.204

0.960 0.002 0.960 -2.622**

CN = 0.428 0.571 0.706 0.710

399
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-1-33-000, MINF = 0.900, Camber = 5/2, ALPT = 10.15, BETA = 0.39, QINF = 296.1,

RNPU = 2.2E+06, CNWP = 0.4739

11 = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x./c CP x/c CP x/c CP

0.020 -0.132 0.000 0.942 0.000 -5.512 * * 0.010 -0.708 * *

0.060 -0.397 0.020 -0.619"* 0.020 -0.323"* 0.020 -0.768**

0. I 10 -0.517 0.040 -0.254 0.060 - 1.213"* 0.060 -0.923

0.200 -0.939 0.060 -0.548 0.090 -0.720 0.110 - 1.027

0.230 -0.810 0.090 -0.645 0.110 -0.866 0.140 - 1.083"*

0.400 -0.804 0.130 -0.751 0.130 -0.877 0.190 -5.378 **

0.490 -0.750 0.150 -0.846 0.150 -0.956 0.250 - 1.150

0.590 -0.706 0.200 -0.861 0.210 - 1.028 0.400 -0.861

0.630 -0.597 0.250 - 1.009 0.250 -0.994 0.490 -0.779

0.700 -0.356 0.260 -0.904 0.340 - 1.041 0.580 -0.733

0.750 -0.238 0.280 -0.979 0.370 - 1.025 0.650 -0.663

0.810 -0.235 0.290 -0.997 0.400 - 1.019 0.700 -0.721

0.840 -0.202 0.310 -0.919 0.410 -0.989 0.750 -0.737

0.900 -0.214 0.320 -0.910 0.430 - 1.083 0.800 -0.856

0.960 -0.204 0.340 -0.967 0.440 - 1.037 0.830 -0.821

0.350 -0.346"* 0.460 -1.043 0.900 -0.273

0.370 -0.920 0.490 -0.986 0.960 -0.182

0.380 -0.955 0.500 - 1.067

0.400 -0.862 0.520 -1.041

0.410 -0.973 0.540 - 1.062

0.430 -0.946 0.550 - 1.036

0.440 -0.864 0.580 -1.011

0.460 - 1.056 0.600 -0.891

0.470 -0.851 0.610 -0.524

0.490 -0.680 0.650 -2.618"*

0.500 -0.539 0.700 -0.507

0.520 -0.515 0.750 -0.581

0.530 -0.452 0.820 -0.510

0.550 -0.450 0.890 -0.464

0.560 -0.418 0.900 -0.448

0.580 -0.403 0.960 -0.425

0.590 -0.413

0.600 -0.44-4

0.640 -2.454**

0.700 -0.390

0.750 -0.316

0.820 -2.630**

0.87O -0.327

0.930 -0.319

0.960 -0.298

Lower Surface

0.020 -0.118 0.020 0.128 0.020 0.236 0.020 0.565

0.110 -0.060 0.060 0.243 0.060 0.375 0.060 3.427"*

0.230 0.107 0.090 0.161 0.090 0.237 0.1 t0 0.187

0.400 -0.092 0.120 0.137 0.120 -0.163 0.250 0.071

0.490 -0.136 0.200 0.124 0.200 0.018 0.400 -0.031

0.630 3.470"* 0.260 -0.011 0.250 0.080 0.490 -0.176

0.750 -0.093 0.400 -2.648** 0.400 -0.052 0.580 -0.324

0.850 -0.014 0.490 -0.141 0.490 -0.008 0.650 -0.111

0.900 0.045 0.580 -0.123 0.580 -0.225 0.750 0.153

0.960 0.019 0.640 0.242 0.650 -0.006 0.830 0.289

0.750 0.101 0.750 0.005 0.900 0.363

0.870 0.155 0.890 ******** 0.960 0.238

0.930 0.097 0.930 0.180

0.960 -0.012 0.960 -2.647"*

CN = 0.488 0.622 0.772 0.815

400
Table G-2. Continued.

Flight 226. Wing sweep = 26 _', Time = 10-7-8-500, MINF = 0.904, Camber = 5/2, ALl:q" = 6.15, BETA = -0,38, QINF = 297.9,

RNPU = 2.3E+06, CNWP = 0.3388

rl = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.217 0.000 0.704 0,000 3.560** 0.010 -0.271

0,060 -0.091 0.020 -0.042 0.020 0.082 0.020 -0.162

0.110 -0.351 0.040 0.033 0.060 -4.712"* 0.060 -0.561

0,200 -0.720 0.060 -0.224 0.090 -0.365 0.110 -0.690

0.230 -0.530 0.090 -0.285 0.110 -0.481 0,140 -0.889

0.400 -0.622 0.130 -0.433 0, 130 -0,530 0.190 - 1.750"*

0.490 -0.541 0.150 -0.651 0.150 -0.802 0.250 -0.851

0,590 -0.568 0.200 -0.669 0,210 -0.673 0.400 -0.673

0.630 -0.464 0.250 -0.708 0.250 -0.728 0.490 -0.539

0.700 -0.148 0.260 -0.705 0.340 -0.727 0,580 -0.478

0.750 -0.145 0.280 -0.690 0.370 -0.743 0.650 -0.468

0.810 -0.143 0.290 -0.705 0.400 -0.829 0.700 -0.449

0.840 -0.086 0.310 -0.740 0.410 -2.753** 0.750 -0.546

0.900 -0.071 0.320 -0,707 0.430 -0.759 0.800 -0.675

0.960 0.021 0.340 -0.680 0,440 -0.719 0.830 -0.609

0.350 -0.440"* 0.460 -0.743 0.900 -0,166

0.370 -0.712 0.490 -0.716 0.960 -0.125

0.380 -0.727 0,500 -0.802

0.400 -0.772 0.520 -0.725

0.410 -0.716 0.540 -0.730

0.430 -0.668 0.550 -0.757

0.440 -0,664 0.580 -0.706

0,460 -0,743 0.600 -0,567

0,470 -0.665 0.610 -0.552

0.490 -0,740 0.650 2.181 **

0.500 -0.772 0.700 -0.651

0.520 -0.768 0.750 -0.688

0.530 -0.745 0.820 -0,401

0.550 -0.788 0.890 -0.091

0.560 -0.679 0.900 -0.060

0.580 -0.762 0.960 -0.003

0.590 -0,806

0.600 -0,805

0,640 -0.796

0,700 -0.764

0,750 -0.032"*

O.820 -0.158

0.870 -0.133

0.930 -0.070

0.960 -0.049

Lower Surface

0.020 - 1.181 0.020 -0.948 0,020 -0,638 0.020 0.083

0.110 -0.444 0.060 -0.128 0.060 0.005 0.060 1.889'*

0.230 -0.046 0.090 -0.195 0.090 1.185"* 0.110 -0.017

0.400 -0.120 0.120 -0.126 0.120 -0.400 0.250 -0.170

0.490 -0.040 0.200 -0.048 0.200 -0.110 0.400 -0.226

0.630 1.950"* 0.260 -0.240 0.250 -0.156 0,490 -0.375

0.750 0.023 0.400 -0.231 0,400 -0.256 0.580 -0.462

0.850 0.133 0.490 -0.205 0.490 -0,070 0.650 -0.340

0.900 0.183 0.580 -0.191 0.580 -0.400 0.750 0.027

0,960 0.175 0.640 0.015 0.650 -0.055 0.830 0.244

0,750 0.181 0.750 0.258 0.900 0.318

0.870 0.239 0.890 0.217 0.960 0.239

0.930 0,196 0.930 0.206

0.960 0.146 0.960 -2.840**

CN = 0.296 0.462 0.472 0.455

401
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-7-21-500, MINF = 0.902, Camber = 5/2, ALPT = 7.05, BETA = -0.44, QINF = 297.5,

RNPU = 2.3E+06, CNWP = 0.3831

tl = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x,/c CP x/c CP

0.020 0.149 0.000 0.751 0.000 3,560"* 0.010 -0.543

0.060 -0.119 0.020 -0.157 0.020 -0.018 0.020 -0.151

0.110 -0,336 0.040 -0.063 0.060 -4.721 ** 0.060 -0.565

0.200 -0,738 0.060 -0.321 0.090 -0.428 0.110 -0.774

0.230 -0.647 0.090 -0,348 0.110 -0.562 0.140 -0.947

0,400 -0,679 0.130 -0.499 0.130 -0.594 0.190 - 1.756"*

0.490 -0.578 0.150 -0.689 0.150 -0,815 0.250 -0.912

0,590 -0.608 0.200 -0.693 0.210 -0,735 0.400 -0.713

0,630 -0.518 0.250 -0.751 0,250 -0.777 0.490 -0,635

0.700 -0,308 0.260 -0.766 0.340 -0.770 0.580 -0.514

0.750 -0.149 0.280 -0.739 0.370 -0.795 0.650 -0.499

0.810 -0.163 0.290 -0.754 0.400 -0.900 0.700 -0.499

0.840 -0.082 0.310 -0.802 0,410 -2.759** 0.750 -0.595

0.900 -0.118 0.320 -0.776 0.430 -0,809 0.800 -0.701

0.960 -0.027 0.340 -0.719 0.440 -0.765 0.830 -0.665

0.350 -0.445* * 0.460 -0,790 0.900 -0.202

0.370 -0,758 0.490 -0,789 0.960 -0.161

0.380 -0.768 0.500 -0.835

0.400 -0.737 0.520 -0.781

0.410 -0.778 0.540 -0.805

0.430 -0.746 0.550 -0.851

0,440 -0.754 0.580 -0.835

0.460 -0.784 0.600 -0.756

0.470 -0,736 0.610 -0.733

0,490 -0,803 0.650 2.179"*

0.500 -0.833 0.700 -0.785

0.520 -0.813 0.750 -0.812

0.530 -0.792 0.820 -0.314

0.550 -0,863 0.890 -0.143

0.560 -0.742 0.900 -0.127

0.580 -0.807 0.960 -0.064

0.590 -0,864

0.600 -0.884

0.640 -0.750

0.700 -0,341

0.750 -0.051 **

0.820 -0.185

0.870 -0.189

0.930 -0.189

0.960 -0.178

Lower Surface

0.020 -0.915 0.020 -0.702 0.020 -0.141 0.020 0.179

0.110 -0.221 0.060 -0.064 0.060 0.028 0.060 1.887"*

0.230 -0,024 0.090 -0.140 0,090 1.182"* 0.110 -0.006

0,400 -0.143 0.120 -0.101 0.120 -0.337 0.250 -0.121

0.490 -0.134 0.200 -0.023 0,200 -0.129 0.400 -0.189

0.630 1.948** 0.260 -0.216 0.250 -0.124 0.490 -0,342

0.750 -0.031 0.400 -0.223 0.400 -0.215 0.580 -0.431

0,850 0.087 0.490 -0.228 0,490 -0.074 0.650 -0,269

0,900 0.175 0.580 -0.215 0.580 -0.272 0.750 0.043

0.960 0.150 0.640 0.000 0.650 -0.059 0,830 0.266

0.750 0.161 0.750 0.232 0.900 0.317

0.870 0,226 0.890 0.210 0.960 0.230

0,930 0.149 0.930 0.188

0.960 0.079 0.960 -2.847 * *

CN = 0.341 0.466 0.553 0.529

402
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-7-24-000, MINF = 0.901, Camber = 5/2, ALPT = 7.03, BETA = -0.85, QINF = 296.4,

RNPU = 2.2E+06, CNWP = 0.3873

rI = 0.93 0,76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.159 0.000 0.752 0.000 3.575"* 0,010 -0.528

0,060 -0,132 0.020 -0.179 0.020 -0.032 0.020 -0.171

0.110 -0.367 0.040 -0,057 0.060 -4.737** 0.060 -0.587

0.200 -0.739 0.060 -0.321 0.090 -0.454 0.110 -0.780

0.230 -0.685 0.090 -0.341 0.110 -0.572 0.140 -0.952

0.400 -0.669 0.130 -0.494 0.130 -0.595 0.190 - 1,761 **

0.490 -0.590 0.150 -0.698 0.150 -0.842 0.250 -0.914

0.590 -0.605 0.200 -0.715 0.210 -0.726 0.400 -0,706

0.630 -0.511 0.250 -0.765 0.250 -0,770 0.490 -0.625

0.700 -0.213 0.260 -0.752 0.340 -0.786 0.580 -0.525

0.750 -0.152 0.280 -0,749 0.370 -0.789 0.650 -0,499

0.810 -0.154 0.290 -0.740 0.400 -0.872 0.700 -0.510

0.840 -0.104 0.310 -0.791 0,410 -2.768** 0.750 -0.610

0.900 -0.099 0.320 -0.782 0.430 -0.810 0.800 -0.717

0.960 -0.032 0.340 -0.712 0,440 -0.756 0.830 -0.651

0.350 -0.445** 0,460 -0.791 0,900 -0.177

0.370 -0.747 0,490 -0.782 0,960 -0.137

0,380 -0.784 0.500 -0.837

0.400 -0.712 0.520 -0.784

0.410 -0.783 0.540 -0,806

0.430 -0.732 0.550 -0,832

0.440 -0.719 0.580 -0.818

0.460 -0.800 0,600 -0.742

0.470 -0.703 0.610 -0.719

0490 -0,813 0,650 2.189**

0.500 -0.807 0,700 -0.764

0.520 -0.814 0.750 -0.813

0.530 -0285 0.820 -0.288

0.550 -0.803 0.890 -0.127

0.560 -0.734 0.900 -0.105

0.580 -0.807 0.960 -0.034

0,590 -0,855

0.600 -0,866

0.640 -0.726

0.700 -0.318

0.750 -0.045**

0.820 -0.169

0,870 -0.181

0.930 -0.155

0.960 -0.129

Lower Surface

0.020 -0,875 0,020 -0,674 0.020 -0.155 0,020 0.175

0,110 -0,227 0.060 -0.063 0.060 0,069 0.060 I, 896" *

0,230 -0.015 0.090 -0.124 0.090 1.188 ** 0.110 -0.009

0.400 -0.127 0.120 -0.085 0.120 -0.337 0.250 -0.120

0,490 -0.125 0.200 -0.014 0.200 -0.092 0.400 -0.189

0,630 1,957"* 0.260 -0,200 0.250 -0,111 0.490 -0.341

0,750 -0,022 0.400 -0.184 0.400 -0.215 0.580 -0.426

0.850 0,089 0.490 -0.204 0,490 -0.073 0.650 -0.178

0.900 0.178 0.580 -0.191 0.580 -0.213 0.750 0.054

0.960 0,152 0.640 0.017 0,650 -0.073 0,830 0.280

0.750 0.172 0.750 0.246 0.900 0.314

0,870 0.182 0.890 0.227 0.960 0.226

0.930 0,151 0.930 0,190

0.960 0.111 0,960 -2.856**

CN = 0.348 0.467 0.560 0.538

403
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-7-30-500, MINF = 0.904, Camber = 5/2, ALPT = 7.99, BETA = -0.67, QINF = 298.4,

RNPU = 2.3E+06, CNWP = 0.4302

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x,/c CP x/c CP

0.020 0.061 0.000 0.792 0.000 3.552"* 0.010 -0.594

0.060 -0.169 0.020 -0.273 0.020 -0.114 0.020 -0.5 l6

0.110 -0.353 0.040 -0.160 0.060 -4.707** 0.060 -0.668

0.200 -0.742 0.060 -0.413 0.090 -0.531 0.110 -0.834

0.230 -0.666 0.090 -0.444 0. I 10 -0.636 0.140 - 1.000

0.400 -0.714 0.130 -0.553 0.130 -0.648 0.190 - 1.750 **

0.490 -0.642 0.150 -0.743 0.150 -0.904 0.250 -0.994

0.590 -0.659 0.200 -0.741 0.210 -0.778 0.400 -0.758

0.630 -0.585 0.250 -0.784 0.250 -0.831 0.490 -0.674

0.700 -0.504 0.260 -0.780 0.340 -0.827 0.580 -0.585

0.750 -0.164 0.280 -0.788 0.370 -0.825 0.650 -0.547

0.810 -0.175 0.290 -0.788 0.400 -0.926 0.700 -0.534

0.840 -0.111 0.310 -0.845 0.410 -2.751 ** 0.750 -0.628

0.900 -0.150 0.320 -0.829 0.430 -0.851 0.800 -0.733

0.960 -0.067 0.340 -0.74 ! 0.440 -0.804 0.830 -0.684

0.350 -0.418"* 0.460 -0.838 0.900 -0.240

0.370 -0.794 0.490 -0.831 0.960 -0.183

0.380 -0.820 0.500 -0.879

0.400 -0.763 0.520 -0.798

0.4 I0 -0.815 0.540 -0.826

0.430 -0.786 0.550 -0.894

0.440 -0.779 0.580 -0.884

0.460 -0.840 0.600 -0.810

0.470 -0.738 0.610 -0.796

0.490 -0.836 0.650 2.174**

0.500 -0.868 0.700 -0.932

0.520 -0.872 0.750 -0.912

0.530 -0.823 0.820 -0.280

0.550 -0.926 0.890 -0.180

0.560 -0.765 0.900 -0.196

0.580 -0.863 0.960 -0.133

0.590 -0.908

0.600 -0.900

0.640 -0.330

0.700 -0.287

0.750 -0.034**

0.820 -0.202

0.870 -0.235

0.930 -0.206

0.960 -0.217

Lower Surface

0.020 -0.720 0.020 -0.301 0.020 -0.030 0.020 0.312

0.110 -0.220 0.060 0.005 0.060 0.149 0.060 1.883"*

0.230 -0.003 0.090 -0.065 0.090 1.180** 0.110 0.071

0.400 -0.126 0.120 -0.018 0.120 -0.275 0.250 -0.076

0.490 -0.110 0.200 0.008 0.200 -0.058 0.400 -0.151

0.630 1.944"* 0.260 -0.148 0.250 -0.048 0.490 -0.306

0.750 -0.061 0.400 -0.169 0.400 -0.174 0.580 -0.379

0. 850 0.037 0.490 -0.207 0.490 -0.058 0.650 -0.170

0.900 0.138 0.580 -0.187 0.580 -0.234 0.750 0.063

0.960 0.113 0.640 0.009 0.650 -0.065 0.830 0.297

0.750 0.160 0.750 0.237 0.900 0.312

0.870 0.204 0.890 0.211 0.960 0.218

0.930 0.121 0.930 0.166

0.960 0.047 0.960 -2.838**

CN = 0.383 0.505 0.641 0.630

404
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-7..40-000, MINF = 0.903, Camber = 502, ALPT = 12.02, BETA = -0.70, QINF = 304.2,

RNPU = 2.3E+06, CNWP = 0.3996

"q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.616 0.000 0,826 0.000 3.447"* 0.010 -0.838

0.060 -0.594 0.020 -0.896 0.020 -0.733 0,020 -0.920

0.110 -0.714 0_040 -0.594 0.060 -4.654** 0.060 -0.998

0.200 -0.904 0.060 -0.764 0.090 -0.852 0.110 - 1.082

0.230 -0.861 0.090 -0.794 0.110 -0.942 0.140 - 1.220

0.400 -0.871 0.130 -0.876 0.130 -0.937 0.190 - 1.753"*

0.490 -0.680 0.150 -I.017 0.150 -1.145 0.250 -1.261

0.590 -0.522 0.200 -0,994 0.210 - 1.002 0.400 - 1.023

0.630 -0.480 0.250 - 1.O31 0,250 - 1.065 0.490 -0.923

0.700 -0.401 0.260 - 1.007 0.340 - 1.056 0.580 -0.700

0.750 -0.441 0.280 -0.972 0.370 - 1.033 0.650 -0.610

0.810 -0.404 0.290 -0.955 0.400 - 1.076 0.700 -0.588

0.840 -0.360 0.310 - 1.010 0.410 -2.735"* 0,750 -0.652

0.900 -0.367 0,320 -0.977 0.430 -0.886 0.800 -0.671

0.960 -0.377 0.340 -0.828 0.440 -0,736 0,830 -0.502

0.350 -0.354** 0.460 -0.688 0.900 -0,370

0.370 -0.718 0.490 -0.629 0.960 -0.286

0.380 -0.680 0.500 -0.660

0.400 -0.579 0.520 -0.575

0.410 -0.586 0.540 -0.603

0.430 -0.559 0.550 -0,628

0.440 -0.555 0.580 -0,653

0.460 -0.594 0.600 -0.574

0,470 -0.512 0.610 -0.548

0.490 -0,560 0.650 2.096"*

0,500 -0,623 0.700 -0.596

0.520 -0,580 0,750 -0,684

0.530 -0.535 0.820 -0.525

0.550 -0.588 0.890 -0.484

0.560 -0.489 0,900 -0.504

0.580 -0.563 0.960 -0,421

0.590 -0.569

0.600 -0.575

0.640 -0.463

0.700 -0.451

0.750 -0.055"*

0.820 -0,418

0.870 -0.432

0.930 -0.406

0.960 -0.386

Lower Surface

0,020 0.024 0.020 0.333 0.020 0.438 0.020 0,680

0.110 -0.006 0.060 0.309 0.060 0.427 0,060 1.81 I **

0.230 0.116 0,090 0.179 0,090 1,121 ** 0.110 0.297

0.400 -0.054 0.120 0.191 0.120 -0.026 0.250 0.123

0.490 -0.086 0.200 0.137 0.200 0.070 0.400 0.017

0.630 1.870"* 0.260 0.039 0,250 0.118 0.490 -0.120

0.750 -0.125 0.400 -0.032 0.400 -0.04 1 0,580 -0,261

0.850 -0.081 0.490 -0.117 0,490 -0.064 0.650 -0.101

0.900 -0.028 0,580 -0.1 64 0.580 -0.165 0.750 0,078

0.960 -0.127 0.640 0.004 0.650 -0.070 0.830 0,296

0.750 0.132 0,750 0.272 0.900 0.313

0.870 0.139 0.890 0.186 0.960 0.192

0,930 0,050 0,930 0.119

0.960 -0.019 0,960 -2.821 **

CN = 0.550 0.677 0.791 0.906

405
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-7-43-000, MINF = 0.898, Camber = 5/2, ALPT = 12.15. BETA = -0.10, QINF = 305.7,

RNPU = 2.3E+06, CNWP = 0.3509

'1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0.595 0.000 0.835 0.000 3.402'* 0.010 -0.853

0.060 -0.599 0.020 -0.909 0.020 -0.751 0.020 -0.935

0. l 10 -0.766 0.040 -0.622 0.060 -4.658 * * 0.060 -0.971

0.200 -0.892 0.060 -0.774 0.090 -0.857 0.110 - 1.132

0.230 -0.873 0.090 -0.797 0.110 -0.945 0.140 - 1,247

0.400 -0.909 0.130 -0.883 0.130 -0.928 0.190 - 1.772"*

0.490 -0.700 0.150 -1.022 0.150 -1,154 0.250 -1.268

0.590 -0.481 0.200 - 1.004 0.210 - 1.029 0.400 -0.976

0.630 -0.461 0.250 -0.871 0.250 - 1.072 0.490 -0.815

0.700 -0.387 0.260 -0.741 0.340 -0.947 0.580 -0.798

0.750 -0.456 0.280 -0.803 0.370 -0.919 0.650 -0.695

0.810 -0.492 0.290 -0.812 0.400 - 1.019 0.700 -0.634

0.840 -0.422 0.310 -0.791 0.410 -2.749** 0.750 -0.612

0.900 -0.302 0.320 -0.744 0.430 -0.733 0.800 -0.604

0.960 -0.273 0.340 -0.569 0.440 -0.660 0.830 -0.534

0.350 -0.304** 0.460 -0.694 0.900 -0.455

0.370 -0.555 0.490 -0.647 0.960 -0.375

0.380 -0.595 0.500 -0.683

0.400 -0.521 0.520 -0.620

0.410 -0.575 0.540 -0.625

0.430 -0.520 0.550 -0.648

0.440 -0.539 0.580 -0.614

0.460 -0.578 0.600 -0.558

0.470 -0.515 0.610 -0.544

0.490 -0.552 0.650 2.057"*

0.500 -0.576 0.700 -0.606

0.520 -0.576 0.750 -0.682

0.530 -0.549 0.820 -0.492

0.550 -0.593 0.890 -0.476

0.560 -0.497 0.900 -0.505

0.580 -0.565 0.960 -0.411

0.590 -0.582

0.600 -0.581

0.640 -0.489

0.700 -0.469

0.750 -0.050**

0.820 -0.492

0.870 -0.511

0.930 -0.439

0.960 -0.405

Lower Surface

0.020 0.005 0.020 0.357 0.020 0.438 0.020 0.690

0.110 0.002 0.060 0.316 0.060 0.439 0.060 1.773"*

0.230 0.124 0.090 0.185 0.090 1.087"* 0.110 0.297

0.400 -0.049 0.120 0.198 0.120 -0.016 0.250 0.127

0.490 -0.084 0.200 0.145 0.200 0.071 0.400 0.018

0.630 1.832 ** 0.260 0.048 0.250 0.141 0.490 -0.118

0.750 -0.138 0.400 -0.030 0.400 -0.025 0.580 -0.233

0.850 -0.072 0.490 -0.119 0.490 -0.092 0.650 -0.110

0.900 -0.005 0.580 -0.170 0.580 -0.170 0,750 0.098

0.960 -0.064 0.640 0.002 0.650 -0.098 0.830 0.304

0.750 0.132 0.750 0.261 0.900 0.313

0.870 0.121 0.890 0.186 0.960 0.181

0.930 0.051 0.930 0.120

0.960 -0.010 0.960 -2.835 **

CN = 0.563 0.664 0.775 0.922

406
Table G-2. Continued.

Flight 200, Wing sweep = 26 °, Time = 8-21-10-000, MINF = 0.898, Camber = 5/6, ALPT = 5.01, BETA = 0.45, QINF = 294.2,

RNPU = 2.2E+06, CNWP = 0.3343

rl = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.347 0,000 0.640 0,000 0,953"* 0.010 -0,062

0.060 0.019 0.020 0.175 0.020 0.267 0,020 -0.001 **

0.110 -0.222 0.040 0.160 0,060 0.859"* 0,060 -0,377* *

0.200 -0.741 0,060 -0.101 0.090 -0,217 0. I 10 -0.580

0.230 -0.625 0,090 -0.200 0,110 -0.446 0.140 -0,767

0.400 -0.482 0.130 -0.349 0,130 -0.498 0.190 - 1,771 **

0,490 -0,391 0,150 -0.559 0.150 -0.680 0.250 -0.598

0.590 -0.168 0.200 -0.588 0.210 -0.657 0.400 -0,603

0.630 -0.187 0,250 -0.680 0.250 -0.644 0,490 -0.378

0.700 -0.199 0.260 -0.616 0,340 -0,696 0.580 -0.315

0.750 -0.584 0,280 -0.653 0.370 -0.714 0.650 -0.365

0.810 -0.542 0.290 -0.644 0,400 -0.686 0.700 -0,360

0.840 -0.564 0.310 -0.625 0.410 -0.673 0.750 -0,460

0.900 -0.096 0,320 -0,622 0.430 -0.674 0,800 -0.841

0.960 -0.017 0.340 -0.610 0.440 -0.650 0.830 -0.785

0,350 -0.314"* 0.460 -0.653 0.900 -0.251

0.370 -0,617 0.490 -0.516 0.960 -0.246"*

0,380 -0.673 0.500 -0.577

0.400 -0.585 0.520 -0,501

0.410 -0,642 0.540 -0.441

0.430 -0,614 0.550 -0.341

0.440 -0,572 0.580 -0.278

0.460 -0.653 0.600 -0,302

0.470 -0.623 0.610 -0,275

0.490 -0.626 0.650 0.039**

0.500 -0.620 0.700 -0.450

0.520 -0.620 0.750 -0.521

0.530 -0,614 0.820 -0.454

0.550 -0.633 0.890 -0,238

0.560 -0.643 0.900 -0.225

0.580 -0.619 0.960 -0.155

0.590 -0.674

0.600 -0,682

0.640 -0.475

0.700 -0.476

0.750 0.042**

0.820 -0,465

0.870 -0,202

0,930 -0.109

0.960 -0,095

Lower Surface

0.020 - 1,234 0.020 - 1. I 17 0.020 -0,948 0.020 -0.117

0.110 -0.431 0.060 -0.813 0,060 -0.170 0,060 -0.121

0.230 -0,046 0.090 -0.351 0.090 -0.198 0.110 -0.192

0.400 -0.028 0.120 -0.220"* 0,120 -0,431 0.250 -0.229

0,490 -0.008 0.200 -0.034 0,200 -0.096 0,400 -0.280

0.630 3.688** 0.260 -0.195 0,250 -0.251 0.490 -0.393

0.750 0.137 0,400 -0.121 0.400 -0,312 0.580 -0.431

0.850 0,201 0,490 -0.086 0.490 0.015 0.650 0.007

0.900 0,299 0.580 -0.038 0,580 -0,097 0.750 0,232

0,960 0.198 0,640 0.178 0.650 0.036 0,830 0,364

0,750 0.295 0.750 0.000** 0,900 0.437

0.870 0,361 0.890 0.397 0,960 0.299

0.930 0.299 0,930 0.317

0.960 0.214 0,960 0.802

CN = 0.340 0.430 0.428 0.392

407
Table G-2. Continued.

Flight 200. Wing sweep = 26 °, Time = 8-21-25-000, MINF = 0.907, Camber = 5/6, ALPT = 6,11, BETA = 0.14, QINF = 298.6,

RNPU = 2.3E+06, CNWP = 0.3882

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.297 0.000 0,703 0.000 0.933'* 0.010 -0.228

0.060 -0.030 0,020 0.114 0.020 0.147 0.020 -0.094"*

0.110 -0.239 0.040 0.109 0.060 0.717"* 0,060 -0.454**

0.200 -0.748 0.060 -0.151 0.090 -0.265 0,110 -0.650

0.230 -0.654 0,090 -0.251 0.110 -0.496 0.140 -0.832

0.400 -0.563 0.130 -0.390 0.130 -0.546 0.190 - 1.736"*

0.490 -0.478 0.150 -0.595 0.150 -0.709 0.250 -0.820

0.590 -0.483 0.200 -0,627 0.210 -0.704 0.400 -0.621

0.630 -0.416 0.250 -0.728 0.250 -0.691 0.490 -0,496

0.700 -0_473 0.260 -0.674 0.340 -0.751 0.580 -0,419

0.750 -0.556 0.280 -0.707 0.370 -0.778 0.650 -0.436

0.810 -0.518 0.290 -0.698 0.400 -0.769 0.700 -0.436

0.840 -0.538 0.310 -0,665 0.410 -0.730 0.750 -0.517

0.900 -0.118 0.320 -0.681 0.430 -0.745 0.800 -0.865

0.960 -0.033 0.340 -0.676 0.440 -0.732 0.830 -0,797

0.350 -0.345** 0.460 -0.766 0.900 -0.335

0370 -0.683 0.490 -0.725 0.960 -0.311 **

0.380 -0.728 0.500 -0.777

0.400 -0.636 0.520 -0.751

0.410 -0.696 0.540 -0.740

0.430 -0.668 0.550 -0.664

0.440 -0.635 0.580 -0.542

0.460 -0,723 0.600 -0.559

0.470 -0.712 0.610 -0.533

0.490 -0.703 0,650 0.015"*

0.500 -0.701 0.700 -0.548

0.520 -0,693 0.750 -0.592

0.530 -0.682 0.820 -0,449

0.550 -0.684 0.890 -0.272

0.560 -0.701 0.900 -0.276

0.580 -0.683 0.960 -0.225

0.590 -0.738

0.600 -0.726

0.640 -0.747

0.700 -0.800

0.750 0.033**

0.820 -0.210

0,870 -0.212

0.930 -0.224

0.960 -0.212

Lower Surface

0.020 - 1.169 0.020 - 1.011 0.020 -0.782 0.020 0.032

0.110 -0.155 0.060 -0.251 0.060 -0.030 0.060 -0.043

0.230 -0.034 0.090 -0.210 0.090 -0.088 0.110 -0.087

0.400 -0.066 0. 120 -0.149 ** 0.120 -0.367 0.250 -0.186

0.490 -0.020 0.200 -0.002 0.200 -0.074 0.400 -0.223

0.630 3.643"* 0.260 -0.190 0.250 -0.179 0.490 -0.362

0.750 0.096 0,400 -0.142 0.400 -0.263 0.580 -0.464

0.850 0.163 0.490 -0.109 0.490 -0.005 0.650 -0.005

0.900 0.270 0.580 -0.061 0.580 -0.101 0.750 0.223

0.960 0.175 0.640 0.156 0.650 0.009 0.830 0.360

0.750 0.286 0.750 -0,020** 0.900 0.443

0.870 0.327 0.890 0,415 0.960 0.293

0.930 0.278 0.930 0,311

0.960 0.184 0.960 0,778

CN = 0.435 0.523 0.539 0.501

408
Table G-2. Continued.

Flight 200, Wing sweep = 26 °, Time = 8-21-28-500, MINF = 0.908, Camber = 5/6, ALPT = 6.99. BETA = 0.08, QINF = 299.1,

RNPU = 2.3E+06, CNWP = 0.4526

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x,/c CP

0.020 0.207 0.000 0.781 0.000 0,910"* 0.010 -0.456

0,060 -0.092 0,020 -0,006 0.020 0.056 0.020 -0,190"*

0.110 -0.202 0.040 0.022 0.060 0.628** 0.060 -0.524**

0.200 -0.761 0.060 -0.230 0.090 -0.377 0.1 I 0 -0.715

0.230 -0.630 0.090 -0.298 0.110 -0.564 0.140 -0.922

0.400 -0.624 0.130 -0.435 0.130 -0.586 0,190 - 1,735"*

0.490 -0.523 0.150 -0.626 0.150 -0,752 0.250 -0.905

0.590 -0.531 0.200 -0,664 0.210 -0.736 0.400 -0.663

0.630 -0.472 0.250 -0,764 0,250 -0.750 0.490 -0,595

0.700 -0.528 0.260 -0.722 0,340 -0.798 0.580 -0.467

0.750 -0.515 0.280 -0,746 0.370 -0.811 0.650 -0.493

0.810 -0.612 0.290 -0.737 0.400 -0.829 0.700 -0.485

0.840 -0.732 0.310 -0.724 0.410 -0.800 0,750 -0.576

0.900 -0.157 0.320 -0.720 0,430 -0.806 0.800 -0,896

0.960 -0.116 0.340 -0.731 0.440 -0.791 0.830 -0.834

0.350 -0.315"* 0.460 -0.816 0.900 -0.380

0.370 -0,724 0.490 -0.771 0.960 -0.362**

0.380 -0.803 0.500 -0.828

0.400 -0.707 0.520 -0.804

0.410 -0.765 0.540 -0.822

0.430 -0.741 0.550 -0.810

0.440 -0.689 0.580 -0.786

0.460 -0.768 0,600 -0.789

0.470 -0,750 0.610 -0.750

0.490 -0.753 0.650 0.019"*

0.500 -0.753 0.700 -0.699

0.520 -0.749 0.750 -0.726

0.530 -0.732 0.820 -0.276

0.550 -0.757 0.890 -0.301

0.560 -0.751 0.900 -0.297

0.580 -0.742 0.960 -0.240

0.590 -0.799

0,600 -0.796

0.640 -0.815

0,700 -0.855

0.750 0,031"*

0.820 -0.238

0.870 -0.250

0.930 -0.247

0.960 -0.232

Lower Surface

0.020 -0.889 0.020 -0.744 0,020 -0.284 0.020 0.192

0.110 -0.168 0.060 -0.050 0,060 0.069 0.060 0.029

0.230 0.016 0.090 -0_ 107 0,090 -0.005 0.110 0.028

0.400 -0.057 0.120 -0.056 ** 0.120 -0.268 0,250 -0.114

0.490 -0.044 0.200 0.029 0.200 -0.020 0.400 -0.188

0.630 3.636 * * 0,260 -0.123 0.250 -0.093 0.490 -0.296

0.750 0.074 0.400 -0.122 0.400 -0.170 0.580 -0.320

0.850 0.133 0_490 -0.095 0,490 0.008 0.650 -0.007

0.900 0.239 0.580 -0.055 0.580 -0.102 0,750 0.235

0.960 0.129 0.640 0.172 0,650 0.014 0.830 0.385

0.750 0.275 0.750 -0.007"* 0.900 0.453

0.870 0.349 0.890 0.405 0.960 0.305

0.930 0.265 0,930 0.316

0.960 0.163 0.960 0.798

CN = 0.467 0.602 0.641 0.608

409
Table G-2. Continued.

Flight 200, Wing sweep = 26 °, Time = 8-21-32-500, MINF = 0.903, Camber = 5/6, ALPT = 8.15, BETA = 0.17, QINF = 296.9,

RNPU = 2.2E+06, CNWP = 0.5111

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.075 0.000 0.837 0.000 0.813"* 0.010 -0.622

0.060 -0.154 0.020 -0.164 0.020 -0.085 0.020 -0.518 **

0.110 -0.324 0.040 -0.096 0.060 0,494'* 0.060 -0.617"*

0.200 -0.784 0,060 -0.346 0.090 -0.511 0.110 -0.844

0.230 -0.686 0.090 -0.409 0.110 -0.682 0.140 - 1.023

0.400 -0.675 0.130 -0.535 0.130 -0.684 0.190 - 1.752" *

0.490 -0.569 0.150 -0.696 0.150 -0.821 0.250 - 1.002

0.590 -0.605 0.200 -0.725 0.210 -0.821 0.400 -0.743

0.630 -0.538 0.250 -0.839 0.250 -0.833 0.490 -0.656

0.700 -0.593 0.260 -0.786 0.340 -0.869 0.580 -0.534

0.750 -0.448 0.280 -0.817 0.370 -0.901 0.650 -0.557

0.810 -0.483 0.290 -0.817 0.400 -0.892 0.700 -0.545

0.840 -0.608 0.310 -0.801 0.4 l0 -0.873 0.750 -0.629

0.900 -0.228 0.320 -0.797 0.430 -0.892 0.800 -0.946

0.960 -0.193 0.340 -0.791 0.440 -0,874 0.830 -0.890

0.350 -0.322** 0.460 -0.899 0.900 -0.446

0.370 -0.796 0.490 -0.842 0.960 -0.410"*

0.380 -0.863 0.500 -0.906

0.400 -0.779 0.520 -0.848

0.410 -0.843 0.540 -0,887

0.430 -0.806 0.550 -0.894

0.440 -0.769 0.580 -0.870

0.460 -0.850 0.600 -0.882

0.470 -0.825 0.610 -0.855

0.490 -0.826 0.650 0.015"*

0.500 -0_823 0.700 -0.913

0.520 -0.822 0.750 -0.882

0.530 -0.806 0.820 -0.180

0.550 -0.831 0.890 -0.340

0.560 -0.836 0.900 -0.341

0.580 -0.820 0.960 -0.286

0.590 -0.877

0.600 -0.886

0.640 -0.857

0.700 -0.423

0.750 0.030**

0.820 -0.260

0.870 -0.282

0.930 -0.287

0.960 -0.272

Lower Surface

0.020 -0.694 0,020 -0.266 0,020 -0.055 0.020 0.314

0.110 -0.160 0,060 0.040 0.060 0.151 0,060 0.091

0.230 0.050 0.090 -0.018 0.090 0.080 0.110 0.085

0.400 -0.050 0.120 0.006"* 0.120 -0.205 0.250 -0.059

0.490 -0.049 0.200 0.058 0.200 0.006 0.400 -0.127

0.630 3.659** 0.260 -0.066 0.250 -0.032 0.490 -0.220

0.750 0.059 0.400 -0.093 0.400 -0,091 0.580 -0.246

0.850 0.107 0.490 -0.085 0.490 0.014 0.650 -0.004

0.900 0.212 0.580 -0.060 0.580 -0.093 0.750 0.252

0.960 0.080 0.640 0.161 0.650 0.025 0.830 0.392

0.750 0.273 0.750 -0.011 ** 0.900 0.458

0.870 0.319 0.890 0.412 0.960 0.297

0.930 0.252 0.930 0.303

0.960 0.142 0.960 0.816

CN = 0.500 0.638 0.752 0.716

410
Table G-2, Continued.

Flight 200, Wing sweep = 26 °, Time = 8-21-41-000, MINF = 0.889, Camber = 5/6, ALPT = 9.11, BETA = 0.25, QINF = 289,3,

RNPU = 2.2E+06, CNWP = 0,5676

rl = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.084 0.000 0,897 0.000 0.819"* 0.010 -0,683

0.060 -0.342 0.020 -0.324 0.020 -0,273 0.020 -0.684**

0. 110 -0.468 0.040 -0.210 0.060 0.390** 0.060 -0.732**

0.200 -0.823 0.060 -0.511 0.090 -0.644 O. 110 -0.947

0.230 -0.741 0.090 -0.569 0,110 -0,810 0.140 -1,104

0.400 -0_754 0.130 -0.657 0.130 -0.792 0.190 - 1.808"*

0,490 -0,665 0.150 -0.820 0.150 -0.944 0.250 - 1.111

0,590 -0.656 0.200 -0.830 0.210 -0.918 0.400 -0.828

0.630 -0.592 0.250 -0.932 0.250 -0.931 0,490 -0.717

0,700 -0.654 0.260 -0,886 0.340 -0.995 0,580 -0.625

0,750 -0,299 0.280 -0,926 0,370 - 1.002 0,650 -0.625

0_810 -0,275 0.290 -0.917 0.400 -0.964 0,700 -0.625

0.840 -0.287 0.310 -0.895 0.410 -0.971 0.750 -0.693

0.900 -0,294 0.320 -0.890 0.430 -0.988 0,800 -0.846

0.960 -0,200 0.340 -0.887 0.440 -0.972 0,830 -0.846

0.350 -0.326** 0.460 -0.994 0.900 -0.396

0.370 -0,895 0.490 -0.930 0.960 -0.376**

0.380 -0.964 0.500 -0.997

0.400 -0.859 0.520 -0.972

0,410 -0,932 0.540 -0.989

0.430 -0.897 0.550 -0.974

0.440 -0,838 0.580 -0.963

0.460 -0.951 0.600 -0.987

0.470 -0.927 0.610 -0.955

0.490 -0.925 0.650 0.032**

0.500 -0.949 0.700 -0.852

0.520 -0.920 0.750 -0.608

0.530 -0.905 0.820 -0,212

0.550 -0.898 0.890 -0.408

0.560 -0,921 0.900 -0.395

0.580 -0.897 0.960 -0.335

0.590 -0.889

0.600 -0.74 I

0.640 -0.337

0200 -0,353

0.750 0,051 **

0.820 -0.273

0.870 -0.291

0.930 -0.305

0.960 -0.289

Lower Surface

0.020 -0.235 0.020 -0.002 0.020 0.110 0.020 0.448

0.110 -0,075 0.060 0.155 0.060 0,243 0.060 O. 167

0.230 0.103 0,090 0,087 0.090 0.175 0.110 O. 128

0.400 -0,020 0.120 0.094"* 0.120 -0.110 0.250 0,014

0.490 -0,015 0.200 0.110 0,200 0,072 0.400 -0.065

0.630 3.744"* 0.260 0.005 0.250 0.048 0,490 -0.128

0,750 0,061 0.400 -0.036 0.400 -0.022 0.580 -0.149

0.850 0.102 0.490 -0.047 0.490 0,035 0.650 0.024

0.900 0.210 0.580 -0.033 0.580 -0.045 0.750 0,284

0.960 0,085 0.640 0.174 0,650 0.030 0.830 0,410

0.750 0.275 0.750 -0.006"* 0.900 0.472

0.870 0,329 0.890 0.420 0.960 0.307

0.930 0.249 0.930 0.308

0.960 0.139 0.960 0.816

CN = 0,561 0.707 0,847 0.818

411
Table G-2. Continued.

Flight 204, Wing sweep = 26 °, Time = 9-33-24-000, MINF = 0.892, Camber = 5/6, ALPT = 8.25, BETA = -0.36, QINF = 269.2,

RNPU = 2.1E+06, CNWP = 0.5367

1"1-- 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 -0.029 0.000 0.893 0.000 0.995** 0.010 -0.688

0.060 -0.295 0.020 -0.244 0.020 -0.223 0.020 -0.643**

0.110 -0.453 0.040 -0.085 0.060 0.044** 0.060 -0.776**

0.200 -0.816 0.060 -0.447 0.090 -0.601 0.110 -0.932

0.230 -0.736 0.090 -0.536 0.110 -0.788 0.140 - 1.078

0.400 -0.736 0.130 -0.591 0.130 -0.773 0.190 - 1.797 * *

0.490 -0.663 0.150 -0.711 0.150 -0.941 0.250 - 1.084

0.590 -0.642 0.200 -0.735 0.210 -0.905 0.400 -0.783

0.630 -0.573 0.250 -0.925 0.250 -0.889 0.490 -0.698

0.700 -0.620 0.260 -0.816 0.340 -0.954 0.580 -0.626

0.750 -0.335 0.280 -0.900 0.370 -0.955 0.650 -0.617

0.810 -0.345 0.290 -0.895 0.400 -0.930 0.700 -0.604

0.840 -0.376 0.310 -0.866 0.410 -0.942 0.750 -0.681

0.900 -0.248 0.320 -0.863 0.430 -0.980 0.800 -0.933

0.960 -0.208 0.340 -0.856 0.440 -0.943 0.830 -0.931

0.350 -0.323** 0.460 -0.711 0.900 -0.426

0.370 -0.857 0.490 -0.933 0.960 -0.387**

0.380 -0.941 0.500 -0.978

0.400 -0.802 0.520 -0.934

0.410 -0.909 0.540 -0.958

0.430 -0.894 0.550 -0.952

0.440 -0.820 0.580 -0.958

0.460 -0.944 0.600 -0.938

0.470 -0.882 0.610 -0.937

0.490 -0.891 0.650 0.051 **

0.500 -0.875 0.700 -1.014

0.520 -0.886 0.750 -0.717

0.530 -0.864 0.820 -0.181

0.550 -0.845 0.890 -0.368

0.560 -0.874 0.900 -0.373

0.580 -0.868 0.960 -0.298

0.590 -0.926

0.600 -0.934

0.640 -0.356

0.700 -0.348

0.750 0.062**

0.820 -0.249

0.870 -0.266

0.930 -0.284

0.960 -0.271

Lower Surface

0.020 -0.329 0.020 -0.066 0.020 0.082 0.020 0.416

0.110 -0.1 04 0.060 0.136 0.060 0.246 0.060 0.027

0.230 0.101 0.090 0.053 0.090 0.187 0.110 0.114

0.400 -0.022 0.120 0.072"* 0.120 -0.167 0.250 -0.001

0.490 -0.025 0.200 0.109 0.200 0.158 0.400 -0.071

0.630 5.529** 0.260 -0.028 0.250 0.030 0.490 -0.163

0.750 0.064 0.400 -0.035 0.400 -0.04 1 0.580 -0.184

0.850 0.121 0.490 -0.052 0.490 0.041 0.650 0.016

0.900 0.218 0.580 -0.049 0.580 -0.057 0.750 0.261

0.960 0.085 0.640 0.190 0.650 0.056 0.830 0.411

0.750 0.267 0.750 0.008** 0.900 0.472

0.870 0.331 0.890 0.386 0.960 0.302

0.930 0.246 0.930 0.305

0.960 0.152 0.960 0.311

CN = 0.552 0.672 0.811 0.791

412
Table G-2. Continued.

Flight 204, Wing sweep = 26 °. Time = 9-35-23-500, MINF = 0.901, Camber = 5/6, ALPT = 9.27, BETA = -0.21, QINF = 275.9,

RNPU = 2.1E+06, CNWP = 0.5518

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.086 0.000 0.899 0.000 0.873** 0,010 -0,672

0.060 -0.342 0.020 -0.426 0.020 -0.30l 0.020 -0.741 **

0.110 -0.477 0.040 -0.142 0.060 -0.030"* 0,060 -0.826* *

0.200 -0.874 0.060 -0.475 0.090 -0.654 0.110 -0,975

0.230 -0.761 0.090 -0.593 0.1 l0 -0.825 0.140 -1.104

0.400 -0.749 0.130 -0.642 0.130 -0.803 0.190 - 1.761 **

0.490 -0.678 0.150 -0.757 0.150 -0.959 0.250 - 1.112

0.590 -0.674 0.200 -0.771 0.210 -0.937 0.400 -0.817

0.630 -0.607 0.250 -0,946 0,250 -0.922 0.490 -0.724

0.700 -0.661 0.260 -0.856 0.340 -0.987 0.580 -0.668

0.750 -0.405 0.280 -0.920 0.370 -0.989 0.650 -0.647

0.810 -0.398 0.290 -0.929 0.400 -0.979 0.700 -0.634

0.840 -0.463 0.310 -0.896 0.410 -0.967 0,750 -0.699

0.900 -0.338 0.320 -0.890 0.430 -0.995 0.800 -0.979

0.960 -0.341 0.340 -0.888 0.440 -0.977 0.830 -0.961

0.350 -0.332** 0.460 -0.747 0.900 -0.517

0.370 -0.883 0,490 -0.909 0.960 -0.453**

0.380 -0.966 0,500 - 1.008

0.400 -0.841 0.520 -0.934

0.410 -0.935 0.540 -0.987

0.430 -0.921 0.550 -0.979

0.,:t40 -0.853 0.580 -0.977

0.460 -0.982 0.600 -0.965

0.470 -0.905 0.610 -0.967

0.490 -0.918 0.650 0.032**

0.500 -0.912 0.700 -1.061

0.520 -0.938 0.750 -0.678

0.530 -0.900 0.820 -0.250

0.550 -0.907 0.890 -0.486

0.560 -0.916 0.900 -0.473

0.580 -0,899 0.960 -0.390

0.590 -0.961

0.600 -0.966

0.640 -0.363

0.700 -0.366

0.750 0.046"*

0.820 -0.286

0.870 -0.314

0.930 -0.324

0.960 -0.319

Lower Surface

0.020 -0.228 0.020 0.046 0.020 0.142 0.020 0.480

O. 110 -0.088 0.060 O. 188 0.060 0.288 0.060 0.004

0.230 O. 109 0.090 0.093 0.090 0.225 O.1 l 0 O. 122

0.400 -0.024 O. 120 0.099 ** O. 120 -0. t 30 0.250 0.019

0.490 -0.055 0,200 0.1 ! 9 0.200 0.161 0.400 -0.053

0.630 5.390"* 0,260 -0.011 0.250 0.051 0.490 -0.142

0.750 0.040 0A00 -0.029 0.400 -0.036 0,580 -0.186

0.850 0.083 0.490 -0.061 0.490 0.025 0,650 0.009

0.900 0.175 0.580 -0.042 0.580 -0.059 0.750 0,263

0.960 0.011 0.640 0.171 0.650 0.032 0.830 0.401

0.750 0.260 0.750 -0.007 * * 0,900 0.464

0.870 0.316 0.890 0.393 0,960 0.288

0.930 0.237 0.930 0.291

0.960 0,146 0.960 0.316

CN = 0.579 0.714 0.851 0.831

413
Table G-2. Continued.

Hight 204, Wing sweep = 26 °, Time = 9-35-34-500, MINF = 0.894, Camber = 5/6, ALPT = 12.19, BETA = 0.51, QINF = 292.8,

RNPU = 2.2E+06, CNWP = 0.4976

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.649 0.000 0.865 0.000 0.875** 0.010 -0.944

0,060 -0.655 0.020 -0.897 0.020 -0.746 0.020 - 1.002"*

0,110 -0.834 0.040 -0.531 0.060 -0.075 ** 0.060 - 1.047"*

0.200 -0.994 0.060 -0.740 0.090 -0.895 0.110 - I. 194

0.230 -0.885 0.090 -0.843 0.110 - 1.053 0.140 - 1.295

0.400 -0.907 0.130 -0.873 0.130 - 1.04 1 0.190 - 1.788"*

0.490 -0.809 0.150 -0.970 0.150 - 1.148 0.250 - 1.335

0.590 -0.595 0.200 -0.984 0.210 -1.137 0.400 - 1.030

0.630 -0.551 0.250 -1.128 0.250 - 1.108 0.490 -0.910

0.700 -0.419 0.260 -1.021 0.340 -1.169 0.580 -0.791

0.750 -0,404 0.280 -1.091 0.370 -1.139 0.650 -0.747

0.810 -0.437 0.290 - 1.082 0.400 - 1.128 0.700 -0.684

0.840 -0.460 0.310 - 1.049 0.410 -1.080 0.750 -0.650

0.900 -0.417 0.320 - 1.029 0.430 - 1.038 0.800 -0.720

0.960 -0.449 0.340 -0.967 0.440 -0.943 0.830 -0.625

0.350 -0.242** 0.460 -0.617 0.900 -0.542

0.370 -0.872 0.490 -0.67 l 0.960 -0_448"*

0.380 -0.857 0.500 -0.705

0.400 -0.645 0.520 -0.658

0.410 -0.644 0.540 -0.678

0.430 -0.614 0.550 -0.675

0.440 -0.561 0.580 -0.688

0.460 -0.639 0.600 -0.643

0.470 -0.588 0.610 -0.634

0.490 -0.584 0.650 -0.012"*

0.500 -0.568 0.700 -0.603

0.520 -0.588 0.750 -0.682

0.530 -0.555 0.820 -0.299

0.550 -0.574 0.890 -0.546

0.560 -0.543 0.900 -0.522

0.580 -0.533 0.960 -0,451

0.590 -0.582

0.600 -0.552

0.640 -0.477

0,700 -0.509

0.750 0.044**

0.820 -0.478

0,870 -0.432

0,930 -0.447

0.960 -0.430

Lower Surface

0.020 0.140 0,020 0.462 0.020 0.462 0.020 0.748

0.110 0.066 0.060 0.403 0.060 0.502 0.060 -0.066

0.230 0.188 0.090 0.295 0.090 0,420 0,110 0.340

0.400 0.04 1 0.120 0.271 ** 0. t 20 0.068 0.250 0.172

0.490 0.015 0.200 0.200 0.200 0.241 0.400 0.082

0.630 4.949** 0.260 0.127 0.250 0.207 0.490 -0.005

0.750 0.054 0.400 0.081 0.400 0.084 0.580 -0.050

0.850 0.083 0.490 0.024 0.490 0.021 0.650 0.088

0.900 0.163 0.580 0.020 0.580 0.006 0.750 0.321

0.960 -0.019 0.640 0.215 0.650 0.027 0.830 0.445

0,750 0.288 0.750 -0.061 ** 0.900 0.494

0.870 0.337 0.890 0.420 0.960 0.296

0.930 0.255 0.930 0.303

0.960 0.143 0.960 0.272

CN = 0.720 0.846 0.922 1.026

414
Table G-2. Continued.

Flight 198_ Wing sweep = 26 °, Time = 14-4-42-500, MINF = 0,898, Camber = 10/2, ALPT = 5,99, BETA = 0,05, QINF = 292.9,

RNPU = 2.2E+06, CNWP = 0.3341

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.570 0.000 0.311 0.000 -5.562"* 0010 0.322**

0.060 O. 1O0 0.020 0.344" * 0.020 0.569"* 0.020 O,233" *

0.110 -0.193 0.040 0.355 0.060 -0.832** 0.060 -0,333

0.200 -0.956 0.060 -0.006 0.090 -0.190 0.110 -0.619

0.230 -0,868 0.090 -0.185 0.110 -0.496 0.140 1,890"*

0.400 -0.694 0.130 -0.433 0.130 -0.671 0,190 -5.427"*

0.490 -0.570 0,150 -0.721 0.150 -0.833 0.250 -0,920

0,590 -0.519 0.200 -0.763 0.210 -0.880 0.400 -0.643

0.630 -0.204 0.250 -0.878 0.250 -0.824 0.490 -0,537

0.700 -0,071 0,260 -0.752 0.340 -0.851 0.580 -0.459

0,750 -0.115 0.280 -0.835 0.370 -0.831 0.650 -0.454

0.810 -0.165 0,290 -0.820 0.400 -0.872 0,700 -0.452

0.840 -0,109 0.310 -0.762 0.410 -0.800 0,750 -0.533

0.900 -0.056 0.320 -0.745 0.430 -0.848 0.800 -0.717

0,960 0.015 0.340 -0.783 0.440 -0.810 0,830 -0.678

0.350 -0.396"* 0.460 -0.823 0.900 -0,136

0.370 -0,747 0.490 -0.731 0.960 -0,078

0.380 -0.779 0.500 -0.853

0.400 -0,681 0.520 -0.810

0.410 -0.803 0.540 -0.822

0.430 -0.771 0,550 -0.786

0.440 -0706 0.580 -0.719

0.460 -0.867 0.600 -0.633

0.470 -0.794 0.610 -0.507

0.490 -0.752 0.650 -2.637**

0,500 -0,735 0.700 -0.530

0,520 -0.744 0.750 -0.596

0.530 -0.729 0,820 -0.456

0.550 -0.758 0.890 -0.057

0,560 -0.756 0.900 -0,039

0.580 -0.732 0,960 0.005

0.590 -0.763

0.600 -0.833

0.640 -2.471 **

0.700 -0.849

0.750 -0.207

0.820 -2.649 * *

0.870 -0.049

0.930 0.014

0.960 0.054

Lower Surface

0.020 -0_948 0.020 - 1,171 0.020 - 1.265 0,020 -0.646

0.110 -0,602 0.060 -0.670 0,060 -0.290 0.060 3,473**

0.230 -0.063 0.090 -0.539 0.090 -0.183 0.110 -0.129

0,400 -0.004 0.120 -0.353 0.120 -0.453 0.250 -0.155

0.490 -0.061 0.200 -0.043 0.200 -0.162 0.400 -0.232

0,630 3.518"* 0.260 -0,206 0.250 -0,136 0.490 -0A05

0.750 0.048 0A00 -2.667** 0.400 -0.269 0.580 -0.500

0.850 0,136 0.490 -0.132 0.490 -0,029 0.650 -0.225

0.900 0,166 0.580 -0.040 0.580 -0,195 0.750 0.110

0.960 0.146 0.640 0.296 0,650 0.033 0.830 0.252

0.750 0.156 0,750 -0.008 0.900 0.343

0.870 0.212 0.890 ******** 0.960 0.247

0.930 0.227 0.930 0.239

0.960 0.171 0.960 -2.666**

CN = 0.303 0.440 0.470 0437

415
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-4-46-000, MINF = 0.898, Camber = 10/2, ALPT = 6.04, BETA = -0.16, QINF = 293.1,

RNPU = 2.2E+06, CNWP = 0.3421

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0,570 0.000 0,315 0,000 -5.558** 0.010 0.322**

0.060 0.062 0.020 0,364** 0.020 0.569** 0.020 0.244**

0.110 -0.192 0.040 0.359 0.060 -0.838"* 0.060 -0.333

0.200 -0,942 0,060 0.010 0,090 -0.206 0.110 -0.618

0.230 -0,839 0.090 -0.194 0.110 -0.496 O. 140 1.901 **

0,400 -0.709 0.130 -0.440 0.130 -0.683 0.190 -5.423 * *

0.490 -0.570 0.150 -0.717 O. 150 -0.832 0.250 -0.919

0.590 -0.531 0.200 -0,762 0,210 -0.889 0.400 -0.636

0.630 -0,242 0.250 -0.878 0.250 -0,824 0.490 -0.541

0,700 -0.075 0.260 -0.765 0,340 -0.851 0.580 -0.480

0.750 -0.115 0,280 -0.835 0,370 -0,846 0.650 -0,462

0.810 -0.157 0.290 -0.829 0,400 -0.856 0.700 -0.463

0.840 -0.109 0.310 -0,764 0.410 -0,800 0,750 -0.525

0.900 -0,053 0.320 -0,749 0.430 -0.847 0.800 -0.724

0.960 0.008 0.340 -0.789 0.440 -0.820 0,830 -0.678

0,350 -0,380"* 0.460 -0.829 0.900 -0,146

0,370 -0.750 0.490 -0.738 0,960 -0,086

0,380 -0.769 0.500 -0.852

0.400 -0.691 0.520 -0,809

0.410 -0.802 0.540 -0,836

0,430 -0.782 0.550 -0,798

0.440 -0,696 0.580 -0.718

0,460 -0.866 0.600 -0,658

0,470 -0.774 0.610 -0.535

0,490 -0.755 0,650 -2,635**

0.500 -0.751 0,700 -0.551

0.520 -0,751 0,750 -0.610

0.530 -0.732 0.820 -0.447

0,550 -0.767 0.890 -0.061

0.560 -0.755 0.900 -0.039

0,580 -0.738 0,960 -0.006

0.590 -0.766

0.600 -0.823

0.640 -2.470**

0,700 -0,845

0.750 -0.203

0.820 -2.647**

0,870 -0.067

0,930 -0.013

0.960 0.021

Lower Surface

0,020 -0,883 0.020 - 1.111 0.020 - 1.256 0,020 -0.639

O. 110 -0.616 0.060 -0.730 0.060 -0.303 0.060 3.471 **

0.230 -0.063 0,090 -0.535 0,090 -0.178 0.110 -0.129

0.400 -0.076 0.120 -0.337 0.120 -0.453 0,250 -0.155

0.490 -0,075 0,200 -0,043 0.200 -0.154 0,400 -0,232

0.630 3.515 ** 0,260 -0.176 0.250 -0.136 0,490 -0,405

0.750 0.044 0.400 -2.665"* 0,400 -0,259 0.580 -0.510

0.850 0.136 0.490 -0.140 0,490 -0.028 0.650 -0.240

0,900 O. 169 0.580 -0.055 0.580 -0.199 0.750 0.110

0.960 0.171 0.640 0.283 0.650 0.026 0.830 0.260

0.750 0.156 0.750 -0.008 0.900 0,349

0.870 0.221 0.890 ****"*** 0,960 0.253

0.930 0.238 0,930 0.231

0,960 0.159 0.960 -2,664**

CN = 0.292 0,442 0.475 0.439

416
Table G-2. Continued.

Flight 198, Wing sweep = 26", Time = 14-5-4-500, MINF = 0.903, Camber = 10/2, ALPT = 6.92, BETA = 0.23, Q1NF = 294.5,

RNPU = 2.2E+06, CNWP = 0.3829

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.553 0.000 0.402 0.000 -5.521 ** 0,010 0.245**

0.060 0.082 0,020 0.313"* 0.020 0.536"* 0.020 0.199"*

0.110 -0.193 0,040 0.330 0.060 -0.850* * 0.060 -0.444

0.200 -0.969 0.060 -0.042 0.090 -0.233 0.110 -0.686

0.230 -0.862 0.090 -0.205 0.110 -0.502 0.140 1.902"*

0.400 -0.718 0.130 -0.447 0.130 -0.695 0.190 -5.386"*

0.490 -0.612 0.150 -0.723 0.150 -0.844 0.250 -0.948

0.590 -0.568 0.200 -0.771 0.210 -0.909 0.400 -0.651

0.630 -0,506 0.250 -0.890 0.250 -0.847 0.490 -0,630

0.700 -0.110 0.260 -0.779 0.340 -0.899 0.580 -0,522

0.750 -0.093 0.280 -0.857 0.370 -0.872 0.650 -0.497

0.810 -0, 143 0.290 -0.856 0.400 -0.864 0.700 -0.483

0.840 -0.090 0.310 -0.804 0.410 -0.826 0.750 -0.580

0.900 -0.060 0.320 -0.775 0.430 -0,880 0.800 -0.747

0.960 -0.004 0.340 -0.826 0.440 -0.858 0.830 -0.708

0.350 -0.405** 0.460 -0.872 0.900 -0.163

0,370 -0.773 0.490 -0.806 0.960 -0.118

0.380 -0.796 0.500 -0.887

0.400 -0.711 0.520 -0.848

0.410 -0.831 0.540 -0.879

0.430 -0.831 0,550 -0.862

0.440 -0.725 0.580 -0.821

0.460 -0.901 0.600 -0.834

0.470 -0.806 0.610 -0.736

0.490 -0.803 0.650 -2.612**

0.500 -0.786 0.700 -0.727

0,520 -0.792 0.750 -0.759

0.530 -0.764 0.820 -0.282

0.550 -0.798 0.890 -0.097

0.560 -0.792 0,900 -0.082

0.580 -0.772 0.960 -0.052

0.590 -0.796

0.600 -0.853

0.640 -2.448**

0.700 -0.294

0.750 -0.177

0.820 -2.624**

0.870 -0.171

0,930 -0.129

0.960 -0.119

Lower Surface

0.020 -0.877 0.020 - 1,182 0,020 - 1.127 0.020 -0.405

O. 1 l 0 -0.589 0.060 -0.479 0.060 -0.191 0.060 3.464"*

0.230 -0.04 1 0.090 -0,328 0.090 -0.076 0.110 0.006

0.400 -0.046 0.120 -0.190 0.120 -0.385 0.250 -0.090

0,490 -0.095 0.200 -0.022 0.200 -0.137 0,400 -0.191

0.630 3,508"* 0.260 -0.143 0.250 -0.073 0.490 -0.362

0.750 0.019 0.400 -2.642"* 0.400 -0.211 0.580 -0.482

0.850 0.111 0.490 -0.145 0.490 -0.026 0.650 -0.290

0.900 0.150 0.580 -0.074 0.580 -0.199 0.750 0.129

0.960 0.15 l 0.640 0.266 0.650 0.017 0.830 0.278

0.750 0.127 0.750 -0.002 0.900 0.357

0,870 0.165 0.890 ******** 0.960 0.256

0,930 0.177 0.930 0.232

0.960 0.075 0.960 -2.641 **

CN = 0.317 0.446 0.546 0.516

417
Table G-2. Continued.

Flight 198, Wing sweep = 26 °. Time = 14-5-13-500, MINF = 0.902, Camber = 10/2, ALPT = 7.95, BETA = 0.57, QINF = 294.6,

RNPU = 2.2E+06, CNWP = 0.4405

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.492 0.000 0.514 0.000 -5.524" * 0.010 0.111 **

0.060 0.030 0.020 0.268** 0.020 0.441 ** 0.020 0.087**

0.110 -0.244 0.040 0.255 0.060 -0.874"* 0.060 -0.519

0.200 -0.998 0.060 -0.095 0.090 -0.291 0. l 10 -0.791

0.230 -0.943 0.090 -0.267 0.110 -0.572 0.140 1.890**

0.400 -0.769 0.130 -0.511 0.130 -0.748 0.190 -5.389"*

0.490 -0.680 0.150 -0.776 0.150 -0.899 0.250 - 1.054

0.590 -0.637 0.200 -0.826 0.210 -0.956 0.400 -0.732

0.630 -0.556 0.250 -0.961 0.250 -0.910 0.490 -0.697

0.700 -0.168 0.260 -0.839 0.340 -0.967 0.580 -0.612

0.750 -0.145 0.280 -0.925 0.370 -0.925 0.650 -0.548

0.810 -0.197 0.290 -0.929 0.400 -0.950 0.700 -0.574

0.840 -0.141 0.310 -0.858 0.410 -0.905 0.750 -0.636

0.900 -0.113 0.320 -0.845 0.430 -0.978 0.800 -0.780

0.960 -0.053 0.340 -0.887 0.440 -0.926 0.830 -0.764

0.350 -0.404** 0.460 -0.955 0.900 -0.224

0.370 -0.848 0.490 -0.871 0.960 -0.173

0.380 -0.878 0.500 -0.970

0.400 -0.782 0.520 -0.905

0.410 -0,898 0.540 -0.953

0.430 -0.893 0.550 -0.940

0.440 -0.805 0.580 -0.941

0.460 -0,978 0.600 -0.910

0.470 -0.884 0.610 -0.841

0.490 -0.863 0.650 -2.615 * *

0.500 -0.867 0.700 -0.954

0.520 -0.889 0.750 -0.954

0.530 -0.842 0.820 -0.333

0.550 -0.866 0.890 -0.204

0.560 -0.866 0.900 -0.230

0.580 -0.843 0.960 -0.189

0.590 -0.839

0.600 -0.724

0.640 -2.451 **

0.700 -0.317

0.750 -0.218

0.820 -2.628**

0.870 -0.219

0.930 -0.216

0,960 -0.232

Lower Surface

0.020 -0.753 0.020 - 1.014 0.020 -0.638 0.020 -0.165

0.110 -0.423 0.060 -0.141 0.060 0.052 0.060 3.458"*

0.230 -0.027 0.090 -0.141 0.090 0.042 0.110 0.042

0.400 -0.059 0.120 -0.037 0.120 -0.296 0.250 -0.031

0.490 -0.137 0.200 -0.012 0.200 -0.121 0.400 -0.121

0.630 3.502** 0.260 -0.074 0.250 -0.032 0.490 -0.299

0.750 -0.039 0.400 -2.646"* 0.400 -0.149 0.580 -0.399

0.850 0.060 0.490 -0.153 0.490 -0.023 0.650 -0.169

0.900 0.121 0.580 -0.112 0.580 -0.241 0.750 0.134

0.960 0.100 0.640 0,245 0.650 -0.021 0.830 0.267

0.750 0.118 0.750 -0.006 0.900 0.358

0.870 0.179 0.890 ******** 0.960 0.245

0.930 0.113 0.930 0.212

0.960 0.022 0.960 -2.644**

CN = 0.367 0.526 0.665 0.635

418
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-5-20-500, MINF = 0.898, Camber = 10/2, ALPT = 7.99, BETA = 0.52, QINF = 293.8,

RNPU = 2.2E+06, CNWP = 0.4551

r I = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP y./c CP

0.020 0.493 0.000 0.509 0.000 -5.549* * 0.010 0.107 * *

0,060 0.002 0.020 0.255** 0.020 0.441 ** 0.020 O. 104**

O. 110 -0,216 0.040 0.261 0.060 -0,930 ** 0.060 -0.536

0.200 - 1.008 0.060 -0,089 0.090 -0.264 O. 110 -0.807

0.230 -0.901 0.090 -0.271 O. 110 -0.592 O. 140 1.908**

0.400 -0.773 0.130 -0.513 0.130 -0.757 0.190 -5.413"*

0.490 -0,668 0.150 -0.780 0.150 -0.904 0.250 - 1.073

0.590 -0.633 0.200 -0,822 0.210 -0.963 0.400 -0.729

0.630 -0.521 0,250 -0.985 0.250 -0.914 0.490 -0.688

0.700 -0.143 0.260 -0.842 0.340 -0.978 0.580 -0.608

0.750 -0.162 0.280 -0,937 0.370 -0.937 0.650 -0.566

0.810 -0.199 0.290 -0.935 0,400 -0,947 0.700 -0.580

0.840 -0.135 0.310 -0,860 0.410 -0.906 0.750 -0.632

0.900 -0.107 0.320 -0.850 0.430 -0.975 0.800 -0.783

0.960 -0.062 0.340 -0.890 0.440 -0.944 0.830 -0.769

0.350 -0.410"* 0.460 -0.961 0,900 -0.209

0.370 -0.848 0.490 -0.830 0.960 -0.159

0.380 -0.883 0.500 -0.976

0.400 -0.800 0.520 -0.937

0.410 -0.901 0.540 -0.979

0.430 -0.890 0,550 -0.937

0.440 -0.819 0.580 -0.920

0.460 -0.990 0.600 -0.940

0.470 -0.921 0.610 -0.851

0.490 -0.868 0.650 -2.632**

0.500 -0.874 0.700 -0.976

0.520 -0.862 0.750 -0.759

0.530 -0.849 0.820 -0.341

0,550 -0.871 0.890 -0.211

0.560 -0.869 0.900 -0.230

0.580 -0.840 0.960 -0.179

0.590 -0.809

0.600 -0.615

0.640 -2,467 * *

0.700 -0.286

0,750 -0.231

0.820 -2.645"*

0,870 -0.254

0.930 -0.237

0.960 -0.207

Lower Surface

0.020 -0.721 0.020 - 1.010 0.020 -0.618 0.020 -0.170

O. 110 -0.425 0.060 -0.146 0.060 0.058 0.060 3.459"*

0.230 -0,017 0.090 -0,123 0.090 0.043 O. 110 0.028

0.400 -0.064 O. 120 -0.023 O.120 -0.299 0.250 -0.043

0.490 -0.124 0.200 -0.006 0.200 -0.130 0.400 -0.130

0.630 3.503** 0.260 -0.075 0.2:30 -0.011 0.490 -0.293

0.750 -0.030 0.400 -2.662 * * 0.400 -0.143 0.580 -0.419

0,850 0.070 0,490 -0.151 0.490 -0.032 0.650 -0.167

0.900 0.124 0,580 -0.118 0.580 -0.243 0.750 0.141

0.960 0.115 0.640 0,258 0.650 0.000 0.830 0.274

0.750 0.101 0.750 -0.015 0.900 0.351

0.870 0.157 0.890 ******** 0.960 0.252

0.930 0,123 0.930 0.218

0.960 0.028 0.960 -2.661 **

CN = 0.364 0.521 0.664 0.633

419
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-5-35-500, MINF = 0.900. Camber = 10/2, ALPT = 9.05, BETA = 0.76, QINF = 297.3,

RNPU = 2.3E+06, CNWP = 0.4444

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.454 0.000 0,602 0.000 -5.498 ** 0.010 -0.023 * *

0.060 -0.050 0.020 0.139"* 0.020 0.346** 0.020 0.028**

0.110 -0.294 0.040 0.173 0.060 -0,965"* 0.060 -0.605

0.200 - 1.023 0.060 -0.181 0,090 -0.409 0.110 -0.892

0.230 -0,947 0,090 -0.329 0.110 -0.640 0.140 1.879**

0,400 -0.810 0.130 -0,575 0.130 -0.797 0.190 -5.364"*

0.490 -0,734 0.150 -0.812 0.150 -0,944 0,250 - 1.140

0.590 °0.433 0.200 -0.863 0.210 - 1.014 0,400 -0.811

0.630 -0,377 0,250 - 1.027 0.250 -0.962 0.490 -0.728

0.700 -0.236 0,260 -0,881 0.340 - 1.014 0.580 -0.675

0,750 -0.219 0,280 -0.966 0.370 -0.982 0,650 -0.600

0.810 -0.243 0.290 -0.978 0.400 - 1.009 0.700 -0.648

0.840 -0.180 0.310 -0.911 0.410 -0.959 0,750 -0.673

0.900 -0.191 0.320 -0.893 0,430 - 1.041 0.800 -0.825

0.960 -0,141 0.340 -0.943 0,440 -1.006 0.830 -0,804

0.350 -0.405"* 0.460 -1.019 0.900 -0,263

0,370 -0,900 0.490 -0.946 0.960 -0.187

0.380 -0.927 0.500 - 1.048

0.400 -0,846 0.520 - 1.011

0.410 -0.956 0.540 - 1.016

0.430 -0.939 0.550 - 1.001

0,440 -0.855 0.580 - 1.016

0,460 - 1.051 0,600 -0.997

0,470 -0.942 0.610 -0.912

0.490 -0.924 0,650 -2.616 * *

0.500 -0.929 0.700 -0,579

0.520 -0.929 0.750 -0,580

0.530 -0,697 0.820 -0.463

0.550 -0.521 0.890 -0,390

0.560 -0.413 0.900 -0,384

0.580 -0.391 0.960 -0,344

0.590 -0.395

0.600 -0.412

0.640 -2,453**

0.700 -0.331

0,750 -0.302

0.820 -2.628**

0.870 -0,295

0.930 -0,286

0.960 -0,276

Lower Surface

0,020 -0.621 0,020 -0.574 0,020 -0.453 0,020 0,025

0.110 -0.171 0.060 0.016 0.060 0.189 0.060 3.403"*

0.230 0.002 0.090 -0.001 0.090 0.133 0.110 0.130

0.400 -0.060 0.120 0.082 0.120 -0,209 0.250 0.017

0,490 -0.145 0.200 0.019 0.200 -0.087 0,400 -0.085

0,630 3.446** 0,260 -0.024 0.250 0,041 0,490 -0.245

0.750 -0.064 0.400 -2.646** 0.400 -0.101 0.580 -0.369

0,850 0.011 0.490 -0.139 0.490 -0.017 0.650 -0.120

0,900 0,065 0.580 -0.121 0.580 -0.233 0.750 0.1 44

0,960 0.038 0.640 0,242 0.650 -0.011 0.830 0.279

0.750 0.122 0.750 -0.012 0.900 0.373

0.870 0.131 0.890 ******** 0.960 0,248

0.930 0,088 0,930 0.200

0.960 0.001 0,960 -2.645 * *

CN = 0.408 0.557 0.712 0,733

420
Table G-2. Continued.

Flight 198, Wing sweep = 26", Time = 14-5-41-000, M1NF = 0.901, Camber = 10/2, ALPT = 10.08, BETA = 0.21, QINF = 301.9,

RNPU = 2.3E+06, CNWP = 0.4682

TI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.364 0.000 0.681 0.000 -5.435** 0.010 -0.080"*

0.060 -0.1 O0 0.020 0.069** 0.020 0.215"* 0.020 -0.082"*

0. 110 -0.351 0.040 0.090 0.060 -0.962** 0.060 -0.695

0,200 - 1.065 0.060 -0.260 0.090 -0.512 0.110 -0.947

0.230 -0.957 0.090 -0,403 0.110 -0.729 0.140 1.834**

0.400 -0.863 0.130 -0.615 0.130 -0.874 0.190 -5.303 * *

0.490 -0.504 0.150 -0.868 0.150 - 1.018 0.250 - 1.228

0.590 -0.382 0.200 -0.915 0.210 - 1.064 0.400 -0.879

0.630 -0.365 0.250 - 1.053 0.250 - 1.018 0.490 -0.788

0.700 -0.286 0.260 -0.934 0,340 - 1.081 0.580 -0.712

0.750 -0.301 0.280 - 1.027 0.370 - 1.051 0.650 -0.646

0.810 -0.323 0.290 - 1.040 0.400 - 1.057 0.700 -0.686

0.840 -0.272 0.310 -0.968 0.410 - 1.027 0.750 -0.715

0.900 -0.265 0.320 -0.950 0.430 - 1.092 0.800 -0.832

0.960 -0,285 0.340 - 1.004 0.440 - 1.048 0,830 -0.824

0.350 -0.414'* 0,460 - 1.075 0.900 -0.273

0.370 -0.960 0.490 -0.995 0.960 -0.152

0.380 -0.981 0.500 -1.090

0,400 -0.881 0.520 - 1.046

0.410 - 1.014 0.540 - 1.068

0.430 -0.989 0.550 -1.052

0.440 -0.905 0.580 - 1.023

0.460 - 1.074 0.600 -0.876

0,470 -0,830 0.610 -0.674

0.490 -0.658 0.650 -2.596**

0.500 -0.559 0.700 -0.522

0.520 -0.542 0.750 -0.623

0.530 -0.468 0.820 -0.535

0.550 -0.473 0.890 -0.465

0.560 -0.443 0.900 -0.454

0.580 -0.436 0.960 -0.438

0.590 -0.445

0.600 -0.464

0.640 -2.436**

0.700 -0.400

0.750 -0.338

0.820 -2.608**

0.870 -0.334

0.930 -0.345

0.960 -0.328

Lower Surface

0.020 -0.734 0.020 -0.242 0.020 -0.078 0.020 0.242

0.110 -0.027 0.060 0.151 0.060 0.275 0.060 3.332**

0.230 0.027 0.090 0.091 0.090 0.195 0.110 0.163

0.400 -0.090 0.120 0.135 0.120 -0.159 0.250 0.072

0.490 -0.148 0.200 0.036 0.200 -0.057 0.400 -0.023

0.630 3.375"* 0.260 0.030 0.250 0.086 0.490 -0.187

0.750 -0.094 0,400 -2.626"* 0.400 -0.055 0,580 -0.328

0.850 -0.028 0.490 -0.119 0.490 -0.015 0.650 -0.116

0.900 0.027 0.580 -0.120 0.580 -0.213 0.750 0.141

0.960 -0.024 0.640 0.230 0.650 -0.013 0,830 0,292

0.750 0.103 0.750 -0.006 0.900 0.362

0,870 0.138 0.890 ******** 0.960 0.236

0.930 0.081 0,930 0.181

0.960 -0,022 0.960 -2.624**

CN = 0.429 0.606 0.766 0.805

421
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-5-53-500. MINF = 0.896, Camber = 10/2, ALPT = 11.04, BETA = 0.26, QINF = 307.8,

RNPU = 2.3E+06, CNWP = 0.3301

rl = 093 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.304 0.000 0.773 0.000 -5,386"* 0,010 -0.262**

0.060 -0.133 0.020 -0.064"* 0.020 0.125"* 0.020 -0.162"*

0.110 -0.446 0.040 0,030 0.060 - 1.073" * 0.060 -0.763

0,200 - 1.075 0.060 -0,329 0.090 -0.604 0. l 10 - 1.024

0.230 -1.010 0,090 -0.517 0.110 -0.811 0.140 -1,225"*

0.400 -0.867 0.130 -0.681 0.130 -0.953 0.190 -5.257"*

0.490 -0,465 0.150 -0.920 0.150 - 1.062 0.250 - 1.288

0,590 -0.400 0.200 -0.967 0.210 - 1.125 0.400 -0.954

0.630 -0.383 0.250 - 1.108 0.250 - 1.096 0.490 -0.873

0.700 -0.340 0.260 -0,995 0.340 - |. 149 0.580 -0.708

0.750 -0.331 0,280 - 1.090 0.370 - 1.099 0.650 -0.600

0.810 -0.349 0.290 - 1.090 0.400 - 1.021 0.700 -0.624

0.840 -0.295 0.310 - 1.031 0.410 -0,747 0.750 -0.594

0.900 -0.300 0.320 -1.017 0.430 -0.710 0,800 -0.530

0.960 -0.272 0,340 -0.970 0.440 -0,643 0.830 -0.521

0.350 -0,365** 0.460 -0.639 0,900 -0.383

0.370 -0.651 0.490 -0.566 0,960 -0.276

0.380 -0.626 0.500 -0.646

0.400 -0.535 0.520 -0.587

0,410 -0.612 0.540 -0.599

0.430 -0,600 0.550 -0.597

0,440 -0.519 0.580 -0,606

0.460 -0,657 0,600 -0,584

0,470 -0.547 0_610 -0.490

0.490 -0.536 0.650 -2.602"*

0.500 -0,526 0.700 -0.511

0,520 -0.516 0,750 -0,589

0.530 -0.485 0.820 -0.512

0.550 -0.524 0.890 -0,470

0.560 -0.496 0.900 -0,459

0.580 -0.472 0.960 -0.464

0.590 -0.491

0.600 -0,520

0.640 -2.445"*

0,700 -0,437

0.750 -0.376

0,820 -2.614"*

0.870 -0.379

0.930 -0,384

0,960 -0.353

Lower Surface

0.020 -0.462 0.020 -0.016 0.020 0.046 0.020 0,375

0.110 0.001 0.060 0.250 0.060 0.348 0.060 3.212"*

0.230 0.053 0.090 0.165 0,090 0.267 0.110 0.231

0,400 -0.069 0.120 0.206 0.120 -0.110 0.250 0.109

0.490 -0.151 0,200 0,064 0,200 -0,049 0,400 0.007

0.630 3,254"* 0,260 0,065 0.250 0.144 0.490 -0.160

0,750 -0.106 0,400 -2.631 ** 0.400 -0.023 0.580 -0.291

0.850 -0.045 0.490 -0.109 0.490 -0.021 0.650 -0.113

0.900 0.012 0.580 -0.124 0.580 -0.201 0,750 0.149

0,960 -0.034 0.640 0.223 0.650 -0.025 0.830 0.288

0.750 0.084 0.750 -0.019 0.900 0.342

0.870 0.146 0.890 ******** 0.960 0.213

0.930 0.063 0.930 O.160

0.960 -0.024 0.960 -2.630* *

CN = 0,455 0,614 0,708 0.838

422
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-28-12-500, MINF = 0.899, Camber = 10/2, ALPT = 6.00, BETA = 0.05, QINF = 300.1,

RNPU = 2.3E+06, CNWP = 0.3627

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.530 0.000 0.307 0.000 0.387** 0.010 0.271

0.060 0.067 0.020 0.429 0.020 0.516 0.020 0.174

0.110 -0.248 0.040 0.397 0.060 1.604** 0.060 -0.392

0.200 -0.955 0.060 -0.024 0.090 -0.257 0.110 -0.672

0.230 -0.880 0.090 -0.226 0.110 -0.474 0.140 -0.994

0.400 -0.747 0,130 -0.452 0.130 - 1.769** 0.190 - 1.769"*

0.490 -0.594 0.150 -0.726 0.150 -0.865 0.250 -0.960

0.590 -0.571 0,200 -0.771 0.210 -0.856 0.400 -0.705

0.630 -0.455 0,250 -0.870 0.250 -0.870 0.490 -0.594

0.700 -0.108 0.260 -0.824 0.340 -0,883 0.580 -0.488

0.750 -0.136 0.280 -0.862 0.370 -0.890 0.650 -0.513

0.810 -0.152 0,290 -0.835 0.400 -0.854 0.700 -0.495

0.840 -0.125 0.310 -0.808 0.410 0.650"* 0,750 -0.559

0.900 -0.096 0.320 -0.815 0.430 -0.891 0.800 -0.742

0.960 -0,010 0.340 -0.812 0.440 -0.866 0.830 -0.689

0.350 -0.409"* 0.460 -0.870 0.900 -0.175

0,370 -0.801 0.490 -0.81 [ 0.960 -0.103

0.380 -0.861 0.500 -0.902

0.400 -0.769 0.520 -0,876

0.410 -0.842 0.540 -0.877

0.430 -0.805 0.550 -0.852

0.440 -0.774 0.580 -0.844

0.460 -0.835 0,600 -0.805

0.470 -0.824 0.610 -0.738

0.490 -0.808 0.650 -0.800

0J00 -0.813 0.700 -0.68 I

0,520 -0.804 0.750 -0.674

0.530 -0.790 0.820 -0.359

0.550 -0.821 0.890 -0.093

0.560 -0.831 0.900 -0.073

0,580 -0.798 0.960 -0.006

0.590 -0.845

0.600 -0.84 I

0,640 -0.849

0.700 -0.413

0.750 -0.052"*

0.820 -0.197

0.870 -0.172

0.930 -0.131

0.960 -0.102

Lower Surface

0.020 -0.847 0.020 - 1.233 0.020 -0.932 0.020 -0.521

0.1 I 0 -0.563 0.060 -0.576 0.060 -0.426 0.060 -0.051

0.230 -0.094 0.090 -0.472 0.090 -0.230 0.110 -0.192

0.400 -0.099 0.120 -0.229 0.120 -0.290 0.250 -0.171

0.490 -0.072 0.200 -0.087 0.200 -0.125 0.400 -0.259

0.630 4,024** 0.260 -0,176 0.250 -0.136 0.490 -0.375

0.750 0.008 0.400 -0.175 0,400 -0.272 0.580 -0.4%

0,850 0.056 0,490 -0.172 0.490 -0,094 0.650 -0.281

0.900 0.156 0.580 -0.151 0.580 -0.239 0.750 0.077

0.960 0.146 0.640 0.016 0.650 -0.072 0.830 0.225

0.750 0.118 0.750 -0.057 0.900 0.286

0.870 0.198 0.890 0.253 0.960 0211

0.930 O.170 0.930 0.209

0.960 0.123 0.960 0.331

CN = 0.318 0.427 0.496 0.458

423
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-29-4-500, MINF = 0.903, Camber = 10/2, ALPT = 8.06, BETA = -0.41, QINF = 297.1,

RNPU = 2.3E+06, CNWP = 0.4635

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.453 0.000 0.475 0.1300 0.341 ** 0.010 0.027

0.060 -0.021 0.020 0.305 0.020 0.375 0.020 0.024

0.110 -0.232 0.040 0.281 0.060 1.375"* 0.060 -0.495

0.200 -1.012 0.060 -0.127 0.090 -0.337 0.110 -0.831

0.230 -0.920 0.090 -0.317 0.110 -0.574 0.140 - 1,088

0.400 -0.813 0.130 -0.529 0.130 -1.750'* 0.190 -1.750"*

0.490 -0.697 0.150 -0.788 0.150 -0.936 0.250 - 1.106

0,590 -0.675 0.200 -0.835 0.210 -0.934 0.400 -0.804

0.630 -0.574 0.250 -0.949 0.250 -0.952 0.490 -0.680

0.700 -0.267 0.260 -0.895 0.340 -0.991 0.580 -0.613

0.750 -0.217 0.280 -0.934 0.370 -0.980 0,650 -0.625

0.810 -0.212 0.290 -0.917 0.400 -0.946 0.700 -0.613

0.840 -0.196 0.310 -0.900 0.410 0.693"* 0.750 -0.654

0.900 -0.187 0.320 -0.907 0,430 -0.999 0.800 -0.807

0.960 -0.104 0.340 -0.910 0,440 -0.973 0.830 -0.772

0,350 -0,423** 0.460 -0.985 0.900 -0.280

0.370 -0.891 0,490 -0.874 0.960 -0.213

0.380 -0.965 0.500 - 1.010

0.400 -0,859 0.520 -0.997

0.410 -0.932 0.540 -0.989

0.430 -0.900 0.550 -0,978

0.440 -0.874 0.580 -0.987

0.460 -0.945 0.600 -0.965

0.470 -0.924 0.610 -0.943

0.490 -0.913 0.650 - 1.093

0.500 -0.925 0.700 - 1.004

0.520 -0.924 0.750 -0.656

0.530 -0.899 0.820 -0.424

0.550 -0.924 0.890 -0.298

0,560 -0.920 0.900 -0.324

0,580 -0.846 0.960 -0.230

0.590 -0.642

0.600 -0,536

0.640 -0,325

0.700 -0.330

0.750 -0.061"*

0.820 -0.292

0.870 -0.289

0.930 -0.282

0.960 -0.274

Lower Surface

0.020 -0.686 0.020 -0.691 0.020 -0,605 0.020 -0.120

0.110 -0.368 0,060 -0.159 0.060 0.057 0.060 -0.045

0.230 -0.054 0.090 -0.071 0,090 0,037 0.110 0.037

0.400 -0.087 0.120 -0.012 0.120 -0.114 0.250 -0.061

0.490 -0.153 0.200 -0.052 0.200 -0.086 0.400 -0.160

0.630 4.101 ** 0.260 -0.070 0.250 -0.042 0.490 -0.282

0.750 -0.086 0.400 -0.136 0.400 -0.178 0.580 -0.404

0.850 -0.026 0.490 -0.179 0.490 -0.096 0.650 -0.225

0.900 0.088 0.580 -0.208 0.580 -0.265 0.750 0.094

0.960 0.062 0.640 -0.016 0.650 -0.080 0.830 0.242

0,750 0.100 0.750 -0.051 0.900 0.289

0.870 0.132 0.890 0.247 0.960 0.196

0.930 0.090 0,930 0.180

0.960 0.013 0,960 0.264

CN = 0,380 0.503 0.680 0.640

424
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-29-1 l-O00, MINF = 0.907, Camber = 10/2, ALl:q" = 8.96, BETA = 0.37, QINF = 301.9,

RNPU = 2,3E+06, CNWP = 0.4647

11= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x./c CP

0.020 0.433 0.000 0.542 0.000 0.435"* 0.010 -0.016

0.060 -0.042 0.020 0.270 0.020 0.302 0.020 -0.015

0. 110 -0,412 0,040 0.232 0.060 1.318"* 0.060 -0.603

0,200 - 1.003 0.060 -0.183 0.090 -0.437 0.110 -0.888

0.230 -0,921 0,090 -0.350 0.110 -0.589 0.140 -1.154

0.400 -0.845 0.130 -0,550 0.130 - 1.735"* 0,190 - 1,735"*

0.490 -0.730 0.150 -0.812 0.150 -0.943 0.250 -1.171

0,590 -0.699 0.200 -0.842 0,210 -0.944 0.400 -0.872

0.630 -0.588 0,250 -0.978 0,250 -0.985 0.490 -0.714

0.700 -0.444 0.260 -0,920 0.340 - 1,033 0,580 -0.656

0.750 -0.272 0.280 -0.966 0.370 - 1.038 0,650 -0.677

0,810 -0.249 0.290 -0.957 0.400 -0.972 0.700 -0.657

0.840 -0.227 0.310 -0.932 0.410 0.670** 0.750 -0.691

0.900 -0.251 0.320 -0.940 0.430 -1.033 0.800 -0.827

0,960 -0,185 0,340 -0,949 0,440 -0.995 0.830 -0.790

0,350 -0.423** 0.460 - 1,020 0.900 -0.359

0.370 -0.929 0.490 -0.924 0.960 -0.269

0.380 -0.998 0.500 - 1.043

0,400 -0.890 0.520 - 1.027

0.410 -0,953 0,540 - 1.026

0.430 -0.932 0.550 - 1.011

0.440 -0.923 0.580 - 1.036

0.460 -0.975 0,600 -0.995

0.470 -0,960 0.610 -0.987

0.490 -0.949 0,650 -0,888

0.500 -0.960 0,700 -0676

0.520 -0.936 0.750 -0.614

0.530 -0.924 0.820 -0.512

0.550 -0.966 0.890 -0421

0.560 -0,795 0,900 -0,447

0,580 -0.587 0.960 -0,364

0.590 -0.511

0,600 -0.466

0.640 -0.368

0.700 -0.373

0.750 -0.083**

0.820 -0.325

0.870 -0.343

0.930 -0,341

0,960 -0,337

Lower Surface

0.020 -0,635 0.020 -0,497 0.020 -0.453 0.020 0.035

O. 110 -0.223 0.060 -0.038 0.060 0,129 0,060 -0.056

0.230 -0.050 0.090 -0,018 0,090 0.104 0.110 0,085

0.400 -0.104 0.120 0.056 0.120 -0.058 0.250 -0.026

0,490 -0,136 0,200 -0,030 0.200 -0,076 0.400 -0,126

0,630 4.025"* 0.260 -0.030 0.250 -0.010 0.490 -0.252

0.750 -0.127 0.400 -0.127 0.400 -0.133 0.580 -0.375

0.850 -0.087 0.490 -0.180 0.490 -0.106 0.650 -0.248

0.900 0.037 0.580 -0,209 0,580 -0,345 0.750 0.090

0,960 -0,009 0.640 -0,031 0.650 -0,091 0.830 0.235

0.750 O. 102 0.750 -0.062 0.900 0.285

0.870 0.133 0.890 0.239 0,960 0.201

0.930 0.070 0.930 0.173

0.960 -0.010 0.960 0.213

CN = 0.429 0.544 0.707 0.708

425
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 9-38-4-500, MINF = 0.906, Camber = 10/2, ALPT = 5.96, BETA = 0.19, QINF = 295.9,

RNPU = 2.2E+06, CNWP = 0.3462

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x,/c CP x/c CP

0,020 0.521 0.000 0.286 0.000 8.526** 0.010 0.352

0.060 0.098 0.020 0.369 0.020 0.540 0.020 0.253

0.110 -0,236 0.040 0.338 0.060 -2.886** 0.060 -0.236

0.200 -0.887 0.060 -0.032 0.090 -0.184 0.110 -0.591

0.230 -0,797 0.090 -0.176 0.110 -0.461 0.140 -0.926

0.400 -0.720 0.130 -0.414 0.130 -0.641 0.190 -1.742"*

0.490 -0,577 0.150 -0.731 0.150 -0.869 0.250 -0.896

0.590 -0.572 0.200 -0.773 0.210 -0.811 0.400 -0.681

0.630 -0.470 0.250 -0.826 0.250 -0.795 0.490 -0.587

0.700 -0.164 0.260 -0.775 0.340 -0.827 0.580 -0.481

0.750 -0.130 0.280 -0.826 0.370 -0.831 0.650 -0.477

0.810 -0.112 0.290 -0.803 0.400 -0.837 0,700 -0.478

0.840 -0.105 0.310 -0.792 0.410 -2.751 * * 0.750 -0,546

0.900 -0.090 0.320 -0.759 0.430 -0.850 0.800 -0.741

0.960 0.010 0.340 -0.778 0.440 -0.792 0.830 -0.661

0.350 -0.455** 0.460 -0.824 0.900 -0.201

0.370 -0.754 0,490 -0.731 0.960 -0.129

0.380 -0.821 0.500 -0.847

0.400 -0.710 0.520 -0,826

0.410 -0.807 0.540 -0.830

0.430 -0.766 0.550 -0.773

0.440 -0.701 0.580 -0.784

0.460 -0.831 0.600 -0.755

0.470 -0.772 0.610 -0.703

0.490 -0.763 0.650 7.137**

0.500 -0.783 0.700 -0.688

0.520 -0.785 0.750 -0.685

0.530 -0.756 0.820 -0.483

0.550 -0.823 0,890 -0.103

0.560 -0.769 0.900 -0.092

0.580 -0.770 0.960 -0.017

0,590 -0,836

0,600 -0.831

0.640 -0.816

0.700 -0.446

0,750 -0.050"*

0.820 -0.189

0.870 -0.164

0,930 -0.130

0,960 -0.119

Lower Surface

0.020 -0.903 0.020 -0.233 0.020 - 1.174 0.020 -0.588

0. 110 -0.636 0.060 -0,631 0.060 -0.256 0.060 6.844**

0.230 -0.107 0.090 -0.481 0.090 3.915 ** 0.110 -0.059

0.400 -0.071 0.120 -0.315 0.120 -0.361 0.250 -0.155

0.490 -0.044 0.200 -0.093 0.200 -0.148 0,400 -0.242

0.630 4,685** 0.260 -0.238 0.250 -0.131 0.490 -0.388

0.750 0.008 0.400 -0.193 0.400 -0.284 0.580 -0.481

0.850 0.111 0.490 -0.178 0.490 -0.089 0.650 -0.565

0.900 0.167 0.580 -0.138 0.580 -0.420 0.750 0.003

0.960 0.165 0.640 0.031 0.650 -0.074 0.830 0.229

0.750 0.153 0.750 0.092 0.900 0.294

0.870 0.193 0.890 0.204 0.960 0.215

0.930 0.165 0,930 0.185

0.960 0.121 0.960 -2.840"*

CN = 0.298 0.401 0.463 0.412

426
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 9-38-25-500, MINF = 0.907, Camber = 10/2, ALPT = 7.09, BETA = 0.25, QINF = 295.8,

RNPU = 2.2E+06, CNWP = 0.3933

i"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x./c CP

0.020 0.480 0.000 0.369 0.000 8.536** 0.010 0.236

0.060 0. l 17 0,020 0.302 0,020 0.474 0.020 0.233

0.110 -0,047 0.040 0.273 0.060 -2.881 ** 0.060 -0.394

0,200 -0.923 0.060 -0.104 0.090 -0.220 0.110 -0.680

0.230 -0.854 0.090 -0.229 0.110 -0.517 0.140 -0.991

0.400 -0.738 0.130 -0.463 0.130 -0.686 0.190 - 1.737"*

0.490 -0.639 0.150 -0.759 0.150 -0.964 0.250 -0.963

0.590 -0.636 0,200 -0.811 0.210 -0.858 0.400 -0.718

0.630 -0,554 0,250 -0.888 0.250 -0.841 0.490 -0.649

0.700 -0.338 0.260 -0.827 0.340 -0.883 0.580 -0.544

0.750 -0.167 0.280 -0.874 0.370 -0,882 0.650 -0.544

0.810 -0.165 0.290 -0.857 0.400 -0.907 0.700 -0.535

0.840 -0.122 0.310 -0.850 0.410 -2.747"* 0.750 -0.600

0.900 -0.125 0.320 -0.841 0,430 -0.906 0.800 -0.764

0.960 -0.042 0.340 -0.814 0.440 -0.865 0,830 -0.707

0.350 -0.486** 0.460 -0,895 0.900 -0.232

0.370 -0,797 0.490 -0.818 0.960 -0.188

0.380 -0.878 0.500 -0.923

0.400 -0.709 0,520 -0.872

0.410 -0.866 0.540 -0,893

0.430 -0.834 0.550 -0.858

0.440 -0.785 0.580 -0.838

0.460 -0.889 0.600 -0.847

0.470 -0.828 0.610 -0.835

0490 -0.837 0.650 7,146"*

0.500 -0.848 0.700 -0.880

0.520 -0.858 0.750 -0.885

0.530 -0.820 0.820 -0.343

0.550 -0.869 0.890 -0.190

0.560 -0.836 0.900 -0.172

0.580 -0.841 0.960 -0.119

0,590 -0.884

0.600 -0.901

0640 -0.401

0,700 -0.311

0.750 -0,067"*

0.820 -0.203

0,870 -0.218

0.930 -0,236

0.960 -0.225

Lower Surface

0.020 -0.958 0.020 -0.229 0.020 -0.853 0.020 -0.358

0.110 -0.488 0.060 -0.492 0.060 -0.146 0.060 6.853"*

0.230 -0.090 0.090 -0.361 0.090 3.922** 0.110 -0.027

0.400 -0,073 0.120 -0.155 0.120 -0.278 0.250 -O 105

0.490 -0.106 0.200 -0.091 0.200 -0.1 44 0.400 -0.185

0.630 4.693** 0.260 -0.145 0,250 -0.081 0.490 -0.353

0,750 -0,025 0.400 -0.188 0.400 -0.243 0,580 -0.471

0.850 0.059 0.490 -0.207 0.490 -0.076 0.650 -0.514

0.900 0.133 0.580 -0.179 0.580 -0.408 0.750 0.051

0.960 0.118 0.640 0.002 0,650 -0.083 0.830 0.254

0.750 0.136 0.750 0.067 0.900 0.300

0.870 0.136 0.890 0.225 0.960 0,209

0.930 0,096 0.930 0.165

0.960 0.041 0.960 -2.835 * *

CN = 0.329 0.424 0.554 0.503

427
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 9-38-41-500, MINF = 0.894, Camber = 10/2, ALPT = 12.06, BETA = 0.19, QINF = 297.7,

RNPU = 2.3E+06, CNWP = 0.2948

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.146 0.000 0.803 0.000 8.419* * 0.010 -0.551

0.060 -0.277 0.020 -0.182 0.020 -0.061 0.020 -0.427

0.110 -0.601 0.040 -0.083 0.060 -2.924** 0.060 -0.778

0.200 - 1.043 0.060 -0.496 0.090 -0.703 0.110 - 1.077

0.230 - 1.058 0.090 -0.631 0.110 -0.892 0.140 - 1.204

0.400 -0.572 0.130 -0.801 0.130 - 1.001 0.190 -1.787**

0.490 -0.525 0.150 - 1.029 0.150 - I. 181 0.250 - 1.314

0.590 -0.533 0.200 - 1.061 0.210 - 1.123 0.400 -0.938

0.630 -0.459 0.250 - 1.149 0.250 - 1.113 0.490 -0.840

0.700 -0.429 0.260 - 1.046 0.340 -0.802 0.580 -0.779

0.750 -0.485 0.280 - 1.013 0.370 -0.759 0.650 -0.716

0.810 -0.438 0.290 -0.864 0.400 -0.791 0.700 -0.705

0.840 -0.394 0.310 -0.728 0.410 -2.791 ** 0.750 -0.670

0.900 -0.401 0.320 -0.701 0.430 -0.750 0.800 -0.612

0.960 -0.407 0.340 -0.665 0.440 -0.700 0.830 -0.616

0.350 -0.368"* 0.460 -0.719 0.900 -0.525

0.370 -0.627 0.490 -0.639 0.960 -0.442

0.380 -0.701 0.500 -0.724

0.400 -0.591 0.520 -0.683

0.410 -0.671 0.540 -0.682

0.430 -0.640 0.550 -0.665

0.440 -0,584 0.580 -0,660

0.460 -0.654 0.600 -0.646

0.470 -0.593 0.610 -0.612

0.490 -0.599 0.650 7.038"*

0.500 -0.621 0.700 -0.620

0.520 -0.596 0.750 -0.687

0.530 -0.561 0.820 -0.547

0.550 -0.612 0.890 -0.530

0.560 -0.554 0.900 -0.515

0.580 -0.566 0.960 -0.441

0.590 -0.623

0.600 -0.579

0.640 -0.478

0.700 -0.487

0.750 -0.056"*

0.820 -0.430

0.870 -0.441

0.930 -0.452

0.960 -0.417

Lower Surface

0.020 -0.078 0.020 -0.182 0.020 0.217 0.020 0.473

0.110 0.017 0.060 0.267 0.060 0.372 0.060 6.747" *

0.230 0.039 0.090 0.177 0.090 3.836" * 0.110 0.374

0.400 -0.051 0.120 0.243 0.120 0.023 0.250 0.141

0.490 -0.091 0.200 0.037 0.200 -0.021 0.400 0.028

0.630 4.601 ** 0.260 0.095 0.250 0.162 0.490 -0.1 04

0.750 -0.131 0.400 -0.006 0.400 -0.009 0.580 -0.232

0.850 -0.079 0,490 -0.100 0,490 -0.091 0.650 -0.099

0.900 -0.007 0.580 -0.156 0.580 -0.157 0.750 0.112

0.960 -0.108 0.640 0.016 0.650 -0.083 0.830 0.315

0.750 0.132 0,750 0.080 0.900 0.303

0.870 0.159 0.890 0,200 0.960 0.173

0.930 0.058 0.930 0.133

0.960 -0.019 0.960 -2.878**

CN = 0.495 0.654 0.745 0.932

428
Table G-2. Continued.

Flight 211, Wing sweep = 26", Time = 11-25-20-500, MINF = 0.898, Camber = 5/10, ALPT = 4.04, BETA = 0.14, QINF = 299.5,

RNPU = 2.3E+06, CNWP = 0.3072

TI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.362 0.000 0.578 0.000 0.552"* 0,010 -0.053

0.060 0.022 0.020 0.232 0.020 0.292 0,020 -0.014

0. 110 -0.229 0.040 0.241 0.060 1.513"* 0.060 -0.383

0.200 -0.749 0.060 -0.071 0.090 -0.237 0.110 -0.545

0.230 -0,629 0.090 -0.208 O.110 -0.399 0.140 -0.770

0.400 -0,496 0.130 -0.357 0.130 -1.772"* 0.190 -1.772"*

0.490 -0.219 0.150 -0.551 0.150 -0.643 0.250 -0.593

0.590 -0.176 0.200 -0.549 0.210 -0.660 0.400 -0.620

0.630 -0.230 0.250 -0.664 0.250 -0.674 0.490 -0.358

0.700 -0.282 0.260 -0.625 0.340 -0.703 0.580 -0,343

0.750 -0.829 0,280 -0.650 0.370 -0.696 0,650 -0.392

0.810 -0.789 0.290 -0.641 0.400 -0.670 0.700 -0.377

0.840 -0.840 0.310 -0.616 0.410 0.652'* 0.750 -0.479

0.900 -0.317 0.320 -0.622 0,430 -0.651 0.800 - 1.020

0.960 -0.32 ! 0.340 -0.620 0.440 -0.600 0.830 -0.915

0.350 -0.337** 0.460 -0.581 0.900 -0.443

0.370 -0.607 0,490 -0.503 0.960 -0.430

0.380 -0.668 0.500 -0.474

0.400 -0.575 0.520 -0.375

0,410 -0.639 0.540 -0.331

0.430 -0,602 0.550 -0.308

0.440 -0.571 0.580 -0.272

0.460 -0.628 0.600 -0.295

0.470 -0.581 0.610 -0.304

0.490 -0.613 0.650 -0,582

0.500 -0.632 0.700 -0.487

0.520 -0.605 0.750 -0.527

0.530 -0.605 0.820 -0.836

0,550 -0.647 0.890 -0.448

0.560 -0.635 0.900 -0.456

0.580 -0.508 0.960 -0.412

0.590 -0.461

0.600 -0.423

0_640 -0.414

0.700 -0.351

0.750 -0,029**

0,820 -0,551

0.870 -0.375

0.930 -0.330

0.960 -0.340

Lower Surface

0.020 - 1.295 0.020 - 1.127 0.020 -0.997 0.020 -0.203

0.110 -0.321 0.060 -0.825 0.060 -0.253 0.060 -0.021

0.230 -0,083 0.090 -0.460 0.090 -0.256 0.110 -0.222

0.400 -0,020 0.120 -0,170 0.120 -0.406 0.250 -0.272

0.490 0.010 0.200 -0.082 0.200 -0.121 0.400 -0.323

0,630 4.033** 0.260 -0.146 0.250 -0.295 0.490 -0.293

0.750 0.162 0.400 -0.073 0.400 -0.152 0.580 -0.146

0.850 0.206 0.490 -0.031 0.490 -0.049 0.650 0.085

0.900 0.290 0.580 0,029 0.580 -0.013 0.750 0.308

0.960 0.102 0.640 0.269 0.650 -0.048 0.830 0.409

0.750 0,331 0.750 -0,023 0.900 0.479

0.870 0.386 0.890 0.421 0.960 0.337

0.930 0.325 0.930 0.351

0.960 0.206 0.960 0.350

CN = 0.414 0.464 0.456 0.489

429
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-25-28-000, MINF = 0,900, Camber = 5/11, ALPT = 5.00, BETA = -0.36, QINF = 300.8,

RNPU = 2.3E+06, CNWP = 0.3527

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.329 0.000 0.625 0.000 0.521 ** 0.010 -0.179

0.060 -0.007 0.020 0.193 0.020 0.211 0.020 -0,098

0.110 -0.275 0.040 0.188 0.060 1.506** 0.060 -0.466

0.200 -0.772 0.060 -0.133 0.090 -0.289 0.110 -0.621

0,230 -0,627 0.090 -0.242 0.110 -0.443 0.140 -0.838

0.400 -0.547 0.130 -0.392 0.130 -1.765"* 0.190 - 1.765"*

0,490 -0.431 0.150 -0.582 0.150 -0.683 0.250 -0.759

0.590 -0.421 0.200 -0.581 0.210 -0.695 0.400 -0.638

0.630 -0.340 0.250 -0.699 0.250 -0.715 0.490 -0.432

0.700 -0.417 0.260 -0.664 0.340 -0.746 0.580 -0.394

0.750 -0.846 0.280 -0.691 0.370 -0.756 0.650 -0.432

0.810 -0.822 0.290 -0.682 0.400 -0.727 0.700 -0.417

0.840 -0.852 0.310 -0.658 0.410 0.649** 0.750 -0.499

0.900 -0.339 0.320 -0,664 0.430 -0.739 0.800 - 1.030

0.960 -0.341 0.340 -0.665 0.440 -0.721 0.830 -0.975

0.350 -0.325** 0,460 -0.728 0.900 -0.468

0,370 -0,660 0.490 -0.614 0.960 -0,453

0.380 -0,706 0.500 -0.645

0.400 -0.628 0.520 -0.642

0.410 -0.685 0.540 -0.614

0.430 -0.646 0.550 -0.588

0.440 -0.627 0.580 -0.480

0.460 -0.697 0,600 -0,414

0,470 -0.689 0.610 -0.384

0,490 -0.670 0.650 -0.568

0.500 -0.673 0.700 -0.489

0.520 -0.665 0.750 -0.540

0.530 -0.653 0.820 -0.779

0.550 -0.690 0.890 -0,439

0.560 -0.688 0.900 -0.450

0.580 -0.660 0.960 -0.403

0.590 -0.707

0.600 -0.711

0,640 -0.738

0.700 -0.624

0,750 -0.022**

0.820 -0,403

0.870 -0.294

0.930 -0.292

0 960 -0.313

Lower Surface

0.020 - 1.241 0.020 - 1.067 0.020 -0.884 0.020 -0.082

0.110 -0.122 0.060 -0.339 0.060 -0.096 0.060 -0.021

0.230 -0.056 0.090 -0.203 0.090 -0.167 0.110 -0.161

0.400 -0.036 0.120 -0.148 0.120 -0.337 0.250 -0.239

0.490 0.010 0.200 -0.053 0.200 -0.105 0.400 -0.279

0.630 4.015" * 0.260 -0.132 0.250 -0.193 0.490 -0,248

0.750 0.165 0.400 -0.062 0.400 -0.123 0.580 -0.136

0.850 0.208 0.490 -0.020 0.490 -0.042 0.650 0.092

0.900 0.294 0.580 0.040 0.580 -0.006 0.750 0.315

0,960 0.118 0.640 0.268 0.650 -0.042 0.830 0.419

0.750 0.329 0.750 -0.027 0.900 0.489

0.870 0.383 0.890 0.459 0.960 0.340

0,930 0.316 0.930 0.386

0.960 0.204 0.960 0.384

CN = 0.513 0.563 0.541 0.570

430
Table G-2. Continued.

Flight 211, Wing sweep = 26", Time = 11-25-34-500, MINF = 0.897, Camber = 5/10. ALPT = 6.01, BETA = 0.19, QINF = 298.2,

RNPU = 2.3E+06, CNWP = 0.4057

11 = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.286 0.000 0.736 0.000 0.558"* 0.010 -0.345

0.060 -0,055 0.020 0.084 0.020 0.103 0.020 -0.200

0.110 -0.294 0.040 0.119 0.060 1.373** 0.060 -0,557

0.200 -0.763 0.060 -0.209 0.090 -0.357 0.110 -0.742

0.230 -0.666 0,090 -0.307 0.110 -0.490 0.140 -0.917

0.400 -0.628 0.130 -0.443 0,130 - 1.777"* 0.190 -1.777"*

0.490 -0.491 0.150 -0.632 0.150 -0.753 0.250 -0.904

0.590 -0.496 0.200 -0.631 0.210 -0.739 0.400 -0.697

0.630 -0.418 0.250 -0.764 0.250 -0.769 0.490 -0.575

0.700 -0,482 0.260 -0.713 0.340 -0.825 0.580 -0.443

0.750 -0.495 0.280 -0.749 0.370 -0.824 0,650 -0.514

0.810 -0.515 0.290 -0.731 0.400 -0.797 0.700 -0.501

0,840 -0.536 0.310 -0.716 0,410 0.657** 0.750 -0.581

0.900 -0.354 0.320 -0.719 0.430 -0.833 0.800 - 1.071

0.960 -0.365 0.340 -0.735 0.440 -0.803 0.830 -0.700

0.350 -0.352** 0.460 -0.817 0.900 -0,478

0.370 -0.725 0.490 -0.776 0.960 -0.470

0.380 -0.801 0.500 -0,850

0.400 -0,708 0.520 -0.833

0.410 -0.776 0.540 -0,820

0.430 -0.715 0,550 -0.810

0.440 -0.700 0.580 -0.766

0.460 -0.762 0.600 -0.678

0.470 -0.762 0.610 -0.628

0.490 -0.752 0.650 -0.711

0.500 -0.764 0.700 -0.630

0.520 -0.730 0.750 -0.642

0.530 -0.741 0,820 -0.524

0.550 -0.775 0.890 -0.412

0.560 -0.751 0.900 -0.445

0.580 -0.743 0.960 -0.400

0,590 -0.791

0.600 -0,779

0.640 -0.821

0.700 -0.850

0,750 -0.004**

0.820 -0.298

0,870 -0.315

0,930 -0.332

0.960 -0.331

Lower Surface

0.020 -0.804 0.020 -0,84! 0.020 -0.608 0.020 0.090

0.110 -0.173 0.060 -0.022 0.060 -0.002 0,060 -0.018

0.230 -0.008 0.090 -0.114 0.090 -0.043 0.110 -0.023

0.400 -0.029 0. 120 -0.080 0.120 -0.227 0.250 -0.172

0.490 0.005 0.200 -0.010 0.200 -0.044 0.400 -0.191

0.630 4.054"* 0.260 -0.078 0.250 -0.118 0.490 -0.179

0.750 0.157 0.400 -0.056 0.400 -0.101 0.580 -0.124

0.850 0.197 0.490 -0.025 0.490 -0.020 0,650 0.126

0.900 0.267 0.580 0.028 0.580 -0.010 0.750 0.331

0,960 0.084 0.640 0.280 0.650 -0.039 0.830 0.453

0.750 0.326 0.750 -0.024 0.900 0.496

0.870 0.390 0,890 0.488 0,960 0.341

0.930 0.329 0.930 0.408

0.960 0.228 0.960 0.371

CN = 0.502 0.659 0,642 0.684

431
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-25-39-500, MINF = 0.898, Camber = 5/10, ALPT = 7.09, BETA = -0.21, QINF = 299.0,

RNPU = 23E+06, CNWP = 0.4689

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP .r./c CP x/c CP

0.020 0.165 0.000 0.784 0.000 0.563* * 0.010 -0.603

0.060 -0.112 0.020 -0.016 0.020 -0.026 0.020 -0.395

0.110 -0.305 0.040 0.019 0.060 1 _227 ** 0.060 -0.640

0.200 -0.784 0.060 -0.287 0.090 -0.482 0.110 -0.804

0.230 -0.687 0.090 -0.361 0.110 -0.574 0.140 -0.969

0.400 -0.672 0.130 -0.498 0.130 - 1.773"* 0.190 -1.773"*

0.490 -0.552 0.150 -0.669 0.150 -0.788 0.250 -0.973

0.590 -0.557 0.200 -0.675 0.210 -0.793 0.400 -0.730

0.630 -0.487 0.250 -0.813 0.250 -0.833 0.490 -0.634

0.700 -0.546 0.260 -0.773 0.340 -0.869 0.580 -0.515

0.750 -0.498 0.280 -0.813 0.370 -0.892 0.650 -0.560

0.810 -0.511 0.290 -0.800 0.400 -0.884 0.700 -0.537

0.840 -0.565 0.310 -0.770 0.410 0.655** 0.750 -0.616

0.900 -0.419 0.320 -0.784 0.430 -0.892 0.800 -0.970

0.960 -0.439 0.340 -0.788 0.440 -0.863 0.830 -0.653

0.350 -0.336** 0.460 -0.871 0.900 -0.490

0.370 -0.775 0.490 -0.827 0.960 -0.478

0.380 -0.844 0.500 -0.905

0.400 -0.758 0.520 -0.899

0.410 -0.824 0.540 -0.901

0.430 -0.783 0.550 -0.876

0.440 -0.748 0.580 -0.861

0.460 -0.815 0.600 -0.857

0.470 -0.819 0.610 -0.842

0.490 -0.799 0.650 -0.831

0.500 -0.813 0.700 -0.750

0.520 -0.791 0.750 -0.766

0.530 -0.785 0.820 -0.494

0.550 -0.804 0.890 -0.420

0.560 -0.824 0.900 -0.435

0.580 -0.793 0.960 -0.4 ! 7

0.590 -0.828

0.600 -0.836

0.640 -0.854

0.700 -0.906

0.750 -0.005"*

0.820 -0.343

0.870 -0.344

0.930 -0.358

0.960 -0.357

Lower Surface

0.020 -0.785 0.020 -0.249 0.020 -0.138 0.020 0.216

0.110 -0.173 0.060 0.064 0.060 0.091 0.060 -0.004

0.230 0.021 0.090 -0.047 0.090 0.031 0.110 0.038

0.400 -0.011 0.120 -0.022 0.120 -0.167 0.250 -0.105

0.490 0.012 0.200 0.022 0.200 -0.014 0.400 -0.140

0.630 4.041 ** 0.260 -0.050 0.250 -0.052 0.490 -0.157

0.750 0.145 0.400 -0.019 0.400 -0.052 0.580 -0.090

0.850 0.184 0.490 -0.018 0.490 -0.017 0.650 0.117

0.900 0.275 0.580 0.046 0.580 0.011 0.750 0.354

0.960 0.073 0.640 0.279 0.650 -0.025 0.830 0.460

0.750 0.348 0.750 -0.010 0.900 0.521

0.870 0.431 0.890 0.490 0.960 0.348

0.930 0.339 0.930 0.398

0.960 0.215 0.960 0.376

CN = 0.547 0.736 0.735 0.757

432
Table G-2. Continued,

Flight 21 l, Wing sweep = 26 °, Time = 11-25-44-500, MINF = 0.894, Camber = 5/10, ALPT = 8.16, BETA = -0.01, QINF = 297.7,

RNPU = 2.3E+06, CNWP = 0.5649

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0,053 0,000 0.850 0.000 0.475** 0.010 -0.702

0.060 -0.245 0.020 -0.122 0.020 -0.178 0.020 -0.619

0.110 -0.417 0.040 -0.082 0,060 1.116"* 0.060 -0.718

0.200 -0.832 0.060 -0.404 0.090 -0.616 0.110 -0.913

0.230 -0.756 0,090 -0.501 0.110 -0.687 0.140 - 1.069

0.400 -0.735 0.130 -0.590 0.130 - 1,787"* 0.190 - 1.787 **

0.490 -0.616 0.150 -0.733 0.150 -0.858 0.250 -1.054

0.590 -0.604 0.200 -0.736 0.210 -0.887 0.400 -0.801

0.630 -0.553 0.250 -0.887 0.250 -0.908 0.490 -0.700

0.700 -0.626 0.260 -0.836 0.340 -0.939 0.580 -0.604

0.750 -0.578 0.280 -0.882 0.370 -0.951 0.650 -0.640

0.810 -0,573 0.290 -0.869 0.400 -0.932 0.700 -0.604

0,840 -0.648 0.310 -0,838 0.410 0.652** 0.750 -0.676

0.900 -0.485 0.320 -0.855 0.430 -0.978 0.800 - 1.057

0.960 -0.493 0.340 -0,859 0.440 -0.952 0.830 -0.684

0.350 -0.334** 0.460 -0.949 0.900 -0.574

0.370 -0.847 0,490 -0.905 0,960 -0.545

0.380 -0.913 0.500 -0.976

0.400 -0.829 0.520 -0.971

0.410 -0.890 0.540 -0.979

0.430 -0.848 0.550 -0.951

0.440 -0.825 0.580 -0.935

0,460 -0.905 0.600 -0.949

0.470 -0.885 0.610 -0.932

0.490 -0.865 0.650 - 1.071

0.500 -0.879 0.700 -0.978

0.520 -0.864 0.750 -1.011

0.530 -0.869 0.820 -0.483

0.550 -0.905 0.890 -0.458

0.560 -0.887 0.900 -0.460

0.580 -0.855 0.960 -0.399

0.590 -0.908

0.600 -0.900

0.640 -0.915

0.700 -0.504

0.750 -0.008"*

0.820 -0.343

0.870 -0.363

0.930 -0.381

0.960 -0.372

Lower Surface

0.020 -0.419 0.020 -0.104 0.020 0.027 0.020 0.345

0.110 -0.110 0.060 0.153 0.060 0.166 0.060 0.005

0.230 0,064 0.090 0.044 0.090 0.115 0.110 0,138

0.400 -0.010 0.120 0.045 0.120 -0.073 0,250 -0.037

0.490 0.021 0.200 0.060 0.200 0.032 0.400 -0,096

0.630 4.053** 0.260 0.002 0,250 0.008 0.490 -0.126

0.750 0.142 0.400 -0.010 0.400 -0.008 0.580 -0.061

0.850 0.175 0.490 0.014 0.490 -0.016 0.650 0.119

0,900 0.274 0.580 0.055 0.580 0.027 0.750 0,364

0.960 0.050 0.640 0.285 0.650 -0.016 0,830 0.456

0.750 0.358 0.750 -0.016 0.900 0.517

0,870 0,413 0.890 0.501 0.960 0.352

0.930 0,338 0.930 0,402

0.960 0.214 0.960 0.390

CN = 0.631 0.774 0.852 0.867

433
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-26-1-500, MINF = 0.889, Camber = 5/11, ALPT = 10.22, BETA = 0.54, QINF = 311.0,

RNPU = 2.4E+06, CNWP = 0.5362

11 = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x./c CP x/c CP x./c CP

0.020 -0.165 0,000 0.873 0.000 0.479** 0.010 -0.812

0,060 -0.425 0.020 -0.510 0.020 -0.518 0.020 -0.822

0.110 -0.594 0,040 -0.260 0.060 1.059"* 0.060 -0.898

0.200 -0.914 0,060 -0.575 0,090 -0.776 0.110 - 1.058

0.230 -0.858 0,090 -0,689 0.110 -0.884 0.140 - 1.190

0.400 -0.843 0.130 -0,788 0.130 -1.806"* 0.190 -1.806"*

0.490 -0,743 0.150 -0,902 0.150 - 1.001 0.250 - 1.224

0.590 -0.736 0,200 -0.896 0.210 - 1.014 0.400 -0.937

0.630 -0.680 0,250 - 1.015 0.250 - 1.045 0.490 -0.810

0.700 -0.735 0.260 -0.966 0.340 - 1.097 0.580 -0.733

0.750 -0.499 0.280 - 1.014 0.370 - 1.094 0.650 -0.759

0.810 -0.548 0.290 - 1.014 0.400 - 1.050 0.700 -0.737

0.840 -0.601 0.310 -0.984 0.410 0.528** 0.750 -0.740

0.900 -0.527 0.320 -0.990 0.430 - 1.1 04 0.800 -0,799

0.960 -0.540 0.340 - 1.009 0.440 - 1.080 0.830 -0.979

0.350 -0.345"* 0.460 - 1.089 0.900 -0.576

0.370 -0.982 0.490 - 1.007 0.960 -0.543

0.380 - 1.059 0.500 - 1.108

0.400 -0.962 0.520 - 1.093

0.410 - 1.020 0.540 - 1.090

0.430 -0.988 0.550 - 1.073

0.440 -0.954 0.580 - 1.056

0.460 - 1.036 0.600 - 1.081

0.470 -0.988 0.610 - 1.070

0,490 -0.996 0.650 -0.784

0.500 - 1.013 0.700 -0.655

0.520 -0.994 0.750 -0,642

0.530 -0,993 0.820 -0,565

0.550 - 1.028 0.890 -0.575

0.560 - 1.032 0.900 -0.562

0.580 -0.995 0.960 -0.503

0.590 -1.045

0.600 -0.895

0.640 -0.441

0.700 -0.457

0.750 0,005**

0.820 -0.407

0.870 -0.416

0,930 -0.420

0.960 -0.411

Lower Surface

0.020 -0.046 0.020 0,235 0.020 0.271 0,020 0.550

0.110 -0.013 0.060 0.293 0.060 0.340 0.060 -0.019

0.230 0.129 0.090 0.184 0.090 0.254 0.110 0.269

0,400 0.017 0.120 0.147 0.120 0.045 0.250 0.063

0.490 0,036 0.200 0.129 0.200 0.096 0.400 0.001

0.630 3.784"* 0.260 0.080 0.250 0.104 0.490 -0,030

0.750 0.131 0.400 0.057 0.400 0.054 0.580 0.000

0.850 0.154 0.490 0.051 0.490 -0.025 0.650 0.169

0.900 0.248 0,580 0.077 0.580 0,059 0.750 0.394

0.960 0.041 0.640 0.300 0.650 -0.018 0.830 0,490

0.750 0.342 0.750 -0.039 0.900 0.541

0.870 0.413 0.890 0.501 0.960 0.351

0.930 0,336 0.930 0.397

0.960 0.206 0.960 0.368

CN = 0,738 0.892 0.941 1.039

434
Table G-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-26-8-000, MINF = 0.895, Camber = 5/10, ALPT = 9.92, BETA = 0.37, QINF = 332.3,

RNPU = 2.5E+06, CNWP = 0.5767

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 °0.088 0.000 0.896 0.000 0.461 ** 0.010 -0.606

0.060 -0.373 0.020 -0.438 0.020 -0.359 0.020 -0.795

0.110 -0.550 0.040 -0.193 0.060 0.853** 0.060 -0.904

0.200 -0.886 0.060 -0.536 0.090 -0.729 0.110 - 1.033

0.230 -0.828 0.090 -0.646 0.110 -0.844 0.140 - 1.142

0.400 -0.814 0.130 -0.745 0.130 -1.783"* 0.190 -1.783**

0.490 -0.718 0.150 -0.851 0.150 -0.970 0.250 - 1.170

0.590 -0.714 0.200 -0.854 0.210 -0.983 0.400 -0.902

0.630 -0.648 0.250 -0.976 0.250 - 1.007 0,490 -0.767

0.700 -0.713 0,260 -0.930 0.340 - 1.066 0.580 -0.697

0.750 -0.552 0.280 -0.982 0.370 - 1.056 0.650 -0.722

0.810 -0.554 0.290 -0.974 0.400 - 1.022 0.700 -0.705

0.840 -0.595 0.310 -0.947 0.410 0.402"* 0.750 -0.711

0.900 °0.543 0.320 -0.943 0.430 - 1.059 0.800 -0.827

0.960 -0.582 0.340 -0.969 0.440 - 1.054 0.830 - 1.004

0.350 -0.358** 0.460 - 1.060 0.900 -0.613

0.370 -0.934 0.490 - 1.002 0.960 -0.574

0.380 -1.017 0.500 -1.071

0.400 -0.916 0.520 - 1.079

0.410 -0.986 0.540 - 1.058

0,430 -0.947 0.550 - 1.041

0.440 -0.921 0.580 - 1.032

0.460 - 1.006 0.600 - 1.061

0.470 -0.991 0.610 - 1.027

0.490 -0.965 0.650 - 1.156

0.500 -0.979 0.700 - 1.062

0.520 -0.962 0.750 -0.706

0.530 -0.961 0.820 -0.576

0.550 -0.9% 0.890 -0.565

0.560 -0.991 0.900 -0.576

0.580 -0.957 0.960 -0.518

0.590 -1.011

0.600 -0.992

0.640 -0.539

0.700 -0.473

0.750 -0.014"*

0.820 -0.420

0.870 -0.422

0.930 -0.412

0.960 -0.423

Lower Surface

0.020 -0.122 0.020 0.201 0.020 0.228 0.020 0.541

O. 110 -0.049 0.060 0.282 0.060 0.307 0.060 -0.030

0.230 0.099 0.090 O.161 0.090 0.225 O.110 0.282

0.400 0.001 0.120 0.132 0.120 0.038 0.250 0.034

0.490 0.018 0.200 0.102 0.200 0.083 0.400 -0.014

0.630 3.450** 0.260 0.066 0.250 0.089 0.490 -0.060

0.750 0.138 0.400 0,035 0.400 0.026 0.580 -0.026

0,850 0.147 0.490 0.030 0.490 -0.029 0.650 0.160

0.900 0.246 0.580 0.060 0.580 0.043 0.750 0.395

0.960 0.040 0.640 0.290 0.650 -0.029 0.830 0.479

0.750 0.345 0.750 -0.129 0.900 0.535

0.870 0.403 0.890 0.499 0.960 0.345

0,930 0.335 0.930 0.393

0,960 0.194 0.960 0.388

CN = 0.708 0.866 0.941 1.005

435
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-11-10-000, MINF = 0.906, Camber = 5/10, ALPT = 5.05, BETA = -0.24, QINF = 303.6,

RNPU = 2.3E+06, CNWP = 0.3583

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 0,295 0.000 0.621 0.000 3.468** 0,010 -0,138

0,060 0.013 0.020 0.000 0.020 0.217 0.020 -0,058

0.110 -0.238 0,040 0.116 0.060 -4.649** 0.060 -0,433

0.200 -0,663 0.060 -0.200 0,090 -0.237 0. 110 -0.566

0.230 -0,699 0.090 -0.219 0.110 -0.444 0.140 -0.786

0.400 -0.524 0.130 -0.389 0.130 -0.478 0.190 - 1.742"*

0,490 -0.454 0.150 -0.585 0.150 -0.725 0.250 -0.734

0.590 -0,467 0.200 -0,584 0.210 -0.614 0.400 -0,599

0,630 -0.334 0.250 -0.653 0,250 -0.631 0.490 -0.395

0.700 -0.410 0,260 -0.612 0.340 -0,658 0.580 -0,399

0.750 -0.681 0.280 -0.615 0.370 -0.695 0,650 -0.3%

0.810 -0.611 0.290 -0.615 0.400 -0.736 0.700 -0.385

0,840 -0.618 0.310 -0.654 0.410 -2,726** 0.750 -0.481

0.900 -0,334 0.320 -0.632 0,430 -0.651 0,800 -0.947

0.960 -0.333 0,340 -0,587 0.440 -0.611 0.830 -0.881

0.350 -0.399** 0.460 -0.668 0.900 -0,434

0.370 -0.604 0.490 -0,579 0.960 -0.425

0.380 -0.636 0.500 -0.616

0,400 -0.577 0,520 -0.512

0.410 -0.630 0.540 -0.523

0.430 -0.591 0,550 -0,543

0.440 -0.533 0.580 -0.502

0.460 -0.663 0.600 -0,409

0,470 -0.603 0.610 -0.377

0.490 -0.649 0.650 2.114"*

0.500 -0,674 0.700 -0.544

0.520 -0.697 0.750 -0.609

0.530 -0,645 0.820 -0.770

0,550 -0.707 0.890 -0.410

0.560 -0.601 0,900 -0.437

0.580 -0,670 0.960 -0,367

0.590 -0.700

0.600 -0.737

0,640 -0.732

0.700 -0.681

0.750 -0.034**

0.820 -0.445

0,870 -0.307

0.930 -0,305

0.960 -0.294

Lower Surface

0.020 - 1.253 0.020 - 1.046 0.020 -0.838 0.020 -0.073

0.110 -0.150 0.060 -0.515 0.060 -0.093 0.060 1.828"*

0.230 -0.071 0,090 -0.236 0.090 1.137"* 0.110 -0.128

0.400 -0,029 0.120 -0.141 0.120 -0,460 0.250 -0.213

0.490 -0,013 0.200 -0.057 0.200 -0.150 0.400 -0,256

0.630 1.887"* 0.260 -0.160 0.250 -0.228 0.490 -0.349

0.750 0.148 0.400 -0.081 0.400 -0.120 0,580 -0.143

0.850 0.244 0.490 -0,054 0.490 -0.036 0.650 0.105

0.900 0.300 0.580 0,035 0,580 0.022 0.750 0.267

0.960 0.122 0.640 0.249 0.650 -0.042 0,830 0.46 I

0.750 0,343 0.750 0.338 0.900 0.497

0.870 0.408 0,890 0.385 0.960 0.343

0,930 0.283 0.930 0.308

0.960 0.172 0.960 -2.812"*

CN = 0.470 0,545 0.524 0.531

436
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-11-33-500, MINF = 0.897, Camber = 5/10, ALPT = 7.08, BETA = -0.27, QINF = 295.4,

RNPU = 2.2E+06, CNWP = 0.4828

r1 = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x,/c CP

0.020 0.148 0,000 0.779 0.003 3.580 ** 0.010 -0.556

0.060 -0.114 0.020 -0.181 0.020 -0.028 0.020 -0.283

0.110 -0.342 0.040 -0.054 0.060 -4.762** 0.060 -0.594

0.200 -0.676 0.060 -0.332 0.090 -0.445 0.110 -0,765

0.230 -0.631 0.090 -0,349 0.110 -0.573 0.140 -0,936

0.400 -0.645 0,130 -0.508 0.130 -0.596 0.190 - 1.775"*

0.490 -0.566 0. 150 -0.700 0.150 -0.859 0.250 -0.923

0.590 -0.605 0.200 -0.688 0.210 -0,729 0.400 -0.699

0.630 -0.464 0.250 -0.769 0.250 -0.765 0.490 -0.614

0.700 -0.505 0.260 -0.744 0.340 -0.767 0.580 -0.521

0.750 -0.510 0.280 -0.740 0,370 -0,755 0.650 -0.494

0.810 -0.546 0.290 -0.736 0,400 -0.868 0.700 -0.491

0.840 -0.544 0.310 -0.786 0.410 -2.786** 0.750 -0.604

0.900 -0.404 0.320 -0.764 0.430 -0.791 0.800 -0.971

0.960 -0.437 0.340 -0.705 0.440 -0.748 0.830 -0,634

0.350 -0.415"* 0.460 -0.790 0.900 -0.451

0.370 -0.735 0.490 -0.771 0,960 -0.453

0.380 -0.768 0.500 -0.841

0.400 -0.699 0.520 -0.766

0.410 -0.762 0.540 -0.798

0.430 -0.721 0.550 -0.828

0.440 -0.712 0.580 -0.819

0.460 -0.799 0.600 -0.738

0.470 -0.707 0.610 -0.739

0.490 -0.791 0.650 2.189**

0.500 -0.822 0.700 -0.762

0.520 -0.795 0.750 -0.808

0,530 -0.772 0.820 -0.455

0.550 -0.833 0.890 -0.379

0.560 -0.718 0.900 -0.434

0,580 -0,793 0.960 -0.360

0.590 -0,839

0.600 -0.857

0.640 -0.841

0.700 -0.809

0.750 0.003**

0.820 -0.289

0.870 -0.311

0.930 -0.316

0,960 -0.326

Lower Surface

0.020 -0.612 0,020 -0.241 0.020 -0.119 0.020 0,222

0.110 -0,157 0.060 -0.010 0.060 0.102 0.060 1.895"*

0.230 0.023 0.090 -0.063 0.090 1.185"* 0.110 0.049

0.400 -0.010 0.120 -0.018 0.120 -0.309 0.250 -0.083

0.490 -0.020 0.200 0.020 0.200 -0.055 0.400 -0.108

0,630 1.956"* 0.260 -0.075 0.250 -0.026 0.490 -0.169

0.750 0.144 0.400 -0.021 0.400 -0.047 0.5 g0 -0. I 01

0.850 0.239 0.490 -0.017 0.490 0.002 0,650 0.131

0.900 0.307 0,580 0.056 0.580 0.046 0.750 0.300

0.960 0.098 0.640 0.265 0.650 -0.020 0.830 0.494

0.750 0.367 0.750 0.371 0.900 0.536

0.870 0.426 0,890 0.412 0.960 0.360

0.930 0.303 0,930 0.348

0.960 0.197 0.960 -2,874**

CN = 0,536 0.702 0.716 0.733

437
Table G-2. Continued.

Flight 201, Wing sweep = 26 °, Time = 9-30-23-000, MINF = 0.893, Camber = 5/10, ALPT = 4.09, BETA = 0.57, QINF = 291.1,

RNPU = 2.2E+06, CNWP = 0.4156

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.365 0.000 0.599 0.000 0.977"* 0.010 -0.021

0.060 0.008 0.020 O. 195 0.020 0.294 0.020 -0.002"*

0.110 -0.237 0,040 0.259 0.060 0.69 l** 0.060 -0.367"*

0.200 -0.737 0.060 -0.087 0.090 -0.199 0.110 -0.512

0.230 -0.613 0.090 -0.194 0.110 -0,423 0.140 -0.795

0,400 -0.418 0.130 -0,340 0.130 -0.504 0.190 - 1.791 **

0.490 -0.085 0.150 -0.551 0.150 -0.671 0.250 -0.562

0.590 -0.179 0.200 -0.574 0.210 -0.640 0.400 -0.568

0.630 -0.230 0.250 -0.675 0.250 -0.637 0.490 -0.344

0.700 -0.303 0.260 -0.616 0.340 -0.682 0.580 -0.319

0.750 -0.847 0.280 -0.634 0.370 -0.690 0.650 -0,370

0.810 -0.800 0.290 -0.619 0.400 -0.663 0.700 -0.339

0.840 -0.838 0.310 -0.609 0.410 -0.634 0.750 -0.459

0.900 -0.287 0.320 -0.602 0,430 -0.590 0.800 - 1.015

0.960 -0.296 0.340 -0.597 0.440 -0.541 0.830 -0.729

0.350 -0.318"* 0.460 -0,284 0.900 -0.394

0.370 -0.598 0.490 -0.312 0.960 -0.391 **

0.380 -0.657 0.500 -0.304

0.400 -0.569 0.520 -0.250

0.410 -0.630 0.540 -0.292

0.430 -0.597 0.550 -0.270

0.440 -0.554 0.580 -0.245

0.460 -0.648 0.600 -0.279

0.470 -0.604 0.610 -0.279

0.490 -0.605 0,650 0.054**

0.500 -0.605 0.700 -0.478

0.520 -0.604 0.750 -0.535

0.530 -0.509 0.820 -0.507

0.550 -0.398 0.890 -0.411

0.560 -0.300 0.900 -0.436

0,580 -0.221 0,960 -0.382

0.590 -0.226

0.600 -0.229

0.640 -0.317

0.700 -0.319

0.750 0.060**

0.820 -0.514

0,870 -0.382

0.930 -0.309

0,960 -0.312

Lower Surface

0.020 - 1.307 0.020 - 1.202 0.020 - 1.023 0.020 -0.188

0.110 -0.255 0.060 -0.904 0.060 -0.273 0.060 - 1.254

0.230 -0,063 0.090 -0.379 0.090 -0.244 0.110 -0.236

0.400 0.017 0.120 -0.119 ** 0.120 -0.445 0.250 -0.250

0.490 0.068 0,200 -0.035 0.200 -0.105 0.400 -0.284

0.630 2.657"* 0.260 -0.124 0.250 -0.228 0.490 -0.229

0.750 0.193 0.400 -0.065 0.400 -0.123 0.580 -0.137

0.850 0.249 0.490 -0.022 0.490 0.051 0.650 0.102

0.900 0,330 0.580 0.048 0.580 0.013 0.750 0.331

0.960 0.135 0.640 0.280 0.650 0.050 0.830 0.446

0.750 0.374 0.750 -0.001 ** 0.900 0.521

0.870 0.431 0.890 0.460 0.960 0.383

0.930 0.350 0.930 0.373

0.960 0.223 0,960 0.473

CN = 0.429 0.445 0.454 0.382

438
Table G-2. Continued.

Flight 201, Wing sweep = 26", Time = 9-30-39-500, MINF = 0.899, Camber = 5/10, ALPT = 6.15, BETA = 0.14, QINF = 290.3,

RNPU = 2.2E+06, CNWP = 0.5217

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.207 0.00O 0.771 0.00O 1.028** 0.010 -0.348

0.060 -0,038 0.020 0.031 0.020 0.076 0.020 -0.163"*

0.110 -0,262 0.040 0.128 0.060 0.495"* 0.060 -0.587 **

0.200 -0.742 0.060 -0.203 0.09t3 -0.339 0.110 -0.739

0.230 -0.641 0.090 -0.281 0.110 -0.503 0.140 -0.914

0.400 -0.586 0. 130 -0.403 0.130 -0.579 0.190 - 1.769"*

0.490 -0.484 0.150 -0.631 0.150 -0.722 0.250 -0.886

0.590 -0.489 0.200 -0,667 0.210 -0.731 0.400 -0.658

0.630 -0.409 0.250 -0.770 0.250 -0.747 0.490 -0.566

0.700 -0_467 0.260 -0.712 0.340 -0.804 0.580 -0.448

0.750 -0,509 0.280 -0.750 0,370 -0.826 0.650 -0.490

0.810 -0.491 0.290 -0.741 0.400 -0.806 0.700 -0.471

0.840 -0.538 0.310 -0.715 0.410 -0.791 0.750 -0.553

0.900 -0.343 0.320 -0.711 0.430 -0.812 0.800 - 1.035

0.960 -0.358 0,340 -0.713 0.440 -0.781 0.830 -0.672

0.350 -0.318"* 0.460 -0.559 0.900 -0.439

0.370 -0.713 0.490 -0.745 0.960 -0.435**

0.380 -0.785 0.500 -0.816

0.400 -0.684 0.520 -0.793

0.410 -0.757 0.540 -0.815

0.430 -0.734 0.550 -0.791

0.440 -0.676 0.580 -0.750

0,460 -0.761 0.600 -0.693

0,470 -0.734 0.610 -0.616

0.490 -0,737 0.650 0.042**

0.500 -0.735 0.700 -0.642

0.520 -0.746 0.750 -0.650

0.530 -0.718 0.820 -0.243

0.550 -0.743 0.890 -0.388

0.560 -0.756 0.900 -0.392

0.580 -0.720 0.960 -0.364

0.590 -0.778

0.600 -0.757

0.640 -0.793

0,700 -0.841

0.750 0.087**

0.820 -0.278

0.870 -0.304

0.930 -0.321

0,960 -0.312

Lower Surface

0.020 -0.925 0.020 -0.835 0.020 -0.468 0.020 0.140

0.110 -0.142 0.060 -0.053 0.060 0.04 1 0.060 - 1.087

0.230 0.019 0.090 -0.098 0.090 -0.011 0.110 0.005

0.400 0.017 0.120 -0.051 * * 0.120 -0.267 0.250 -0.127

0.490 0.033 0.200 0.029 0.200 -0.017 0.400 -0.146

0.630 2.692"* 0.260 -0.068 0.250 -0.070 0.490 -0.164

0.750 0.182 0.400 -0.034 0.400 -0.060 0.580 -0. 110

0.850 0.223 0,490 -0.0O2 0.490 0,063 0.650 0.149

0.900 0.323 0.580 0.064 0.580 0.033 0.750 0.373

0.960 0.112 0.640 0.285 0.650 0.077 0.830 0.485

0.750 0.363 0.750 0.018** 0.900 0.559

0.870 0.453 0.890 0.518 0.960 0.387

0.930 0,370 0.930 0.416

0.960 0.247 0.960 0.519

CN = 0.515 0,673 0.669 0.605

439
Table G-2, Continued.

Flight 201, Wing sweep = 26 °, Time = 9-30-47-000, MINF = 0.888, Camber = 5/10, ALPT = 8.98, BETA = 0.31, QINF = 285.9,

RNPU = 2.2E+06, CNWP = 0.6378

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.174 0.000 0.898 0.000 0,837** 0,010 -0.716

0.060 -0.394 0.020 -0.561 0,020 -0,333 0.020 -0.771 **

0.110 -0.496 0.040 -0.189 0.060 0.242** 0.060 -0,854**

0.200 -0,847 0.060 -0.532 0.090 -0.684 0.110 - 1.014

0.230 -0.783 0.090 -0.626 0.110 -0,863 0.140 - 1.134

0.400 -0.762 0.130 -0.691 0.130 -0,852 0.190 - 1.813"*

0.490 -0.687 0.150 -0,857 0.150 -0.954 0.250 - 1.153

0.590 -0.674 0.200 -0.866 0.210 -0.963 0.400 -0.867

0.630 -0.609 0,250 -0.971 0,250 -0,972 0.490 -0.749

0,700 -0.657 0.260 -0.902 0.340 - t .038 0,580 -0,668

0.750 -0.520 0.280 -0.961 0,370 - 1.021 0,650 -0,663

0.810 -0.518 0,290 -0.945 0.400 -0.989 0,700 -0.646

0.840 -0.578 0.310 -0.933 0,410 -1.005 0.750 -0,722

0.900 -0.478 0.320 -0,933 0.430 - 1.030 0.800 -0.856

0.960 -0.506 0.340 -0.926 0.440 - 1,009 0,830 -0.788

0,350 -0.322** 0,460 -0.787 0,900 -0.537

0.370 -0.912 0,490 -0,987 0.960 -0,530**

0,380 -0.989 0,500 - 1.043

0,400 -0.883 0.520 -0.998

0.410 -0.955 0.540 - 1.029

0,430 -0.952 0,550 - 1.025

0.440 -0.894 0.580 -0.998

0,460 - 1.001 0.600 -0.995

0.470 -0,959 0.610 -0,994

0,490 -0,955 0.650 0,027* *

0.500 -0.963 0.700 -0.699

0.520 -0.961 0,750 -0.638

0,530 -0.925 0.820 -0.268

0.550 -0.946 0.890 -0.540

0.560 -0,959 0.900 -0.498

0.580 -0.936 0,960 -0,441

0.590 -0,997

0,600 -0.990

0.640 -0.448

0.700 -0.414

0.750 0.095**

0,820 -0.326

0.870 -0.347

0.930 -0,362

0.960 -0,341

Lower Surface

0.020 -0.201 0,020 0,054 0,020 0.162 0.020 0.486

0. l 10 -0.026 0.060 0.206 0.060 0.274 0.060 -0.919

0.230 0.134 0,090 0.126 0.090 0.222 0.110 0.159

0,400 0.029 0.120 0.135"* 0.120 -0,056 0,250 0.035

0.490 0.049 0.200 0.128 0.200 0.080 0,400 -0.011

0.630 2.718"* 0.260 0.044 0.250 0.081 0,490 -0,049

0.750 0.144 0.400 0.033 0.400 0.032 0.580 -0.028

0.850 0.193 0.490 0.030 0.490 0.071 0,650 0.174

0.900 0.275 0.580 0.073 0.580 0.078 0.750 0.393

0,960 0,079 0.640 0.293 0,650 0.085 0.830 0.503

0,750 0,364 0,750 0.003** 0.900 0,568

0,870 0.444 0.890 0.533 0.960 0.371

0.930 0.341 0.930 0.399

0.960 0.231 0.960 0.519

CN = 0.695 0,834 0.916 0,859

440
Table G-2. Continued.

Flight 201, Wing sweep = 26 °, Time = 8-40-10-000, MINF = 0.902, Camber = 10/10, ALPT = 4.04, BETA = 0.45, QINF = 387.2,

RNPU = 2.9E+06, CNWP = 0.3596

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.647 0.000 0.174 0.000 0.787"* 0.010 0.512

0.060 0.180 0.020 0.637 0.020 0.685 0.020 0.395"*

0.110 -0.139 0.040 0.516 0.060 0.563** 0.060 -0.116"*

0.200 -0.852 0.060 0.116 0.090 -0.103 0.110 -0.465

0.230 -0.713 0.090 -0.086 0.110 -0.353 0.140 -0.855

0,400 -0.582 0.130 -0.304 0,130 -0.578 0,190 - 1,754"*

0,490 -0,397 0,150 -0.602 0.150 -0.749 0,250 -0,630

0.590 -0,146 0.200 -0.690 0.210 -0.724 0.400 -0.585

0.630 -0.175 0.250 -0,717 0.250 -0.704 0.490 -0,311

0,700 -0,213 0,260 -0,681 0.340 -0.716 0.580 -0.291

0.750 -0.801 0.280 -0.693 0.370 -0.706 0.650 -0.356

0,810 -0.741 0.290 -0.662 0.400 -0,682 0.700 -0.329

0.840 -0.796 0.310 -0.642 0.410 -0.667 0.750 -0.435

0,900 -0.210 0.320 -0.647 0.430 -0.675 0.800 -0.970

0.960 -0.207 0.340 -0.646 0,440 -0.661 0.830 -0.941

0,350 -0.361 ** 0.460 -0.471 0,900 -0.410

0,370 -0,651 0.490 -0.468 0.960 -0.399**

0.380 -0.673 0.500 -0.415

0.400 -0,595 0.520 -0.325

0.410 -0.632 0,540 -0.296

0.430 -0,618 0.550 -0.275

0.440 -0.588 0.580 -0.235

0.460 -0.651 0.600 -0.253

0.470 -0.633 0,610 -0.275

0.490 -0.636 0.650 -0,008"*

0.500 -0.613 0.700 -0.445

0,520 -0,615 0.750 -0.465

0,530 -0.597 0,820 -0,570

0.550 -0.622 0,890 -0,413

0.560 -0.623 0.900 -0,400

0.580 -0,609 0.960 -O362

0.590 -0.612

0,600 -0.508

0,640 -0.466

0.700 -0.484

0.750 0.011"*

0,820 -0,377

0.870 -0.240

0.930 -0,261

0,960 -0.266

Lower Surface

0,020 -0,999 0,020 -0.848 0.020 - 1.406 0,020 -0,777

0.110 -0.744 0,060 -0,860 0.060 - 1.030 0.060 - 1.091

0.230 -0.167 0.090 -0.872 0.090 -0.955 0,110 -0,248

0.400 0.059 0,120 -0,712** 0.120 -0.530 0.250 -0.342

0.490 0.068 0.200 -0.131 0.200 -0.133 0,400 -0.236

0,630 1.590* * 0.260 -0.200 0.250 -0,147 0.490 -0.386

0.750 0.143 0.400 -0.075 0,400 -0,131 0.580 -0.145

0.850 0.153 0.490 -0.004 0,490 -0,007 0.650 0,097

0,900 0,206 0.580 0.073 0.580 0.004 0.750 0.333

0.960 0,110 0.640 0.240 0.650 0.001 0.830 0.438

0.750 0.290 0,750 -0,035** 0.900 0,523

0.870 0,365 0,890 0,457 0.960 0.390

0,930 0,299 0.930 0.355

0.960 0,184 0.960 0.360

CN = 0,358 0.398 0.395 0,375

441
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-2-12-500, MINF = 0.899. Camber = 10/10, ALPT = 5.09, BETA = 0.02, QINF = 299.1,

RNPU = 2.3E+06. CNWP = 0.3417

11= 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.546 0.000 0,197 0.000 3.520** 0.0 l0 0.420

0.060 0.136 0.020 0.376 0.020 0.580 0.020 0.291

0.110 -0.203 0.040 0.376 0.060 -4,718"* 0.060 -0.162

0.200 -0.873 0,060 -0.002 0.090 -0.147 0.110 -0.495

0.230 -0.749 0.090 -0.161 0.110 -0.444 0.140 -0.904

0.400 -0.645 0.130 -0.392 0.130 -0.615 0.190 - 1.768 **

0.490 -0.485 0.150 -0.702 0.150 -0,846 0.250 -0.821

0.590 -0.470 0,200 -0,745 0.210 -0.790 0.400 -0.643

0.630 -0.354 0.250 -0,800 0.250 -0.742 0.490 -0.423

0.700 -0.416 0.260 -0.737 0.340 -0.773 0.580 -0.404

0.750 -0.570 0.280 -0.764 0.370 -0.776 0.650 -0.422

0.810 -0,604 0.290 -0.746 0.400 -0.798 0.700 -0.417

0.840 -0.627 0.310 -0.746 0.410 -2.766** 0,750 -0.495

0.900 -0.263 0.320 -0.729 0.430 -0.766 0.800 - 1.023

0.960 -0.272 0.340 -0.711 0.440 -0.733 0.830 -0.860

0.350 -0.441"* 0.460 -0.762 0.900 -0.438

0.370 -0.693 0.490 -0.678 0.960 -0.439

0.380 -0.769 0.500 -0.798

0.400 -0.66 l 0.520 -0.721

0.410 -0.745 0.540 -0.666

0.430 -0.704 0.550 -0.575

0.440 -0.657 0.580 -0.438

0.460 -0.768 0.600 -0.388

0.470 -0.707 0.610 -0.367

0.490 -0.713 0.650 2.146**

0.500 -0.745 0.700 -0.522

0.520 -0.723 0.750 -0.595

0.530 -0.703 0.820 -0.590

0.550 -0.738 0.890 -0.389

0.560 -0.706 0,900 -0.394

0.580 -0.711 0.960 -0.343

0.590 -0.755

0.600 -0.772

0.640 -0.770

0.700 -0.800

0,750 -0.030**

0.820 -0.342

0.870 -0,274

0.930 -0.302

0.960 -0.286

Lower Surface

0.020 -0.898 0.020 -0.183 0.020 - 1.303 0.020 -0.713

0.110 -0.609 0.060 -0.680 0.060 -0.626 0.060 1.856"*

0.230 -0.080 0.090 -0.498 0.090 1.155** 0.110 -0,069

0.400 0.035 0.120 -0.281 0.120 -0,363 0.250 -0.176

0.490 0.062 0.200 -0.076 0,200 -0.143 0.400 -0.230

0.630 1.916'* 0.260 -0.144 0,250 -0.092 0.490 -0.242

0.750 0. t 12 0.400 -0.036 0.400 -0.102 0.580 -0.155

0. 850 0.186 0.490 -0.013 0.490 -0,032 0.650 0.107

0.900 0.217 0.580 0.059 0.580 0,023 0.750 0.290

0.960 0.085 0,640 0.242 0.650 -0.057 0.830 0.460

0.750 0,306 0.750 0.3 l 8 0.900 0.508

0.870 0.378 0.890 0.370 0,960 0.352

0.930 0.288 0.930 0.299

0.960 0.183 0.960 -2.854**

CN = 0.430 0.558 0.525 0.569

442
Table G-2. Continued,

Flight 226, Wing sweep = 26 °, Time = 10-2-36-500, MINF = 0.899, Camber = 10/10, ALPT = 5.99, BETA = -0.21, QINF = 301.3,

RNPU = 2.3E+06, CNWP = 0.4245

rl = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0,512 0.000 0.280 0.000 3.481 ** 0,010 0,294

0.060 0.109 0.020 0.319 0.020 0.514 0.020 0.228

0.110 -0.085 0,040 0,324 0.060 -4.696** 0.060 -0.304

0.200 -0.883 0.060 -0.030 0.090 -0.200 0.110 -0.606

0.230 -0.870 0.090 -0,200 0.110 -0,484 0.140 -0,931

0.400 -0,683 0.130 -0.381 0,130 -0.656 0,190 -1.767"*

0.490 -0.542 0.150 -0.739 0.150 -0.888 0.250 -0.918

0.590 -0.548 0.200 -0.777 0.210 -0.829 0.400 -0.664

0.630 -0.414 0.250 -0.842 0.250 -0.792 0.490 -0.512

0.700 -0.467 0.260 -0.776 0.340 -0.825 0.580 -0.441

0.750 -0.486 0.280 -0,817 0.370 -0.815 0,650 -0.477

0.810 -0,491 0.290 -0.799 0.400 -0.842 0.700 -0.463

0.840 -0.472 0.310 -0.796 0.410 -2.759"* 0.750 -0.536

0.900 -0.319 0.320 -0.779 0.430 -0.833 0.800 - 1.048

0.960 -0.325 0.340 -0.758 0.440 -0.797 0.830 -0.906

0.350 -0.452** 0.460 -0.821 0.900 -0.464

0.370 -0.741 0.490 -0.753 0,960 -0.465

0.380 -0.824 0.500 -0.856

0,400 -0.698 0.520 -0.798

0.410 -0.805 0.540 -0,808

0.430 -0.754 0.550 -0.776

0.440 -0,674 0.580 -0.712

0.460 -0.819 0,600 -0.634

0,470 -0.745 0.610 -0.603

0.490 -0.769 0.650 2,118"*

0,500 -0,775 0.700 -0.589

0,520 -0.715 0.750 -0.647

0.530 -0.752 0,820 -0.529

0.550 -0,803 0.890 -0.392

0.560 -0.760 0.900 -0,423

0,580 -0.777 0.960 -0,370

0,590 -0.818

0.600 -0,833

0,640 -0,824

0.700 -0.853

0.750 -0,028**

0.820 -0.31 t

0,870 -0.299

0.930 -0.334

0.960 -0.329

Lower Surface

0.020 -0.881 0.020 -0.172 0.020 - 1.152 0.020 -0.571

0. I 10 -0.530 0,060 -0.531 0.060 -0,297 0.060 1,830**

0,230 -0.066 0.090 -0.455 0.090 1.133" * 0.110 -0.026

0.400 0.040 0,120 -0.110 0.120 -0,333 0.250 -0.133

0.490 0.056 0,200 -0.073 0.200 -0.147 0.400 -0.176

0.630 1.889"* 0.260 -0.065 0.250 -0.046 0.490 -0,216

0.750 0.117 0.400 -0.026 0,400 -0.089 0.580 -0.142

0.850 0.187 0,490 -0.014 0,490 -0.022 0,650 0,108

0.900 0.228 0.580 0.069 0.580 0.039 0.750 0,305

0.960 0.075 0,640 0.220 0,650 -0.051 0,830 0.476

0.750 0.290 0.750 0,343 0,900 0.518

0.870 0,340 0.890 0.391 0.960 0.358

0.930 0,259 0.930 0,321

0,960 0.165 0.960 -2.845**

CN = 0.464 0.611 0,626 0.652

443
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-2-57-500, MINF = 0.902, Camber = 10/10, ALPT = 7.98, BETA = -0.15, QINF = 308.0,

RNPU = 2.3E+06, CNWP = 0.5400

_q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0,448 0.000 0.444 0.000 3.377"* 0.010 0.126

0.060 0.016 0.020 0.239 0.020 0.403 0.020 0.082

0. 110 -0,363 0.040 0.232 0.060 -4.622** 0.060 -0.459

0.200 -0.931 0.060 -0.134 0.090 -0.287 0.110 -0.764

0,230 -0.851 0.090 -0.271 0.110 -0.561 0.140 -0.979

0,400 -0.733 0.130 -0.505 0.130 -0.736 0,190 - 1.757"*

0.490 -0.647 0.150 -0.793 0.150 -0.950 0,250 - 1.035

0.590 -0.599 0.200 -0.831 0.210 -0.900 0.400 -0.764

0.630 -0,524 0.250 -0.910 0.250 -0.872 0.490 -0.646

0,700 -0.577 0.260 -0.851 0.340 -0.923 0.580 -0.562

0,750 -0,547 0.280 -0.891 0.370 -0.926 0.650 -0.565

0.810 -0,549 0.290 -0.891 0.400 -0.966 0.700 -0.563

0.840 -0,555 0.310 -0.884 0.410 -2.727** 0.750 -0.633

0,900 -0.443 0.320 -0.874 0.430 -0.945 0.800 - 1.092

0.960 -0.483 0.340 -0.847 0,440 -0,890 0.830 -0.832

0.350 -0.472** 0,460 -0.931 0.900 -0,550

0.370 -0.834 0.490 -0.861 0.960 -0.549

0.380 -0.912 0.500 -0.955

0.400 -0.800 0.520 -0.911

0.410 -0.884 0,540 -0.922

0.430 -0.849 0.550 -0.901

0.440 -0.810 0.580 -0.883

0,460 -0,928 0.600 -0.877

0.470 -0.854 0.610 -0.878

0.490 -0.870 0.650 2.043"*

0.500 -0.885 0.700 -0.982

0.520 -0.933 0.750 -0.992

0.530 -0.855 0.820 -0.497

0.550 -0.908 0.890 -0.461

0.560 -0.845 0.900 -0.464

0.580 -0.869 0.960 -0.412

0.590 -0.916

0.600 -0.924

0.640 -0.908

0.700 -0.660

0,750 -0,016"*

0.820 -0.369

0.870 -0.352

0.930 -0.394

0.960 -0.389

Lower Surface

0.020 -0.580 0.020 -0.158 0.020 -0.535 0.020 -0.159

0. 110 -0,304 0,060 -0.259 0.060 0,048 0.060 1.762"*

0,230 -0.030 0.090 -0.135 0.090 1.080** 0.110 0.1 04

0.400 0.029 0.120 0.078 0.120 -0.208 0.250 -0,027

0.490 0.034 0.200 -0.035 0,200 -0.123 0.400 -0.087

0.630 1.820"* 0.260 0.014 0.250 0.035 0,490 -0.145

0.750 0.115 0.400 0.008 0.400 -0,028 0.580 -0.099

0.850 0.176 0,490 -0.002 0.490 -0.010 0.650 0.136

0.900 0.224 0.580 0,068 0,580 0.060 0.750 0.331

0.960 0.045 0.640 0.257 0.650 -0.038 0.830 0.499

0,750 0,332 0.750 0.351 0.900 0.543

0.870 0.387 0.890 0.447 0.960 0.356

0.930 0.283 0.930 0.365

0.960 0.177 0.960 -2.812"*

CN = 0.573 0.726 0.810 0.810

444
Table G-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 10-3-6-500, MINF = 0.899, Camber = 10/10, ALPT = 10.23, BETA = -0.15, QINF = 316.8,

RNPU = 2.4E+06, CNWP = 0.5804

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP xA" CP

0.020 0.343 0.000 0.641 0,000 3.225"* 0.010 -0.047

0.060 -0.095 0.020 0.076 0.020 0.203 0.020 -0.109

0.110 -0.384 0.040 0.077 0.060 -4.554** 0.060 -0.622

0.200 -0.984 0.060 -0.279 0.090 -0,497 0.110 -0.909

0.230 -0.718 0.090 -0.386 0.110 -0.706 0.140 - 1.186

0.400 -0.857 0.130 -0.630 O. 130 -0.830 0.190 - 1.768"*

0.490 -0.743 O. 150 -0.883 O. 150 - 1.058 0.250 - 1.198

0.590 -0.759 0,200 -0.917 0.210 -0,994 0.400 -0.912

0.630 -0.660 0,250 - 1.024 0.250 -0,968 0.490 -0.784

0.700 -0.706 0.260 -0.941 0.340 - 1.029 0.580 -0.692

0.750 -0.489 0.280 -0.980 0.370 - 1.022 0.650 -0.681

0.810 -0.497 0.290 -0.997 0.400 - 1.033 0,700 -0.676

0.840 -0.515 0.310 -0.988 0.410 -2.711 ** 0,750 -0.716

0.900 -0.464 0.320 -0.963 0.430 -1.064 0.800 -0.869

0,960 -0.507 0.340 -0.964 0,440 - 1.023 0.830 -0.987

0.350 -0.480** 0.460 - 1,038 0.900 -0,608

0.370 -0.946 0.490 -0.961 0.960 -0.565

0.380 - 1.026 0.500 - 1.067

0,400 - 1.037 0.520 - 1.028

0.410 - 1.004 0,540 - 1.044

0.430 -0.953 0.550 - 1.010

0.440 -0.942 0.580 - 1.022

0.460 -1.041 0.600 -1.015

0.470 -0.978 0.610 - 1.012

0.490 -0.974 0.650 1.928"*

0.500 -1.005 0.700 -0.858

0.520 -0.983 0.750 -0.737

0.530 -0.983 0.820 -0.562

0.550 - 1.020 0.890 -0.582

0.560 -0.994 0.900 -0.563

0.580 -0.982 0.960 -0.505

0.590 -1.001

0.600 -1.027

0.640 -0.500

0.700 -0.489

0.750 -0.022**

0.820 -0.397

0.870 -0405

0.930 -0.443

0.960 -0.430

Lower Surface

0.020 -0.665 0.020 -0.174 0.020 -0.049 0.020 0.263

0.110 0.002 0.060 0.144 0.060 0.271 0.060 1.654**

0.230 0,032 0,090 0,102 0.090 0.992"* 0.110 0.194

0.400 0.040 0.120 0,148 0.120 -0.049 0.250 0.079

0.490 0.044 0.200 0.028 0.200 -0.049 0,400 0.005

0.630 1.711 ** 0.260 0.106 0.250 0.134 0.490 -0,055

0.750 0.125 0.400 0.062 0.400 0,035 0.580 -0.042

0.850 0.184 0.490 0.032 0,490 0.001 0.650 0.178

0.900 0.254 0.580 0.075 0.580 0.090 0.750 0.363

0.960 0.041 0.640 0.287 0.650 -0.055 0.830 0.533

0.750 0.355 0.750 0.311 0.900 0.568

0.870 0.424 0.890 0.472 0,960 0.360

0.930 0.320 0.930 0.366

0.960 0.190 0.960 -2.794 * *

CN = 0.673 0.838 0.930 0.989

445
Table G-2. Continued.

Flight 215, Wing sweep = 26 °, Time = 10-6-14-500, MINF = 0.899, Camber = 10/15, ALPT = 3.98, BETA = -0.24, QINF = 301.8,

RNPU = 2.3E+06, CNWP = 0.2946

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0,450 0.000 0.144 0.000 -0.140"* 0.010 0.293

0.060 0.143 0.020 0.306 0.020 0.604 0.020 0.298

0.110 -0.221 0.040 0.333 0.060 0.549"* 0.060 -0.212

0.200 -0.901 0.060 -0.079 0.090 -0.161 0.110 -0.540

0.230 -0.866 0.090 -0.274 0.110 -0.433 0.140 - 1.002

0.400 -0.702 0.130 -0.499 0.130 -0.733 0.190 - 1.766 **

0.490 -0.401 0,150 -0.787 0,150 -0.816 0.250 -0.804

0.590 -0.306 0.200 -0.862 0.210 -0.902 0.400 -0.613

0.630 -0.231 0.250 - 1.235 0.250 -0.862 0.490 -0.374

0.700 -0.393 0.260 -0.826 0.340 -0.859 0.580 -0.370

0.750 -0.731 0.280 -0.750 0.370 -0.869 0.650 -0.408

0.810 -0.658 0.290 -0.845 0.400 -0.841 0,700 -0.393

0,840 -0.649 0.310 -0.809 0.410 -2.754"* 0.750 -0.501

0.900 -0.553 0.320 -0.698 0.430 -0.853 0.800 -0.902

0.960 -0.562 0.340 -0.808 0.440 -0.696 0.830 -0.764

0.350 -0.395** 0.460 -0.791 0.900 -0.687

0.370 -0.792 0.490 -0.563 0.960 -0.703

0.380 -0.858 0.500 -0.560

0.400 -0.986 0.520 -0.374

0.410 -0.824 0.540 -0.347

0.430 -0.662 0.550 -0.781

0.440 -0.723 0.580 -0.993

0.460 -0.725 0.600 -0.311

0.470 -0.792 0.610 -0.391

0.490 -0.682 0.650 -0.901

0.500 -0.684 0.700 -0.615

0.520 -0.778 0.750 -0.691

0.530 -0.768 0.820 -0.704

0.550 -0.697 0.890 -0.660

0.560 -0.792 0.900 -0.637

0.580 -0.749 0.960 -0.589

0.590 -0.717

0.600 -0.620

0.640 -0.625

0.700 -0.622

0.750 -0.157"*

0,820 -0.623

0.870 -0.497

0.930 -0,525

0.960 -0.527

Lower Surface

0.020 - 1.014 0.020 - 1.066 0.020 - 1.410 0.020 -0.820

0.110 -0.747 0.060 -0.700 0.060 - 1.178 0.060 -0.152

0.230 -0.213 0.090 -0.582 0.090 -0.529 0. I 10 -0.400

0.400 0.053 0.120 -0.467 0.120 -0.534 0.250 -0.343

0.490 -0.018 0.200 -0.206 0.200 -0.822 0.400 -0.323

0.630 3.040"* 0.260 -0.305 0.250 -0.207 0.490 -0.267

0.750 0.052 0.400 -0.126 0,400 -0.165 0.580 -0.133

0.850 0.081 0.490 -0.072 0.490 -0.053 0.650 0.221

0.900 0.127 0.580 0.004 0.580 -0.331 0.750 0.410

0.960 -0.055 0.640 0.132 0.650 -0.172 0.830 0.375

0.750 0.168 0.750 -0.045 0.900 0.559

0.870 0.355 0.890 0.344 0.960 0.432

0.930 0.217 0.930 0.381

0.960 0.127 0.960 0.391

CN = 0.394 0.545 0.440 0.534

446
Table G-2. Continued.

Flight 215, Wing sweep = 26 °. Time = 10-7-7-500, MINF = 0.898, Camber = 10/15, ALPT = 4.05, BETA = -0.07, QINF = 298.5,

RNPU = 2.3E+06, CNWP = 0.3422

1] = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.588 0.000 0.155 0.000 0.014"* 0,010 0.438

0.060 0.144 0.020 0.380 0.020 0.616 0.020 0.329

0.1 | 0 -0.186 0,040 0.482 0.060 0.675"* 0,060 -0.201

0,200 -0,899 0,060 0.032 0,090 -0,135 O. 110 -0.493

0.230 -0.734 0.090 -0.158 0.1 I0 -0.410 0.140 -0,935

0.400 -0,576 O. 130 -0,363 0.130 -0.628 0,190 - 1,772"*

0,490 -0,392 O, 150 -0,654 O.150 -0,797 0,250 -0,671

0.590 -0,182 0,200 -0.724 0,210 -0,780 0,400 -0.599

0,630 -0.217 0,250 -0,772 0.250 -0,740 0,490 -0,379

0,700 -0,270 0.260 -0,708 0,340 -0.771 0,580 -0,329

0,750 -0.678 0.280 -0,736 0.370 -0.720 0.650 -0.385

0.810 -0,552 0,290 -0.704 0,400 -0.745 0.700 -0.384

0.840 -0.536 0,310 -0.687 0,410 -2,771"* 0.750 -0.500

0,900 -0.442 0.320 -0,688 0.430 -0,705 0.800 -0.739

0.960 -0.463 0.340 -0.689 0.440 -0.676 0.830 -0.598

0.350 -0.381 ** 0.460 -0.663 0.900 -0.540

0.370 -0.673 0.490 -0.434 0.960 -0.550

0.380 -0.731 0.500 -0.429

0,400 -0.880 0.520 -0.356

0.410 -0,699 0.540 -0.323

0.430 -0.656 0.550 -0.320

0.440 -0.603 0.580 -0.299

0.460 -0.733 0.600 -0.315

0.470 -0.667 0,610 -0.318

0A90 -0.662 0,650 -0.778

0.500 -0.683 0.700 -0.494

0.520 -0.667 0.750 -0.571

0.530 -0.631 0.820 -0.576

0.550 -0.700 0.890 -0.528

0.560 -0,667 0,900 -0.533

0.580 -0.603 0,960 -0,440

0.590 -0.566

0.600 -0,485

0.640 -0.483

0.700 -0.446

0.750 -0,017"*

0.820 -0.498

0.870 -0,375

0.930 -0.392

0.960 -0.402

Lower Surface

0,020 -0.967 0.020 -0.961 0.020 - 1.412 0.020 -0.788

O, 110 -0.594 0.060 -0,547 0.060 - 1.038 0.060 -0,040

0.230 -0.074 0,090 -0.462 0,090 -0,384 O. 110 -0.377

0,400 0,049 O.120 -0.330 O, 120 -0,404 0.250 -0.220

0.490 0.094 0.200 -0.084 0,200 -0.127 0.400 -0.199

0.630 3.088"* 0.260 -0.181 0.250 -0.075 0.490 -0.149

0.750 0.165 0.400 -0.007 0.400 -0.039 0.580 0.003

0.850 0.201 0.490 0.043 0.490 -0.047 0.650 0.230

0,900 0.250 0.580 0.128 0.580 0.135 0.750 0.432

0.960 0,088 0.640 0.271 0.650 -0.050 0.830 0.484

0.750 0.301 0.750 -0.018 0.900 0.572

0.870 0.372 0.890 0,457 0.960 0.424

0.930 0.346 0.930 0.406

0.960 0.238 0,q60 0.506

CN = 0.420 0.531 0.483 0.546

447
Table G-2. Continued.

Flight 215, Wing sweep = 26 °, Time = 10-7-21-000, MINF = 0,904, Camber = 10/15, ALPT = 4.07, BETA = 0.02, QINF = 302.5,

RNPU = 2.3E+06, CNWP = 0.2596

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0,358 0,000 -0.046 0.000 -0.092** 0,010 0.082

0.060 -0. l 14 0.020 0.170 0.020 0.280 0.020 0.066

0.110 -0,410 0.040 0.267 0.060 0,303"* 0.060 -0.381

0.200 - 1.209 0.060 -0.176 0.090 -0.484 0.110 -0,723

0,230 -0.999 0,090 -0.367 0. l 10 -0.642 0.140 - 1.126

0,400 -0.941 0.130 -0,708 0.130 -0.811 0.190 - 1.747"*

0.490 -0.632 0.150 -0.872 0.150 - 1.016 0.250 -0,858

0.590 -0.583 0.200 -0.945 0,210 -0.986 0.400 -0,969

0.630 -0.580 0.250 - 1.112 0.250 - 1.074 0,490 -0.705

0.700 -0.479 0,260 -0.916 0.340 -0.942 0.580 -0.569

0,750 - 1.043 0.280 - 1.071 0.370 - 1.078 0.650 -0.618

0.810 -0.819 0.290 -0.942 0,400 -0.959 0.700 -0.715

0.840 -0.789 0.310 -1.018 0,410 -2,734** 0,750 -0.823

0,900 -0.772 0.320 -0,900 0.430 -0,949 0.800 - 1.011

0.960 -0,666 0.340 - 1.016 0.440 -0.908 0.830 -0,873

0.350 -0.605 ** 0.460 -0.936 0.900 -0.905

0.370 - 1.004 0.490 -0.757 0.960 -0.771

0.380 -0.926 0.500 -0.908

0,400 - 1.060 0.520 -0.667

0.410 - 1.035 0.540 -0.604

0.430 -0.984 0.550 -0.683

0.440 -0.834 0.580 -0,663

0.460 -0.945 0,600 -0.533

0.470 -0,895 0.610 -0.544

0,490 -0.888 0,650 -0.922

0.500 -0,914 0,700 -0.711

0,520 -0.897 0,750 -0.791

0,530 -0.860 0.820 -0.792

0,550 -0.915 0,890 -0,853

0.560 -0.887 0.900 -0.739

0,580 -0.885 0,960 -0,672

0.590 -0.914

0,600 -0.931

0.640 -0.844

0.700 -0.751

0.750 -0,223"*

0.820 -0,578

0.870 -0.575

0.930 -0.720

0.960 -0.722

Lower Surface

0.020 - I. 144 0.020 - 1.245 0.020 - 1.602 0.020 -0.999

0. I 10 -0.929 0,060 -0.812 0.060 - 1.248 0.060 -0.362

0.230 -0,296 0.090 -0.662 0.090 -0.594 0.110 -0.590

0.400 -0.168 0.120 -0.535 0.120 -0.614 0,250 -0.546

0,490 -0.138 0,200 -0.416 0,200 -0.363 0.400 -0.525

0.630 3,048"* 0.260 -0.486 0.250 -0.297 0.490 -0.251

0.750 -0.053 0.400 -0.325 0.400 -0,225 0.580 -0.218

0.850 -0,033 0.490 -0.162 0.490 -0.263 0.650 0.018

0.900 0.004 0,580 -0.198 0,580 -0.210 0.750 0,086

0,960 -0.157 0,640 0.04 1 0.650 -0.158 0.830 0.168

0.750 0,082 0,750 -0.249 0.900 0.240

0.870 0.162 0.890 0.133 0,960 0.114

0,930 0.143 0.930 0,206

0.960 -0.083 0.960 0.244

CN = 0,475 0.530 0.512 0.547

448
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-8-15-000, MINF = 0.905, Camber = 0/11, ALPT = 4.07, BETA = -0.03, QINF = 295.2,

RNPU = 2.2E÷06. CNWP = 03235

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.005 0.000 0.896 0.000 -5.503 ** 0.010 -0.679* *

0.060 -0.069 0.020 -0.417"* 0,020 -0.225"* 0.020 -0.617"*

0.110 -0.173 0.040 -0_ 143 0.060 -0.992" * 0.060 -0.579

0.200 -0.183 0,060 -0,273 0.090 -0.425 0.110 -0.564

0.230 -0.310 0.090 -0,251 0.110 -0.472 0.140 1.930"*

0.400 -0.098 0,130 -0.307 0.130 -0.378 0.190 -5,368" *

0.490 -0.119 0.150 -0.404 0.150 -0.407 0.250 -0.498

0.590 -0.197 0.200 -0.302 0.210 -0.455 0.400 -0.502

0.630 -0,222 0.250 -0.471 0.250 -0.469 0,490 -0.252

0,700 -0.328 0.260 -0.383 0.340 -0,564 0.580 -0.276

0.750 -0.829 0.280 -0.444 0.370 -0.546 0.650 -0.337

0.810 -0.828 0.290 -0.464 0.400 -0.465 0.700 -0.311

0.840 -0,794 0.310 -0.429 0.410 -0.408 0.750 -0.432

0.900 -0.304 0.320 -0.415 0.430 -0.483 0.800 -0.986

0.960 -0.340 0.340 -0.463 0.440 -0.478 0.830 -0.946

0.350 -0.347** 0.460 -0.477 0.900 -0.432

0.370 -0.451 0.490 -0.214 0.960 -0.432

0.380 -0.470 0,500 -0,252

0.400 -0.359 0.520 -0.195

0.410 -0.491 0.540 -0.213

0.430 -0.470 0.550 -0.197

0.440 -0.399 0,580 -0,203

0.460 -0.567 0,600 -0,227

0,470 -0.461 0.610 -0.160

0.490 -0.334 0.650 -2.600"*

0.500 -0.192 0,700 -0.430

0.520 -0.157 0.750 -0.4%

0.530 -0.120 0.820 -0.913

0.550 -0.160 0.890 -0.491

0.560 -0.125 0.900 -0.506

0.580 -0.120 0.960 -0.509

0.590 -0.163

0.600 -0.218

0.640 -2.437**

0.700 -0.366

0.750 -0.653

0.820 -2.613"*

0.870 -0,340

0.930 -0.340

0.960 -0.345

Lower Surface

0,020 -0.717 0.020 -0.411 0.020 -0.183 0.020 0,258

0.110 -0.486 0.060 -0.138 0.060 0.010 0.060 3.461 **

0.230 -0.025 0.090 -0.218 0.090 -0.127 0.110 -0.181

0.400 -0,008 0.120 -0.335 0.120 -0.538 0.250 -0,380

0.490 0.003 0.200 -0.473 0.200 -0.434 0.400 -0.285

0.630 3.505"* 0.260 -0.248 0.250 -0.380 0.490 -0.425

0.750 0.228 0.400 -2.631 ** 0.400 -0.104 0.580 -0.093

0.850 0.313 0.490 -0.022 0.490 0.028 0.650 0.126

0.900 0.358 0.580 0.117 0,580 0.029 0.750 0.347

0.960 0.153 0.640 0.490 0.650 0.306 0.830 0.454

0,750 0.354 0.750 0.022 0.900 0.555

0.870 0.426 0.890 ******** 0.960 0.390

0.930 0.378 0.930 0.42 l

0.960 0.225 0.960 -2.629**

CN = 0.306 0.401 0.417 0.424

449
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-8-25-500, MINF = 0.909, Camber = 0/10, ALPT = 5.16, BETA = 0.15, QINF = 296.5,

RNPU = 2.2E+06, CNWP = 0.3633

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0,020 -0.137 0.000 0.918 0.000 -5.471 * * 0.010 -0,683 * *

0.060 -0.328 0.020 -0,596** 0.020 -0.303** 0.020 -0.728**

0.110 -0.191 0.040 -0.240 0.060 - 1.079* * 0.060 -0.697

0.200 -0.278 0.060 -0.467 0.090 -0.558 0.110 -0.668

0.230 -0.316 0.090 -0,450 0.110 -0,643 0.140 1.896"*

0.400 -0.426 0.130 -0.471 0.130 -0,516 0.190 -5.337 **

0.490 -0.381 0.150 -0.481 0.150 -0.514 0.250 -0.715

0.590 -0.380 0.200 -0.386 0.210 -0.598 0.400 -0,556

0.630 -0.313 0.250 -0.567 0.250 -0.548 0.490 -0.435

0,700 -0.393 0.260 -0.478 0.340 -0.647 0.580 -0.420

0.750 -0.752 0.280 -0.567 0.370 -0.670 0.650 -0.419

0.810 -0.808 0.290 -0.551 0.400 -0.683 0.700 -0.413

0.840 -0.745 0.310 -0.510 0.410 -0.602 0.750 -0.482

0.900 -0.315 0.320 -0.490 0,430 -0.644 0.800 - 1.017

0.960 -0.374 0.340 -0.538 0.440 -0.631 0.830 -0.958

0.350 -0.342"* 0.460 -0.642 0,900 -0.437

0.370 -0.525 0.490 -0.557 0.960 -0.437

0.380 -0.543 0.500 -0.567

0.400 -0.452 0.520 -0.518

0.410 -0.568 0.540 -0.550

0.430 -0.558 0.550 -0.514

0.440 -0.481 0.580 -0.495

0.460 -0.651 0,600 -0.480

0.470 -0.545 0.610 -0.365

0.490 -0.563 0.650 -2.581 **

0,500 -0.595 0.700 -0.479

0.520 -0.566 0.750 -0.559

0,530 -0.547 0.820 -0.766

0.550 -0.573 0.890 -0.432

0.560 -0.560 0.900 -0.445

0.580 -0.554 0.960 -0.451

0.590 -0.581

0,600 -0.637

0.640 -2.418"*

0.700 -0.526

0.750 -0.560

0.820 -2.594"*

0.870 -0.313

0,930 -0.334

0,960 -0.317

Lower Surface

0.020 -0.421 0.020 -0.233 0.020 -0.032 0.020 0.373

0.110 -0.410 0.060 -0.051 0.060 0.083 0.060 3.454"*

0.230 -0.032 0.090 -0.146 0.090 -0.042 0.110 -0.105

0.400 -0.018 0.120 -0,244 0.120 -0,454 0.250 -0.238

0.490 -0.007 0.200 -0.096 0.200 -0.295 0,400 -0.243

0.630 3.497** 0.260 -0.291 0.250 -0.275 0.490 -0.377

0.750 0.215 0.400 -2.611 ** 0.400 -0.095 0.580 -0.120

0.850 0.300 0.490 -0.032 0.490 0.025 0.650 0.119

0.900 0.339 0.580 0.105 0,580 0.015 0.750 0.358

0.960 0.142 0.640 0.469 0.650 0.298 0.830 0.471

0.750 0.360 0.750 0.030 0,900 0.570

0.870 0.442 0.890 ******** 0.960 0.381

0.930 0.384 0.930 0.420

0,960 0.217 0.960 -2.610"*

CN = 0.418 0.544 0,546 0.562

450
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-8-31-000, MINF = 0.909, Camber = 0/10, ALPT = 6.15, BETA = 0,47, QINF = 296.0,

RNPU = 2.2E+06, CNWP = 0.4054

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.269 0,000 0.923 0.000 -5.477 * * 0.010 -0.659* *

0.060 -0.381 0.020 -0,632"* 0.020 -0.509"* 0.020 -0.747"*

0. 110 -0.349 0.040 -0.424 0.060 - 1.129"* 0.060 -0.838

0.200 -0.434 0,060 -0.541 0.090 -0.608 0.110 -0.746

0.230 -0.369 0.090 -0.527 0.110 -0.695 0.140 0.261"*

0.400 -0.476 0,130 -0.554 0.130 -0.601 0.190 -5.343**

0.490 -0.441 0.150 -0.567 0.150 -0.595 0.250 -0.770

0,590 -0.411 0.200 -0.467 0.210 -0.673 0.400 -0.582

0.630 -0.375 0.250 -0.645 0.250 -0.634 0.490 -0.562

0.700 -0.428 0.260 -0.538 0.340 -0.707 0.580 -0.471

0.750 -0.754 0.280 -0.628 0,370 -0.676 0.650 -0.463

0.810 -0.814 0.290 -0.630 0,400 -0.740 0.700 -0.464

0.840 -0.765 0.310 -0.590 0.410 -0.671 0,750 -0.546

0.900 -0.348 0,320 -0.575 0.430 -0.719 0.800 - 1.052

0.960 -0.399 0.340 -0.607 0A40 -0.691 0.830 -0.928

0.350 -0.329** 0.460 -0.708 0.900 -0.467

0,370 -0,588 0.490 -0.592 0.960 -0,467

0.380 -0.622 0.500 -0.749

0.400 -0,548 0,520 -0.722

0,410 -0,650 0.540 -0.716

0.430 -0,640 0.550 -0.677

0.440 -0.551 0.580 -0.614

0.460 -0.734 0.600 -0.539

0.470 -0,621 0.610 -0.461

0.490 -0.619 0.650 - 2.582"*

0.500 -0.636 0.700 -0.613

0,520 -0,625 0.750 -0.622

0.530 -0,608 0.820 -0.630

0.550 -0.634 0,890 -0.449

0.560 -0.627 0,900 -0.452

0.580 -0.598 0.960 -0.459

0.590 -0.630

0.600 -0.694

0.640 -2.419"*

0.700 -0.693

0,750 -0.473

0.820 -2.595**

0.870 -0.299

0,930 -0.350

0.960 -0.332

Lower Surface

0.020 -0.217 0.020 -0.080 0.020 0.068 0.020 0.494

0.110 -0.353 0.060 0.039 0,060 0.153 0.060 3.463"*

0,230 -0.021 0.090 -0.060 0.090 0.028 0.110 -0.019

0.400 -0.015 0.120 -0.098 0.120 -0.400 0.250 -0.181

0.490 0.000 0.200 -0.056 0.200 -0.216 0.400 -0.195

0.630 3.507"* 0.260 -0.221 0,250 -0.175 0.490 -0.231

0.750 0.189 0.400 -2.612"* 0.400 -0.091 0.580 -0.117

0.850 0,278 0.490 -0.021 0.490 0.036 0.650 0.138

0.900 0,326 0.580 0.109 0.580 0.026 0.750 0.382

0.960 0.129 0.640 0.485 0.650 0.309 0.830 0.484

0.750 0.350 0.750 0.019 0.900 0.575

0.870 0.431 0.890 ******** 0.960 0.391

0.930 0.381 0.930 0.432

0.960 0.210 0.960 -2.611 **

CN = 0.472 0.629 0,626 0.656

451
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-8-42-500, MINF = 0.889. Camber = 0/10, ALPT = 7.06, BETA = 0.47. QINF = 283.6,

RNPU = 2.2E+06, CNWP = 0.5175

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.603 0.000 0.901 0.000 -5.721 * * 0.010 -0.922 * *

0,060 -0.611 0.020 -0.907"* 0,020 -0.717"* 0.020 -0.858"*

0.110 -0.653 0,040 -0,596 0.060 - 1.228"* 0.060 -0.997

0.200 -0.537 0.060 -0.733 0.090 -0.779 0.110 -0.872

0.230 -0.473 0.090 -0.695 0.110 -0.877 0.140 -0.834**

0.400 -0.526 0.130 -0.748 0.130 -0.770 0.190 -5.581 **

0.490 -0.492 0.150 -0.740 0.150 -0.760 0.250 -0.882

0.590 -0.506 0.200 -0.616 0.210 -0.801 0.400 -0,670

0,630 -0.405 0.250 -0.772 0.250 -0.774 0.490 -0.666

0.700 -0,463 0.260 -0,673 0.340 -0.856 0.580 -0.563

0.750 -0,824 0,280 -0.758 0.370 -0.819 0.650 -0,536

0.8 I0 -0.903 0.290 -0.771 0.400 -0.831 0.700 -0.541

0.840 -0.827 0.310 -0.727 0.410 -0,780 0,750 -0,624

0,900 -0.384 0.320 -0.710 0.430 -0.837 0.800 -0.641

0.960 -0.421 0.340 -0,740 0,440 -0,809 0.830 -0.514

0,350 -0.354"* 0,460 -0.830 0.900 -0.413

0.370 -0.733 0,490 -0.724 0.960 -0.416

0,380 -0.752 0.500 -0.853

0.400 -0.664 0.520 -0.816

0,410 -0,773 0.540 -0,840

0,430 -0,745 0,550 -0.828

0.440 -0.662 0.580 -0.834

0,460 -0.856 0,600 -0.783

0.470 -0,775 0.610 -0.707

0,490 -0.746 0.650 -2,700**

0,500 -0.721 0.700 -0,727

0.520 -0,770 0.750 -0,775

0,530 -0,725 0.820 -0.445

0.550 -0.754 0,890 -0.370

0,560 -0.749 0,900 -0.375

0,580 -0,738 0.960 -0,384

0.590 -0,740

0,600 -0,832

0,640 -2.529**

0,700 -0.762

0,750 -0.399

0.820 -2.713"*

0.870 -0.274

0,930 -0.292

0,960 -0.301

Lower Surface

0.020 -0.096 0.020 0.084 0.020 0.181 0.020 0.546

0.110 -0.173 0.060 0.138 0.060 0,241 0,060 3.610"*

0.230 -0.019 0.090 0,039 0.090 0.093 0.110 0.012

0,400 -0.008 0.120 -0.013 0.120 -0,347 0.250 -0.108

0,490 -0.016 0,200 0.009 0,200 -0.107 0,400 -0.101

0.630 3,656'* 0,260 -0.136 0,250 -0.086 0.490 -0.167

0.750 0.176 0.400 -2.731 ** 0.400 -0.036 0,580 -0.090

0.850 0.260 0.490 -0.023 0,490 0,037 0.650 0.139

0,900 0.311 0.580 0.113 0,580 0.038 0.750 0.389

0.960 0.111 0.640 0,496 0.650 0.303 0,830 0.489

0.750 0,350 0.750 0.030 0,900 0.585

0.870 0.403 0.890 ******** 0.960 0,382

0,930 0.350 0.930 0.422

0.960 0.207 0.960 -2.730**

CN = 0,574 0,739 0,748 0.722

452
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-9-15-000, MINF = 0.891, Camber = 0/10, ALPT = 7.95, BETA = 0.26, QINF = 293.2,

RNPU = 2.2E+06, CNWP = 0.5712

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.703 0.000 0.835 0.000 -5.587"* 0.010 - 1.014"*

0.060 -0.740 0.020 -1.055"* 0.020 -0.804"* 0.020 - 1.053"*

0.110 -0.744 0.040 -0.721 0.060 - 1.294"* 0.060 - 1.080

0.200 -0.671 0.060 -0.858 0.090 -0.889 0.110 -0.977

0.230 -0.579 0.090 -0.840 0.110 -0.994 0.140 -0.986**

0.400 -0.655 0.130 -0.856 0.130 -0.873 0.190 -5.451 * *

0.490 -0.577 0.150 -0.861 0.150 -0.870 0.250 - 1.005

0.590 -0.573 0.200 -0.734 0.210 -0.902 0.400 -0.739

0.630 -0.503 0.250 -0.872 0.250 -0.860 0.490 -0.695

0.700 -0.542 0.260 -0.777 0.340 -0.947 0.580 -0.633

0.750 -0.937 0.280 -0.869 0.370 -0.937 0.650 -0.582

0.810 - 1.039 0.290 -0.866 0.400 -0.945 0.700 -0.602

0.840 -0.983 0.310 -0.806 0.410 -0.897 0.750 -0.690

0.900 -0.494 0.320 -0.807 0.430 -0.944 0.800 -0.847

0.960 -0.551 0.340 -0.830 0.440 -0.902 0.830 -0.643

0.350 -0.387** 0.460 -0.938 0.900 -0.529

0.370 -0.809 0.490 -0.858 0.960 -0.502

0.380 -0.829 0.500 -0.945

0.400 °0.761 0.520 -0.905

0.410 -0.874 0.540 -0.948

0.430 -0.846 0.550 -0.907

0.440 -0.775 0.580 -0.903

0.460 -0.944 0.600 -0.890

0.470 -0.848 0.610 -0.820

0.490 -0.828 0.650 -2.664**

0.500 -0.841 0.700 -0.930

0.520 -0.846 0.750 -0.938

0.530 -0.825 0.820 -0.434

0.550 -0.846 0.890 -0.406

0.560 -0.840 0.900 -0.407

0.580 -0.823 0.960 -0.438

0.590 -0.848

0.600 -0.903

0.640 -2.499 * *

0.700 -0.492

0.750 -0.276

0.820 -2.677**

0.870 -0.309

0.930 -0.331

0.960 -0.321

Lower Surface

0.020 0.013 0.020 0.232 0.020 0.327 0.020 0.654

0.110 -0.113 0.060 0.236 0.060 0.307 0.060 3.440"*

0.230 -0.014 0.090 0.127 0.090 0.200 0.110 0.099

0.400 -0.008 0.120 0.068 0.120 -0.272 0.250 -0.044

0.490 -0.004 0.200 0.054 0.200 -0.041 0.400 -0.045

0.630 3.484"* 0.260 -0.079 0.250 -0.015 0.490 -0.138

0.750 0.148 0.400 -2.694 ** 0.400 0.004 0.580 -0.058

0.850 0.248 0.490 0.005 0.490 0.062 0.650 0.150

0.900 0.282 0.580 0.110 0.580 0.037 0.750 0.414

0.960 0.086 0.640 0.476 0.650 0.315 0.830 0.507

0.750 0.331 0.750 0.037 0.900 0.599

0.870 0.411 0.890 ******** 0.960 0.374

0.930 0.335 0.930 0.424

0.960 0.189 0.960 -2.693**

CN = 0.68 l 0.797 0.872 0.846

453
Table G-2. Continued.

Flight 198, Wing sweep = 26 °, Time = 14-9-25-000, MINF = 0.892, Camber = 0/10, ALPT = 9.21, BETA = 0.55, QINF = 303.2,

RNPU = 2.3E+06, CNWP = 0.5879

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0,020 -0.774 0.000 0.814 0.000 -5.455"* 0.010 - 1.067" *

0.060 -0.797 0.020 - 1.119"* 0.020 -0.869"* 0.020 - 1.090 **

0.110 -0.796 0,040 -0.800 0.060 - 1.323 ** 0.060 - 1.137

0.200 -0.756 0.060 -0,915 0.090 -0.942 0.110 - 1.066

0.230 -0.625 0.090 -0.905 0.110 - 1.056 0.140 - 1.066 **

0.400 -0.695 0.130 -0,888 0.130 -0.940 0.190 -5.324"*

0.490 -0.642 0.150 -0.897 0.150 -0.917 0.250 - 1.080

0.590 -0.623 0.2(_ -0.804 0.210 -0.961 0.400 -0.807

0.630 -0.549 0.250 -0.938 0.250 -0.920 0.490 -0.723

0.700 -0.613 0.260 -0.814 0.340 - 1.001 0.580 -0.679

0.750 -0.813 0.280 -0.917 0.370 -0.993 0.650 -0.610

0.810 -0,959 0.290 -0.924 0.400 -0.980 0.700 -0.647

0.840 -0.945 0.310 -0.853 0.410 -0.931 0.750 -0.705

0.900 -0.516 0.320 -0.837 0.430 - 1.012 0.800 -0.828

0.960 -0.576 0.340 -0.895 0.440 -0.971 0.830 -0.700

0.350 -0.378"* 0.460 -0.979 0.900 -0.512

0.370 -0.874 0.490 -0.911 0.960 -0.534

0.380 -0.897 0.500 - 1.004

0.400 -0.788 0.520 -0.965

0.410 -0.912 0.540 -0.981

0.430 -0.900 0.550 -0.960

0.440 -0.808 0,580 -0.952

0.460 - 1.010 0.600 -0.942

0.470 -0.895 0,610 -0,885

0.490 -0.881 0.650 -2.629**

0.500 -0.891 0.700 -0.983

0.520 -0.887 0.750 -0.691

0.530 -0.876 0.820 -0.498

0.550 -0.888 0.890 -0.468

0.560 -0.889 0.900 -0.453

0,580 -0.864 0,960 -0.458

0.590 -0.888

0.600 -0.950

0.640 -2.469**

0.700 -0.395

0.750 -0.315

0.820 -2.641"*

0.870 -0.326

0.930 -0,344

0.960 -0,334

Lower Surface

0,020 0.074 0.020 0.278 0.020 0.401 0.020 0.741

0.110 -0.059 0.060 0.289 0.060 0.393 0.060 3.274'*

0.230 0.015 0.090 0.187 0.090 0.265 0.110 0.177

0.400 0.020 0.120 0.141 0.120 -0.187 0.250 0.000

0.490 0.001 0.200 0.114 0.200 0.065 0.400 -0.009

0.630 3.317"* 0.260 -0.032 0.250 0.049 0,490 -0.083

0.750 0.160 0.400 -2.658 ** 0.400 0.030 0.580 -0.043

0.850 0.220 0.490 0.026 0.490 0.066 0.650 0.188

0,900 0.286 0.580 0.130 0.580 0.063 0.750 0,435

0.960 0.067 0.640 0.481 0.650 0.310 0.830 0.503

0,750 0.344 0.750 -0.002 0.900 0.610

0.870 0.419 0.890 ******** 0.960 0.373

0.930 0.355 0.930 0.432

0.960 0.203 0.960 -2.657 * *

CN = 0.729 0.860 0.930 0.925

454
Table G-2. Concluded.

Flight 198, Wing sweep = 26 °, Time = 14-9-29-000, MINF = 0.887, Camber = 0/10, ALPT = 10.01, BETA = -0.06, QINF = 304,7,

RNPU = 2.3E+06, CNWP = 0.6142

rl = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.925 0.000 0.727 0.000 -5.457** 0.010 - 1.181 **

0,060 -0.944 0.020 -1.271"* 0.020 - 1.000"* 0.020 - 1.177"*

O. 110 -0.934 0.040 -0,913 0.060 - 1.351 ** 0.060 - 1.210

0.200 -0,890 0,060 -1.017 0,090 -1.046 0.110 -1.188

0.230 -0.725 0.090 -0.979 0.110 -1.145 0,140 -1.144"*

0,400 -0.767 0.130 -1.011 0.130 -1.034 0.190 -5.327**

0,490 -0,720 0,150 -0.995 0.150 -0.993 0.250 - 1.147

0.590 -0.694 0.200 -0,903 0.210 - 1.056 0.400 -0.866

0,630 -0.633 0.250 - 1.060 0,250 - 1,017 0.490 -0.764

0.700 -0,701 0.260 -0.921 0.340 -1.072 0.580 -0.728

0,750 -0.600 0.280 - 1.002 0.370 - 1.074 0.650 -0.664

0.810 -0.722 0.290 " -1.001 0,400 -1,092 0.700 -0.723

0.840 -0.729 0.310 -0,936 0.410 - 1.033 0.750 -0.760

0.900 -0.575 0,320 -0.940 0.430 - 1.099 0.800 -0.797

0.960 -0.644 0,340 -0.990 0.440 - 1.075 0.830 -0.731

0.350 -0.407** 0,460 -1.095 0.900 -0.549

0.370 -0.938 0.490 -0.944 0,960 -0.547

0.380 -0.979 0.500 - 1.091

0.400 -0.885 0.520 - 1.044

0.410 - 1.014 0.540 - 1.060

0.430 -0,982 0.550 - 1.032

0.440 -0.890 0,580 - 1.015

0,460 - 1,089 0,600 - 1.013

0.470 -0.951 0.610 -0.966

0.490 -0.957 0,650 -2.645 * *

0.500 -0.955 0.700 -0,638

0.520 -0.966 0.750 -0.640

0.530 -0.941 0.820 -0.540

0.550 -0.984 0,890 -0.517

0.560 -0.956 0.900 -0,496

0.580 -0.954 0,960 -0.497

0.590 -0.947

0.600 -0.744

0.640 -2.487 * *

0,700 -0.398

0,750 -0,337

0,820 -2.658**

0.870 -0.344

0.930 -0,369

0.960 -0,345

Lower Surface

0,020 0.135 0,020 0.443 0,020 0.475 0.020 0.776

0.110 -0.008 0,060 0.341 0.060 0,453 0.060 3.227"*

0.230 0.036 0.090 0.240 0.090 0.308 0,110 0.260

0.400 0.018 0.120 0.172 0.120 -0.125 0.250 0.049

0.490 0.010 0.200 0.147 0.200 0.089 0.400 0.019

0.630 3.269** 0.260 0.006 0.250 0,098 0,490 -0.055

0.750 0.154 0.400 -2.675 * * 0.400 0,054 0.580 -0,005

0.850 0.207 0.490 0,039 0.490 0.042 0.650 0.193

0.900 0.265 0.580 0.134 0.580 0,082 0,750 0,422

0.960 0.059 0.640 0.471 0.650 0.314 0.830 0.524

0.750 0.326 0.750 -0.018 0.900 0.594

0,870 0,420 0.890 ******** 0.960 0.381

0.930 0,348 0.930 0.410

0.960 0.200 0.960 -2.673**

CN = 0.780 0.914 0,974 1.007

455
APPENDIX H

Wing Pressure Coefficients for Dynamic Pressures From

300 to 800 lb/ft 2 and Mach Numbers from 0.61 to 1.41.

Leading-edge wing sweep is 26 ° unless otherwise indicated at flight number. Table H-I contains a summary of

the data listing in table H-2. The asterisks (*) in table H-2 indicate invalid values. Flight 229 has less data in two

upper rows because the pressure transducers were used for boundary-layer data. Camber is _)LE,,TE"Refer to

Nomenclature for definitions.

Table H-1. Summary of data.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

201 8-49-1-500 0.944 0/2 5.05 0.14 303.4 2.8E+06 0.3340

201 8-49-6-500 0.943 0/2 5.07 0.14 383.7 2.8E+06 0.3326

221 14-17-53-500 0.949 0/2 6.09 0.08 298.4 2.2E+06 0.2762

221 14-18-4-000 0.952 0/2 7.06 -0.24 301.5 2.2E+06 0.3371

221 14-18-7-000 0.953 0/2 8.08 -0.67 302.1 2.2E+06 0.3593

221 14-18-10-000 0.949 0/2 9.25 -0.76 299.8 2.2E+06 0.4154

221 14-18-12-000 0.944 0/2 10.28 -0.85 296.7 2.2E+06 0.4688

229 11-42-7-000 0.950 0/2 6.07 0.28 301.4 2.2E+06 0.2974

229 11-42-16-500 0.949 0/2 6.10 0.31 300.4 2.2E+06 0.3195

229 11-42-32-500 0.949 0/2 7.16 0.02 300.6 2.2E+06 0.3334

229 11-42-54-000 0.945 0/2 8.10 -0.30 298.5 2.2E+06 0.3625

229 11-42-59-500 0.948 0/2 9.14 -0.30 302.9 2.2E+06 0.4088

221 14-14-17-500 0.939 0/2 8.06 -0.24 305.6 2.3E+06 0.3526

229 11-46-10-000 0.947 5/2 6.50 -0.10 301.2 2.2E+06 0.3148

229 11-46-40-500 0.946 5/2 6.10 0.19 299.6 2.2E+06 0.2930

217 9-21-19-500 0.606 0/2 5.98 0.48 299.2 3.0E+06 0.3170

217 9-21-36-500 0.651 0/2 4.59 0.37 344.3 3.3E+06 0.2748

217 9-21-44-000 0.700 0/2 4.77 0.11 400.5 3.6E+06 0.2929

217 9-21-49-500 0.751 0/2 4.06 0.37 462.6 4.0E+06 0.2450

217 9-21-55-000 0.803 0/2 3.79 0.48 531.0 4.3E+06 0.2570

217 9-22-0-500 0.851 0/2 4.32 0.89 598.9 4.7E+06 0.2841

217 9-22-6-500 0.883 0/2 4.23 0.48 642.7 4.9E+06 0.2886

217 9-22-11-500 0.900 0/2 4.47 0.86 665.0 5.0E+06 0.3201

217 9-22-18-000 0.909 0/2 4.21 0.72 674.5 5.1E+06 0.2999

217 9-22-20-000 0.907 0/2 4.06 0.92 670.8 5.1E+06 0.3037

217 9-22-27-000 0.900 0/2 4.42 1.03 658.1 5.0E+06 0.3250

2181 10-18-15-500 0.930 0/2 6.04 0.69 337.2 2.5E+06 0.5016

1Wing sweep of 45 ° 2Wing sweep of 58 °

456
TableH-1.Continued.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

2181 10-18-24-500 0.940 0/2 5.73 0.51 337.1 2.5E+06

2181 10-18-30-500 0.950 0/2 7.03 0.34 341.1 2.5E+06

2181 10-18-37-000 0.960 0/2 6.65 0.48 344.1 2.5E+06

2181 10-18-42-000 0.970 0/2 7.59 0.37 347.0 2.5E+06

2181 10-18-52-000 0.980 0/2 8.09 0.45 344.1 2.5E+06

2181 10-19-17-500 0.990 0/2 7.60 0.34 339.2 2.4E+06

2181 10-19-20-500 1.000 0/2 8.73 0.34 348.6 2.5E+06

2181 10-19-25-500 1.006 0/2 8.44 0.43 359.4 2.6E+06

2181 10-20-12-000 1.050 0/2 6.76 0.45 410.3 2.9E+06

2181 10-20-23-500 1.100 0/2 7.28 0.14 465.0 3.2E+06

2181 10-20-39-000 1.151 0/2 5.88 0.28 523.0 3.5E+06

2181 10-20-53-500 1.200 0/2 7.09 0.19 585.5 3.8E+06

2181 10-20-56-500 1.205 0/2 6.35 0.19 589.8 3.9E+06

2181 10-21-7-500 1.233 0/2 4.63 0.28 615.3 4.0E+06

1942 12-5-0-000 0.884 0/2 8.85 -0.30 304.1 2.3E+06

1942 12-5-2-500 0.890 0/2 8.96 0.18 308.3 2.4E+06

1942 12-5-6-000 0.900 0/2 8.54 0.47 315.2 2.4E+06

1942 12-5-15-000 0.929 0/2 8.04 0.36 334.1 2.5E+06

1942 12-5-21-500 0.950 0/2 7.72 0.36 347.1 2.6E+06

1942 12-5-37-500 1.000 0/2 6.71 0.28 377.8 2.7E+06

1942 12-5-54-000 1.050 0/2 7.07 0.28 414.2 2.9E+06

1942 12-6-9-500 1.100 0/2 6.54 0.34 456.2 3.1E+06

1942 12-6-22-000 1.150 0/2 5.91 0.31 501.4 3.3E+06

1942 12-6-34-000 1.200 0/2 5.70 0.31 551.5 3.6E+06

1942 12-6-46-000 1.249 0/2 5.15 0.23 602.4 3.9E+06

1942 12-7-1-500 1.299 0/2 4.53 0.26 657.7 4.2E+06

2172 11-4-36-500 1.213 0/2 5.51 0.22 595.8 3.9E+06

2172 11-4-52-000 1.216 0/2 4.85 0.17 595.5 3.9E+06

2172 11-5-9-000 1.221 0/2 5.00 0.25 602.6 3.9E+06

2172 11-5-13-500 1.222 0/2 3.56 0.25 603.3 3.9E+06

2172 11-5-15-000 1.224 0/2 2.68 0.25 605.9 3.9E+06

2172 11-5-17-500 1.227 0/2 3.56 0.34 611.8 4.0E+06

2172 11-5-18-500 1.227 0/2 4.60 0.31 614.8 4.0E+06

2172 11-5-19-500 1.228 0/2 5.85 0.28 617.9 4.0E+06

2172 11-5-20-500 1.226 0/2 6.83 0.31 618.7 4.0E+06

2172 11-5-21-500 1.225 0/2 7.64 0.28 618.8 4.0E+06

0.4059

O.3389

0.2727

0.3436

1Wing sweep of 45 ° 2Wing sweep of 58 °

457
TableH-1.Continued.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

2172 11-5-22-500 1.220 0/2 8.44 0.34 616.2 4.0E+06

2172 11-5-26-500 1.195 0/2 9.20 0.31 587.5 3.8E+06

2172 11-7-27-500 1.185 2/1 5.52 0.34 573.8 3.8E+06

2182 10-23-32-500 1.211 0/2 4.52 0.45 587.2 3.8E+06

2182 10-23-35-000 1.213 0/2 3.57 0.45 588.8 3.8E+06

2182 10-23-38-500 1.218 0/2 2.78 0.54 596.0 3.9E+06

2182 10-23-43-500 1.228 0/2 6.60 0.43 620.2 4.0E+06

2182 10-23-44-500 1.227 0/2 7.86 0.45 622.6 4.0E+06

2182 10-23-45-000 1.226 0/2 8.42 0.45 622.9 4.0E+06

2182 10-23-46-000 1.222 0/2 9.47 0.45 621.6 4.0E+06

2182 10-23-47-000 1.216 0/2 10.51 0.48 615.9 4.0E+06

2182 10-23-48-000 1.206 0/2 11.26 0.51 606.1 4.0E+06

2182 10-26-14-000 1.214 2/1 5.12 0.37 599.3 3.9E+06

2182 10-26-26-000 1.215 2/1 5.12 0.37 604.3 3.9E+06

2182 10-26-29-500 1.217 1/2 3.55 0.37 607.7 4.0E+06

2182 10-26-32-500 1.222 0/3 2.56 0.43 615.5 4.0E+06

2182 10-26-36-500 1.235 1/3 3.80 0.31 641.9 4.2E+06

2182 10-26-37-000 1.237 1/3 4.71 0.37 646.5 4.2E+06

2182 10-26-37-500 1.238 1/2 5.82 0.37 649.7 4.2E+06

2182 10-26-38-000 1.238 2/1 6.70 0.43 651.6 4.2E+06

2182 10-26-38-500 1.237 3/0 7.54 0.45 653.3 4.2E+06

2182 10-26-39-500 1.235 5/-1 8.70 0.43 655.6 4.2E+06

2182 10-26-40-500 1.231 7/- 1 9.74 0.43 654.0 4.2E+06

2182 10-26-41-000 1.228 9/-1 10.14 0.34 651.8 4.2E+06

2182 10-26-42-500 1.216 12/-1 11.03 0.34 639.0 4.2E+06

2182 10-28-24-000 1.197 4/-1 7.55 0.51 565.8 3.7E+06

2182 10-30-25-000 1.218 0/2 7.49 0.43 572.7 3.7E+06

2182 10-30-33-000 1.220 0/2 8.31 0.37 575.5 3.7E+06

2222 11-35-51-500 1.395 0/2 4.24 0.43 790.9 4.9E+06

2222 11-36-0-000 1.395 0/2 3.56 0.45 789.7 4.9E+06

2222 11-36-3-500 1.399 0/2 2.43 0.48 795.4 5.0E+06

2222 11-36-6-000 1.403 0/2 2.48 0.48 805.4 5.0E+06

2222 11-36-9-000 1.408 0/2 3.65 0.45 822.3 5.1E+06

2222 11-36-10-500 1.410 0/2 5.41 0.45 832.6 5.2E+06

2222 11-36-13-000 1.405 0/2 7.58 0.45 836.9 5.2E+06

2222 11-36-14-000 1.400 0/2 8.35 0.45 833.5 5.2E+06

0.1637

lWing sweep of 45 ° 2Wing sweep of 58 °

458
TableH-1. Concluded.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

2222 11-36-16-000 1.385 0/2 8.95 0.40 816.0 5.1E+06

2222 11-42-6-000 1.403 1/2 4.20 0.40 786.1 4.9E+06

2222 11-42-18-000 1.404 1/2 3.93 0.43 785.5 4.9E+06

2222 11-42-26-500 1.406 0/3 3.51 0.43 788.3 4.9E+06

2222 11-42-29-500 1.409 0/3 2.38 0.45 792.6 4.9E+06

2222 11-42-30-500 1.411 0/3 2.38 0.45 795.2 4.9E+06

2222 11-42-32-500 1.411 0/3 4.74 0.40 800.8 5.0E+06

2222 11-42-34-000 1.408 1/1 6.44 0.43 802.3 5.0E+06

2222 11-42-35-000 1.405 2/0 7.35 0.43 800.8 5.0E+06

2222 11-42-36-500 1.397 3# 1 8.55 0.45 793.3 4.9E+06

2222 11-42-38-000 1.387 5/-1 9.32 0.45 779.3 4.9E+06

2222 11-42-40-000 1.369 5/-I 9.50 0.48 750.7 4.7E+06

1Wing sweep of 45 ° 2Wing sweep of 58 °

459
Table H-2. Listing of data.

Flight 201, Wing sweep = 26 °, Time = 8-49-1-500, MINF = 0.944, Camber = 0/2, ALPT = 5.05, BETA = 0.14, QINF = 383.4,

RNPU = 2.8E+06, CNWP = 0.3340

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.131 0.000 0.925 0.000 0.865** 0.010 -0.553

0.060 -0.313 0.020 -0.321 0.020 -0.167 0.020 -0.652 **

0.110 -0.347 0.040 -0.209 0.060 0.097** 0.060 -0.626**

0.200 -0.463 0.060 -0.388 0.090 -0.468 0.110 -0.628

0.230 -0.406 0.090 -0.404 0.110 -0.571 0.1 40 -0.660

0.400 -0.470 0.130 -0.430 0.130 -0.486 0.190 - 1.603 **

0.490 -0.449 0.150 -0.466 0.150 -0.507 0.250 -0.671

0.590 -0.469 0.200 -0.399 0.210 -0.524 0.400 -0.521

0.630 -0.450 0.250 -0.522 0.250 -0.544 0.490 -0.534

0.700 -0.524 0.260 -0.501 0.340 -0.605 0.580 -0.371

0.750 -0.623 0.280 -0.535 0.370 -0.628 0.650 -0.413

0.810 -0.573 0.290 -0.535 0.400 -0.627 0.700 -0.393

0.840 -0.609 0.310 -0.516 0.410 -0.610 0.750 -0.460

0.900 -0.029 0.320 -0.520 0.430 -0.623 0.800 -0.606

0.960 0.007 0.340 -0.518 0.440 -0.604 0.830 -0.587

0.350 -0.340** 0.460 -0.440 0.900 -0.780

0.370 -0.528 0.490 -0.596 0.960 -0.274**

0.380 -0.581 0.500 -0.650

0.400 -0.510 0.520 -0.618

0.410 -0.562 0.540 -0.606

0.430 -0.537 0.550 -0.583

0.440 -0.506 0.580 -0.493

0.460 -0.586 0.600 -0.484

0.470 -0.552 0.610 -0.488

0.490 -0.560 0.650 -0.099"*

0.500 -0.558 0.700 -0.598

0.520 -0.551 0.750 -0.604

0.530 -0.543 0.820 -0.376

0.550 -0.566 0.890 -0.293

0.560 -0.581 0.900 -0.198

0.580 -0.564 0.960 -0.100

0.590 -0.595

0.600 -0.622

0.640 -0.648

0.700 -0.692

0.750 -0.176**

0.820 -0.457

0.870 -0.316

0.930 -0.112

0.960 -0.107

Lower Surface

0.020 -0.366 0.020 -0.173 0.020 0.007 0.020 0.432

0.110 -0.391 0.060 -0.007 0.060 0.088 0.060 -0.817

0.230 -0.419 0.090 -0.107 0.090 0.006 0.110 -0.039

0.400 -0.308 0.120 -0.185 ** 0.120 -0.258 0.250 -0.270

0.490 -0.319 0.200 -0.275 0.200 -0.220 0.400 -0.174

0.630 1.775"* 0.260 -0.290 0.250 -0.299 0.490 -0.323

0.750 -0.262 0.400 -0.328 0.400 -0.284 0.580 -0.460

0.850 0.052 0.490 -0.413 0.490 -0.198 0.650 -0.654

0.900 0.168 0.580 -0.499 0.580 -0.448 0.750 -0.385

0.960 0.147 0.640 -0.588 0.650 -0.191 0.830 -0.107

0.750 -0.140 0.750 -0.164** 0.900 0.074

0.870 0.025 0.890 0.079 0.960 0.165

0.930 0.143 0.930 0.102

0.960 0.124 0.960 0.289

CN = 0.155 0.237 0.319 0.256

460
Table H-2. Continued.

Flight 201, Wing sweep = 26 °, Time = 8-49-6-500. MINF = 0,943, Camber = 0/2, ALPT = 5.07, BETA = 0.14, QINF = 383.7,

RNPU = 2.8E÷06, CNWP = 0,3326

l] = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0,020 -0.127 0,000 0.915 0.000 0.871"* 0.010 -0,568

0.060 -0,306 0,020 -0.380 0.020 -0.176 0.020 -0,650"*

0.110 -0.332 0.040 -0.190 0.060 0.058** 0.060 -0,613"*

0.200 -0.466 0.060 -0.403 0.090 -0.490 0.110 -0,635

0,230 -0,363 0,090 -0.412 0.110 -0.571 0.140 -0.663

0.400 -0,467 0.130 -0,437 0.130 -0.489 0, 190 - 1.605"*

0,490 -0,461 0,150 -0.462 0.150 -0.521 0,250 -0.679

0,590 -0,480 0,200 -0.404 0.210 -0.531 0,400 -0.541

0.630 -0.447 0.250 -0,536 0.250 -0.553 0.490 -0,522

0.700 -0.518 0.260 -0,510 0.340 -0.608 0.580 -0.377

0.750 -0.595 0.280 -0.543 0.370 -0.624 0.650 -0.424

0.810 -0.560 0.290 -0.543 0.400 -0,606 0.700 -0,396

0.840 -0.571 0.310 -0.521 0.410 -0.618 0.750 -0.474

0.900 -0.028 0.320 -0.520 0.430 -0.614 0.800 -0.615

0.960 0,009 0,340 -0.521 0.440 -0,602 0,830 -0,583

0.350 -0.343"* 0.460 -0.446 0.900 -0.787

0.370 -0.540 0.490 -0.581 0.960 -0.279**

0,380 -0.585 0.500 -0.645

0.400 -0.515 0.520 -0.607

0.410 -0,566 0,540 -0,620

0,430 -0,542 0.550 -0.569

0.440 -0.492 0.580 -0.494

0.460 -0.580 0.600 -0,489

0.470 -0.556 0.610 -0.502

0.490 -0.562 0.650 -0.103"*

0.500 -0.555 0.700 -0.598

0.520 -0,553 0.750 -0.581

0.530 -0,551 0.820 -0,374

0.550 -0,580 0,890 -0.308

0.560 -0,584 0.900 -0.205

0.580 -0.561 0,960 -0,106

0.590 -0.613

0.600 -0.625

0,640 -0.655

0.700 -0_686

0.750 -0.188"*

0,820 -0.460

0,870 -0.328

0.930 -0,116

0.960 -0.099

Lower Surface

0.020 -0.351 0,020 -0.213 0.020 -0.007 0.020 0.410

0, | 10 -0,394 0.060 -0.040 0.060 0.074 0.060 -0.825

0,230 -0.427 0.090 -0.124 0.090 0,003 0.110 -0,070

0.400 -0.338 0.120 -0.199"* 0.120 -0.261 0.250 -0.289

0.490 -0,313 0.200 -0.304 0.200 -0,228 0.400 -0.177

0.630 1,770"* 0.260 -0.311 0.250 -0.308 0.490 -0.334

0.750 -0.234 0.400 -0.351 0.400 -0.291 0.580 -0.474

0.850 0.049 0.490 -0.430 0.490 -0.212 0.650 -0.674

0,900 0.168 0.580 -0.510 0.580 -0.463 0.750 -0.388

0.960 0.147 0.640 -0.593 0.650 -0.194 0.830 -0.121

0.750 -0.137 0.750 -0.167"* 0.900 0.060

0.870 0,032 0.890 0.081 0,960 0.154

0,930 0.131 0,930 0.093

0,960 0,115 0.960 0,262

CN = 0.151 0.228 0.315 0.249

461
Table H-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 14-17-53-500, MINF = 0.949, Camber = 0/2, ALPT = 6.09, BETA = 0.08, QINF = 298.4,

RNPU = 2.2E+06, CNWP = 0.2762

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.280 0.000 0.880 0.000 0.951 ** 0.010 -0.618

0.060 -0.375 0.020 -0.443 0.020 -0.487 0.020 -0.735

0.110 -0.435 0.040 -0.425 0.060 -3.041 * * 0.060 -0.782

0.200 -0.483 0.060 -0.537 0.090 -0.592 0. I 10 -0.710

0.230 -0.421 0.090 -0.537 0.110 -0.643 0.140 -0.753

0.400 -0.512 0.130 -0.535 0.130 -0.542 0.190 - 1.587 **

0.490 -0.488 0.150 -0.559 0.150 -0.617 0.250 -0.747

0.590 -0.540 0.200 -0.464 0.210 -0.581 0.400 -0.570

0.630 -0.474 0.250 -0.598 0.250 -0.596 0.490 -0.592

0.700 -0.502 0.260 -0.532 0.340 -0.648 0.580 -0.478

0.750 -0.694 0.280 -0.583 0.370 -0.649 0.650 -0.436

0.810 -0.700 0.290 -0.601 0.400 -0.685 0.700 -0.440

0.840 -0.677 0.3 I0 -0.597 0.410 -2.588"* 0.750 -0.531

0.900 -0.170 0.320 -0.588 0.430 -0.672 0.800 -0.672

0.960 -0.189 0.340 -0.575 0.440 -0.632 0.830 -0.603

0.350 -0.408** 0.460 -0.674 0.900 -0.803

0.370 -0.571 0.490 -0.583 0.960 -0.449

0.380 -0.628 0.500 -0.717

0.400 -0.514 0.520 -0.652

0.4 l 0 -0.623 0.540 -0.674

0.430 -0.600 0.550 -0.692

0.440 -0.543 0.580 -0.695

0.460 -0.658 0.600 -0.613

0.470 -0.603 0.610 -0.565

0.490 -0.624 0.650 0.491 **

0.500 -0.621 0.700 -0.646

0.520 -0.637 0.750 -0.734

0.530 -0.610 0.820 -0.631

0.550 -0.673 0.890 -0.642

0.560 -0.624 0.900 -0.438

0.580 -0.627 0.960 -0.251

0.590 -0.667

0.600 -0.702

0.640 -0.676

0.700 -0.697

0.750 -0.232**

0.820 -0.511

0.870 -0.482

0.930 -0.277

0.960 -0.255

Lower Surface

0.020 -0.326 0.020 -0.070 0.020 0.081 0.020 0.472

0.110 -0.359 0.060 -0.027 0.060 0.109 0.060 0.978"*

0.230 -0.370 0.090 -0.097 0.090 1.522"* 0.110 -0.042

0.400 -0.294 0.120 -0.210 0.120 -0.342 0.250 -0.179

0.490 -0.330 0.200 -0.158 0.200 -0.171 0.400 -0.237

0.630 2.286** 0.260 -0.314 0.250 -0.251 0.490 -0.376

0.750 -0.579 0.400 -0.311 0.400 -0.277 0.580 -0.462

0.850 -0.083 0.490 -0.430 0.490 -0.253 0.650 -0.675

0.900 0.051 0.580 -0.495 0.580 -0.451 0.750 -0.320

0.960 0.041 0.640 -0.548 0.650 -0.251 0.830 -0.120

0.750 -0.203 0.750 -0.143 0.900 0.038

0.870 -0.088 0.890 0.017 0.960 0.096

0.930 0.027 0.930 0.043

0.960 0.002 0.960 -2.222**

CN = 0.146 0.292 0.392 0.390

462
Table H-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 14-18-4-000, MINI: -- 0.952, Camber = 0/2, ALPT = 7.06, BETA = -0.24, QINF -- 301.5,

RNPU = 2.2E+06, CNWP = 0.3371

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.472 0.000 0.862 0,000 0.839** 0.010 -0.783

0.060 -0.498 0.020 -0.707 0.020 -0.559 0.020 -0.774

0.110 -0.493 0,040 -0.502 0.060 -2.976** 0.060 -0.799

0.200 -0.546 0.060 -0.614 0.090 -0.695 0.110 -0.766

0.230 -0.477 0.090 -0.590 0.110 -0.714 0.140 -0.786

0.400 -0.549 0.130 -0.597 0.130 -0.612 0.190 - 1.576 **

0.490 -0.495 0.150 -0.624 0.150 -0.683 0.250 -0.815

0.590 -0.563 0.200 -0.517 0.210 -0.621 0.400 -0.611

0.630 -0.504 0.250 -0.648 0.250 -0,653 0.490 -0.600

0.700 -0.539 0.260 -0.579 0.340 -0.706 0.580 -0.53 I

0.750 -0.715 0.280 -0.651 0.370 -0.694 0.650 -0.477

0.810 -0.719 0.290 -0.643 0.400 -0.742 0.700 -0.456

0.840 -0.682 0.310 -0.647 0.410 -2.567** 0.750 -0.545

0.900 -0.265 0.320 -0.640 0.430 -0.722 0.800 -0.669

0.960 -0.291 0.340 -0.613 0.440 -0.682 0.830 -0.629

0.350 -0.435** 0.460 -0.721 0,900 -0.818

0.370 -0.621 0.490 -0.694 0.960 -0.523

0.380 -0.695 0.500 -0.737

0.400 -0.575 0.520 -0.667

0.410 -0.667 0.540 -0.713

0.430 -0,645 0.550 -0.738

0.440 -0.585 0.580 -0.745

0.460 -0.689 0.600 -0.671

0.470 -0.640 0.610 -0.671

0.490 -0.666 0.650 0.352**

0.500 -0.685 0.700 -0.691

0.520 -0.690 0,750 -0.761

0.530 -0.662 0.820 -0.671

0.550 -0.716 0.890 -0,780

0.560 -0.665 0.900 -0.728

0.580 -0.685 0.960 -0.337

0.590 -0.722

0600 -0.758

0.640 -0.723

0,700 -0.742

0.750 -0.235**

0.820 -0.578

0.870 -0.580

0.930 -0.382

0.960 -0.333

Lower Surface

0.020 -0.225 0.020 -0.259 0.020 0.152 0.020 0.509

0.110 -0.321 0.060 0.050 0,060 0.170 0.060 0.963 * *

0.230 -0.360 0.090 -0.046 0.090 1,502"* 0.110 0.029

0.400 -0.266 0.120 -0.100 0.120 -0.277 0.250 -0.154

0.490 -0.317 0.200 -0.129 0.200 -0.151 0.400 -0.203

0.630 2.257** 0.260 -0.287 0.250 -0.196 0.490 -0.337

0.750 -0.563 0.400 -0,283 0.400 -0.225 0.580 -0.412

0.850 -0.114 0.490 -0.404 0.490 -0.248 0.650 -0.651

0.900 0.020 0.580 -0.457 0.580 -0.429 0.750 -0.284

0.960 -0.022 0.640 -0.518 0.650 -0.246 0.830 -0.078

0.750 -0.185 0.750 -0,146 0.900 0.110

0.870 -0.023 0.890 0.033 0.960 0.134

0.930 0.029 0.930 0.045

0.960 -0.018 0.960 -2.165**

CN = 0.200 0.391 0.488 0.466

463
Table H-2. Continued,

Flight 221, Wing sweep = 26 °, Time = 14-18-7-000, MINF = 0,953, Camber = 0/2, ALPT = 8.08, BETA = -0.67, QINF = 302.1,

RNPU = 2.2E+06, CNWP = 0.3593

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.567 0.000 0.848 0,000 0,892** 0.010 -0.789

0.060 -0.549 0,020 -0.805 0.020 -0.639 0.020 -0.873

0.110 -0.570 0.040 -0,545 0.060 -3.056** 0,060 -0,882

0,200 -0.594 0.060 -0.690 0.090 -0.721 0.110 -0.844

0.230 -0.517 0.090 -0.690 0.110 -0.762 0.140 -0.859

0.400 -0.609 0.130 -0.677 0.130 -0.668 0.190 - 1.574**

0.490 -0.546 0.150 -0.696 0.150 -0.758 0.250 -0.841

0.590 -0.597 0.200 -0.622 0.210 -0.685 0.400 -0.645

0.630 -0.520 0.250 -0.711 0.250 -0.714 0.490 -0.614

0.700 -0.570 0.260 -0.625 0.340 -0,766 0.580 -0.537

0.750 -0.731 0.280 -0.680 0.370 -0.764 0.650 -0.503

0.810 °0.732 0.290 -0,680 0.400 -0.808 0.700 -0,498

0.840 -0.697 0.310 -0.695 0.410 -2.562"* 0.750 -0.574

0.900 -0.378 0.320 -0.682 0.430 -0.789 0,800 -0.690

0.960 -0.372 0.340 -0.667 0.440 -0.729 0.830 -0.641

0.350 -0.432** 0.460 -0.782 0.900 -0.830

0.370 -0.657 0.490 -0.687 0.960 -0.540

0.380 -0.745 0.500 -0.802

0.400 -0.645 0,520 -0.751

0.410 -0.740 0.540 -0.767

0.430 -0,693 0.550 -0,784

0.440 -0.628 0.580 -0.782

0.460 -0,748 0.600 -0.716

0.470 -0.696 0.610 -0.709

0.490 -0.724 0.650 0,223**

0.500 -0.740 0.700 -0.815

0.520 -0.713 0.750 -0.837

0.530 -0.700 0.820 -0.702

0.550 -0.770 0,890 -0.801

0.560 -0,694 0.900 -0.877

0.580 -0.710 0.960 -0.393

0.590 -0.760

0.600 -0.772

0.640 -0.763

0.700 -0.785

0.750 -0.222**

0.820 -0.616

0.870 -0,598

0.930 -0.422

0.960 -0.414

Lower Surface

0.020 -0.156 0.020 -0.241 0.020 0.243 0.020 0.600

0.110 -0.295 0.060 0.116 0.060 0.221 0.060 0.974**

0.230 -0.301 0.090 0.0 ]4 0.090 1.497" * 0. l 10 0.068

0.400 -0.238 0.120 -0.051 0.120 -0.236 0.250 -0.117

0.490 -0.310 0.200 -0.083 0,200 -0.122 0.400 -0.161

0.630 2.251 ** 0.260 -0.230 0.250 -0.131 0.490 -0.315

0.750 -0.544 0.400 -0.254 0.400 -0.221 0.580 -0.388

0.850 -0.115 0.490 -0.397 0.490 -0.242 0.650 -0.625

0.900 -0.009 0.580 -0.435 0.580 -0.408 0.750 -0.214

0.960 -0.058 0.640 -0.510 0.650 -0.240 0.830 -0.025

0.750 -0.118 0.750 -0.125 0.900 0.180

0.870 0.013 0.890 0.057 0.960 0.138

0.930 0.035 0.930 0.080

0.960 -0.015 0.960 -2.131 **

CN = 0.266 0.477 0.568 0.535

464
Table H-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 14-18-10-000, MINF = 0.949, Camber = 0/2, ALPT = 9.25, BETA = -0.76, QINF = 299.8,

RNPU = 2.2E+06, CNWP = 0.4154

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.638 0,000 0.789 0.000 0.717"* 0.010 -0.927

0.060 -0.670 0.020 -0.929 0.020 -0.749 0.020 -0.969

0.1 I0 -0,687 0.040 -0.680 0.060 -3.128"* 0.060 - 1.006

0.200 -0.672 0.060 -0.791 0.090 -0.827 0,110 -0.959

0,230 -0.581 0.090 -0.770 0.110 -0.862 0.140 -0.976

0.400 -0.653 0.130 -0.761 0.130 -0.771 0.190 -1.587"*

0,490 -0.617 0.150 -0.789 0.150 -0.844 0.250 -0.974

0,590 -0.653 0.200 -0.711 0.210 -0.779 0.400 -0.720

0.630 -0,580 0.250 -0.789 0,250 -0.788 0.490 -0.627

0.700 -0,605 0.260 -0,711 0,340 -0.833 0,580 -0.600

0.750 -0.766 0,280 -0.767 0.370 -0.835 0.650 -0.564

0.810 -0.774 0.290 -0.767 0,400 -0.881 0.700 -0.570

0.840 -0.747 0.310 -0.776 0.410 -2.583** 0.750 -0.630

0.900 -0.545 0,320 -0,767 0.430 -0.856 0.800 -0.723

0.960 -0,492 0.340 -0.754 0.440 -0.823 0.830 -0.678

0.350 -0.458** 0.460 -0.853 0,900 -0,858

0.370 -0,743 0,490 -0.769 0.960 -0.582

0.380 -0.804 0.500 -0.879

0.400 -0.686 0.520 -0.829

0.410 -0.797 0.540 -0.839

0.430 -0.771 0.550 -0.862

0.440 -0.720 0.580 -0.880

0.460 -0.835 0.600 -0.804

0.470 -0.765 0.610 -0.795

0.490 -0.792 0.650 0.134"*

0,500 -0.813 0,700 -0.943

0.520 -0.805 0.750 - 1.000

0.530 -0,790 0.820 -0.773

0.550 -0.810 0.890 -0.801

0.560 -0.778 0,900 -0.572

0.580 -0.795 0.960 -0.417

0.590 -0.836

0.600 -0.858

0.640 -0.834

0.700 -0.853

0.750 -0.158"*

0.820 -0.587

0.870 -0.508

0.930 -0.460

0.960 -0.455

Lower Surface

0,020 -0.073 0,020 -0.215 0.020 0.329 0.020 0.669

0.110 -0.196 0.060 0.187 0.060 0.290 0.060 0.995**

0.230 -0.236 0.090 0.069 0.090 1.507"* 0.110 0.102

0.400 -0.211 0,120 0.006 0.120 -0.181 0.250 -0.064

0.490 -0.283 0.200 -0.037 0.200 -0.067 0,400 -0,122

0.630 2,267** 0.260 -0.203 0.250 -0.074 0.490 -0.281

0.750 -0.158 0.400 -0.215 0,400 -0.174 0.580 -0,377

0.850 -0.064 0.490 -0.356 0.490 -0.178 0.650 -0.608

0.900 0.000 0.580 -0.409 0,580 -0,375 0.750 -0.126

0.960 -0.103 0.640 -0.470 0.650 -0.177 0.830 0.101

0,750 0.007 0.750 -0.120 0.900 0.240

0.870 0.082 0,890 0.129 0.960 0.141

0.930 0.057 0.930 0.117

0.960 -0.009 0,960 -2.153"*

CN = 0.436 0.585 0.683 0.652

465
Table H-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 14-18-12-000, MINF = 0.944, Camber = 0/2, ALPT = 10.28, BETA = -0.85, QINF = 296.7,

RNPU = 2.2E+06, CNWP = 0.4688

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.727 0.000 0.748 0.000 0.703"* 0.010 - 1.029

0.060 -0.739 0.020 - 1.021 0.020 -0.831 0.020 - 1.029

0.110 -0.750 0.040 -0.757 0.060 -3.202"* 0.060 - 1.087

0.200 -0.729 0.060 -0.832 0.090 -0.917 0.110 -1.034

0.230 -0.685 0.090 -0.851 0.110 -0.939 0.140 - 1.045

0.400 -0.699 0.130 -0.844 0.130 -0.843 0.190 - 1.604**

0.490 -0.654 0.150 -0.861 0.150 -0.949 0.250 - 1.028

0.590 -0.700 0.200 -0.779 0.210 -0.848 0.400 -0.769

0.630 -0.626 0.250 -0.862 0.250 -0.856 0.490 -0.677

0.700 -0.643 0.260 -0.78 l 0.340 -0.889 0.580 -0.645

0.750 -0.819 0.280 -0.831 0.370 -0.901 0.650 -0.607

0.810 -0.804 0.290 -0.840 0.400 -0.928 0.700 -0.614

0.840 -0.786 0.310 -0.838 0.410 -2.611 ** 0.750 -0.674

0.900 -0.648 0.320 -0.823 0.430 -0.927 0.800 -0.751

0.960 -0.537 0.340 -0.810 0.440 -0.881 0.830 -0.708

0.350 -0.454** 0.460 -0.918 0.900 -0.890

0,370 -0.804 0.490 -0.831 0.960 -0.636

0.380 -0.877 0.500 -0.931

0.400 -0.768 0.520 -0.891

0.410 -0.860 0.540 -0.888

0.430 -0.824 0.550 -0.925

0,440 -0.782 0.580 -0.945

0.460 -0.889 0.600 -0.859

0.470 -0.831 0.610 -0.857

0.490 -0.854 0.650 0.044**

0.500 -0.863 0.700 -0.987

0.520 -0.870 0.750 - 1.075

0.530 -0.845 0.820 -0.809

0.550 -0.887 0.890 -0.540

0.560 -0.834 0,900 -0.591

0.580 -0.857 0.960 -0.482

0.590 -0.903

0.600 -0.927

0.640 -0.892

0.700 -0.907

0.750 -0. l 13**

0.820 -0.473

0.870 -0.503

0.930 -0.488

0.960 -0.486

Lower Surface

0.020 -0,029 0.020 -0.211 0.020 0.401 0.020 0.716

0.110 -0.150 0.060 0.233 0.060 0.373 0.060 1.020**

0.230 -0.209 0.090 0.113 0.090 1.522"* 0.110 0.179

0.400 -0.165 0.120 0.050 0.120 -0.143 0.250 -0.039

0.490 -0.272 0.200 -0.005 0.200 -0.027 0.400 -0.099

0.630 2.289"* 0.260 -0.170 0.250 -0.043 0.490 -0.263

0,750 -0.130 0.400 -0.192 0.400 -0.132 0.580 -0.346

0.850 -0.101 0.490 -0.330 0.490 -0.129 0.650 -0.597

0.900 -0.003 0.580 -0.391 0.580 -0.358 0.750 -0.027

0.960 -0.115 0.640 -0.132 0.650 -0.136 0.830 0.197

0.750 0.079 0.750 -0,107 0.900 0.263

0.870 0.106 0.890 0.184 0,960 0.151

0.930 0.060 0.930 0.125

0.960 -0.013 0.960 -2.170* *

CN = 0.513 0.684 0.769 0.741

466
Table H-2. Continued.

Flight 229, Wing sweep = 26 °, Time = 11-42-7-000, MINF = 0.950, Camber = 0/2, ALPT = 6.07, BETA = 0.28, QINF = 301.4,

RNPU = 2.2E+06, CNWP = 0.2974

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.303 0.000 0.850 0.000 7.939"* 0.010 -0.545

0.060 -0.400 0.020 -0.415 0.020 -0.492 0.020 -0.609

0,110 -0.426 0.040 - 1.169"* 0.060 -3.570"* 0.060 -0.624

0.200 -0.449 0.060 -0.527 0.090 -0.597 0.110 -0.621

0.230 -0.375 0.090 -0.501 0.110 -0.677 0.140 -0.652

0.400 -0.454 0.130 -0.518 0.130 -0.503 0.190 -1.581"*

0.490 -0.493 0.150 -0.580 0.150 -0.598 0.250 -0.666

0.590 -0.541 0.200 -0.460 0.210 -0.577 0.400 -0.588

0.630 -0.487 0.250 0.423** 0.250 -0.585 0.490 -0.539

0.700 -0.526 0.260 -0.535 0.340 -0.096** 0.580 -0.438

0.750 -0.679 0.280 0.686** 0.370 3.068** 0.650 -0.442

0.810 -0.645 0.290 0.396** 0.400 -0.667 0.700 -0.410

0.840 -0.636 0.310 -0.176"* 0.410 2.912"* 0.750 -0.492

0.900 -0.188 0.320 0.036"* 0.430 -0.117"* 0.800 -0.619

0.960 -0.147 0.340 0.239** 0.440 -0.149"* 0.830 -0.565

0.350 2.165"* 0.460 -0.207 ** 0.900 -0.755

0.370 0.052"* 0.490 -0.625 0.960 -0.424

0.380 -0.053** 0.500 -0.193"*

0.400 -0.537 0.520 -0.066**

0.410 0.545** 0.540 -0.101 **

0.430 0.422** 0.550 -0.272**

0.440 -0.551 0.580 -0.632

0.460 0.473"* 0.600 -0.102"*

0.470 0.992** 0.610 -0.069"*

0.490 -0.617 0.650 6.341"*

0.500 0.670** 0.700 -0.605

0.520 1.150"* 0.750 -0.715

0.530 -0.610 0.820 -0.599

0.550 0.817"* 0.890 -0.667

0.560 0.074** 0.900 -0.455

0.580 -0.616 0.960 -0.272

0.590 1.237"*

0.600 -0.299**

0.640 -0.692

0.700 -0.660

0.750 -0.233**

0.820 -0.527

0.870 -0.269

0.930 -0.280

0.960 -0.255

Lower Surface

0.020 -0.299 0.020 -0.270 0.020 0.084 0.020 0.476

0.110 -0.333 0.060 -0.015 0.060 0.137 0.060 4.598**

0.230 -0.350 0.090 -0.094 0.090 4.199"* 0.110 0.003

0.400 -0.309 0.120 -0.196'* 0.120 -0.317 0.250 -0.166

0.490 -0.322 0.200 -0.163 0.200 -0.152 0.400 -0.201

0.630 2.518"* 0.260 -0.263 0.250 -0.215 0.490 -0.335

0.750 -0.584 0.400 -0.311 0.400 -0.289 0.580 -0.452

0.850 -0.135 0.490 -0.421 0.490 -0.239 0.650 -0.649

0.900 0.028 0.580 -0.493 0.580 -0.413 0.750 -0.318

0.960 -0.002 0.640 -0.523 0.650 -0.25 | 0.830 -0.106

0.750 -0.175 0.750 -0.159 0.900 0.060

0.870 -0.065 0.890 -0.001 0.960 0.114

0.930 0.028 0.930 0.040

0.960 -0.005 0.960 2.360**

CN = 0.122 0.283 0.392 0.363

467
Table H-2. Continued.

Flight 229, Wing sweep = 26 °, Time = 11-42-16-500, MINF = 0.949, Camber = 0/2, ALPT = 6.10, BETA = 0.31, QINF = 300.4,

RNPU = 2.2E+06, CNWP = 0.3195

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.314 0.000 0.845 0.000 7.966"* 0.010 -0.568

0.060 -0.406 0.020 -0.435 0.020 -0.495 0.020 -0.653

0.110 -0.451 0.040 -1.184* * 0.060 -3.583"* 0.060 -0.584

0.200 -0.451 0.060 -0.545 0.090 -0.595 0.110 -0.643

0.230 -0.395 0.090 -0.512 0.110 -0.680 0.140 -0.673

0.400 -0.490 0.130 -0.527 0.130 -0.526 0.190 - 1.587 * *

0.490 -0.506 0.150 -0.575 0.150 -0.601 0.250 -0.683

0.590 -0.536 0.200 -0.474 0.210 -0.573 0.400 -0.597

0.630 -0.493 0.250 0.452** 0.250 -0.588 0.490 -0.546

0.700 -0.532 0.260 -0.551 0.340 -0.096** 0.580 -0.367

0.750 -0.701 0.280 0.670** 0.370 3.070** 0.650 -0.429

0.810 -0.655 0.290 0.347"* 0.400 -0.684 0.700 -0.417

0.840 -0.646 0.310 -0.244"* 0.410 2.921"* 0.750 -0.494

0.900 -0.182 0.320 -0.097** 0.430 -0.103"* 0.800 -0.629

0.960 -0.148 0.340 0.042"* 0.440 -0.150** 0.830 -0.568

0.350 2.172"* 0.460 -0.214"* 0.900 -0.758

0.370 -0.112"* 0.490 -0.650 0.960 -0.402

0.380 -0.114** 0.500 -0.179**

0.400 -0.528 0.520 -0.084**

0.410 0.250"* 0.540 -0.130"*

0.430 0.185** 0.550 -0.286'*

0.440 -0.557 0.580 -0.634

0.460 0.292"* 0.600 -0.115 * *

0.470 0.719"* 0.610 -0.I 11"*

0.490 -0.627 0.650 6.363 **

0.500 0.435** 0.700 -0.696

0.520 0,987" * 0.750 -0.718

0.530 -0.623 0.820 -0.606

0.550 0.708** 0.890 -0.538

0.560 -0.043** 0.900 -0.389

0.580 -0.626 0.960 -0.245

0.590 1.189**

0.600 -0.306**

0.640 -0.680

0.700 -0.670

0.750 -0.230**

0.820 -0.530

0.870 -0.260

0.930 -0.245

0.960 -0.252

Lower Surface

0.020 -0.271 0.020 -0.079 0.020 0.053 0.020 0.492

0.110 -0.326 0.060 0.003 0.060 0.139 0.060 4.613"*

0.230 -0.360 0.090 -0.098 0.090 4.213"* 0.110 -0.017

0.400 -0307 0.120 -0.t97'* 0.120 -0.319 0.250 -0.181

0.490 -0.331 0.200 -0.164 0.200 -0.139 0.400 -0.209

0.630 2.526** 0.260 -0.272 0,250 -0.224 0.490 -0.340

0.750 -0.579 0.400 -0.316 0.400 -0.291 0.580 -0.469

0.850 -0.105 0.490 -0.423 0.490 -0.233 0.650 -0.659

0.900 0.035 0.580 -0.495 0.580 -0.422 0.750 -0.295

0.960 0.020 0,640 -0.525 0.650 -0.260 0.830 -0.107

0.750 -0.160 0.750 -0.145 0.900 0.054

0.870 -0.056 0.890 0.021 0.960 0.117

0.930 0.031 0.930 0.047

0.960 0.020 0.960 2.367"*

CN = 0.141 0.289 0.399 0.356

468
Table H-2. Continued.

Flight 229, Wing sweep = 26 °, Time = 11-42-32-500, MINF = 0.949, Camber = 0/2, ALPT = 7.16, BETA = 0.02, QINF = 300.6,

RNPU = 2.2E+06, CNWP = 0.3334

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.496 0.000 0.823 0.000 7,961 ** 0.010 -0.672

0.060 -0.509 0.020 -0.681 0.020 -0,583 0.020 -0.715

0.110 -0.554 0.040 -1.255"* 0.060 -3.581 ** 0.060 -0.694

0.200 -0.526 0.060 -0.622 0.090 -0.698 0.110 -0,681

0.230 -0.340 0.090 -0.589 0.110 -0.752 0.140 -0.743

0.400 -0.542 0.130 -0.611 0.130 -0.578 0.190 - 1.586"*

0.490 -0.528 0.150 -0.664 0.150 -0.676 0.250 -0.766

0.590 -0.582 0.200 -0.547 0.210 -0.628 0.400 -0.659

0.630 -0.527 0.250 0.413"* 0.250 -0.653 0.490 -0.569

0.700 -0.562 0.260 -0.605 0.340 -0.143"* 0.580 -0.471

0.750 -0.708 0.280 0.624** 0.370 3.052** 0.650 -0.469

0.810 -0.676 0.290 0.208** 0.400 -0.735 0.700 -0.453

0.840 -0.668 0.310 -0.325** 0.410 2.919"* 0.750 -0.515

0.900 -0.252 0.320 -0.192"* 0.430 -0.180"* 0.800 -0.642

0.960 -0.219 0.340 -0.064** 0.440 -0.214"* 0.830 -0.589

0.350 2.170** 0.460 -0.276** 0.900 -0.775

0.370 -0.202** 0.490 -0.702 0.960 -0.458

0.380 -0.151 ** 0.500 -0.231 **

0.400 -0.615 0.520 -0.136**

0.410 0.093** 0.540 -0.171 **

0.430 0.042** 0.550 -0.352**

0.440 -0.621 0.580 -0.651

0.460 0.158** 0.600 -0.188**

0.470 0.470"* 0.610 -0.153"*

0.490 -0.674 0.650 6.359**

0.500 0.225** 0.700 -0.739

0.520 0.788** 0.750 -0.769

0.530 -0.676 0.820 -0.660

0.550 0.522** 0.890 -0.633

0.560 -0.127"* 0.900 -0.452

0.580 -0.672 0.960 -0.290

0.590 1.165"*

0.600 -0.390'*

0.640 -0.736

0.700 -0.709

0.750 -0.219"*

0.820 -0.555

0.870 -0.256

0.930 -0.329

0.960 -0.314

Lower Surface

0.020 -0.191 0.020 -0.156 0.020 0.162 0.020 0.536

0.110 -0.293 0.060 0.060 0.060 0.165 0.060 4.610* *

0.230 -0.340 0.090 -0.048 0.090 4.210"* 0.110 0.084

0.400 -0.344 0.120 -0.108"* 0.120 -0.258 0.250 -0.151

0.490 -0.286 0.200 -0.131 0.200 -0.115 0.400 -0,180

0.630 2.525"* 0.260 -0.250 0.250 -0.162 0.490 -0.314

0.750 -0.544 0.400 -0.282 0.400 -0.251 0.580 -0.404

0.850 -0,132 0.490 -0.404 0.490 -0.225 0.650 -0.643

0.900 0.006 0.580 -0.468 0.580 -0.400 0.750 -0.257

0.960 -0.029 0.640 -0.502 0.650 -0.238 0.830 -0.056

0.750 -0.127 0.750 -0. 130 0.900 0.126

0.870 -0.001 0.890 0.042 0.960 0.140

0.930 0.049 0.930 0.055

0.960 0.017 0.960 2.366"*

CN = 0.187 0.380 0.479 0.454

469
Table H-2. Continued.

Flight 229, Wing sweep = 26 °, Time = II-42-54-000, MINF = 0.945, Camber = 0/2, ALPT = 8.10, BETA = -0.30, QINF = 298.5,

RNPU = 2.2E+06, CNWP = 0.3625

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.581 0.000 0.797 0.000 8.015"* 0.010 -0.732

0.060 -0.640 0.020 -0.690 0.020 -0.668 0.020 -0.810

0.110 -0.648 0.040 - 1.333" * 0.060 -4.071 ** 0.060 -0.773

0.200 -0.591 0.060 -0.705 0.090 -0.741 0.110 -0.775

0.230 -0.514 0.090 -0.682 0.110 -0.816 0.140 -0.815

0.400 -0.584 0.130 -0.654 0.130 -0.666 0.190 - 1.598'*

0.490 -0.587 0.150 -0.739 0.150 -0.759 0.250 -0.841

0.590 -0.602 0.200 -0.644 0.210 -0.702 0.400 -0.699

0.630 -0.567 0.250 0.021 ** 0.250 -0.723 0.490 -0.606

0.700 -0.582 0.260 -0.678 0.340 -0.192"* 0.580 -0.533

0.750 -0.734 0.280 O. 143"* 0.370 3.055** 0.650 -0.524

0.810 -0.724 0.290 -0.213** 0.400 -0,822 0.700 -0.483

0.840 -0.680 0.3 lO -0.396** 0.410 2.939** 0.750 -0.564

0.900 -0.295 0.320 -0.351 ** 0.430 -0.198"* 0.800 -0.674

0.960 -0.256 0.340 -0.256** 0.440 -0.244** 0.830 -0.630

0.350 2.185"* 0.460 -0.304** 0.900 -0.803

0.370 -0.355"* 0.490 -0.761 0.960 -0.432

0.380 -0.147"* 0.500 -0.282" *

0.400 -0.683 0.520 -0.158"*

0.410 -0.258** 0.540 -0.216"*

0.430 -0.220"* 0.550 -0.393'*

0.440 -0.688 0.580 -0.764

0.460 -0.169"* 0.600 -0.225**

0.470 -0.095"* 0.610 -0.210"*

0.490 -0.744 0.650 6.402 **

0.500 -0.305"* 0.700 -0.855

0.520 -0.088"* 0.750 -0.927

0.530 -0.741 0.820 -0.709

0.550 -0.245** 0.890 -0.434

0.560 -0.211 ** 0.900 -0.382

0.580 -0.742 0.960 -0.310

0.590 0.497**

0.600 -0.415 * *

0.640 -0.799

0.700 -0.781

0.750 -0.188"*

0.820 -0,511

0.870 -0.236

0.930 -0.358

0.960 -0.339

Lower Surface

0.020 -0.148 0.020 0.124 0,020 0.271 0.020 0.624

0.110 -0.241 0.060 0.123 0.060 0.247 0.060 4.641 **

0.230 -0.275 0.090 0.028 0.090 4.238 ** 0.110 0.139

0.400 -0.264 0.120 -0.037"* 0.120 -0.220 0.250 -0.101

0.490 -0.274 0.200 -0.081 0.200 -0.075 0.400 -0.138

0.630 2.541 ** 0.260 -0.216 0.250 -0.105 0.490 -0.279

0.750 -0.275 0.400 -0.266 0.400 -0.228 0.580 -0.393

0.850 -0.095 0.490 -0.385 0.490 -0.183 0.650 -0.619

0.900 -0.007 0.580 -0.438 0.580 -0.374 0.750 -0.172

0.960 -0.061 0.640 -0.480 0.650 -0.204 0.830 0.017

0.750 -0.051 0.750 -0.132 0.900 0.201

0.870 0.060 0.890 0.071 0.960 0.150

0.930 0.064 0.930 0.084

0.960 0.024 0.960 2.382"*

CN = 0,326 0.470 0.572 0.548

470
Table H-2. Continued.

Flight 229, Wing sweep = 26 °, Time = 11-42-59-500, MINF = 0,948, Camber = 0/2, ALPT = 9.14, BETA = -0.30, QINF = 302_9,

RNPU = 2.2E+06, CNWP = 0.4088

rl = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.645 0.000 0.782 0.000 7.882 ** 0.010 -0,826

0.060 -0,673 0,020 -0.873 0.020 -0,716 0,020 -0,847

0,110 -0.636 0.040 - 1.410"* 0.060 -4.027 ** 0,060 -0.842

0,200 -0,634 0,060 -0,743 0.090 -0.820 0_ 110 -0.862

0.230 -0.675 0.090 -0.751 0.110 -0.880 0.140 -0,901

0,400 -0,599 0.130 -0,753 0.130 -0,728 0.190 -1.591 **

0,490 -0,623 0.150 -0.791 0.150 -0.801 0,250 -0.914

0.590 -0,630 0,200 -0,700 0.210 -0.758 0.400 -0,759

0,630 -0.591 0.250 0.138** 0,250 -0,786 0,490 -0,602

0,700 -0.616 0.260 -0.737 0,340 -0.276"* 0.580 -0.568

0,750 -0,752 0.280 0.334** 0.370 2.991"* 0.650 -0.538

0.810 -0.714 0.290 -0.188"* 0.400 -0,855 0.700 -0.529

0.840 -0.679 0.310 -0.489"* 0.410 2,880"* 0.750 -0,600

0.900 -0.533 0.320 -0.417"* 0.430 -0.305"* 0,800 -0,678

0.960 -0,429 0.340 -0.309** 0,440 -0.333** 0.830 -0.625

0.350 2.136"* 0.460 -0.391 ** 0.900 -0.804

0.370 -0,425** 0.490 -0.804 0,960 -0,538

0,380 -0.141 ** 0.500 -0.360**

0,400 -0,724 0,520 -0.261 **

0.410 -0,264** 0.540 -0,297**

0,430 -0,250'* 0.550 -0.478"*

0,440 -0.731 0,580 -0,792

0.460 -0.193"* 0.600 -0.321 **

0.470 -0_020"* 0.610 -0.306* *

0.490 -0,790 0,650 6.292 * *

0.500 -0.264** 0.700 -0,891

0,520 0.051 ** 0.750 -0.984

0.530 -0,783 0,820 -0,743

0,550 -0.092** 0.899 -0,533

0,560 -0.303** 0.900 -0.494

0.580 -0,791 0,960 -0.382

0.590 0,753**

0.600 -0,464**

0.640 -0.833

0.700 -0.825

0.750 -0.169"*

0.82O -O.550

0,870 -0.205

0,930 -0,427

0,960 -0,422

Lower Surface

0.020 -0.043 0,020 0,001 0,020 0.342 0,020 0.697

0,110 -0,161 0,060 0,191 0,060 0,309 0,060 4.557**

0.230 -0.220 0.090 0,078 0,090 4.160"* 0.110 0.211

0.400 -0.214 0.120 0.001 ** 0.120 -0.153 0.250 -0,056

0,490 -0.264 0.200 -0,027 0.200 -0.017 0.400 -0.090

0.630 2.488** 0.260 -0.171 0.250 -0.057 0.490 -0.239

0,750 -0,154 0.400 -0.211 0,400 -0.182 0.580 -0.378

0,850 -0,099 0,490 -0.343 0.490 -0.153 0.650 -0,578

0,900 -0.018 0.580 -0.414 0,580 -0.337 0.750 -0.120

0.960 -0.123 0,640 -0,464 0.650 -0.181 0.830 0.113

0,750 0.04 1 0.750 -0.131 0.900 0.259

0.870 0,085 0.890 0.126 0,960 0_ 173

0,930 0,073 0.930 0,096

0,960 0.022 0,960 2.330**

CN = 0.431 0,563 0,659 0.640

471
Table H-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 14-14-17-500, MINF = 0.939, Camber = 0/2, ALPT -- 8.06, BETA -- -0.24, QINF = 305.6,

RNPU -- 2.3E+06, CNWP = 0.3526

rl -- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.589 0.000 0.830 0.000 0.740** 0.010 -0.835

0.060 -0.565 0.020 -0.855 0.020 -0.682 0.020 . -0.908

0.110 -0.601 0.040 -0.586 0.060 -3.041 ** 0.060 -0.923

0.200 -0.613 0.060 -0.718 0.090 -0.768 0.110 -0.882

0.230 -0.570 0.090 -0.714 0.110 -0.810 0.1 40 -0.906

0.400 -0.636 0.130 -0.710 0.130 -0.710 0.190 -1.619"*

0.490 -0.591 0.150 -0.740 0.150 -0.796 0.250 -0.932

0.590 -0.628 0.200 -0.654 0.210 -0.727 0.400 -0.689

0.630 -0.560 0.250 -0.742 0.250 -0.749 0.490 -0.628

0.700 -0.586 0.260 -0.656 0.340 -0.806 0.580 -0.586

0.750 -0.773 0.280 -0.727 0.370 -0.791 0.650 -0.541

0.810 -0.749 0.290 -0.727 0.400 -0.831 0.700 -0.537

0.840 -0.744 0.310 -0.732 0.410 -2.596"* 0.750 -0.614

0.900 -0.240 0.320 -0.726 0.430 -0.814 0.800 -0.720

0.960 -0.257 0.340 -0.711 0.440 -0.785 0.830 -0.683

0.350 -0.457** 0.460 -0.811 0.900 -0.842

0.370 -0.704 0.490 -0.794 0.960 -0.430

0.380 -0.771 0.500 -0.843

0.400 -0.670 0.520 -0.798

0.410 -0.765 0.540 -0.80l

0.430 -0.752 0.550 -0.827

0.440 -0.697 0.580 -0.829

0.460 -0.802 0.600 -0.759

0.470 -0.724 0.610 -0.758

0.490 -0.752 0.650 0.151 **

0.500 -0.773 0.700 -0.878

0.520 -0.770 0.750 -0.941

0.530 -0.748 0.820 -0.760

0.550 -0.795 0.890 -0.363

0.560 -0.744 0.900 -0.382

0.580 -0.759 0.960 -0.296

0.590 -0.803

0.600 -0.797

0.640 -0.807

0.700 -0.830

0.750 -0.173"*

0.820 -0.376

0.870 -0.312

0.930 -0.338

0.960 -0.305

Lower Surface

0.020 -0.159 0.020 -0.246 0.020 0.236 0.020 0.595

0.110 -0.294 0.060 0.103 0.060 0.214 0.060 0.959**

0.230 -0.290 0.090 0.004 0.090 1.417' * 0. 110 0.063

0.400 -0.261 0.120 -0.062 0.120 -0.246 0.250 -0.132

0.490 -0.310 0.200 -0.093 0.200 -0.110 0.400 -0.177

0.630 2.162"* 0.260 -0.253 0.250 -0.145 0.490 -0.330

0.750 -0.154 0.400 -0.281 0.400 -0.203 0.580 -0.407

0.850 -0.024 0.490 -0.404 0.490 -0.200 0.650 -0.655

0.900 0.048 0.580 -0.456 0.580 -0.414 0.750 -0.187

0.960 -0.004 0.640 -0.509 0.650 -0.199 0.830 0.019

0.750 -0.044 0.750 -0.135 0.900 0.182

0.870 0.063 0.890 0.077 0.960 0.127

0.930 0.074 0.930 0.090

0.960 0.017 0.960 -2.118"*

CN = 0.356 0.470 0.580 0.566

472
Table H-2. Continued.

Flight 229, Wing sweep = 26 °, Time = 11-46-10-000, MINF = 0.947, Camber = 512, ALPT = 6.50, BETA = -0.10, QINF = 301.2,

RNPU = 2.2E+06, CNWP = 0.3148

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x,/c CP x/c CP

0.020 0.232 0,000 0.722 0.000 7.935"* 0.010 -0.109

0.060 -0.047 0.020 -0.017 0,020 0.098 0.020 -0.049

0.110 -0.256 0,040 -0,703** 0.060 -3.997** 0.060 -0.395

0.200 -0.641 0.060 -0.198 0.090 -0.333 0.110 -0.610

0.230 -0.621 0.090 -0.257 0.110 -0.512 0.140 -0.792

0.400 -0.594 0.130 -0.381 0.130 -0.464 0.190 - 1,591 **

0.490 -0.535 0.150 -0.604 0.150 -0.687 0.250 -0.771

0.590 -0.517 0,200 -0.581 0.210 -0.634 0.400 -0.616

0.630 -0.520 0.250 -0.064** 0.250 -0.652 0.490 -0.556

0.700 -0.551 0.260 -0.624 0.340 -0,106"* 0.580 -0.438

0.750 -0.701 0.280 0.041"* 0.370 2.888** 0,650 -0.437

0.810 -0.675 0.290 -0,223** 0.400 -0.793 0.700 -0.431

0,840 -0.656 0.310 -0.300"* 0,410 2.904"* 0.750 -0.501

0,900 -0.185 0.320 -0.279"* 0.430 -0.112"* 0.800 -0,626

0.960 -0.14 l 0,340 -0.177"* 0.440 -0.160"* 0.830 -0,572

0.350 2.157"* 0,460 -0.226** 0.900 -0.762

0.370 -0.263** 0.490 -0.695 0.960 -0.387

0.380 -0.148"* 0.500 -0.176"*

0.400 -0,615 0.520 -0.095"*

0.410 -0.192"* 0,540 -0.123"*

0,430 -0.128"* 0.550 -0.304**

0.440 -0.616 0.580 -0.681

0.460 -0.149 ** 0.600 -0.130 * *

0.470 -0.047"* 0.610 -0.118"*

0.490 -0.671 0.650 6.336**

0.500 -0.232** 0.700 -0.691

0.520 -0.121 ** 0,750 -0.746

0.530 -0.671 0.820 -0,612

0.550 -0.206** 0.890 -0.419

0.560 -0.118** 0.900 -0.340

0.580 -0.682 0.960 -0.230

0.590 0.291"*

0.600 -0.331"*

0.640 -0.742

0.700 -0.730

0.750 -0.191"*

0.820 -0.439

0.870 -0.230

0.930 -0.274

0.960 -0.260

Lower Surface

0.020 - 1.033 0.020 -0.797 0.020 -0,577 0.020 0.189

0.110 -0.403 0.060 -0.095 0.060 0,055 0.060 4.591 **

0.230 -0.078 0.090 -0.172 0.090 4.192"* 0.1 l0 0.004

0.400 -0.233 0.120 -0.135"* 0.120 -0.356 0.250 -0.139

0.490 -0.257 0.200 -0.089 0.200 -0.124 0,400 -0.180

0.630 2.510"* 0.260 -0.185 0,250 -0.137 0.490 -0.329

0.750 -0.44 1 0.400 -0.290 0.400 -0.259 0.580 -0.402

0.850 -0.061 0.490 -0.408 0.490 -0.204 0.650 -0.647

0.900 0.054 0.580 -0.453 0.580 -0.407 0.750 -0.282

0,960 0.029 0,640 -0.447 0.650 -0.216 0.830 -0.077

0.750 -0.073 0.750 -0.139 0.900 0.111

0.870 0,029 0.890 0.034 0.960 0.1 44

0,930 0.045 0.930 0.061

0.960 0.016 0,960 2.352 * *

CN = 0.240 0.321 0,422 0.386

473
Table H-2. Continued.

Flight 229, Wing sweep = 26 °, Time = 11-46-40-500, MINF = 0.946, Camber = 5/2, ALPT = 6.10, BETA = 0.19, QINF = 299.6,

RNPU = 2.2E+06, CNWP = 0.2930

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.238 0.000 0.687 0.000 7.982** 0.010 -0.209

0.060 0.027 0.020 -0.008 0.020 0.113 0.020 -0.060

0.110 -0.268 0.040 -0,684** 0.060 -4.014"* 0.060 -0.371

0.200 -0.627 0.060 -0.194 0.090 -0.309 0.110 -0.579

0.230 -0.589 0.090 -0.245 0.110 -0.507 0.140 -0.770

0,400 -0.585 0.130 -0.393 0.130 -0.450 0.190 - 1.595 * *

0.490 -0.544 0.150 -0.575 0.150 -0.658 0.250 -0.785

0.590 -0.565 0.200 -0.568 0.210 -0.638 0.400 -0.622

0.630 -0.522 0.250 -0.046** 0.250 -0.636 0.490 -0.545

0.700 -0.541 0.260 -0.624 0.340 -0.086** 0.580 -0.436

0.750 -0.711 0.280 0.064** 0.370 2,877** 0.650 -0.439

0.810 -0.685 0.290 -0.182** 0.400 -0.837 0.700 -0.423

0.840 -0.662 0.310 -0.281 ** 0.410 2.925"* 0.750 -0,491

0.900 -0.164 0.320 -0.262** 0.430 -0.092** 0.800 -0.633

0.960 -0.130 0.340 -0.159** 0.440 -0.150** 0.830 -0,576

0.350 2.173"* 0.460 -0.212"* 0.900 -0.752

0.370 -0.251 ** 0.490 -0.708 0.960 -0.352

0.380 -0.144** 0.500 -0.163"*

0.400 -0.650 0.520 -0.073"*

0.410 -0.166"* 0.540 -0.119"*

0.430 -0.100"* 0.550 -0.274**

0.440 -0.614 0.580 -0.660

0,460 -0.108"* 0.600 -0.114"*

0.470 -0,024 ** 0.610 -0.115 * *

0.490 -0.662 0.650 6.375**

0.500 -0.243** 0.700 -0.672

0.520 -0.074** 0.750 -0.738

0.530 -0.674 0.820 -0.617

0.550 -0.169"* 0.890 -0.408

0.560 -0.094** 0.900 -0.320

0,580 -0.683 0,960 -0.209

0.590 0.301"*

0.600 -0.332**

0.640 -0.743

0.700 -0.715

0.750 -0.187"*

0.820 -0.369

0.870 -0.242

0.930 -0.282

0.960 -0.268

Lower Surface

0.020 - 1.101 0.020 -0,850 0.020 -0.637 0.020 0.113

0.110 -0.402 0.060 -0.173 0.060 0.019 0.060 4.621 **

0.230 -0.103 0.090 -0.218 0.090 4.219* * 0. t l0 -0.047

0,400 -0.210 0.120 -0.163 ** 0.120 -0.394 0.250 -0.183

0.490 -0.276 0.200 -0.095 0.200 -0.182 0.400 -0.191

0.630 2.529** 0.260 -0.203 0.250 -0.177 0.490 -0.356

0.750 -0.435 0.400 -0,302 0.400 -0.275 0,580 -0.439

0.850 -0.060 0.490 -0.417 0,490 -0.200 0.650 -0.657

0.900 0.066 0.580 -0.481 0.580 -0.419 0,750 -0.298

0.960 0.051 0.640 -0.456 0.650 -0.224 0.830 -0.113

0.750 -0.085 0.750 -0.135 0.900 0.092

0.870 0.034 0.890 0.017 0.960 0.122

0.930 0.03 l 0.930 0.066

0,960 0.021 0.960 2.369**

CN = 0.236 0.301 0,400 0.354

474
Table H-2. Continued.

Flight 217, Wing sweep = 26 °, Time = 9-21-19-500, MINF = 0.606, Camber = 0/2, ALPT = 5.98. BETA = 0.48, QINF = 299.2,

RNPU = 3.0E+06, CNWP = 0.3170

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.489 0.000 0.684 0.000 6.135"* 0.010 - 1.678

0.060 -0.316 0.020 -0.961 0.020 - 1.135 0.020 -0.976

0.110 -0.30l 0.040 -0.626 0.060 -1.349"* 0.060 -0.793

0.200 -0.243 0.060 -0.573 0.090 -0.510 0.110 -0.556

0.230 -0.268 0.090 -0.411 0.110 -0.554 0.140 -0.547

0.400 -0.182 0.130 -0.407 0.130 -0.502 0.190 -3.888 **

0.490 -0.213 0.150 -0.404 0.150 -0.483 0.250 -0,403

0.590 -0.209 0.200 -0.364 0.210 -0,484 0.400 -0.351

0,630 -0.197 0.250 -0,349 0.250 -0.359 0.490 -0.273

0,700 -0.167 0.260 -0.322 0.340 -0.384 0.580 -0,292

0.750 -0.213 0.280 -0.335 0.370 -0.373 0.650 -0.339

0.810 -0.184 0.290 -0.318 0.400 -0.328 0.700 -0.306

0.840 -0.176 0.310 -0.312 0.410 0.602"* 0.750 -0.287

0.900 -0.101 0.320 -0.320 0.430 -0.348 0,800 -0.300

0.960 -0.013 0.340 -0.317 0.440 -0.339 0.830 -0.268

0.350 -0,178"* 0.460 -0.328 0.900 -0.181

0.370 -0.282 0,490 -0.267 0,960 -0.015

0.380 -0.314 0.500 -0.319

0.400 -0.236 0,520 -0.298

0.410 -0.298 0.540 -0.315

0.430 -0.268 0.550 -0.249

0.440 -0.260 0,580 -0.227

0.460 -0.268 0.600 -0.304

0.470 -0,293 0.610 -0.309

0.490 -0.262 0.650 4.761 **

0.500 -0.262 0.700 -0.331

0.520 -0.292 0.750 -0.326

0.530 -0.258 0.820 -0.286

0.550 -0.319 0.890 -0.134

0.560 -0.290 0.900 -0.098

0.580 -0.259 0.960 0.014

0.590 -0.279

0.600 -0.276

0.640 -0.285

0.700 -0.283

0.750 -0.030**

0.820 -0.226

0.870 -0.209

0.930 -0.095

0.960 -0.047

Lower Surface

0.020 -0.030 0.020 0.165 0.020 0.316 0,020 0.585

0.110 -0.066 0.060 0.121 0.060 0.235 0.060 -0.880

0.230 0.003 0.090 0,066 0.090 1.081 ** 0.110 0.193

0.400 -0.022 0.120 0.022 0.120 -0.062 0.250 -0.086

0,490 0.005 0.200 -0.010 0,200 -0,014 0.400 -0.081

0.630 1.842"* 0.260 -0.057 0.250 -0.041 0.490 -0.111

0.750 0.006 0,400 -0.060 0.400 -0.083 0.580 -0.157

0.850 0.077 0,490 -0,086 0.490 -0.017 0.650 -0.055

0.900 0,152 0.580 -0,092 0.580 -0.105 0.750 0.127

0.960 0.137 0.640 0.042 0.650 -0.039 0.830 0.283

0.750 0.183 0,750 0.183 0,900 0.303

0.870 0.248 0.890 0.265 0,960 0.252

0.930 0.200 0.930 0.221

0.960 0.149 0.960 0.514"*

CN = 0.208 0.345 0,350 0.333

475
Table H-2. Continued.

Flight 217, Wing sweep = 26 °, Time = 9-21-36-500, MINF = 0.651, Camber = 0/2, ALPT = 4.59, BETA = 0.37, QINF = 344.3,

RNPU = 3.3E+06, CNWP = 0.2748

"q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.175 0.000 0.831 0.000 5.343 * * 0.010 - 1.301

0.060 -0.184 0.020 -0.506 0.020 -0.639 0.020 -0.700

O.l lO -0.248 0.040 -0.370 0.060 -3.437** 0.060 -0.587

0.200 -O.184 0.060 -0.383 0.090 -0.377 O.110 -0.455

0.230 -0.159 0.090 -0.289 0.110 -0.411 0.140 -0.451

0.400 -0.155 0.130 -0.298 0.130 -0.402 0.190 -3.367"*

0.490 -0.157 0.150 -0.309 0.150 -0.397 0.250 -0.369

0.590 -0.205 0.200 -0.282 0.210 -0.397 0.400 -0.306

0.630 -0.182 0.250 -0.282 0.250 -0.287 0.490 -0.260

0.700 -0.156 0.260 -0.268 0.340 -0.322 0.580 -0.242

0.750 -0.202 0.280 -0.283 0.370 -0.338 0.650 -0.331

0.810 -0.185 0.290 -0.269 0.400 -0.292 0.700 -0.293

0.840 -0.172 0.310 -0.258 0.410 0.535** 0.750 -0.288

0.900 -0.110 0.320 -0.271 0.430 -0.297 0.800 -0.301

0.960 -0.008 0.340 -0.258 0.440 -0.296 0.830 -0.265

0.350 -0.170** 0.460 -0.292 0.900 -0.181

0.370 -0.239 0.490 -0.252 0.960 -0.020

0.380 -0.271 0.500 -0.284

0.400 -0.203 0.520 -0.295

0.4 l0 -0.254 0.540 -0.268

0.430 -0.234 0.550 -0.217

0.440 -0.216 0.580 -0.219

0.460 -0.227 0.600 -0.269

0.470 -0.256 0.610 -0.287

0.490 -0.231 0.650 4.150**

0.500 -0.254 0.700 -0.336

0.520 -0.240 0.750 -0.303

0.530 -0.234 0.820 -0.281

0.550 -0.268 0.890 -0.130

0.560 -0.259 0.900 -0.091

0.580 -0.231 0.960 0.014

0.590 -0.268

0.600 -0.268

0.640 -0.275

0.700 -0.268

0.750 -0.033**

0.820 -0.226

0.870 -0.204

0.930 -0.095

0.960 -0.029

Lower Surface

0.020 -0.258 0.020 -0.107 0.020 0.076 0.020 0.369

0.110 -0. t 56 0.060 -0.059 0.060 0.084 0.060 -0.848

0.230 -0.073 0.090 -0.058 0.090 0.951 ** 0.110 0.002

0.400 -0.071 0.120 -0.077 0.120 -0.165 0.250 -0.172

0.490 -0.048 0.200 -0.070 0.200 -0.110 0.400 -0.141

0.630 1.613 ** 0.260 -0.119 0.250 -0.134 0.490 -0.169

0.750 0.009 0.400 -0.114 0.400 -0.133 0.580 -0.198

0.850 0.093 0.490 -0.125 0.490 -0.028 0.650 -0.093

0.900 0.167 0.580 -0.130 0.580 -0.143 0.750 0.121

0.960 0.158 0.640 0.035 0.650 -0.047 0.830 0.269

0.750 0.167 0.750 0.172 0.900 0.298

0.870 0.249 0.890 0.267 0.960 0.253

0.930 0.193 0.930 0.223

0.960 0.149 0.960 0.459**

CN = 0.135 0.247 0.266 0.241

476
Table H-2. Continued.

Flight 217, Wing sweep = 26 °, Time = 9-21-44-000, MINF = 0,700. Camber = 0/2, ALPT = 4.77, BETA = O11, QINF = 400.5,

RNPU = 3.6E+06, CNWP = 0.2929

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.196 0.000 0.837 0,000 4,574"* 0.010 - 1.215

0,060 -0.205 0,020 -0,475 0,020 -0.720 0,020 -0.881

0.110 -0.211 0.040 -0.392 0,060 -2,973"* 0.060 -0.648

0.200 -0,194 0.060 -0.409 0.090 -0.405 0.110 -0.463

0.230 -0.183 0,090 -0.317 0.110 -0.431 0.140 -0,478

0.400 -0,148 0.130 -0,322 0.130 -0.428 0.190 -2,912"*

0.490 -0.160 0.150 -0,333 0.150 -0 395 0.250 -0.335

0.590 -0,203 0.200 -0.296 0.210 -0,433 0,400 -0.313

0.630 -0.182 0.250 -0,293 0.250 -0,315 0.490 -0.257

0,700 -0.170 0,260 -0.290 0,340 -0,341 0.580 -0,258

0.750 -0,203 0.280 -0,298 0.370 -0,347 0,650 -0.335

0,810 -0.205 0,290 -0.292 0.400 -0.299 0,700 -0,309

0,840 -0.179 0.310 -0,277 0.410 0.441 ** 0,750 -0,305

0.900 -0.109 0.320 -0.288 0.430 -0,320 0.800 -0,306

0,960 0.003 0.340 -0.282 0.440 -0.298 0.830 -0.276

0,350 -0.181 ** 0,460 -0.303 0.900 -0.189

0.370 -0.250 0,490 -0,270 0.960 -0.030

0,380 -0.281 0,500 -0.296

0.400 -0.213 0.520 -0.294

0.410 -0.262 0.540 -0.289

0.430 -0.244 0.550 -0.236

0.440 -0,218 0.580 -0.226

0.460 -0.234 0.600 -0.290

0,470 -0,266 0.610 -0.300

0,490 -0.229 0.650 3,548**

0.500 -0.257 0.700 -0,330

0.520 -0.251 0.750 -0.318

0.530 -0,242 0.820 -0.286

0.550 -0,275 0.890 -0.121

0.560 -0.267 0.900 -0,080

0,580 -0.242 0,960 0,025

0.590 -0.270

0,600 -0.265

0.640 -0.289

0.700 -0.272

0.750 -0.037**

0.820 -0.226

0.870 -0,200

0.930 -0.083

0.960 -0.020

Lower Surface

0.020 -0.263 0.020 -0.074 0,020 0.074 0.020 0.395

0.110 -0.162 0.060 -0.020 0,060 0.128 0.060 -0,715

0.230 -0.072 0,090 -0.055 0,090 0.799"* 0.110 -0.001

0.400 -0.045 0,120 -0.096 0.120 -0,143 0.250 -0.171

0,490 -0.050 0,200 -0.074 0.200 -0.112 0,400 -0.154

0.630 1.367"* 0,260 -0.127 0.250 -0.135 0,490 -0,181

0.750 0.025 0.400 -0.116 0,400 -0.150 0.580 -0,216

0.850 0,097 0.490 -0,122 0,490 -0.033 0,650 -0.089

0.900 0.176 0,580 -0.126 0,580 -0.153 0,750 0,124

0.960 0.159 0,640 0.039 0.650 -0,048 0.830 0.279

0.750 0.180 0.750 0.189 0.900 0.307

0.870 0.292 0.890 0,281 0.960 0.266

0.930 0.201 0.930 0.233

0.960 0.168 0.960 0.375 **

CN = 0.143 0,262 0.282 0.259

477
Table H-2. Continued.

Flight 217, Wing sweep = 26 °, Time = 9-21-49-500, MINF -- 0.751, Camber = 0/2, ALPT = 4.06, BETA = 0.37, QINF = 462.6,

RNPU = 4.0E+06, CNWP = 0.2450

rl = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.059 0,000 0.852 0.000 3.947"* 0.010 -1.006

0.060 -0.160 0.020 -0.338 0.020 -0.492 0,020 - 1.032

O. 110 -0.203 0.040 -0.284 0.060 -2.587"* 0.060 -0.597

0,200 -0.177 0.060 -0.337 0.090 -0.312 0.110 -0.426

0.230 -0.213 0.090 -0.259 0.110 -0.380 0.140 -0.462

0.400 -0.161 0.130 -0.271 0.130 -0.387 0.190 -2.535**

0.490 -0.171 0.150 -0.298 0.150 -0.383 0.250 -0.349

0.590 -0.203 0.200 -0.273 0.210 -0.407 0.400 -0.307

0.630 -0.203 0.250 -0.283 0.250 -0.300 0.490 -0.266

0.700 -0.180 0,260 -0.268 0.340 -0.319 0.580 -0.266

0.750 -0.222 0.280 -0.283 0,370 -0,333 0.650 -0.338

0.810 -0.200 0.290 -0,283 0.400 -0.295 0.700 -0.321

0.840 -0.178 0.310 -0.267 0.410 0.369** 0.750 -0.315

0.900 -0.101 0.320 -0.272 0.430 -0.305 0.800 -0.309

0.960 0.010 0.340 -0.265 0.440 -0.298 0.830 -0.278

0.350 -0.200** 0.460 -0.300 0.900 -0.191

0.370 -0.241 0.490 -0.262 0.960 -0.012

0.380 -0.269 0.500 -0.292

0.400 -0.283 0.520 -0.285

0.410 -0.258 0.540 -0.285

0.430 -0.242 0.550 -0.236

0.440 -0.230 0.580 -0.226

0.460 -0.239 0.600 -0.286

0.470 -0.264 0.610 -0.303

0.490 -0.240 0.650 3.059**

0.500 -0.249 0.700 -0.339

0.520 -0.255 0.750 -0.325

0.530 -0.243 0.820 -0.307

0.550 -0.275 0.890 -0.128

0.560 -0.268 0.900 -0,082

0.580 -0.244 0.960 0.025

0.590 -0,274

0.600 -0.268

0.640 -0.310

0.700 -0.291

0.750 -0.040**

0.820 -0.247

0.870 -0.215

0.930 -0.089

0.960 -0.023

Lower Surface

0.020 -0.405 0,020 -0.254 0.020 -0.049 0,020 0.284

0.110 -0.235 0.060 -0.123 0.060 -0.004 0.060 -0.685

0.230 -0.132 0.090 -0.138 0.090 0.679 ** 0.110 -0.062

0.400 -0.074 0.120 -0.162 0.120 -0.201 0.250 -0.235

0.490 -0.056 0.200 -0.127 0.200 -0.180 0.400 -0.210

0.630 1.171 ** 0.260 -0.189 0.250 -0.205 0.490 -0.228

0.750 0.031 0.400 -0.150 0.400 -0.192 0.580 -0.260

0.850 0.101 0.490 -0.156 0.490 -0.051 0.650 -0.114

0.900 0.189 0.580 -0.145 0.580 -0.188 0.750 0.128

0.960 0.170 0,640 0.030 0.650 -0.048 0.830 0.274

0.750 0.178 0.750 0.199 0,900 0.316

0.870 0.252 0.890 0.291 0.960 0.265

0.930 0.213 0.930 0.242

0.960 0.171 0.960 0.312"*

CN = 0.127 0.220 0.239 0.233

478
Table H-2. Continued.

Flight 217, Wing sweep = 26 °, Time = 9-21-55-000, MINF = 0.803, Camber = 0/2, ALPT = 3.79, BETA = 0.48, QINF = 531.0,

RNPU = 4.3E÷06, CNWP = 0.2570

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0.018 0.000 0.856 0.000 3.432** 0.010 -0.831

0.060 -0.136 0.020 -0.270 0.020 -0.409 0.020 -0.883

O. 110 -0.288 0.040 -0.245 0.060 -2.261 ** 0.060 -0.681

0.200 -0.183 0.060 -0.327 0.090 -0.350 O. 110 -0.329

0.230 -0. 193 0.090 -0.253 0.110 -0.364 0.140 -0.500

0.400 -0.171 0.130 -0.273 0.130 -0.391 0.190 -2.216"*

0.490 -0.162 0.150 -0.304 0.150 -0.379 0.250 -0.351

0.590 -0.215 0.200 -0.284 0.210 -0.425 0.400 -0.310

0.630 -0.213 0.250 -0.290 0.250 -0.314 0.490 -0.271

0.700 -0.186 0.260 -0.276 0.340 -0.319 0.580 -0.263

0.750 -0.220 0.280 -0.289 0.370 -0.333 0.650 -0.363

0.810 -0.198 0.290 -0.289 0.400 -0.294 0.700 -0.340

0.840 -0.192 0.310 -0.275 0.410 0.314"* 0.750 -0.350

0.900 -0.093 0.320 -0.284 0.430 -0.315 0.800 -0.316

0.960 0.032 0.340 -0.273 0.440 -0.308 0.830 -0.285

0.350 -0.212'* 0.460 -0.303 0.900 -0.179

0.370 -0.253 0.490 -0.270 0.960 0.002

0.380 -0.276 0.500 -0.302

0.400 -0.210 0.520 -0.294

0.410 -0.264 0.540 -0.287

0.430 -0.244 0.550 -0.245

0.440 -0.231 0.580 -0.238

0.460 -0.246 0.600 -0.302

0.470 -0.260 0.610 -0.317

0.490 -0.245 0.650 2.657"*

0.500 -0.252 0.700 -0.36l

0.520 -0.247 0.750 -0.326

0.530 -0.251 0.820 -0.313

0.550 -0.273 0.890 -0.115

0.560 -0.272 0.900 -0.070

0.580 -0.242 0.960 0.038

0.590 -0.281

0.600 -0.277

0.640 -0.335

0.700 -0.294

0.750 -0.047**

0.820 -0.248

0.870 -0.213

0.930 -0.079

0.960 -0.011

Lower Surface

0.020 -0.517 0.020 -0.346 0.020 -0.112 0.020 0.333

0.110 -0.283 0.060 -0.165 0.060 -0.033 0.060 -0.625

0.230 -0.163 0.090 -0.183 0.090 0.584** 0.110 -0.118

0.400 -0.101 0.120 -0.219 0.120 -0.230 0.250 -0.285

0.490 -0.073 0.200 -0.167 0.200 -0.264 0.400 -0.260

0.630 1.013"* 0.260 -0.233 0.250 -0.260 0.490 -0.282

0.750 0.036 0.400 -0.176 0.400 -0.230 0.580 -0.308

0.850 0.111 0.490 -0.175 0.490 -0.060 0.650 -0.132

0.900 0.204 0.580 -0.160 0.580 -0.220 0.750 0.120

0.960 0.185 0.640 0.021 0.650 -0.049 0.830 0.277

0.750 0.185 0.750 0.204 0.900 0.319

0.870 0.233 0.890 0.299 0.960 0.277

0.930 0.223 0.930 0.253

0.960 0.181 0.960 0.264"*

CN = 0.117 0.199 0.227 0.211

479
Table H-2. Continued.

Flight 217, Wing sweep = 26 °, Time = 9-22-0-500, MINF = 0.851, Camber = 0/2, ALPT = 4.32, BETA = 0.89, QINF = 598.9,

RNPU = 4.7E÷06, CNWP = 0.2841

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.041 0.000 0,871 0.000 3.036"* 0.010 -0,697

0.060 -0.179 0.020 -0.336 0.020 -0.419 0.020 -0.776

0.110 -0.242 0.040 -0.298 0.060 -2.012"* 0.060 -0.635

0.200 -0.214 0.060 -0.365 0.090 -0.618 0.110 -0.671

0.230 -0.276 0,090 -0.310 0.110 -0.605 0.140 -0,679

0.400 -0.187 0.130 -0.352 0,130 -0.533 0.190 -1.971"*

0,490 -0,191 0.150 -0.331 0.150 -0.496 0,250 -0.501

0.590 -0.239 0,200 -0.340 0,210 -0,477 0.400 -0,292

0.630 -0.246 0,250 -0,364 0,250 -0,299 0.490 -0.289

0.700 -0.197 0,260 -0,290 0,340 -0.394 0.580 -0.293

0,750 -0.220 0.280 -0.312 0.370 -0.340 0,650 -0.397

0.810 -0.196 0.290 -0.332 0.400 -0.363 0.700 -0.358

0.840 -0.191 0.310 -0.325 0.410 0.271 ** 0.750 -0.394

0.900 -0.083 0.320 -0.319 0.430 -0.338 0.800 -0.395

0.960 0,035 0.340 -0.311 0,440 -0.322 0.830 -0.424

0.350 -0,256** 0.460 -0.317 0.900 -0.153

0,370 -0,282 0.490 -0.279 0.960 0.022

0.380 -0,305 0.500 -0.312

0.400 -0.262 0.520 -0.307

0.410 -0.283 0.540 -0.285

0.430 -0.260 0,550 -0.250

0.440 -0.248 0.580 -0,234

0.460 -0.271 0,600 -0,287

0.470 -0.287 0.610 -0.312

0,490 -0,265 0.650 2.349**

0.500 -0.272 0,700 -0.536

0.520 -0.279 0,750 -0.480

0,530 -0.270 0.820 -0.288

0.550 -0.313 0.890 -0.087

0,560 -0,300 0.900 -0.046

0.580 -0.266 0.960 0.059

0.590 -0.299

0,600 -0.271

0.640 -0.512

0.700 -0.443

0.750 -0.051 **

0.820 -0.241

0.870 -0.204

0.930 -0,058

0.960 0.004

Lower Surface

0,020 -0,553 0.020 -0.341 0.020 -0.105 0.020 0.357

0.110 -0.411 0.060 -0.152 0.060 -0,027 0,060 -0,556

0.230 -0.180 0.090 -0.183 0.090 0.511 ** 0.110 -0.116

0,400 -0.120 0.120 -0,244 0.120 -0.226 0,250 -0.311

0.490 -0.093 0.200 -0.284 0.200 -0,299 0,400 -0.305

0,630 0.891 ** 0.260 -0.291 0.250 -0,324 0,490 -0.368

0.750 0.025 0.400 -0.207 0.400 -0.287 0.580 -0,389

0.850 0.112 0.490 -0.188 0.490 -0.078 0.650 -0.145

0.900 0.197 0.580 -0.178 0.580 -0.253 0.750 0.119

0,960 0.191 0.640 0.026 0.650 -0.063 0.830 0.275

0.750 0.188 0.750 0.212 0.900 0.322

0,870 0.264 0.890 0.306 0,960 0.283

0.930 0.232 0,930 0,260

0.960 0.191 0.960 0.228**

CN = 0,106 0.226 0,264 0.245

480
Table H-2, Continued,

Flight 217, Wing sweep = 26 °, Time = 9-22-6-500, MINF = 0.883, Camber = 0/2, ALPT = 4.23, BETA = 0.48. QINF = 642.7,

RNPU = 4,9E+06, CNWP = 0.2886

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.031 0.000 0.860 0,000 2.833** 0.010 -0.616

0,060 -0.200 0,020 -0.282 0.020 -0.341 0.020 -0.710

O. 110 -0,297 0.040 -0.272 0,060 - 1.870"* 0.060 -0.575

0,200 -0.234 0.060 -0.452 0.090 -0.564 0,110 -0.631

0.230 -0,348 0,090 -0.418 0.110 -0.561 0.140 -0.646

0.400 -0.160 0,130 -0,358 0.130 -0.511 0.190 -1.833"*

0.490 -0.174 0.150 -0,368 0,150 -0,495 0.250 -0,594

0.590 -0.225 0.200 -0,335 0,210 -0,501 0,400 -0.609

0.630 -0.256 0,250 -0.476 0.250 -0,558 0.490 -0.228

0.700 -0.354 0.260 -0.470 0.340 -0,628 0.580 -0.236

0,750 -0.200 0,280 -0.483 0,370 -0,638 0.650 -0,339

0.810 -0.195 0.290 -0,495 0.400 -0.563 0.700 -0.319

0,840 -0.186 0.310 -0.477 0.410 0.257 ** 0.750 -0.389

0.900 -0.077 0.320 -0.498 0.430 -0.267 0.800 -0.553

0.960 0.047 0.340 -0.518 0.440 -0.230 0_830 -0.535

0.350 -0.387** 0.460 -0.210 0.900 -0.110

0.370 -0.513 0.490 -0.176 0.960 0.044

0.380 -0.548 0.500 -0.208

0.400 -0.478 0.520 -0,212

0.410 -0.295 0.540 -0.212

0.430 -0.160 0.550 -0.178

0.440 -0.153 0,580 -0,184

0.460 -0,146 0,600 -0,220

0,470 -0.166 0.610 -0.247

0490 -0,159 0.650 2,193"*

0,500 -0.176 0.700 -0,461

0.520 -0.188 0,750 -0.422

0.530 -0.201 0.820 -0.583

0,550 -0.241 0.890 -0.065

0.560 -0,235 0.900 -0,017

0.580 -0.220 0.960 0.074

0.590 -0.255

0.600 -0.251

0.640 -0.463

0,700 -0.414

0.750 -0.075**

0,820 -0.450

0.870 -0,189

0.930 -0,034

0.960 0.028

Lower Surface

0.020 -0.714 0.020 -0.412 0.020 -0.126 0.020 0.357

0.110 -0.504 0,060 -0.159 0.060 -0.017 0.060 -0.520

0.230 -0.285 0,090 -0.188 0.090 0,480** 0,110 -0.133

0.400 -0.094 0.120 -0.268 0.120 -0.220 0.250 -0.307

0.490 -0.088 0.200 -0.490 0.200 -0.329 0.400 -0.340

0.630 0.834** 0.260 -0.372 0.250 -0.381 0.490 -0.431

0,750 0,055 0400 -0.194 0,400 -0,393 0.580 -0.534

0,850 0.128 0,490 -0. 184 0.490 -0,135 0.650 -0.119

0.900 0,218 0,580 -0.171 0,580 -0,210 0.750 0,107

0.960 0.198 0.640 0.036 0.650 -0.084 0.830 0.263

0.750 0,193 0.750 0.224 0.900 0.315

0.870 0.280 0,890 0.314 0.960 0.280

0,930 0,242 0.930 0.272

0.960 0.206 0.960 0.216"*

CN = 0.107 0.243 0.277 0.260

481
Table H-2. Continued.

Flight 217, Wing sweep = 26 °, Time = 9-22-11-500, MINF = 0.900, Camber = 0/2, ALPT = 4.47, BETA = 0.86, QINF = 665.0,

RNPU = 5.0E+06, CNWP = 0.3201

11= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x./c CP

0.020 -0.056 0.000 0.875 0.000 2.746"* 0.010 -0.588

0.060 -0.290 0.020 -0.313 0.020 -0.331 0.020 -0.710

0.110 -0.252 0.040 -0.246 0.060 - 1.800"* 0.060 -0.567

0.200 -0.359 0.060 -0.432 0.090 -0.557 0.1 l0 -0.624

0.230 -0.336 0.090 -0.429 0.110 -0.556 0.140 -0,659

0.400 -0.433 0.130 -0,436 0.130 -0.520 0.190 - 1.764"*

0.490 -0.360 0.150 -0.424 0.150 -0.511 0.250 -0.672

0.590 -0.160 0.200 -0.388 0.210 -0.530 0.400 -0.600

0.630 -0.193 0.250 -0.512 0.250 -0.563 0.490 -0.415

0.700 -0.162 0,260 -0.509 0.340 -0.634 0.580 -0.360

0.750 -0.210 0.280 -0.519 0.370 -0.650 0.650 -0.409

0.810 -0.199 0.290 -0.515 0.400 -0.618 0.700 -0.382

0.840 -0.186 0.310 -0.485 0.410 0.256** 0.750 -0.439

0.900 -0.064 0.320 -0.501 0.430 -0.627 0.800 -0.558

0.960 0.054 0.340 -0.522 0.440 -0.632 0.830 -0.569

0.350 -0.390** 0.460 -0.627 0.900 -0.071

0.370 -0.510 0.490 -0.503 0.960 0.036

0.380 -0.551 0.500 -0.545

0.400 -0.481 0.520 -0.539

0.410 -0.536 0.540 -0.539

0.430 -0.524 0.550 -0.504

0.440 -0.493 0.580 -0.483

0.460 -0.549 0.600 -0.465

0.470 -0.561 0.610 -0.406

0.490 -0.557 0.650 2.127**

0.500 -0.571 0.700 -0.491

0.520 -0.551 0.750 -0.441

0.530 -0.558 0.820 -0.539

0.550 -0.586 0.890 -0.018

0.560 -0.601 0.900 0.022

0.580 -0.571 0.960 0.087

0.590 -0.600

0.600 -0.605

0.640 -0.547

0.700 -0.204

0.750 -0.091 **

0.820 -0.190

0.870 -0.171

0.930 -0.028

0.960 0.041

Lower Surface

0.020 -0.624 0.020 -0.383 0.020 -0.103 0.020 0.391

0.110 -0.485 0.060 -0.136 0.060 -0.002 0.060 -0.490

0.230 -0.548 0.090 -0.162 0.090 0.472"* 0.110 -0.101

0.400 -0.092 0.120 -0.248 0.120 -0.196 0.250 -0.262

0.490 -0.092 0.200 -0.484 0.200 -0.290 0.400 -0.317

0.630 0.814"* 0.260 -0.373 0.250 -0.372 0.490 -0.413

0.750 0.052 0.400 -0.398 0.400 -0.375 0.580 -0.531

0.850 0.124 0.490 -0.333 0.490 -0.141 0.650 -0.471

0.900 0.209 0.580 -0.115 0.580 -0.541 0.750 0.063

0.960 0.203 0.640 0.052 0.650 -0.105 0.830 0.231

0.750 0.194 0.750 0.223 0.900 0.3 l 8

0.870 0.282 0.890 0.326 0.960 0.276

0.930 0.243 0.930 0.286

0.960 0.213 0.960 0.217"*

CN = 0.115 0.260 0.329 0.288

482
Table H-2, Continued.

Flight 217, Wing sweep = 26 °, Time = 9-22-18-000, MINF = 0.909, Camber = 0/2, ALPT = 4.21, BETA = 0.72, QINF = 674.5,

RNPU = 5.1E+06, CNWP = 0.2999

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.010 0.000 0.868 0.000 2.716"* 0.010 -0.568

0,060 -0.156 0.020 -0.253 0,020 -0,268 0,020 -0,654

0.110 -0.248 0,040 -0.224 0,060 -1.765** 0,060 -0.525

0.200 -0.318 0.060 -0.404 0,090 -0.499 0.110 -0.581

0.230 -0,308 0.090 -0.350 0.110 -0.507 0.140 -0,603

0,400 -0.407 0.130 -0.323 0.130 -0.462 0.190 - 1.730**

0.490 -0.389 0.150 -0,357 0.150 -0.455 0.250 -0.612

0.590 -0.169 0.200 -0.313 0.210 -0.465 0,400 -0.564

0,630 -0.154 0,250 -0.434 0.250 -0.516 0,490 -0.366

0,700 -0.148 0.260 -0.442 0,340 -0.594 0.580 -0.326

0,750 -0.214 0.280 -0.457 0.370 -0.585 0.650 -0.387

0.810 -0.199 0.290 -0.453 0.400 -0,560 0,700 -0.370

0.840 -0.183 0.310 -0,439 0.410 0,262** 0.750 -0.407

0.900 -0,053 0,320 -0.458 0,430 -0.571 0,800 -0.585

0.960 0.081 0.340 -0.491 0.440 -0.526 0.830 -0,525

0.350 -0.374** 0,460 -0.486 0.900 -0.107

0.370 -0.491 0,490 -0,462 0,960 0.035

0.380 -0.521 0,500 -0.503

0.400 -0.488 0.520 -0.518

0.410 -0,527 0,540 -0.523

0.430 -0,490 0,550 -0.477

0.440 -0.481 0.580 -0,402

0,460 -0.531 0,600 -0,364

0.470 -0.525 0.610 -0.323

0.490 -0.532 0.650 2.107**

0.500 -0.550 0.700 -0.449

0,520 -0.522 0,750 -0,430

0.530 -0.520 0.820 -0.516

0.550 -0.563 0,890 -0.016

0.560 -0.547 0.900 0.033

0.580 -0,489 0,960 0,096

0,590 -0.510

0.600 -0.528

0,640 -0.548

0.700 -0.486

0,750 -0.093**

0,820 -0.142

0,870 -0,145

0.930 0.003

0,960 0.054

Lower Surface

0.020 -0,737 0,020 -0,402 0.020 -0.115 0.020 0.367

0.110 -0.492 0,060 -0.132 0,060 -0.015 0.060 -0.502

0.230 -0.556 0,090 -0.170 0.090 0,474** 0.110 -0.122

0,400 -0.077 0.120 -0.257 0.120 -0.212 0,250 -0,374

0.490 -0.049 0.200 -0.540 0,200 -0,344 0,400 -0,290

0.630 0.812"* 0.260 -0.374 0,250 -0,402 0,490 -0.427

0,750 0,080 0.400 -0.431 0,400 -0.380 0.580 -0.542

0.850 0.148 0.490 -0.533 0,490 -0.158 0.650 -0.725

0.900 0.232 0.580 -0.082 0,580 -0.572 0,750 -0.037

0.960 0.207 0.640 0,074 0,650 -0.110 0.830 0.151

0.750 0.214 0.750 0.128 0,900 0,301

0.870 0.269 0,890 0.267 0.960 0.290

0,930 0.270 0,930 0,244

0,960 0.235 0.960 0.223"*

CN = 0.112 0.228 0,252 0.200

483
Table H-2. Continued.

Flight 217, Wing sweep = 26 °, Time = 9-22-20-000, MINF = 0.907, Camber = 0/2, ALPT = 4.06, BETA = 0.92, QINF = 670.8,

RNPU = 5.1E+06, CNWP = 0.3037

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0_020 0.011 0.000 0.877 0.000 2.734** 0.010 -0.555

0.060 -0.167 0.020 -0.206 0.020 -0.255 0.020 -0,645

0.110 -0.260 0.040 -0.217 0.060 - 1.771 ** 0.060 -0.525

0.200 -0.317 0.060 -0.392 0.090 -0.496 0.110 -0.581

0.230 -0.349 0.090 -0.354 0.I 10 -0.499 0.140 -0.612

0.400 -0.408 0.130 -0.313 0. t 30 -0.448 0.190 - 1.735"*

0.490 -0.404 0.150 -0.349 0.150 -0.448 0.250 -0.602

0.590 -0.147 0.200 -0.308 0.210 -0.459 0.400 -0.570

0.630 -0.168 0.250 -0.439 0.250 -0.522 0.490 -0.374

0.700 -0.151 0.260 -0.444 0.340 -0.597 0.580 -0.324

0.750 -0.212 0.280 -0.461 0.370 -0.605 0.650 -0.373

0.810 -0.197 0.290 -0,473 0.400 -0.569 0.700 -0.353

0.840 -0.180 0.310 -0.459 0.410 0.267** 0.750 -0.409

0.900 -0.057 0.320 -0.472 0.430 -0.573 0.800 -0.556

0.960 0.067 0.340 -0.496 0.440 -0.512 0.830 -0.517

0.350 -0.391 ** 0.460 -0.489 0.900 -0.121

0.370 -0.503 0.490 -0.457 0.960 0.029

0.380 -0.529 0.500 -0.515

0.400 -0.515 0.520 -0.514

0.410 -0.519 0.540 -0.519

0.430 -0.504 0.550 -0.483

0.440 -0.495 0.580 -0.394

0.460 -0.527 0.600 -0.329

0.470 -0.537 0.610 -0.309

0.490 -0.530 0.650 0.860**

0.500 -0.541 0.700 -0,443

0.520 -0.541 0.750 -0.414

0.530 -0.529 0.820 -0.506

0.550 -0.556 0.890 -0.020

0.560 -0.525 0.900 0.020

0.580 -0.507 0.960 0.08 l

0.590 -0.523

0.600 -0.510

0.640 -0.539

0.700 -0.392

0.750 -0.099'*

O.820 -0.177

0.870 -0.151

0.930 -0.016

0.960 0.053

Lower Surface

0.020 -0.782 0.020 -0.403 0.020 -0.146 0.020 0.365

0.110 -0.493 0.060 -0.142 0.060 -0.027 0.060 -0.507

0.230 -0.565 0.090 -0.185 0.090 0.480"* 0.110 -0.119

0.400 -0.077 0.120 -0.271 0.120 -0.206 0.250 -0.378

0.490 -0.060 0.200 -0.541 0.200 -0.350 0.400 -0.294

0.630 0.820** 0.260 -0.392 0.250 -0.401 0.490 -0.429

0.750 0.066 0.400 -0.428 0.400 -0.380 0.580 -0.560

0.850 0.136 0.490 -0.531 0.490 -0.155 0.650 -0.723

0.900 0.223 0.580 -0.071 0.580 -0.575 0.750 -0.027

0.960 0.215 0.640 0.072 0.650 -0.107 0.830 0.138

0.750 0.208 0.750 0.119 0.900 0.286

0.870 0.284 0.890 0.256 0.960 0.284

0.930 0.261 0.930 0.258

0.960 0.227 0.960 0.228**

CN = 0,112 0.220 0.249 0.195

484
Table H-2. Continued.

Flight 217, Wing sweep = 26 °, Time = 9-22-27-000, MINF = 0,900, Camber = 0/2, ALPT = 4.42, BETA = 1.03, QINF = 658.1,

RNPU = 5.0E+06, CNWP = 0.3250

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0,020 -0.056 0.000 0.874 0,000 2.794"* 0.010 -0.587

0.060 -0,285 0.020 -0,295 0.020 -0.320 0,020 -0.701

0.110 -0.262 0.040 -0.245 0.060 -1.799** 0.060 -0.566

0.200 -0.345 0.060 -0.433 0.090 -0,564 0.110 -0.630

0,230 -0,326 0.090 -0.415 0.1 ! 0 -0.552 0.140 -0.643

0.400 -0,430 0.130 -0,425 0.130 -0.511 0.190 -1.762**

0,490 -0.350 0.150 -0.418 0.150 -0.498 0.250 -0.666

0.590 -0.158 0,200 -0,382 0.210 -0.526 0.400 -0,593

0.630 -0.189 0.250 -0.511 0,250 -0.561 0.490 -0.409

0,700 -0.160 0,260 -0,505 0.340 -0.636 0.580 -0.348

0.750 -0.219 0.280 -0.508 0.370 -0,646 0.650 -0,410

0.810 -0,204 0,290 -0,505 0.400 -0,577 0.700 -0.387

0.840 -0.190 0.310 -0.478 0,410 0.278** 0,750 -0.437

0,900 -0.067 0.320 -0,490 0.430 -0.616 0.800 -0.576

0.960 0.055 0.340 -0.518 0,440 -0.626 0.830 -0.550

0.350 -0.386'* 0.460 -0.612 0.900 -0.089

0,370 -0,501 0,490 -0,494 0.960 0.045

0.380 -0.544 0.500 -0.539

0.400 -0.522 0,520 -0.537

0.410 -0.535 0.540 -0.541

0.430 -0,528 0,550 -0.507

0.440 -0,503 0,580 -0.475

0.460 -0.544 0,600 -0.443

0.470 -0.561 0.610 -0.379

0,490 -0,552 0.650 0.883'*

0.500 -0,559 0.700 -0.467

0,520 -0,560 0.750 -0.429

0.530 -0.552 0.820 -0.526

0,550 -0.594 0.890 -0.028

0.560 -0.605 0,900 0.014

0.580 -0.567 0.960 0.088

0.590 -0.607

0.600 -0.598

0.640 -0,544

0.700 -0.183

0.750 -0.095**

0.820 -0.194

0.870 -0.176

0.930 -0,017

O,96O 0.039

Lower Surface

0,020 -0.638 0,020 -0.356 0.020 -0,090 0.020 0,393

0.110 -0.481 0.060 -0.130 0.060 -0,009 0.060 -0,498

0.230 -0.561 0.090 -0.170 0.090 0.496"* 0.110 -0.104

0.400 -0.087 0.120 -0.250 0.120 -0.199 0.250 -0.253

0.490 -0.087 0.200 -0.482 0,200 -0.281 0.400 -0.329

0.630 0,842** 0.260 -0.383 0.250 -0,363 0.490 -0.414

0.750 0.056 0,400 -0,407 0.400 -0.387 0,580 -0.551

0,850 0.125 0.490 -0,435 0.490 -0.149 0,650 -0.527

0.900 0.215 0,580 -0.110 0.580 -0.546 0.750 0.052

0.960 0.203 0.640 0,050 0.650 -0.105 0.830 0.225

0,750 0.193 0.750 0.218 0.900 0.312

0.870 0.276 0.890 0.323 0.960 0.279

0,930 0.254 0.930 0.280

0.960 0.212 0.960 0,239**

CN = 0.114 0.244 0.320 0.274

485
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-18-15-500, MINF = 0.930, Camber = 0/2, ALPT = 6.04, BETA = 0.69, QINF = 337.2,

RNPU = 2.5E+06, CNWP = 0.5016

'fl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.162 0,000 0.895 0.000 7.229"* 0.010 -0.555

0.060 -0.420 0.020 -0.371 0.020 -0.504 0.020 -0.680

0.110 -0.464 0.040 -0.448 0.060 -3.503** 0.060 -0.675

0.200 -0.513 0.060 -0.520 0.090 -0.609 0.110 -0.662

0.230 -0.384 0.090 -0.499 0.110 -0.621 0.140 -0.676

0.400 -0.473 0.130 -0.535 0.130 -0.594 0.190 - 1.650**

0.490 -0.495 0.150 -0.549 0.150 -0.604 0.250 -0.732

0.590 -0.526 0.200 -0.488 0.210 -0.603 0.400 -0.587

0.630 -0.485 0.250 -0.605 0.250 -0.616 0.490 -0.557

0.700 -0.518 0.260 -0.574 0.340 -0.713 0.580 -0.425

0.750 -0.256 0.280 -0.613 0.370 -0.723 0.650 -0.476

0.810 -0.189 0.290 -0.609 0.400 -0.631 0.700 -0.458

0.840 -0.160 0.310 -0.602 0.410 - 1.772" * 0.750 -0.513

0.900 0.024 0.320 -0.600 0.430 -0.701 0.800 -0.658

0.960 0.070 0.340 -0.618 0.440 -0.698 0.830 -0.629

0.350 -0.359** 0.460 -0.703 0.900 -0.248

0.370 -0.595 0.490 -0.670 0.960 -0.178

0.380 -0.669 0.500 -0.722

0.400 -0.606 0.520 -0.748

0.410 -0.640 0.540 -0.730

0.430 -0.596 0.550 -0.661

0.440 -0.585 0.580 -0.655

0.460 -0.649 0.600 -0.696

0.470 -0.664 0.610 -0.667

0,490 -0.632 0.650 1.931 **

0.500 -0.646 0.700 -0.658

0.520 -0.641 0.750 -0.684

0.530 -0.634 0.820 -0.609

0.550 -0.719 0.890 -0.147

0.560 -0.654 0.900 -0.126

0.580 -0.655 0.960 -0.099

0.590 -0.682

0.600 -0.676

0.640 -0.699

0.700 -0.748

0.750 -0.110"*

0.820 -0.157

0,870 -0.149

0.930 -0.132

0.960 -0.129

Lower Surface

0.020 -0.269 0.020 -0.073 0.020 0.160 0.020 0.533

0. I 10 -0.323 0.060 0.026 0,060 0.186 0,060 -0.787

0.230 -0.394 0.090 -0.013 0.090 1.058"* 0.110 0.084

0.400 -0.296 0.120 -0.110 0.120 -0.132 0.250 -0.169

0.490 -0.291 0.200 -0.125 0.200 -0.127 0.400 -0.176

0.630 1.903** 0.260 -0.218 0.250 -0.189 0.490 -0.296

0.750 0.017 0.400 -0.301 0.400 -0.270 0.580 -0.407

0.850 0.100 0.490 -0.393 0.490 -0.115 0.650 -0.643

0.900 0.188 0.580 -0.495 0.580 -0.429 0.750 -0.147

0.960 0.176 0.640 -0.191 0.650 -0.111 0.830 0.025

0.750 0.084 0.750 -0.086 0.900 0.162

0.870 0.205 0.890 0.133 0.960 0.248

0.930 0.188 0.930 0.178

0.960 0.130 0.960 - 1.849**

CN = 0.196 0.377 0.454 0.347

486
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-18-24-500, MINF = 0.940, Camber = 0/2, ALPT = 5.73, BETA = 0.51, QINF = 337.1,

RNPU = 2.5E+06, CNWP = 0.4059

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.109 0.000 0.894 0.000 7.266** 0,010 -0,504

0.060 -0.324 0.020 -0,353 0.020 -0.427 0,020 -0,622

0.110 -0.411 0.040 -0.411 0.060 -3.471 ** 0.060 -0.617

0.200 -0.487 0.060 -0.469 0.090 -0.514 0.110 -0.642

0.230 -0.330 0.090 -0.457 0.110 -0.583 0.140 -0.642

0400 -0.471 0.130 -0.510 0.130 -0.531 0.190 -1.617"*

0.490 -0.442 0.150 -0.503 0.150 -0.543 0.250 -0.655

0.590 -0.504 0.200 -0,450 0,210 -0.539 0.400 -0.548

0.630 -0.449 0.250 -0.564 0.250 -0.543 0.490 -0.497

0.700 -0.502 0.260 -0.511 0.340 -0.665 0,580 -0.377

0.750 -0,320 0,280 -0.550 0.370 -0.652 0.650 -0.444

0.810 -0.276 0.290 -0.550 0.400 -0.629 0.700 -0,397

0.840 -0.231 0, 310 -0.561 0.410 - 1.739"* 0.750 -0.472

0.900 0.006 0.320 -0.567 0.430 -0.659 0.800 -0.637

0.960 0.059 0.340 -0.555 0,440 -0.641 0,830 -0.615

0.350 -0.343** 0,460 -0,644 0.900 -0.351

0.370 -0.532 0.490 -0.614 0.960 -0.215

0.380 -0.622 0.500 -0,677

0.400 -0.535 0.520 -0.692

0.410 -0.607 0.540 -0.667

0.430 -0.578 0.550 -0.622

0.440 -0.539 0.580 -0.556

0.460 -0.611 0.600 -0.589

0.470 -0.604 0.610 -0.509

0.490 -0,587 0,650 1.966"*

0.500 -0.557 0.700 -0.626

0.520 -0.563 0.750 -0.643

0.530 -0.582 0.820 -0.603

0.550 -0.636 0.890 -0.158

0.560 -0.609 0.900 -0.143

0.580 -0.581 0.960 -0.094

0.590 -0.649

0.600 -0.640

0.640 -0.634

0.700 -0.704

0.750 -0.143"*

0.820 -0.289

0.870 -0.150

0.930 -0.117

0.960 -0.098

Lower Surface

0.020 -0.206 0,020 -0.090 0.020 0.160 0.020 0.519

0.110 -0,290 0.060 0,022 0.060 0.183 0.060 -0.823

0.230 -0.399 0.090 -0,053 0.090 1.092"* 0.110 0.074

0.400 -0.287 0.120 -0.146 0.120 -0.144 0.250 -0.149

0.490 -0.263 0.200 -0.123 0.200 -0.131 0.400 -0.196

0.630 1.938** 0.260 -0.222 0,250 -0.199 0.490 -0.287

0.750 -0.008 0.400 -0.289 0.400 -0.240 0.580 -0.448

0.850 0.135 0,490 -0.399 0.490 -0.142 0.650 -0.621

0.900 0.180 0.580 -0.461 0.580 -0.395 0.750 -0.210

0.960 0.170 0,640 -0.548 0.650 -0.141 0.830 -0.043

0.750 0.002 0.750 -0.150 0.900 0.127

0.870 0.129 0.890 0.058 0.960 0.204

0.930 0.177 0.930 0.127

0.960 0.139 0.960 -1.816"*

CN = 0.186 0.301 0.385 0.295

487
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = I0-18-30-500, MINF = 0.950, Camber = 0/2, ALPT = 7.03, BETA = 0.34, QINF = 341.I,

RNPU = 2.5E+06, CNWP = 0.3389

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.738 0.000 0.466 0.000 7.194"* 0.010 -0.831

0.060 -0.751 0.020 -0.921 0.020 -0.812 0.020 -0.880

0.110 -0.724 0.040 -0,762 0.060 -3.415 * * 0.060 -0,796

0.200 -0.749 0.060 -0.828 0,090 -0.826 0,110 -0.748

0.230 -0.667 0.090 -0.771 0,110 -0,890 0.140 -0.746

0.400 -0.627 0.130 -0.794 0.130 -0.801 0.190 - 1.584 **

0.490 -0.240 0,150 -0,802 0.150 -0.773 0.250 -0.497

0.590 -0.032 0.200 -0.714 0,210 -0.784 0,400 -0.366

0.630 0.017 0.250 -0.762 0.250 -0.708 0.490 -0,307

0.700 0,048 0.260 -0,746 0.340 -0.536 0.580 -0.346

0.750 -0.038 0.280 -0.784 0,370 -0,512 0.650 -0.385

0.810 -0.055 0.290 -0,762 0.400 -0.429 0.700 -0.412

0.840 -0.001 0.310 -0.747 0.410 - 1.704"* 0.750 -0.467

0.900 0.025 0,320 -0.760 0.430 -0,442 0.800 -0.596

0,960 0.091 0.340 -0.747 0.440 -0.421 0.830 -0.549

0.350 -0.374** 0,460 -0.422 0,900 -0,723

0.370 -0,706 0,490 -0.345 0.960 -0.333

0,380 -0.781 0.500 -0.421

0.400 -0.578 0.520 -0.409

0.410 -0.523 0.540 -0.392

0,430 -0.438 0,550 -0.344

0.440 -0,424 0.580 -0.322

0.460 -0.423 0.600 -0.377

0.470 -0.412 0,610 -0,354

0.490 -0.386 0.650 1.957 **

0.500 -0,402 0.700 -0,510

0,520 -0.385 0,750 -0.549

0.530 -0.380 0,820 -0,589

0,550 -0.416 0.890 -0.141

0.560 -0.408 0.900 -0.052

0,580 -0,381 0.960 -0.041

0.590 -0.432

0.600 -0.404

0.640 -0.473

0,700 -0,494

0.750 -0,008**

0,820 -0.017

0.870 0.002

0.930 0,049

0.960 0.057

Lower Surface

0.020 -0.075 0.020 0.095 0.020 0.216 0.020 0,453

0.110 -0.142 0.060 0.077 0.060 0,175 0.060 -0.763

0.230 -0,150 0.090 -0,016 0.090 1.093"* 0.110 0.113

0.400 -0.145 0.120 -0.036 0.120 -0,100 0.250 -0.077

0,490 -0.081 0.200 -0.087 0,200 -0.064 0.400 -0. t 02

0.630 1.929"* 0,260 -0.150 0.250 -0.108 0.490 -0.227

0.750 0.031 0.400 -0.064 0.400 -0,183 0.580 -0.329

0.850 0. t 22 0.490 -0.121 0,490 -0.022 0.650 -0.412

0.900 0.176 0.580 -0.131 0,580 -0.294 0.750 0,014

0.960 0.210 0,640 0.047 0.650 -0,031 0.830 0.203

0,750 0.162 0.750 0.140 0.900 0.247

0,870 0.184 0.890 0.191 0.960 0.156

0.930 0.162 0.930 0.154

0.960 0.159 0,960 - 1,781 **

CN = 0.272 0.465 0.458 0.390

488
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-18-37-000, MINF = 0.960, Camber = 0/2, ALPT = 6.65, BETA = 0.48, QINF = 344.1,

RNPU = 2.5E+06, CNWP = 0.2727

11= 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.753 0.000 0.407 0.000 7.153"* 0.010 -0.822

0.060 -0.769 0.020 -0.865 0.020 -0.833 0.020 -0.822

0.110 -0.750 0.040 -0.756 0.060 -3.365** 0.060 -0.782

0.200 -0.733 0.060 -0.797 0,090 -0.820 0.110 -0.712

0.230 -0.637 0.090 -0.763 0.110 -0.872 0.140 -0.681

0.400 -0.276 0.130 -0.788 0.130 -0.784 0.190 - 1.549"*

0.490 -0.179 0.150 -0.787 0.150 -0.769 0.250 -0.442

0.590 -0.100 0.200 -0.726 0.210 -0.751 0.400 -0.33 I

0.630 -0.017 0.250 -0.782 0.250 -0.453 0.490 -0.265

0.700 0.052 0.260 -0.727 0.340 -0.375 0.580 -0.288

0.750 -0.001 0.280 -0.753 0.370 -0.405 0.650 -0.367

0.810 0.014 0.290 -0.699 0.400 -0.351 0.700 -0.366

0.840 0.010 0.310 -0.536 0.410 - 1.668 ** 0.750 -0.441

0.900 0.043 0.320 -0.526 0.430 -0.382 0.800 -0.517

0.960 0.105 0.340 -0.420 0.440 -0.374 0.830 -0.508

0.350 -0.249** 0.460 -0.349 0.900 -0.635

0,370 -0.364 0.490 -0.324 0.960 -0.378

0.380 -0.3% 0.500 -0.387

0.400 -0.244 0.520 -0.367

0.410 -0,382 0.540 -0.370

0.430 -0.364 0.550 -0.286

0.440 -0.334 0.580 -0.308

0.460 -0.366 0.600 -0.339

0,470 -0.348 0.610 -0,352

0.490 -0.336 0.650 1.961 **

0.500 -0.332 0.700 -0.4%

0.520 -0.362 0.750 -0.511

0.530 -0.318 0.820 -0.561

0.550 -0.386 0.890 -0.160

0.560 -0.380 0.900 -0.086

0.580 -0.360 0.960 -0.048

0.590 -0.397

0.600 -0.391

0.640 -0.464

0.700 -0.473

0.750 -0.036**

O.82O -0.075

0.870 -0.007

0.930 0.049

0.960 0.060

Lower Surface

0.020 -0.092 0.020 0.014 0.020 0.224 0.020 0.420

0.110 -0.178 0.060 0.017 0.060 0.134 0.060 -0.797

0.230 -0.190 0.090 -0.054 0.090 1.105"* 0.110 0.078

0.400 -0.156 0.120 -0.045 0.120 -0.133 0.250 -0.069

0.490 -0.067 0.200 -0.121 0.200 -0.075 0.400 -0.141

0.630 1.933** 0.260 -0.182 0.250 -0.147 0,490 -0.202

0.750 0.053 0.400 -0.225 0.400 -0.213 0.580 -0.333

0.850 0. 115 0.490 -0.050 0.490 -0.053 0.650 -0.385

0.900 0.166 0.580 -0.093 0.580 -0.384 0.750 -0.062

0.960 0.182 0.640 0.026 0.650 -0.022 0.830 0.124

0.750 0.111 0.750 0.114 0.900 0.166

0.870 0.148 0.890 0.179 0.960 0.097

0.930 0.148 0.930 0.137

0.960 0.123 0.960 - 1.744 **

CN = 0.208 0.386 0.382 0.322

489
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-18-42-000, M1NF = 0.970, Camber = 0/2, ALPT = 7.59, BETA = 0.37, QINF = 347.0,

RNPU = 2.5E+06

= 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x,/c CP x/c CP

0.020 - 1.052 0.000 0.054 0.000 7.110"* 0.010 -0.991

0.060 - 1.011 0.020 - 1.116 0.020 - 1.052 0.020 -0.966

0.110 -0.924 0.040 -0.999 0.060 -3.318"* 0.060 -0.915

0.200 -0.791 0.060 - 1.029 0.090 -0.958 O. 110 -0.698

0.230 -0.519 0.090 -0.960 O. 110 - 1.023 O. 140 -0.534

0.400 -0.222 0.130 -0.952 0.130 -0.917 0.190 -1.518"*

0.490 -0.232 O.150 -0.944 O.150 -0.702 0.250 -0.427

0.590 -0.033 0.200 -0.880 0.210 -0.601 0.400 -0.286

0.630 -0.006 0.250 -0.575 0.250 -0.367 0.490 -0.292

0.700 0.037 0.260 -0.499 0.340 -0.345 0.580 -0.374

0.750 -0.014 0.280 -0.502 0.370 -0.367 0.650 -0.415

0.810 0.013 0.290 -0.460 0.400 -0.335 0.700 -0.385

0.840 0.037 0.310 -0.417 0.410 - 1.637"* 0.750 -0.349

0.900 0.043 0.320 -0.419 0.430 -0.359 0.800 -0.447

0.960 0.079 0.340 -0.352 0.440 -0.330 0.830 -0.396

0.350 -0.198"* 0.460 -0.351 0.900 -0.532

0.370 -0.305 0.490 -0.308 0.960 -0.318

0.380 -0.378 0.500 -0.345

0.400 -0.331 0.520 -0.362

0,410 -0.367 0.540 -0.356

0,430 -0.331 0.550 -0.311

0.440 -0.288 0.580 -0.258

0.460 -0.342 0.600 -0.332

0.470 -0.369 0.610 -0.332

0.490 -0.329 0.650 1.962'*

0.500 -0.367 0.700 -0.435

0,520 -0.392 0.750 -0.491

0.530 -0.362 0.820 -0.427

0.550 -0.433 0.890 -0.179

0.560 -0.406 0.900 -0.129

0.580 -0.375 0.960 -0.072

0.590 -0.407

0.600 -0.381

0.640 -0.444

0.700 -0.466

0.750 -0.018'*

0.820 -0.035

0.870 0.009

0.930 0.064

0.960 0.047

Lower Surface

0.020 0.026 0.020 0.089 0.020 0.252 0.020 0.346

O. 110 -0.049 0.060 0.072 0.060 O. 165 0.060 -0.778

0.230 -0.062 0.090 0.008 0.090 1.113"* O. 110 O. 116

0.400 -0,187 O. 120 0.018 O. 120 -0.075 0.250 -0.037

0.490 -0.147 0.200 -0.057 0.200 -0.082 0.400 -0.080

0.630 1.935"* 0.260 -0.094 0.250 -0.040 0.490 -0.122

0.750 -0.040 0.400 -0.035 0.400 -0.114 0.580 -0.219

0.850 0.074 0.490 -0,054 0.490 -0.016 0.650 -0.195

0.900 O. 141 0.580 -0.056 0.580 -0.183 0.750 -0.119

0.960 O. 140 0.640 0.070 0.650 -0.062 0.830 O.109

0.750 0.090 0.750 O. 1O0 0.900 O.138

0.870 O. 118 0.890 O. 140 0.960 O. 109

0.930 0.096 0.930 O.113

0.960 0.074 0.960 - 1.712"*

490
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-18-52-000, MINF = 0.980, Camber = 0/2, ALPT = 8.09, BETA = 0.45. QINF = 344.1,

RNPU = 2.5E+06

rl = 0.93 0.76 0,59 0.40

Upper Surface

x,/c CP x./c CP x/c CP x/c CP

0,020 -1.027 0.000 -0.158 0,000 7.214"* 0,010 -1.053

0.060 -0,937 0.020 -0.927 0.020 - 1.156 0.020 - 1.053

0.110 -0,723 0.040 -0,743 0.060 -3,303** 0,060 -0,965

0,200 -0,520 0.060 -0.766 0,090 -0.808 0.110 -0.566

0,230 -0.497 0.090 -0.735 0.110 -0.883 0.140 -0.398

0.400 -0.289 0.130 -0.714 0.130 -0.800 0.190 - 1.487" *

0.490 -0.231 0.150 -0.724 0.150 -0.754 0,250 -0,309

0.590 -0.174 0.200 -0.706 0.210 -0,685 0.400 -0.319

0.630 -0.106 0.250 -0.678 0.250 -0.306 0.490 -0.355

0.700 -0.042 0,260 -0.609 0,340 -0.268 0,580 -0.228

0.750 O014 0.280 -0.669 0.370 -0,296 0.650 -0,268

0.810 0.023 0.290 -0.614 0.400 -0.260 0.700 -0.252

0,840 0,044 0.310 -0.589 0.410 - 1.607"* 0,750 -0.262

0,900 0.067 0.320 -0.591 0,430 -0.290 0.800 -0,323

0.960 0.099 0.340 -0.587 0.440 -0.294 0,830 -0.371

0,350 -0.293** 0,460 -0.307 0,900 -0.153

0.370 -0,466 0.490 -0,257 0.960 -0.046

0.380 -0.480 0,500 -0.325

0.400 -0,349 0.520 -0.320

0.410 -0.357 0.540 -0,305

0,430 -0.281 0,550 -0.268

0,440 -0.218 0.580 -0,263

0,460 -0.257 0.600 -0.345

0.470 -0.274 0.610 -0.341

0,490 -0,268 0,650 2,022**

0.500 -0,252 0,700 -0,374

0,520 -0,280 0.750 -0.450

0,530 -0,306 0,820 -0,407

0,550 -0.321 0.890 -0,255

0,560 -0,338 0.900 -0.203

0,580 -0.314 0.960 -0.109

0,590 -0,358

0,600 -0.345

0.640 -0.331

0.700 -0.300

0.750 -0,027**

0,820 -0.022

0.870 0.009

0.930 0.042

0,960 0,048

LowerSurf_e

0,020 0.164 0.020 0,075 0.020 0.236 0.020 0,295

0.110 0.016 0,060 0,079 0.060 0.179 0.060 -0,797

0,230 0,019 0.090 0,005 0.090 1.166"* 0.110 0.118

0,400 -0.107 0. 120 0.041 0.120 -0.056 0.250 -0.039

0,490 -0.099 0.200 -0.022 0.200 -0.041 0.400 -0.OOl

0.630 1.995"* 0,260 0.000 0.250 -0,025 0,490 -0.051

0,750 -0.078 0.400 0.001 0.400 -0.109 0.580 -0,090

0.850 0.021 0,490 -0,023 0.490 -0,044 0.650 -0.148

0.900 0.095 0.580 -0,008 0.580 -0.073 0.750 -0.111

0.960 0.109 0,640 0.098 0.650 -0.059 0.830 0.043

0.750 0.086 0.750 0.076 0.900 0.103

0,870 0.108 0.890 0,129 0.960 -0.052

0.930 0,078 0,930 0.114

0,960 0,066 0,960 - 1,682"*

491
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-19-17-500, MINF = 0.990, Camber = 0/2, ALPT -- 7.60, BETA = 0.34, QINF = 339.2,

RNPU = 2.4E+06

TI= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.969 0.000 -0.153 0.000 7.369* * 0.010 - 1.007

0.060 -0.714 0.020 - 1.037 0.020 - 1.084 0.020 - 1.037

0.110 -0.524 0.040 -0.782 0.060 -3.300** 0.060 -0.886

0.200 -0.530 0.060 -0.756 0.090 -0.774 O. 110 -0.569

0.230 -0.510 0.090 -0.689 O.110 -0.837 O. 140 -0.376

0.400 -0.405 O. 130 -0.671 O. 130 -0.734 O. 190 - 1.459"*

0.490 -0.340 O. 150 -0.681 O. 150 -0.708 0.250 -0.289

0.590 -0.307 0.200 -0.681 0.210 -0.596 0.400 -0.274

0.630 -0.208 0.250 -0.667 0.250 -0.232 0.490 -0.344

0.700 -0.115 0.260 -0.569 0.340 -0.284 0.580 -0.265

0.750 -0.054 0.280 -0.600 0.370 -0.304 0.650 -0.260

O.810 -0.061 0.290 -0.561 0.400 -0.289 0.700 -0.250

0.840 -0.015 0.310 -0.532 0.410 - 1.580** 0.750 -0.266

0.900 -0.017 0.320 -0.529 0.430 -0.306 0.800 -0.321

0.960 0.038 0.340 -0.450 0.440 -0.288 0.830 -0.327

0.350 -0.249** 0.460 -0.304 0.900 -0.137

0.370 -0.352 0,490 -0.267 0.960 -0.077

0.380 -0.366 0.500 -0.318

0.400 -0.263 0.520 -0.307

0.410 -0.303 0.540 -0.304

0.430 -0.287 0.550 -0.250

0.440 -0.219 0.580 -0.270

0.460 -0.283 0.600 -0.317

0.470 -0.297 0.610 -0.317

0.490 -0.287 0.650 2.102 **

0.500 -0.290 0.700 -0.346

0.520 -0.316 0.750 -0.466

0.530 -0.288 0.820 -0.434

0.550 -0.352 0.890 -0.280

0.560 -0.350 0.900 -0.219

0.580 -0.320 0.960 -0.148

0.590 -0.348

0.600 -0.375

0.640 -0.360

0.700 -0.398

0.750 -0.052**

0.820 -0.104

0.870 -0.080

0.930 -0.050

0.960 -0.041

Lower Surface

0.020 0.060 0.020 O. 101 0.020 0.240 0.020 0.275

O. 110 -0.021 0.060 0.062 0.060 O. 182 0.060 -0.820

0.230 -0.005 0.090 -0.009 0.090 1.234"* O. 110 O. 197

0.400 -0.130 O.120 0.007 O.120 -0.084 0.250 -0.021

0.490 -0.079 0.200 -0.04 1 0.200 -0.042 0.400 -0.046

0.630 2.074"* 0.260 -0.102 0.250 0.000 0.490 -0.057

0.750 -0.141 0.400 -0.031 0.400 -0.118 0.580 -0.087

0.850 -0.068 0.490 -0.047 0.490 -0.047 0.650 -0.159

0.900 -0.008 0.580 -0.028 0.580 -0.093 0.750 -0.125

0.960 0.017 0.640 0.087 0.650 -0,072 0.830 0.040

0.750 0,073 0.750 0.061 0.900 O. 114

0.870 0.066 0.890 0,090 0.960 -0.039

0.930 0.032 0.930 0.090

0.960 0.006 0.960 - 1.657"*

492
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-19-20-500, MINF = 1.000, Camber = 0/2, ALPT = 8.73, BETA = 0.34, QINF = 348.6,

RNPU = 2.5E+06

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.073 0.000 -0.188 0.000 7.16 l ** 0.010 - 1.038

0.060 -0.980 0.020 -0.767 0.020 - 1.107 0.020 - 1.073

0.110 -0.654 0.040 -0.703 0.060 -3.222** 0.060 -0.944

0,200 -0.562 0.060 -0.761 0.090 -0.844 0.110 -0.591

0.230 -0.593 0.090 -0,775 0.110 -0.907 0.140 -0.384

0.400 -0.367 0.130 -0,783 0.130 -0.823 0.190 - 1.430"*

0.490 -0.339 0.150 -0.794 0.150 -0.811 0,250 -0.333

0.590 -0.411 0.200 -0.785 0,210 -0,768 0.400 -0.337

0.630 -0.337 0.250 -0.733 0.250 -0.532 0.490 -0.418

0.700 -0.261 0.260 -0.682 0.340 -0.237 0.580 -0.280

0.750 -0.149 0.280 -0.707 0.370 -0.302 0.650 -0.271

0.810 -0.163 0.290 -0.692 0.400 -0.267 0.700 -0.256

0840 -0.142 0.310 -0.663 0.410 - 1.548"* 0.750 -0.239

0.900 -0.067 0.320 -0.667 0.430 -0.297 0.800 -0.286

0.960 -0.034 0.340 -0.659 0.440 -0.279 0.830 -0.344

0.350 -0.329** 0,460 -0,306 0.900 -0.107

0.370 -0.603 0.490 -0.271 0.960 -0.086

0.380 -0.650 0.500 -0.311

0.400 -0.541 0.520 -0.320

0.410 -0.568 0.540 -0.317

0.430 -0.469 0.550 -0,269

0.440 -0.393 0.580 -0.285

0.460 -0.397 0,600 -0.308

0.470 -0.370 0.610 -0.329

0.490 -0.261 0.650 2.035" '_

0.500 -0.245 0.700 -0.386

0.520 -0.260 0.750 -0.477

0,530 -0.254 0.820 -0.448

0.550 -0.296 0.890 -0.348

0.560 -0.300 0.900 -0.292

0.580 -0.320 0.960 -0.193

0.590 -0.299

0.600 -0.345

0.640 -0.357

0,700 -0.360

0.750 -0.043**

0.820 -0.107

0.870 -0.080

0.930 -0.057

0.960 -0.051

Lower Surface

0.020 0.081 0.020 0.175 0.020 0.288 0.020 0.317

O. 110 0.023 0,060 0.107 0.060 O. 195 0.060 -0.747

0.230 0.025 0.090 0.037 0.090 1.190'* 0.110 0.188

0.400 -0,103 O, 120 0.058 O. 120 -0.028 0.250 0.022

0.490 -0.127 0.200 0.018 0.200 0.002 0,400 0.013

0.630 2.008"* 0.260 0.015 0.250 0.027 0.490 -0.019

0.750 -0.156 0.400 -0.012 0.400 -0.099 0.580 -0.061

0.850 -0.104 0.490 -0.005 0,490 -0.056 0.650 -0.140

0.900 -0.054 0.580 -0.009 0.580 -0.026 0.750 -0.1 O0

0.960 -0.034 0.640 0.080 0.650 -0.057 0.830 0.079

0,750 0.085 0.750 0.096 0.900 O. 107

0.870 0.068 0.890 0.129 0,960 -0.032

0.930 0.033 0.930 0.084

0.960 -0.005 0.960 - 1.623 **

493
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-19-25-500, MINF = 1.006, Camber = 0/2, ALPT = 8.44, BETA = 0.43, QINF = 359.4,

RNPU = 2.6E+06, CNWP = 0.3436

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.828 0.000 0.310 0.000 6.919"* 0.010 -0.839

0.060 -0.823 0.020 -0.920 0.020 -0.862 0.020 -0.880

0.110 -0.772 0.040 -0.817 0.060 -3.150** 0.060 -0.836

0.200 -0.779 0.060 -0.854 0.090 -0.825 0.110 -0.740

0.230 -0.684 0.090 -0.806 0.110 -0.907 0.140 -0.676

0.400 -0.666 0.130 -0.798 0.130 -0.837 0.190 - 1.412 **

0.490 -0.302 0.150 -0.808 0.150 -0.806 0.250 -0.411

0.590 -0.218 0.200 -0.754 0.210 -0.806 0.400 -0.317

0.630 -0.219 0.250 -0.805 0.250 -0.754 0.490 -0.234

0.700 -0.220 0.260 -0.758 0.340 -0.436 0.580 -0.276

0.750 -0.365 0.280 -0.796 0.370 -0.398 0.650 -0.404

0.810 -0.346 0.290 -0.753 0.400 -0.331 0.700 -0.427

0.840 -0.347 0.310 -0.739 0.410 -1.527"* 0.750 -0.423

0.900 -0.260 0.320 -0.745 0.430 -0.335 0.800 -0.384

0.960 -0.083 0.340 -0.765 0.440 -0.327 0.830 -0.522

0.350 -0.327** 0.460 -0.312 0.900 -0.568

0.370 -0.582 0.490 -0.268 0.960 -0.507

0.380 -0.543 0.500 -0.319

0.400 -0.455 0.520 -0.302

0.410 -0.455 0.540 -0.307

0.430 -0.417 0.550 -0.276

0.440 -0.356 0.580 -0.263

0.460 -0.385 0.600 -0.332

0.470 -0.368 0.610 -0.332

0.490 -0.336 0.650 1.948 **

0.500 -0.333 0.700 -0.390

0.520 -0.343 0.750 -0.439

0.530 -0.314 0.820 -0.480

0.550 -0.352 0.890 -0.269

0.560 -0.335 0.900 -0.210

0.580 -0.315 0.960 -0.148

0.590 -0.319

0.600 -0.332

0.640 -0.367

0.700 -0.411

0.750 -0.038**

0.820 -0.369

0.870 -0.352

0.930 -0.182

0.960 -0.151

Lower Surface

0.020 0.107 0.020 0.282 0.020 0.370 0.020 0.524

O. 110 -0.033 0.060 0.177 0.060 0.290 0.060 -0.666

0.230 -0.076 0.090 0.108 0.090 1.129** 0.110 0.245

0.400 -0.132 0.120 0.102 0.120 0.008 0.250 0.066

0.490 -0.109 0.200 0.026 0.200 0.007 0.400 0.007

0.630 1.922** 0.260 -0.049 0.250 0.022 0.490 -0.076

0.750 -0.135 0.400 -0.105 0.400 -0.099 0.580 -0.219

0.850 -0.079 0.490 -0.020 0.490 -0.031 0.650 -0.221

0.900 0.000 0.580 -0.030 0.580 -0.247 0.750 -0.002

0.960 -0.005 0.640 0.051 0.650 -0.048 0.830 0.224

0.750 0.095 0.750 0.154 0.900 0.237

0.870 0.112 0.890 0.183 0.960 0.160

0.930 0.041 0.930 0.133

0.960 -0.017 0.960 - 1.599"*

CN = 0.365 0.525 0.473 0.436

494
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-20-12-000, MINF = 1.050, Camber = 0/2, ALPT = 6.76, BETA = 0.45, QINF = 410.3,

RNPU = 2.9E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.890 0.000 0.047 0.000 6.002"* 0.010 -0.818

0.060 -0.595 0.020 -0.945 0.020 -0.890 0.020 -0.828

0.110 -0.543 0.040 -0.839 0.060 -2.818 ** 0.060 -0.642

0.200 -0.425 0.060 -0.643 0.090 -0.541 0.110 -0.406

0.230 -0.304 0.090 -0.557 0,110 -0,602 0.140 -0.281

0.400 -0.180 0.130 -0.536 0.130 -0.522 0.190 - 1.296 **

0.490 -0.180 0.150 -0.524 0.150 -0.425 0.250 -0.184

0.590 -0.224 0.200 -0.472 0.210 -0.275 0.400 -0.176

0.630 -0.218 0.250 -0.288 0.250 -0.147 0,490 -0.246

0,700 -0.200 0.260 -0.227 0.340 -0.201 0.580 -0.139

0.750 -0.125 0.280 -0,231 0.370 -0.230 0,650 -0.170

0.810 -0.116 0.290 -0.222 0.400 -0.221 0.700 -0.157

0.840 -0.118 0,310 -0.210 0.410 -1.396** 0.750 -0.201

0.900 -0.075 0.320 -0.220 0,430 -0.214 0.800 -0.282

0.960 -0,007 0.340 -0.229 0.440 -0.197 0.830 -0.249

0.350 -0.125"* 0.460 -0.210 0.900 -0.376

0.370 -0.201 0.490 -0.159 0.960 -0.010

0.380 -0.244 0.500 -0.218

0.400 -0.175 0.520 -0.204

0.410 -0.235 0.540 -0.201

0.430 -0,229 0.550 -0.195

0.440 -0.165 0.580 -0.191

0.460 -0.221 0.600 -0.238

0.470 -0.234 0.610 -0.212

0.490 -0.213 0.650 1.648"*

0.500 -0.230 0.700 -0.263

0.520 -0.189 0.750 -0.335

0.530 -0.248 0.820 -0.370

0.550 -0,273 0,890 -0.216

0.560 -0.253 0.900 -0.129

0.580 -0.214 0,960 -0.077

0.590 -0.255

0,600 -0.271

0.640 -0.277

0.700 -0.329

0.750 0.004**

0.820 -0.099

O.87O -O.O59

0.930 -0.013

0.960 -0.005

Lower Surface

0.020 0.013 0.020 0.177 0,020 0.243 0.020 0.305

0. | 10 -0.035 0.060 0.107 0.060 0.180 0.060 -0.644

0.230 0,043 0.090 0.059 0.090 0.930"* 0.110 0.109

0.400 -0.07 l 0.120 0.098 0.120 -0.031 0.250 -0.004

0.490 -0.021 0.200 0.024 0.200 0.005 0.400 0.002

0.630 1.408"* 0.260 -0.050 0.250 -0.006 0.490 -0.025

0.750 -0.097 0,400 -0.121 0.400 -0.053 0.580 -0.119

0.850 -0.037 0.490 -0.022 0.490 -0.015 0.650 -0.103

0.900 0,016 0.580 -0.006 0.580 -0.186 0,750 -0.059

0.960 0.022 0.640 0.093 0.650 -0.036 0.830 0.084

0.750 0.135 0,750 0.088 0.900 0.160

0_870 0.120 0.890 0,133 0.960 0.003

0.930 0.093 0.930 0.1 04

0.960 0.063 0.960 - 1.459"*

495
Table H-2. Continued.

Flight 218, Wing sweep = 45", Time = 10-20-23-500, MINF = 1.100, Camber = 0/2, ALPT = 7.28, BETA = 0.14, QINF = 465.0,

RNPU = 3.2E+06

"q= 0,93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0,020 -0.854 0,000 0,032 0.000 5.258** 0.010 -0.787

0.060 -0.533 0.020 -0.897 0.020 -0.844 0.020 -0,799

0.110 -0.481 0,040 -0.614 0.060 -2,525"* 0.060 -0.689

0,200 -0,442 0.060 -0,589 0,090 -0,540 0.110 -0,449

0.230 -0,389 0,090 -0.544 0.110 -0.597 0.140 -0.319

0.400 -0.238 0.130 -0.521 0,130 -0,542 0.190 -1.181"*

0.490 -0.206 0.150 -0.519 0.150 -0.528 0.250 -0.177

0,590 -0.209 0,200 -0,498 0.210 -0,445 0,400 -0,207

0,630 -0.189 0.250 -0,428 0,250 -0.132 0,490 -0.239

0.700 -0.176 0.260 -0,360 0.340 -0.146 0.580 -0.097

0.750 -0.114 0,280 -0,355 0.370 -0.190 0.650 -0.151

0.810 -0.122 0.290 -0.307 0.400 -0.154 0.700 -0.163

0.840 -0.098 0.310 -0.267 0.410 - 1,270"* 0.750 -0.156

0.900 -0.060 0.320 -0.282 0.430 -0.204 0.800 -0.199

0,960 -0,044 0,340 -0,238 0.440 -0.171 0.830 -0.226

0.350 -0.125"* 0.460 -0.188 0.900 -0,065

0.370 -0.196 0,490 -0.137 0.960 -0.007

0,380 -0.224 0.500 -0,198

0.400 -0.156 0.520 -0.193

0.410 -0,202 0.540 -0.193

0,430 -0.178 0,550 -0.168

0.440 -0.137 0.580 -0.125

0.460 -0, | 89 0.600 -0.201

0.470 -0.204 0.610 -0.211

0.490 -0.177 0.650 1.416'*

0.500 -0.198 0,700 -0.236

0.520 -0.198 0.750 -0.309

0.530 -0.197 0.820 -0,347

0.550 -0.231 0.890 -0.255

0,560 -0.225 0,900 -0,203

0.580 -0.213 0.960 -0,090

0.590 -0,241

0,600 -0.241

0.640 -0.259

0,700 -0.288

0.750 0.000"*

0,820 -0,077

0.870 -0,049

0,930 -0.008

0.960 -0,007

Lower Surface

0,020 0.053 0,020 0.204 0.020 0.248 0.020 0,325

0.110 0,008 0.060 0.124 0,060 0.191 0.060 -0.565

0,230 -0.015 0.090 0.032 0.090 0.782** 0.110 0.160

0,400 -0,038 0.120 0,066 0.120 -0.022 0.250 -0,003

0.490 -0.049 0.200 0.099 0,200 0.016 0.400 0.004

0.630 1.204"* 0.260 -0,004 0,250 0,038 0.490 -0.018

0.750 -0,098 0.400 -0.077 0.400 -0.042 0,580 -0,065

0.850 -0.032 0.490 -0.028 0.490 0.001 0.650 -0.078

0.900 0,016 0.580 0,000 0,580 -0.142 0,750 -0.037

0,960 0.012 0.640 0.109 0.650 -0,013 0.830 0.062

0.750 0.144 0.750 0.099 0.900 0.124

0.870 0.128 0.890 0.129 0.960 0.001

0.930 0.101 0,930 0.118

0.960 0.071 0,960 - 1.326"*

496
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-20-39-000, MINF = 1.151, Camber = 0/2. ALPT = 5.88, BETA = 0.28, QINF = 523.0,

RNPU = 3.5E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.669 0.000 0.122 0.000 4.647"* 0.010 -0.641

0.060 -0.644 0.020 -0.752 0.020 -0.692 0.020 -0.647

0.110 -0.381 0.040 -0.658 0.060 -2.273** 0.060 -0.561

0.200 -0.254 0.060 -0.676 0.090 -0.637 0.110 -0.419

0.230 -0.154 0.090 -0.622 0.110 -0.673 0.140 -0.318

0.400 -0.106 0.130 -0.389 0.130 -0.488 0.190 - 1.078" *

0.490 -0.127 0.150 -0.391 0.150 -0.374 0.250 -0.161

0.590 -0.170 0.200 -0.365 0.210 -0.266 0.400 -0.123

0.630 -0.176 0.250 -0.174 0.250 -0.093 0.490 -0.146

0.700 -0.176 0.260 -0.116 0.340 -0.132 0.580 -0.082

0.750 -0.237 0.280 -0.153 0.370 -0.140 0.650 -0.13 I

0.810 -0.231 0.290 -0.148 0.400 -0.144 0.700 -0.120

0.840 -0.227 0.310 -0.145 0.410 -1.157"* 0.750 -0.146

0.900 -0.111 0.320 -0.161 0.430 -0.154 0.800 -0.162

0.960 -0.071 0.340 -0.153 0.440 -0. 136 0.830 -0.184

0.350 -0.085 ** 0.460 -0.151 0.900 -0.056

0.370 -0.143 0.490 -0.125 0.960 -0.040

0.380 -0.169 0.500 -0.156

0.400 -0.115 0.520 -0.152

0.410 -0.150 0.540 -0.136

0.430 -0.141 0.550 -0.113

0.440 -0.119 0.580 -0.121

0.460 -0.137 0.600 -0.157

0.470 -0.160 0.610 -0.1 64

0.490 -0.147 0.650 1.231 **

0.500 -0.158 0.700 -0.215

0.520 -0.156 0.750 -0.259

0.530 -0.167 0.820 -0.285

0.550 -0.199 0.890 -0.260

0.560 -0.191 0.900 -0.163

0.580 -0,174 0.960 -0.074

0.590 -0.203

0.600 -0.200

0.640 -0,218

0.700 -0.248

0.750 -0.020**

0.820 -0.149

0.870 -0.080

0.930 -0.012

0.960 -0.005

Lower Surface

0.020 0.022 0.020 0.104 0.020 0.165 0.020 0.311

0.110 -0.030 0.060 0.080 0.060 0.150 0.060 -0.485

0.230 -0.033 0.090 -0.018 0.090 0.668"* 0.110 0.105

0.400 -0.192 0.120 0.018 0.120 -0.066 0.250 -0.026

0.490 -0.046 0.200 0.029 0.200 -0.048 0.400 -0.041

0.630 1.043"* 0.260 -0.042 0.250 -0.018 0.490 -0.075

0.750 -0.071 0.400 -0.065 0.400 -0.054 0.580 -0.102

0.850 -0.04 1 0.490 -0.154 0.490 -0.033 0.650 -0.115

0.900 0.001 0.580 -0.118 0.580 -0.146 0.750 -0.052

0.960 -0.002 0.640 0.052 0.650 -0.033 0.830 0.010

0.750 0.108 0.750 0.085 0.900 0.083

0.870 0.091 0. 890 0.107 0.960 -0.022

0.930 0.085 0.930 0.094

0.960 0.056 0.960 - 1.207"*

497
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-20-53-500, MINF = 1.200, Camber = 0/2, ALPT = 7.09, BETA = 0.19, QINF = 585.5,

RNPU = 3.8E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0,671 0.000 0.112 0.000 4.122"* 0.010 -0.624

0.060 -0.637 0.020 -0.734 0.020 -0.677 0.020 -0.663

0.110 -0.618 0.040 -0.645 0.060 -2.059 ** 0.060 -0.601

0.200 -0.560 0.060 -0.679 0.090 -0.629 0.110 -0.518

0.230 -0.340 0.090 -0.616 0.110 -0.673 0.140 -0.389

0.400 -0.164 0.130 -0.619 0.130 -0,617 0.190 -0.992**

0.490 -0.107 0.150 -0.607 0.150 -0.561 0.250 -0.226

0.590 -0.114 0.200 -0,571 0.210 -0.455 0.400 -0.182

0.630 -0.124 0.250 -0.353 0.250 -0.279 0.490 -0.240

0,700 -0.132 0.260 -0.324 0.340 -0.134 0.580 -0,082

0.750 -0.226 0.280 -0.331 0.370 -0.160 0,650 -0,131

0.810 -0.199 0.290 -0.327 0.400 -0.136 0.700 -0.118

0.840 -0.225 0.310 -0.304 0.410 -1.062"* 0.750 -0.127

0.900 -0,088 0.320 -0.306 0.430 -0.135 0.800 -0.170

0.960 -0.034 0.340 -0.277 0.440 -0.142 0.830 -0.187

0.350 -0.145"* 0,460 -0.155 0.900 -0.067

0.370 -0.203 0.490 -0.126 0.960 -0.029

0,380 -0.204 0.500 -0.167

0.400 -0.134 0.520 -0,161

0.410 -0.157 0.540 -0.160

0.430 -0.130 0.550 -0.123

0.440 -0.103 0.580 -0.138

0.460 -0.122 0.600 -0.153

0.470 -0.143 0,610 -0.156

0.490 -0.127 0.650 1.071 **

0.500 -0.146 0.700 -0,205

0.520 -0.155 0.750 -0.265

0.530 -0.156 0.820 -0.301

0.550 -0.186 0.890 -0.336

0.560 -0.184 0.900 -0.239

0.580 -0.173 0.960 -0.113

0.590 -0.192

0.600 -0.202

0,640 -0.222

0.700 -0.242

0.750 -0.023**

0.820 -0.125

0.870 -0.051

0.930 -0.032

0.960 -0.024

Lower Surface

0.020 0.068 0.020 0.141 0.020 0.199 0.020 0.328

0.110 0.014 0.060 0.124 0.060 0,185 0.060 -0.384

0.230 0.017 0.090 0.028 0.090 0.568** 0.110 0.151

0.400 -0.139 0.120 0.058 0.120 -0.017 0.250 0,020

0.490 -0.053 0.200 0.058 0.200 -0.005 0.400 -0.003

0.630 0.902"* 0.260 0.002 0.250 0.024 0.490 -0.018

0.750 -0.055 0.400 -0,048 0.400 -0.021 0.580 -0.070

0.850 -0.023 0,490 -0.100 0.490 -0.020 0,650 -0.057

0.900 0.006 0.580 -0,188 0.580 -0.105 0.750 -0.026

0.960 0.013 0.640 0.066 0.650 -0.026 0.830 0.010

0.750 0.119 0.750 0.092 0.900 0.060

0. 870 0.103 0.890 0.126 0.960 -0.006

0.930 0.074 0.930 0.092

0.960 0,046 0.960 - 1.107" *

498
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-20-56-500, M1NF = 1.205, Camber = 0/2, ALPT = 6.35, BETA = 0.19, QINF = 589.8,

RNPU = 3,9E+06

1] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.611 0.000 0.141 0.000 4.093" * 0.010 -0.594

0.060 -0.600 0.020 -0.695 0.020 -0.651 0.020 -0.618

0.110 -0.591 0,040 -0.604 0.060 -2.042 * * 0.060 -0,542

0.200 -0.456 0.060 -0.628 0.090 -0.583 0.110 -0.466

0.230 -0.271 0.090 -0.578 0.110 -0.619 0.140 -0.345

0.400 -0.092 0.130 -0,577 0.130 -0.572 0.190 -0.983"*

0.490 -0.061 0.150 -0.571 0.150 -0.549 0.250 -0.230

0.590 -0.117 0.200 -0.530 0.210 -0.442 0.400 -0.147

0.630 -0.119 0.250 -0.305 0.250 -0.201 0.490 -0.177

0.700 -0.134 0.260 -0.269 0.340 -0.134 0.580 -0.070

0.750 -0,228 0.280 -0.272 0.370 -0.152 0.650 -0.120

0.810 -0.229 0.290 -0.241 0.400 -0.129 0.700 -0.1 04

0.840 -0.229 0.310 -0.208 0.410 - 1.053"* 0.750 -0.120

0.900 -0.098 0.320 -0.206 0.430 -0.138 0,800 -0.173

0.960 -0.061 0.340 -0.168 0.440 -0.125 0.830 -0.188

0.350 -0.089** 0.460 -0.130 0.900 -0.065

0.370 -0.129 0.490 -0.1 04 0.960 -0.036

0.380 -0.140 0,500 -0.147

0.400 °0.103 0.520 -0.1 44

0.410 -0.141 0.540 -0.133

0.430 -0.120 0,550 -0.114

0.440 -0.115 0.580 -0.129

0.460 -0.131 0.600 -0.148

0.470 -0.141 0.610 -0.152

0.490 -0.131 0.650 1.064"*

0.500 -0.139 0.700 -0.198

0.520 -0.139 0.750 -0.242

0.530 -0.1 44 0.820 -0.277

0.550 -0.171 0.890 -0.307

0.560 -0.169 0.900 -0.203

0.580 -0.160 0,960 -0.117

0.590 -0.184

0.600 -0.188

0.640 -0.202

0.700 -0.226

0.750 -0.032**

0.820 -0.145

0.870 -0.082

0.930 -0.027

0.960 -0.010

Lower Surface

0,020 0.064 0.020 0.115 0.020 0.165 0.020 0.268

0.110 -0.009 0.060 0.098 0.060 0.164 0.060 -0.424

0,230 -0.017 0,090 0.017 0.090 0.565** 0A 10 0.151

0.400 -0.1 44 0.120 0.000 0.120 -0.054 0,250 0.026

0.490 -0.160 0.200 0,028 0.200 -0.021 0.400 -0.023

0,630 0.897"* 0.260 -0.013 0.250 -0.004 0.490 -0,058

0.750 -0.049 0.400 -0.066 0.400 -0.048 0.580 -0.096

0.850 -0.030 0.490 -0.103 0.490 -0.011 0.650 -0.077

0.900 0.006 0.580 -0.197 0.580 -0.135 0.750 -0.041

0.960 0.010 0.640 0.046 0.650 -0.024 0.830 -0.003

0.750 0.1 04 0.750 0.089 0.900 0.059

0.870 0.103 0.890 0.108 0.960 -0.028

0.930 0.074 0.930 0.074

0,960 0,044 0,960 - 1.097"*

499
Table H-2. Continued.

Flight 218, Wing sweep = 45 °, Time = 10-21-7-500, MINF = 1.233, Camber = 0/2, ALPT = 4.63, BETA = 0.28, QINF = 615.3,

RNPU -- 4.0E+06

I] -- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.495 0.000 0.222 0.000 3.927"* 0.010 -0.471

0.060 -0.444 0.020 -0.548 0.020 -0.505 0.020 -0.481

O.110 -0.437 0.040 -0.448 0.060 - 1.955 ** 0.060 -0.421

0.200 -0.159 0.060 -0.507 0.090 -0.458 O. 110 -0.358

0.230 -0.042 0.090 -0.453 O.110 -0.482 O. 140 -0.269

0.400 -0.045 O.130 -0.454 O.130 -0.399 O. 190 -0.940"*

0.490 -0.046 O. 150 -0.431 O,150 -0.289 0.250 -0.177

0.590 -0.086 0.200 -0.350 0.210 -0.286 0.400 -0.094

0.630 -0.099 0.250 -0.135 0.250 -0.130 0.490 -0.070

0.700 -0.106 0.260 -0.098 0.340 -0.096 0.580 -0.055

0.750 -0.199 0.280 -0.105 0.370 -0.094 0.650 -0.091

0.810 -0.199 0.290 -0.103 0.400 -0.071 0.700 -0.078

0.840 -0.196 0.310 -0.088 0.410 - 1.006 ** 0.750 -0.094

0.900 -0.107 0.320 -0.096 0.430 -0.080 0.800 -0.113

0.960 -0.042 0.340 -0.086 0.440 -0.083 0.830 -0.154

0.350 -0.066** 0.460 -0.085 0.900 -0.033

0.370 -0.083 0.490 -0.094 0.960 -0.026

0.380 -0.1 04 0.500 -0.088

0.400 -0.047 0.520 -0.092

0.410 -0.096 0.540 -0.092

0.430 -0.080 0.550 -0.060

0.440 -0.049 0.580 -0.052

0.460 -0.076 0.600 -0.087

0.470 -0.087 0.610 -0.099

0.490 -0.082 0.650 1.023**

0.500 -0.105 0.700 -0.139

0.520 -0.098 0.750 -0.183

0.530 -0.092 0.820 -0.208

0.550 -0.121 0.890 -0.242

0.560 -0.109 0.900 -0.165

0.580 -0.111 0.960 -0.057

0.590 -0.133

0.600 -0.132

0.640 -0.148

0.700 -0.167

0.750 -0.016"*

0.820 -0.120

0.870 -0.135

0.930 -0.006

0.960 0.025

Lower Surface

0.020 0.003 0.020 0.089 0.020 O. 138 0.020 0.242

O. 110 -0.040 0.060 0.068 0.060 O. 126 0.060 -0.461

0.230 -0.035 0.090 -0.018 0.090 0.544** O. 110 0.040

0.400 -0.125 O. 120 -0.014 O. 120 -0.069 0.250 0.018

0.490 -0.144 0.200 0.001 0.200 -0.050 0.400 -0.027

0.630 0.863** 0.260 -0.057 0.250 -0.034 0.490 -0.077

0.750 -0.030 0.400 -0.082 0.400 -0,094 0.580 -0.107

0.850 -0.005 0.490 -0.119 0.490 -0.027 0.650 -0.086

0.900 0.031 0.580 -0.174 0.580 -0.145 0.750 -0.069

0.960 0.023 0.640 0.008 0.650 -0.024 0.830 -0.003

0.750 0.092 0.750 0.070 0.900 0.085

0.870 0.110 0.890 0.120 0.960 -0.011

0,930 0.096 0.930 0.081

0.960 0.077 0.960 - 1.049**

500
Table H-L Continued.

Flight 194, Wing sweep = 58 °, Time = 12-5-0-000, MINF = 0,884, Camber = 0/2, ALPT = 8.85, BETA = -0.30, QINF = 304.1.

RNPU = 2.3E+06

11 = 0.93 0.76 0.59 040

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.864 0.000 -0.393 0.000 -4.314 0.010 - 1.546

0.060 -0.688 0.020 -0.772 0.020 -0,888 0.020 -1.486

0.110 -0.341 0,040 -0.695 0.060 -0.867 0.060 - 1.284

0.200 -0.374 0.060 -0.699 0.090 -0.716 O. 110 -0.531

0.230 -0.294 0.090 -0.708 0.110 -0.702 O. 140 -0.311

0.400 -0.177 O. 130 -0.740 O.130 -0.706 O. 190 -5.348

0.490 -0.192 O. 150 -0.705 O.150 -0.676 0.250 -0.257

0.590 -0.154 0.200 -0.671 0.210 -0.788 0.400 -0.392

0.630 -0.134 0.250 -0.527 0.250 -0.606 0.490 -0.467

0.700 -0.095 0.260 -0.473 0.340 -0.236 0.580 -0.266

0.750 -0.045 0.280 -0.442 0.370 -0.205 0.650 -0.259

0.810 -0.071 0.290 -0.403 0.400 -0.222 0.700 -0.227

0.840 -0.057 0.310 -0.344 0.410 -0.197 0.750 -0.279

0.900 -0.020 0.320 -0.336 0.430 -0.204 0.800 -0.162

0.960 -0.013 0.340 -0,339 0,440 -0,203 0.830 -0.213

0.350 -0.121 0,460 0.046 0.900 -0.013

0.370 -0.288 0.490 -0.135 0,960 -0.002

0.380 -0.268 0,500 -0.185

0.400 -0.223 0.520 -0.182

0.410 -0.263 0.540 -0.165

0.430 -0.250 0.550 -0.166

0.440 -0.228 0.580 -0.155

0.460 -0.259 0.600 -0.165

0.470 -0,242 0.610 -0.080

0.490 -0,225 0.650 -2.662

0.500 -0.222 0,700 -0.157

0.520 -0.206 0,750 -0.156

0.530 -0,192 0.820 -0.205

0.550 -0.175 0.890 -0.047

0.560 -0.145 0.900 -0.063

0.580 -0.123 0.960 -0.002

0.590 -0.122

0.600 -0.123

0.640 -2.503

0.700 -0.027

0.750 -0,006

0.820 -2.667

0.870 0.017

0.930 0.031

0,960 0,038

Lower Surface

0,020 0.177 0.020 0.272 0.020 0.262 0.020 0.277

0. 110 0.017 0.060 0.202 0.060 0.231 0.060 6.547

0.230 -0.010 0.090 0.156 0.090 0.156 0.110 0.092

0,400 -0,037 0.120 0.153 0,120 0.001 0.250 0.027

0.490 -0,037 0.200 0.148 0.200 0.055 0.400 0.018

0.630 1.926 0,260 0.078 0.250 0.058 0.490 -0.012

0.750 0.000 0.400 -2.691 0.400 0.026 0.580 -0.063

0.850 0.010 0.490 0,038 0.490 0.002 0.650 -0.029

0.900 0.042 0.580 0.070 0.580 0.017 0.750 0.046

0,960 0.043 0.640 0.297 0.650 0.089 0.830 0.152

0.750 0.059 0.750 0.182 0.900 0.238

0.870 0.077 0.890 _'*** '_* 0.960 -0.016

0.930 0.083 0.930 0.154

0.960 0,023 0.960 -2,560

501
Table H-2. Continued.

Flight 194, Wing sweep -- 58 °, Time = 12-5-2-500, MINF = 0.890, Camber = 0/2, ALPT = 8.96, BETA -- 0.18, QINF -- 308.3,

RNPU = 2.4E+06

¢1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0,883 0,000 -0,380 0.000 -4.256 0.010 - 1.515

0.060 -0.732 0,020 -0.798 0,020 -0,749 0.020 - 1.487

O. 110 -0,303 0.040 -0,709 0.060 -0.824 0.060 - 1.256

0.200 -0.394 0,060 -0,779 0,090 -0.737 O. 110 -0.610

0.230 -0.362 0.090 -0.825 O.110 -0,763 O. 140 -0.370

0.400 -0,226 O. 130 -0.858 O.130 -0.873 O. 190 -5.277

0.490 -0.196 O. 150 -0.827 O. 150 -0,869 0.250 -0.281

0,590 -0.111 0.200 -0.775 0.210 -0.971 0.400 -0.332

0.630 -0.095 0,250 -0.444 0,250 -0.598 0.490 -0.479

0.700 -0.072 0.260 -0.314 0.340 -0,278 0,580 -0.329

0,750 -0.033 0.280 -0.331 0,370 -0.217 0.650 -0.316

0.810 -0.051 0.290 -0.296 0.400 -0.204 0.700 -0.275

0,840 -0.042 0.310 -0.265 0.410 -0.179 0.750 -0.314

0.900 -0.012 0.320 -0,260 0.430 -0.201 0.800 -0.160

0.960 -0.013 0.340 -0.266 0.440 -0.210 0.830 -0.210

0,350 -0.094 0.460 0,040 0.900 -0.013

0.370 -0.263 0,490 -0.169 0.960 -0.002

0.380 -0.260 0.500 -0.192

0.400 -0.231 0.520 -0.179

0.410 -0.284 0.540 -0.176

0,430 -0.304 0.550 -0.164

0,440 -0.266 0.580 -0.144

0,460 -0.297 0.600 -0.157

0,470 -0.283 0.610 -0,078

0.490 -0,249 0.650 -2,626

0.500 -0,235 0,700 -0.154

0.520 -0.233 0.750 -0.146

0.530 -0.207 0.820 -0.198

0.550 -0.198 0.890 -0,082

0.560 -0.173 0,900 -0.096

0.580 -0.146 0.960 -0.017

0.590 -0.141

0,600 -0.150

0.640 -2.469

0.700 -0.041

0.750 -0.013

0,820 -2.631

0.870 0.010

0,930 0,041

0.960 0,038

Lower Surface

0.020 O. 175 0,020 0.265 0.020 0.273 0.020 0.286

O. 110 0.017 0,060 0.207 0.060 0.241 0.060 6,460

0.230 -0.010 0,090 0.160 0.090 0,159 0.110 0.091

0,400 -0.036 O. 120 O.151 O. 120 0.009 0,250 0.027

0.490 -0,036 0.200 O. 149 0,200 0.061 0.400 0.015

0,630 1.900 0.260 0.084 0,250 0.057 0.490 -0,015

0.750 0.000 0.400 -2.655 0.400 0.026 0,580 -0.062

0.850 0,007 0.490 0.04 1 0.490 0.002 0,650 -0.029

0,900 0,031 0.580 0.065 0.580 0.014 0.750 0.046

0,960 0,043 0,640 0,293 0.650 0.088 0.830 O. 159

0.750 0,063 0.750 O. 187 0.900 0.244

0.870 0,090 0.890 ****** 0.960 -0.022

0.930 0.085 0,930 O, 152

0.960 0.026 0.960 -2.526

5O2
Table H-2. Continued.

Flight 194, Wing sweep = 58 °, Time = 12-5-6-000, MINF = 0.900, Camber = 0/2, ALPT = 8.54, BETA = 0.47, QINF = 315.2,

RNPU = 2.4E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.929 0.000 -0.321 0,000 -4.161 0.010 - 1.465

0.060 -0.886 0.020 -0.952 0.020 -0.739 0.020 - 1.413

0.110 -0.266 0.040 -0.817 0.060 -0.800 0.060 - 1.151

0.200 -0.373 0.060 -0.878 0.090 -0.744 O.110 -0.609

0.230 -0.279 0.090 -0.873 0.110 -0.785 0.140 -0.400

0.400 -0.141 0.130 -0.870 0.130 -0.864 0.190 -5.160

0.490 -0.125 0.150 -0.761 0.150 -0.871 0.250 -0.301

0.590 -0.1 O0 0.200 -0.650 0.210 -0.953 0.400 -0.284

0.630 -0.073 0.250 -0.262 0.250 -0.382 0.490 -0.4 l 3

0.700 -0.055 0.260 -0.229 0.340 -0.329 0.580 -0.315

0.750 -0.041 0.280 -0.192 0.370 -0.315 0.650 -0.322

0.810 -0.052 0.290 -0.198 0.400 -0.303 0.700 -0.277

0.840 -0.054 0.310 -0.186 0.410 -0.226 0.750 -0.348

0.900 -0.004 0.320 -0.176 0.430 -0.225 0.800 -0.237

0.960 -0.012 0.340 -0.220 0.440 -0.194 0.830 -0.201

0.350 -0.080 0.460 0.043 0.900 -0.030

0.370 -0.218 0.490 -0.150 0.960 -0.005

0.380 -0.207 0.500 -0.201

0.400 -0.197 0.520 -0.172

0.410 -0.220 0.540 -0.158

0.430 -0.243 0.550 -0.161

0.440 -0.210 0.580 -0.113

0.460 -0.252 0.600 -0.161

0.470 -0.234 0.610 -0.062

0,490 -0.238 0.650 -2.567

0.500 -0.217 0.700 -0.147

0.520 -0.190 0.750 -0.129

0.530 -0.192 0.820 -0.179

0.550 -0.190 0.890 -0,066

0.560 -0.135 0.900 -0.079

0.580 -0.144 0.960 -0.033

0.590 -0.135

0.600 -0.141

0.640 -2.414

0.700 -0,046

0.750 -0.033

0.820 -2,572

0.870 0.007

0.930 0.041

0.960 0.038

Lower Surface

0.020 0.224 0.020 0.236 0.020 0.254 0.020 0.286

0.110 0.011 0.060 0.178 0.060 0.223 0.060 6.318

0.230 -0.030 0.090 O. 143 0.090 O. 147 O. 110 0.057

0.400 -0.020 O.120 O. 114 O. 120 -0.021 0.250 -0.006

0.490 -0.052 0.200 O.144 0.200 0.033 0.400 -0.006

0.630 1.859 0.260 0.055 0.250 0.029 0.490 -0.042

0.750 -0.009 0.400 -2.595 0.400 0.003 0.580 -0.070

0.850 0.018 0.490 0.020 0.490 0.003 0.650 -0.055

0.900 0.035 0.580 0.065 0.580 0.007 0.750 0.046

0.960 0.050 0.640 0.290 0.650 0.066 0.830 O. 156

0.750 0.060 0.750 O. 170 0.900 0.219

0.870 0.088 0.890 ****** 0.960 -0.020

0.930 0.081 0,930 O. 157

0.960 0.037 0.960 -2.469

503
Table H-2. Continued.

Flight 194. Wing sweep = 58 °, Time = 12-5-15-000. MINF = 0.929, Camber = 0/2, ALPT = 8.04, BETA = 0.36. QINF = 334.1,

RNPU = 2.5E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.04 1 0.000 -0.237 0.000 -3.915 0.010 - 1.313

0.060 - 1.033 0.020 -0.764 0.020 -0.898 0.020 - 1.286

0.110 -0.264 0.040 -0.680 0.060 -0.852 0.060 -0.988

0.200 -0.322 0.060 -0.706 0.090 -0.896 0.110 -0.613

0.230 -0.246 0.090 -0.688 0.110 -0.894 0.140 -0.428

0.400 -0.136 0.130 -0.702 0.130 -0.871 0.190 -4.857

0.490 -0.111 0.150 -0.642 0.150 -0.763 0.250 -0.362

0.590 -0.111 0.200 -0.590 0.210 -0.738 0.400 -0.341

0.630 -0.099 0.250 -0.532 0.250 -0.185 0.490 -0.436

0.700 -0.091 0.260 -0.513 0.340 -0.243 0.580 -0.261

0.750 -0.028 0.280 -0.519 0.370 -0.292 0.650 -0.239

0.810 -0.049 0.290 -0.487 0.400 -0.276 0.700 -0.197

0.840 -0.047 0.310 -0.474 0.410 -0.270 0.750 -0.253

0.900 -0.004 0.320 -0.439 0.430 -0.284 0.800 -0.201

0.960 0.018 0.340 -0.468 0.440 -0.298 0.830 -0.331

0.350 -0.185 0.460 -0.087 0.900 -0.049

0.370 -0.400 0.490 -0.278 0.960 -0.030

0.380 -0.353 0.500 -0.308

0.400 -0.270 0.520 -0.302

0.410 -0.299 0.540 -0.297

0.430 -0.224 0.550 -0.280

0.440 -0.211 0.580 -0.264

0.460 -0.216 0.600 -0.255

0.470 -0.167 0.610 -0.176

0.490 -0.135 0.650 -2.412

0.500 -0.119 0.700 -0.164

0.520 -0.106 0.750 -0.138

0.530 -0.058 0.820 -0.I 27

0.550 -0.042 0.890 -0.053

0.560 -0.015 0.900 -0.062

0.580 -0.010 0.960 -0.011

0.590 -0.025

0.600 -0.040

0.640 -2.267

0.700 -0.029

0.750 -0.027

0.820 -2.416

0.870 0.010

0.930 0.033

0.960 0.046

Lower Surface

0.020 O.115 0.020 0.210 0.020 0.210 0.020 0.258

0.110 -0.012 0.060 0.159 0.060 0.170 0.060 5.970

0.230 -0.034 0.090 0.114 0.090 0.104 0.110 0.028

0.400 -0.042 0.120 0.105 0.120 -0.059 0.250 -0.020

0.490 -0.052 0.200 0.106 0.200 0.000 0.400 -0.038

0.630 1.764 0.260 0.043 0.250 -0.002 0.490 -0.056

0.750 -0.004 0.400 -2.438 0.400 -0.004 0.580 -0.122

0.850 0.018 0.490 0.017 0.490 -0.007 0.650 -0.088

0.900 0.051 0.580 0.042 0.580 -0.016 0.750 0.005

0.960 0.062 0.640 0.262 0.650 0.086 0.830 0.130

0.750 0.067 0.750 0.184 0.900 0.218

0.870 0.075 0.890 ****** 0.960 -0.046

0.930 0.089 0.930 0.159

0.960 0.039 0.960 -2.319

504
Table H-2. Continued.

Flight 194, Wing sweep = 58", Time = 12-5-21-500, MINF = 0,950, Camber = 0/2, ALPT = 7.72, BETA = 0.36, QINF = 347.1,

RNPU = 2.6E+06

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.099 0.000 -0.206 0.000 -3.758 0.010 - 1.220

0.060 -0.972 0.020 -0.705 0.020 - 1.079 0,020 - 1.222

0.110 -0.720 0,040 -0.598 0.060 -0.839 0.060 -1.099

0.200 -0.323 0,060 -0,628 0.090 -0.892 0.110 -0.639

0,230 -0.238 0.090 -0.695 0.110 -0.870 0.140 -0.431

0.400 -0.074 0.130 -0.740 0.130 -0.804 0.190 -4.664

0.490 -0,086 0.150 -0.719 0,150 -0,679 0.250 -0.338

0,590 -0.072 0.200 -0.693 0.210 -0.618 0.400 -0.312

0.630 -0.074 0.250 -0.604 0.250 -0.257 0,490 -0.405

0.700 -0.064 0.260 -0.549 0.340 -0.303 0.580 -0,285

0.750 -0.005 0.280 -0.563 0.370 -0.324 0.650 -0.295

0.810 -0.016 0,290 -0.538 0.400 -0.3 ! 8 0.700 -0.274

0.840 -0.021 0.310 -0.485 0.410 -0,289 0.750 -0.321

0.900 0.018 0.320 -0,480 0.430 -0.328 0.800 -0.264

0.960 0.034 0.340 -0.471 0.440 -0.325 0.830 -0.401

0.350 -0.189 0.460 -0.113 0.900 -0.049

0.370 -0.406 0.490 -0.307 0.960 -0.035

0.380 -0.361 0.500 -0.332

0.400 -0.300 0.520 -0.345

0.410 -0.315 0.540 -0.330

0.430 -0.258 0.550 -0.324

0.440 -0.229 0.580 -0.316

0.460 -0.241 0.600 -0.321

0.470 -0.174 0.610 -0.256

0.490 -0.115 0.650 -2.310

0,500 -0.070 0.700 -0.234

0.520 -0.051 0.750 -0.221

0.530 -0.027 0.820 -0.147

0.550 -0,027 0.890 -0.049

0.560 -0.016 0.900 -0,048

0.580 0.000 0.960 0.004

0.590 -0.011

0.600 -0.040

0.640 -2.171

0.700 -0.017

0,750 -0.013

0.820 -2,315

0.870 0.023

0.930 0.055

0.960 0.061

Lower Surface

0.020 0.152 0.020 0.185 0.020 0.187 0,020 0.241

0.110 -0,014 0.060 0.132 0.060 0.139 0.060 5,757

0.230 -0.018 0.090 0.108 0.090 0.060 0.110 0.029

0.400 -0. I 12 0.120 0.105 0.120 -0.081 0.250 -0.054

0.490 -0.049 0.200 0.100 0.200 -0.034 0.400 -0.054

0.630 1.708 0.260 0.039 0.250 -0.029 0.490 -0.094

0.750 0.010 0.400 -2.336 0.400 -0.015 0.580 -0.146

0.850 0.029 0.490 0.014 0.490 -0.009 0.650 -0.126

0.900 0.061 0.580 0.045 0.580 -0.023 0.750 -0.022

0.960 0.076 0.640 0,255 0.650 0.068 0.830 0.112

0.750 0.059 0.750 0.175 0.900 0.203

0.870 0.086 0.890 ****** 0.960 -0.046

0.930 0.094 0.930 0.158

0.960 0.048 0.960 -2.221

5O5
Table H-2. Continued.

Flight 194. Wing sweep = 58 °, Time = 12-5-37-500, MINF = 1.000. Camber = 0/2. ALPT = 6.71. BETA = 0.28. QINF = 377.8.

RNPU = 2.7E+06

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.974 0.000 -0.058 0.000 -3.428 0.010 - 1.003

0.060 -0.628 0.020 - 1.045 0.020 - 1.012 0.020 -0.989

0.110 -0.434 0.040 -0.717 0.060 -0.773 0.060 -0.859

0.200 -0.392 0.060 -0.659 0.090 -0.670 0.110 -0.495

0.230 -0.371 0.090 -0.616 0.110 -0.625 0.140 -0.383

0.400 -0.299 0.130 -0.579 0.130 -0.504 0.190 -4.261

0.490 -0.302 0.150 -0.505 0.150 -0.274 0.250 -0.256

0.590 -0.308 0.200 -0.431 0.210 -0.297 0.400 -0.220

0.630 -0.249 0.250 -0.299 0.250 -0.263 0.490 -0.301

0.700 -0.196 0.260 -0.273 0.340 -0.263 0.580 -0.220

0.750 -0.136 0.280 -0.288 0.370 -0.275 0.650 -0.254

0.810 -0.162 0.290 -0.298 0.400 -0.267 0.700 -0.226

0.840 -0.163 0.310 -0.274 0.410 -0.243 0.750 -0.282

0.900 -0.070 0.320 -0.279 0.430 -0.273 0.800 -0.228

0.960 -0.017 0.340 -0.294 0.440 -0.274 0.830 -0.342

0.350 -0.149 0.460 -0.081 0.900 -0.075

0.370 -0.292 0.490 -0.222 0.960 -0.065

0.380 -0.283 0.500 -0.278

0.400 -0.240 0.520 -0.275

0.410 -0.297 0.540 -0.271

0.430 -0.280 0.550 -0.268

0.440 -0.282 0.580 -0.268

0.460 -0.312 0.600 -0.290

0.470 -0.312 0.610 -0.235

0.490 -0.297 0.650 -2.098

0.500 -0.303 0.700 -0.340

0.520 -0.299 0.750 -0.365

0.530 -0.307 0.820 -0.424

0.550 -0.322 0.890 -0.242

0.560 -0.330 0.900 -0.182

0.580 -0.311 0.960 -0.141

0.590 -0.341

0.600 -0.364

0.640 -1.970

0.700 -0.407

0.750 -0.211

0.820 -2.102

0.870 -0.101

0.930 -0.061

0.960 -0.035

Lower Surface

0.020 0.059 0.020 0.042 0.020 0.138 0.020 0.188

0.110 -0.089 0.060 0.014 0.060 0.094 0.060 5.314

0.230 -0.029 0.090 -0.040 0.090 0.014 0.110 -0.018

0.400 -0.175 0.120 -0.025 0.120 -0.152 0.250 -0.054

0.490 -0.194 0.200 -0.039 0.200 -0.054 0.400 -0.083

0.630 1.594 0.260 -0.159 0.250 -0.113 0.490 -0.126

0.750 -0.147 0.400 -2.122 0.400 -0.111 0.580 -0.192

0.850 -0.106 0.490 -0.077 0.490 -0.071 0.650 -0.167

0.900 -0.059 0.580 -0.024 0.580 -0.266 0.750 -0.107

0.960 -0.019 0.640 0.196 0.650 -0.069 0.830 -0.045

0.750 0.040 0.750 0.042 0.900 0.057

0.870 0.060 0.890 ****** 0.960 -0.073

0.930 0.032 0.930 0.052

0.960 -0.018 0.960 -2.016

5O6
Table H-2. Continued.

Flight 194, Wing sweep = 58 °, Time = 12-5-54-000, MINF = 1.050, Camber = 0/2, ALPT = 7.07, BETA = 0.28, QINF = 414.2,

RNPU = 2.9E+06

_q = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,929 0.000 -0.007 0.000 -3.120 0.010 -0.917

0.060 -0.591 0.020 -0.938 0.020 -0.924 0.020 -0.934

0.110 -0.506 0.040 -0.672 0.060 -0.756 0.060 -0.801

0.200 -0.460 0.060 -0.640 0.090 -0.628 0.110 -0.466

0.230 -0.418 0.090 -0.597 0.110 -0.620 0.140 -0.32 l

0.400 -0.223 0.130 -0,579 0.130 -0.562 O. 190 -3.879

0.490 -0.242 0.150 -0.530 0.150 -0.396 0.250 -0.205

0,590 -0.255 0.200 -0.472 0.210 -0,273 0.400 -0.208

0.630 -0.248 0.250 -0.319 0.250 -0,217 0.490 -0.307

0.700 -0.212 0.260 -0.270 0.340 -0.222 0.580 -0.180

0.750 -0.115 0.280 -0.276 0.370 -0.239 0.650 -0.213

0.810 -0.141 0,290 -0.270 0.400 -0.237 0.700 -0.193

0.840 -0,145 0.310 -0.240 0,410 -0,210 0,750 -0.234

0.900 -0.091 0.320 -0.242 0.430 -0.232 0.800 -0.179

0.960 -0,047 0.340 -0,250 0.440 -0.229 0,830 -0.287

0.350 -0.111 0.460 -0.054 0.900 -0.043

0.370 -0.251 0.490 -0.2 | 7 0.960 -0.031

0.380 -0.240 0.500 -0.239

0.400 -0.195 0.520 -0.235

0.410 -0,254 0.540 -0.228

0.430 -0.227 0.550 -0,229

0.440 -0.231 0.580 -0.229

0.460 -0.254 0.600 -0.245

0.470 -0.261 0.610 -0.206

0,490 -0.248 0.650 - 1.907

0.500 -0.260 0200 -0.289

0.520 -0.239 0.750 -0.323

0.530 -0,254 0.820 -0.388

0.550 -0.252 0,890 -0.265

0.560 -0.277 0,900 -0,209

0.580 -0.255 0.960 -0.154

0.590 -0.282

0.600 -0.314

0.640 - 1.790

0,700 -0.343

0.750 -0.195

0.820 - 1.910

0.870 -0,079

0.930 -0.035

0.960 -0.017

Lower Surface

0.020 0.068 0.020 O.133 0.020 O. 183 0.020 0.253

O. 110 -0.048 0.060 0.084 0.060 O. 144 0.060 4.855

0.230 0.010 0.090 0.024 0.090 0.063 O. 110 0.027

0.400 -0.112 O. 120 0.038 0.120 -0.076 0.250 -0.015

0.490 -0.133 0.200 0.027 0.200 0.004 0.400 -0.037

0.630 1.462 0.260 -0.085 0.250 -0.043 0,490 -0.070

0.750 -0.133 0.400 - 1.928 0.400 -0.051 0.580 -0.139

0,850 -0.082 0.490 -0.058 0.490 -0.020 0.650 -0.124

0,900 -0.042 0,580 -0.004 0.580 -0.238 0.750 -0.055

0.960 -0.027 0.640 0.201 0,650 -0.008 0,830 0.004

0.750 0,059 0.750 0.080 0,900 0.081

0,870 0.070 0.890 ****** 0.960 -0.024

0,930 0.066 0.930 0.075

0.960 0,012 0.960 -1.832

507
Table H-2. Continued.

Flight 194, Wing sweep = 58 °, Time = 12-6-9-500, MINF = 1.100, Camber = 0/2, ALPT = 6.54, BETA = 0.34, QINF = 456.2,

RNPU = 3.1E+06

lq = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.770 0.000 0.083 0.000 -2.836 0.010 -0.806

0.060 -0.525 0.020 -0.845 0.020 -0.786 0.020 -0.801

O. I 10 -0.469 0.040 -0.741 0.060 -0.735 0.060 -0.749

0.200 -0.301 0.060 -0.524 0.090 -0.530 O.110 -0.443

0.230 -0.263 0.090 -0.479 O. 110 -0.510 O. 140 -0.307

0.400 -0.181 O. 130 -0,482 O. 130 -0.473 O. 190 -3.526

0.490 -0.201 O. 150 -0.433 O. 150 -0.331 0.250 -0.162

0.590 -0.211 0,200 -0.379 0.210 -0.227 0.400 -0.151

0.630 -0.222 0.250 -0.207 0.250 -0.157 0.490 -0.217

0.700 -0.257 0.260 -0.185 0.340 -0.165 0.580 -0.123

0.750 -0.149 0.280 -0.201 0.370 -0.180 0.650 -0.172

0.810 -0.172 0.290 -0.209 0.400 -0.180 0.700 -0.148

0.840 -0.160 0.310 -0.193 0.410 -0.162 0.750 -0.197

0.900 -0.098 0.320 -0.193 0.430 -0.184 0.800 -0.145

0.960 -0.074 0.340 -0.207 0.440 -0.181 0.830 -0.239

0.350 -0.085 0.460 -0.024 0.900 -0.030

0.370 -0.207 0.490 -0.166 0.960 -0.022

0.380 -0.194 0.500 -0.185

0.400 -0.152 0.520 -0.185

0.410 -0.199 0.540 -0.183

0.430 -0.185 0.550 -0.177

0.440 -0.156 0.580 -0.179

0.460 -0.203 0.600 -0.192

0.470 -0.209 0.6 I0 -0.154

0.490 -0.196 0.650 - 1.735

0.500 -0.201 0.700 -0.226

0.520 -0.201 0.750 -0.261

0.530 -0.206 0.820 -0.330

0.550 -0.217 0.890 -0.243

0.560 -0.221 0.900 -0.180

0.580 -0.204 0.960 -0.107

0.590 -0.228

0.600 -0.263

0.640 - 1.629

0.700 -0.286

0.750 -0.224

0.820 -1.738

0.870 -0.075

0.930 -0.026

0.960 -0.002

Lower Surface

0.020 0.081 0.020 0.088 0.020 O. 157 0.020 0.288

O. 1 t 0 -0.046 0.060 0.073 0.060 O.128 0.060 4.405

0.230 -0.057 0.090 0.003 0.090 0.053 0.110 0.017

0.400 -0.105 O.120 0.016 O.120 -0.108 0.250 -0.048

0.490 -0.103 0.200 0.045 0.200 -0.035 0.400 -0.051

0.630 1.256 0.260 -0.019 0.250 -0.023 0.490 -0.087

0.750 -0,095 0.400 - 1.754 0.400 -0.080 0.580 -0.134

0.850 -0.058 0.490 -0.167 0.490 -0.022 0.650 -0.133

0.900 -0.024 0,580 -0.022 0.580 -0.177 0.750 -0.044

0.960 -0.019 0.640 O. 186 0.650 -0.015 0.830 -0.011

0.750 0.065 0.750 0.079 0.900 0.087

0.870 0.076 0.890 ****** 0.960 -0.029

0.930 0.076 0.930 0.090

0.960 0.031 0.960 - 1.667

5O8
Table H-2. Continued.

Flight 194, Wing sweep = 58 °, Time = 12-6-22-000, MINF = 1.150, Camber = 0/2, ALPT = 5.91, BETA = 0.31, QINF = 501.4,

RNPU = 3.3E+06

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.651 0.000 0.139 0.000 -2.587 0.010 -0.675

0.060 -0.638 0.020 -0.733 0.020 -0.666 0.020 -0.685

O. 110 -0.386 0.040 -0.643 0.060 -0.687 0.060 -0.625

0.200 -0.195 0.060 -0.622 0.090 -0.639 0.110 -0.436

0.230 -0.134 0.090 -0.609 0.110 -0.643 0.140 -0.336

0.400 -0.126 0.130 -0.402 0.130 -0.415 0.190 -3.215

0.490 -0.155 0.150 -0.365 0.150 -0.298 0.250 -0.179

0.590 -0.180 0.200 -0.292 0.210 -0.224 0.400 -0.110

0.630 -0.195 0.250 -0.148 0.250 -0.128 0.490 -0.159

0.700 -0.218 0.260 -0.142 0.340 -0.129 0.580 -0.097

0.750 -0.238 0.280 -0.157 0.370 -0.147 0.650 -0.143

0.810 -0.258 0.290 -0.164 0.400 -0.144 0.700 -0.126

0.840 -0.265 0.310 -0.140 0.410 -0.133 0.750 -0.1 64

0.900 -0.115 0.320 -0.154 0.430 -0.147 0.800 -0.121

0.960 -0.082 0.340 -0.166 0.440 -0.146 0.830 -0.208

0.350 -0.071 0.460 -0.005 0.900 -0.034

0.370 -0.167 0.490 -0.131 0.960 -0.027

0.380 -0.153 0.500 -0.152

0.400 -0.113 0.520 -0.144

0.410 -0.161 0.540 -0.148

0.430 -0.146 0.550 -0.142

0.440 -0.137 0.580 -0.159

0.460 -0.169 0.600 -0.156

0.470 -0.154 0.610 -0.113

0.490 -0.157 0.650 - 1.585

0.500 -0.161 0.700 -0.195

0.520 -0.157 0.750 -0.225

0.530 -0.156 0.820 -0.277

0.550 -0.177 0.890 -0.253

0.560 -0.185 0.900 -0.174

0.580 -0.160 0.960 -0.100

0.590 -0.191

0.600 -0.214

0.640 -1.488

0.700 -0.243

0.750 -0.206

0.820 -1.588

0.870 -0.077

0.930 -0.024

0.960 -0.004

Lower Surface

0.020 0.061 0.020 0.069 0.020 0.098 0.020 0.275

O.110 -0.057 0,060 0,042 0.060 O. 102 0,060 4.001

0,230 -0,034 0,090 -0.015 0.090 0.034 O. 110 0.045

0,400 -0.200 O. 120 -0.019 O. 120 -0.126 0.250 -0.042

0,490 -0.093 0.200 0.034 0,200 -0,047 0,400 -0,058

0,630 1.136 0.260 -0.056 0.250 -0.043 0.490 -0.104

0.750 -0.082 0,400 - 1.603 0,400 -0,083 0.580 -0.153

0.850 -0,053 0,490 -0.148 0.490 -0.031 0.650 -0.139

0.900 -0.022 0.580 -0.096 0.580 -0.163 0,750 -0.059

0,960 -0,009 0.640 O. 151 0,650 -0,094 0.830 -0.032

0.750 0,058 0.750 0.074 0.900 0.062

0.870 0.068 0.890 ****** 0.960 -0.033

0.930 0,066 0.930 0.070

0,960 0.028 0.960 - 1.523

5O9
Table H-2. Continued.

Flight 194. Wing sweep = 58 °, Time = 12-6-34-000, MINF = 1.200. Camber = 0/2. ALPT = 5.70. BETA = 0.31, QINF = 551.5,

RNPU = 3.6E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.564 0.000 0.190 0.000 -2.362 0.010 -0.592

0.060 -0.558 0.020 -0.641 0.020 -0.570 0.020 -0.605

0.110 -0.511 0.040 -0.545 0.060 -0.587 0.060 -0.562

0.200 -0.235 0.060 -0.551 0.090 -0.569 0.110 -0.441

0.230 -0.1 64 0.090 -0.546 0.110 -0.558 0.140 -0.324

0.400 -0.071 0.130 -0.548 0.130 -0.522 0.190 -2.932

0.490 -0.092 0.150 -0.514 0.150 -0.369 0.250 -0.217

0.590 -0.127 0.200 -0.316 0.210 -0.300 0.400 -0.098

0.630 -0.152 0.250 -0.157 0.250 -0.150 0.490 -0.123

0.700 -0.176 0.260 -0.123 0.340 -0.111 0.580 -0.090

0.750 -0.223 0.280 -0.127 0.370 -0.123 0.650 -0.134

0.810 -0.249 0.290 -0.128 0.400 -0.113 0.700 -0.100

0.840 -0.249 0.310 -0.108 0.410 -0.106 0.750 -0.142

0.900 -0.102 0.320 -0.113 0.430 -0.I 19 0.800 -0.104

0.960 -0.065 0.340 -0.130 0.440 -0.115 0.830 -0.183

0.350 -0.044 0.460 0.017 0.900 -0.022

0.370 -0.126 0.490 -0.097 0.960 -0.018

0.380 -0.121 0.500 -0.122

0.400 -0.079 0.520 -0.115

0.410 -0.123 0.540 -0.121

0.430 -0.104 0.550 -0.113

0.440 -0.102 0.580 -0.118

0.460 -0.128 0.600 -0.119

0.470 -0.127 0.610 -0.097

0.490 -0.120 0.650 - 1.451

0.500 -0.120 0.700 -0.156

0.520 -0.120 0.750 -0.188

0.530 -0.126 0.820 -0.243

0.550 -0.140 0.890 -0.263

0.560 -0.145 0.900 -0.180

0.580 -0.129 0.960 -0.102

0.590 -0.154

0.600 -0.172

0.640 - 1.363

0.700 -0.213

0.750 -0.175

0.820 -1.454

0.870 -0.087

0.930 -0.015

0.960 0.006

Lower Surface

0.020 0.073 0.020 0.088 0.020 0.113 0.020 0.242

0.110 -0.040 0.060 0.050 0.060 0.124 0.060 3.628

0.230 -0.030 0.090 0.001 0.090 0.061 0.110 0.058

0.400 -0.161 0.120 -0.019 0.120 -0.099 0.250 0.000

0.490 -0.194 0.200 0.010 0.200 -0.036 0.400 -0.042

0.630 1.024 0.260 -0.035 0.250 -0.055 0.490 -0.092

0.750 -0.053 0.400 - 1.467 0.400 -0.077 0.580 -0.146

0.850 -0.034 0.490 -0.1 04 0.490 -0.022 0.650 -0.114

0.900 -0.008 0.580 -0.159 0.580 -0.174 0.750 -0.044

0.960 0.000 0.640 0.132 0.650 -0.149 0.830 -0.032

0.750 0.068 0.750 0.086 0.900 0.054

0.870 0.075 0.890 ****** 0.960 -0.027

0.930 0.069 0.930 0.070

0.960 0.028 0.960 - 1.395

510
Table H-2. Continued.

Flight 194, Wing sweep = 58 °, Time = 12-6-46-000, MINF = 1.249, Camber = 0/2, ALPT = 5.15, BETA = 0.23, QINF = 602.4,

RNPU = 3.9E+06

_q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.477 0.000 0.232 0.000 -2.169 0.010 -0.518

0.060 -0.477 0.020 -0.575 0.020 -0.476 0.020 -0.519

0.110 -0.417 0.040 -0.462 0.060 -0.500 0.060 -0.500

0.200 -0.277 0.060 -0.481 0.090 -0.486 0.110 -0.421

0.230 -0.164 0.090 -0.460 0.110 -0.466 0.140 -0.291

0.400 -0.061 0.130 -0.469 0.130 -0.437 0.190 -2.692

0.490 -0.070 0.150 -0.440 0.150 -0.334 0.250 -0.233

0.590 -0.085 0.200 -0.388 0.210 -0.324 0.400 -0.107

0.630 -0.107 0.250 -0.163 0.250 -0.192 0.490 -0.110

0.700 -0.133 0.260 -0.140 0.340 -0.109 0.580 -0.079

0.750 -0.184 0.280 -0.141 0.370 -0.1 04 0.650 -0.118

0.810 -0.209 0.290 -0.143 0.400 -0.107 0.700 -0.093

0.840 -0.214 0.310 -0. l 11 0.410 -0.082 0.750 -0.123

0.900 -0.138 0.320 -0. l 12 0.430 -0.101 0.800 -0.095

0.960 -0.059 0.340 -0.112 0.440 -0.096 0.830 -0.170

0.350 -0.053 0.460 0.020 0.900 -0.029

0.370 -0.101 0.490 -0.070 0.960 -0.024

0.380 -0.088 0.500 -0.090

0.400 -0.063 0.520 -0.095

0.410 -0.100 0.540 -0.090

0.430 -0.082 0.550 -0.092

0.440 -0.078 0.580 -0.086

0.460 -0.101 0.600 -0.098

0.470 -0.110 0.610 -0.067

0.490 -0.095 0.650 - 1.335

0.500 -0.095 0.700 -0.155

0.520 -0.094 0.750 -0.167

0.530 -0.095 0.820 -0.215

0.550 -0.109 0.890 -0.254

0.560 -0.106 0.900 -0.195

0.580 -0.109 0.960 -0.093

0.590 -0.127

0.600 -0.143

0.640 - 1.255

0.700 -0.176

0.750 -0.160

0.820 -1.338

0.870 -0.133

0.930 -0.016

0.960 0.008

Lower Surface

0.020 0.040 0.020 0.075 0.020 0.119 0.020 0.229

0.110 -0.062 0.060 0.039 0.060 0.123 0.060 3.314

0.230 -0.037 0.090 -0.015 0.090 0.058 0.110 -0.027

0.400 -0.144 0.120 -0.021 0.120 -0.086 0.250 0.011

0.490 -0.156 0.200 0.004 0.200 -0.037 0.400 -0.031

0.630 0.930 0.260 -0.050 0.250 -0.057 0.490 -0.095

0.750 -0.037 0.400 - 1.350 0.400 -0.090 0.580 -0.134

0.850 -0.030 0.490 -0.130 0.490 -0.031 0.650 -0.102

0.900 -0.005 0.580 -0.138 0.580 -0.170 0.750 -0.036

0.960 0.013 0.640 0.087 0.650 -0.1 40 0.830 -0.045

0.750 0.047 0.750 0.071 0.900 0.047

0.870 0.060 0.890 ****** 0.960 -0.032

0.930 0.072 0.930 0.072

0.960 0.031 0.960 - 1.284

511
Table H-2. Continued.

Hight 194, Wing sweep = 58 °, Time = 12-7-1-500, MINF = 1.299, Camber = 0/2, ALPT = 4.53, BETA = 0.26, QINF = 657.7,

RNPU = 4.2E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,388 0.000 0.272 0.000 - 1.995 0.010 -0.418

0.060 -0.376 0.020 -0.454 0.020 -0.376 0.020 -0.448

O. 110 -0.344 0.040 -0.373 0.060 -0.451 0.060 -0.432

0.200 -0.341 0.060 -0.386 0.090 -0.385 O. 110 -0.376

0.230 -0.282 0.090 -0.376 O.110 -0.387 O. 140 -0.256

0.400 -0.060 O. 130 -0.363 O.130 -0.336 O. 190 -2.474

0.490 -0.049 O.150 -0.356 O.150 -0.291 0.250 -0.241

0.590 -0.056 0.200 -0.306 0.210 -0.282 0.400 -0.107

0.630 -0.071 0.250 -0.241 0.250 -0.241 0.490 -0.090

0.700 -0.107 0.260 -0.211 0.340 -0.109 0.580 -0.055

0.750 -0.148 0.280 -0.168 0.370 -0.101 0.650 -0.097

0.8 t 0 -0.165 0.290 -0.145 0.400 -0.103 0.700 -0.073

0.840 -0,168 0.310 -0.114 0.410 -0.076 0.750 -0.101

0.900 -0.239 0.320 -0.115 0.430 -0.091 0.800 -0.078

0.960 -0.060 0.340 -0.111 0,440 -0.085 0.830 -0.145

0.350 -0.053 0.460 0.020 0.900 -0.031

0,370 -0.101 0.490 -0.059 0.960 -0.024

0.380 -0.087 0.500 -0.085

0.400 -0.055 0.520 -0.073

0.410 -0.083 0.540 -0.065

0.430 -0.066 0.550 -0.064

0.440 -0.066 0.580 -0.061

0.460 -0.084 0.600 -0.076

0.470 -0.085 0.610 -0.045

0.490 -0.066 0.650 - 1.232

0.500 -0.065 0.700 -0.126

0.520 -0.067 0.750 -0.144

0.530 -0.068 0.820 -0.180

0.550 -0.069 0.890 -0.245

0.560 -0.091 0.900 -0.215

0.580 -0.074 0.960 -0.093

0.590 -0.093

0.600 -0.113

0.640 -1.158

0.700 -0.144

0.750 -0.132

0.820 -1.234

0.870 -0.118

0.930 -0.073

0.960 0.007

Lower Surface

0.020 0.079 0.020 0.073 0.020 0.094 0.020 0.229

O. 110 -0.068 0.060 0.046 0.060 O. 134 0.060 3.027

0.230 -0.055 0.090 -0.021 0.090 0.080 O. 110 -0.031

0.400 -0.122 O. 120 -0.028 O. 120 -0.075 0.250 0.019

0.490 -0.148 0.200 0.023 0.200 -0.023 0.400 -0.037

0.630 0.843 0.260 -0.061 0.250 -0.051 0.490 -0.087

0.750 -0.043 0.400 - 1.245 0.400 -0.083 0.580 -0.125

O.850 -0.018 0.490 -0.128 0.490 -0.037 0.650 -0.101

0.900 0.009 0.580 -0.167 0.580 -0.181 0.750 -0.039

0.960 0.018 0.640 0.021 0.650 -0.176 0.830 -0.039

0.750 0.048 0.750 0.043 0.900 0.066

0.870 0.048 0.890 ****** 0.960 -0.038

0.930 0.064 0.930 0.092

0.960 0.035 0.960 - 1.185

512
Table H-2. Continued.

Flight 217, Wing sweep = 58 °, Time = 11-4-36-500, MINF = 1.213, Camber = 0/2, ALPT = 5.51, BETA = 0.22, QINF = 595.8,

RNPU = 3.9E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.690 0.000 -0.008 0,000 4.062"* 0.010 -0.618

0,060 -0.734 0.020 -0.824 0.020 -0.760 0.020 -0.739

0.110 -0.701 0.040 -0.728 0.060 -0.927** 0.060 -0.674

0.200 -0.406 0.060 -0.739 0.090 -0.725 O.110 -0.619

0.230 -0.429 0.090 -0.658 O. 110 -0.752 O. 140 -0.494

0.400 -0.248 O, 130 -0.713 O. 130 -0.698 O. 190 -0.971 **

0.490 -0.249 O. 150 -0.696 O.150 -0.643 0.250 -0.397

0.590 -0.297 0.200 -0.658 0.210 -0.404 0.400 -0.311

0.630 -0.310 0.250 -0.396 0,250 -0,342 0.490 °0.291

0.700 -0.318 0.260 -0.249 0.340 -0.415 0.580 -0.238

0.750 -0.361 0.280 -0.348 0.370 -0.256 0.650 -0.243

0.810 -0.413 0.290 -0.326 0.400 -0.285 0.700 -0.229

0,840 -0.418 0.310 -0.308 0.410 1.283** 0.750 -0.313

0.900 -0.290 0.320 -0.313 0.430 -0.194 0.800 -0.217

0.960 -0.244 0.340 -0.196 0.440 -0,301 0.830 -0.258

0.350 -0.265** 0.460 -0.305 0.900 -0.238

0.370 -0.296 0.490 -0.320 0.960 -0.217

0.380 -0.313 0.500 -0257

0.400 -0.265 0.520 -0.317

0.410 -0.307 0.540 -0.301

0.430 -0.293 0.550 -0.173

0.440 -0.276 0.580 -0.289

0.460 -0.243 0.600 -0.321

0.470 -0.300 0.610 -0.319

0.490 -0.299 0.650 1.951 **

0.500 -0.309 0.700 -0.364

0.520 -0.313 0.750 -0.397

0.530 -0.315 0.820 -0.440

0.550 -0.344 0.890 -0.475

0.560 -0.341 0.900 -0.376

0.580 -0.271 0.960 -0.269

0.590 -0.344

0.600 -0.345

0.640 -0.372

0.700 -0.392

0.750 -0.210"*

0.820 -0,330

0.870 -0.295

0.930 -0.199

0.960 -0.183

Lower Surface

0.020 -0.163 0.020 -0.085 0.020 0.022 0.020 O.114

O. 110 -0.211 0.060 -0.113 0.060 -0.040 0.060 -0.612

0.230 -0,219 0.090 -0.146 0.090 1.524' * O. 110 -0.095

0.400 -0.325 O. 120 -0.183 O. 120 -0.233 0.250 -0.175

0.490 -0.352 0.200 -0. | 81 0.200 -0.221 0.400 -0.167

0.630 1.906"* 0.260 -0.216 0.250 -0.106 0.490 -0.258

0.750 -0.231 0.400 -0.266 0.400 -0.148 0.580 -0.31 I

0.850 -0.209 0.490 -0.297 0.490 -0.210 0.650 -0.282

0.900 -0.175 0.580 -0.381 0.580 -0.339 0.750 -0.233

0.960 -0.175 0.640 -0.151 0.650 -0.1 64 0.830 -0.199

0.750 -0.035 0.750 -0.117 0.900 -0.129

0.870 -0.082 0.890 -0.076 0.960 -OAO1

0.930 -0.099 0.930 -0.106

0,960 -0.128 0.960 1.239"*

513
Table H-2. Continued,

Flight 217, Wing sweep = 58 °, Time = 11-4-52-000, MINF = 1.216, Camber = 0/2, ALPT = 4.85, BETA = 0.17, QINF = 595.5,

RNPU = 3.9E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0.928 0.000 -0.205 0.000 4.069"* 0.010 -0.911

0.060 -0.935 0.020 -0.972 0.020 -0,944 0.020 -0.911

0.110 -0.884 0.040 -0.902 0.060 -0,922** 0.060 -0,856

0.200 -0.569 0.060 -0.932 0.090 -0.902 0.110 -0,764

0.230 -0.467 0.090 -0.897 0.110 -0.926 0.140 -0.691

0,400 -0.464 0.130 -0.883 0.130 -0.845 0.190 -0.967"*

0,490 -0.484 0.150 -0.875 0.150 -0.715 0.250 -0.607

0.590 -0.521 0.200 -0.688 0.210 -0.678 0.400 -0.510

0.630 -0.538 0,250 -0.531 0,250 -0.533 0.490 -0.492

0.700 -0.542 0.260 -0.511 0.340 -0,387 0.580 -0.470

0.750 -0.634 0.280 -0.515 0.370 -0.518 0.650 -0.511

0.810 -0.633 0.290 -0.519 0.400 -0.501 0,700 -0.501

0,840 -0.638 0.310 -0.510 0.410 1.289"* 0.750 -0.518

0.900 -0.517 0.320 -0.517 0.430 -0.514 0.800 -0.538

0.960 -0.464 0.340 -0.516 0.440 -0.504 0.830 -0.579

0.350 -0.480** 0.460 -0,512 0.900 -0.464

0.370 -0.507 0.490 -0,487 0.960 -0.437

0.380 -0.521 0.500 -0.520

0.400 -0.423 0.520 -0.524

0.410 -0.516 0.540 -0.512

0.430 -0.502 0.550 -0.489

0,440 -0.487 0.580 -0.487

0.460 -0.509 0.600 -0.520

0.470 -0.524 0.610 -0.520

0.490 -0.511 0.650 1.957**

0.500 -0.519 0.700 -0.568

0.520 -0.518 0.750 -0.604

0.530 -0.523 0.820 -0.641

0.550 -0,549 0,890 -0.668

0.560 -0.547 0.900 -0.578

0.580 -0.545 0.960 -0.477

0.590 -0.550

0.600 -0.564

0.640 -0.579

0.700 -0,599

0.750 -0.439**

0.820 -0.547

0.870 -0.541

0.930 -0.425

0.960 -0.398

Lower Surface

0.020 -0,387 0.020 -0.343 0.020 -0.279 0.020 -0.180

0.110 -0.452 0.060 -0.340 0.060 -0.274 0.060 -0.897

0.230 -0.458 0.090 -0.438 0.090 1.530"* 0. 110 -0,390

0.400 -0.549 0.120 -0.433 0.120 -0.470 0.250 -0.402

0.490 -0.573 0,200 -0.427 0.200 -0.465 0.400 -0.455

0.630 1.912"* 0.260 -0.456 0.250 -0.441 0.490 -0.489

0,750 -0.449 0.400 -0.505 0.400 -0.492 0.580 -0.540

0.850 -0.429 0.490 -0.542 0.490 -0.323 0.650 -0.513

0.900 -0.395 0.580 -0.605 0.580 -0.566 0.750 -0.476

0.960 -0.397 0.640 -0.393 0.650 -0.445 0.830 -0,423

0.750 -0.329 0.750 -0.350 0.900 -0.337

0.870 -0.310 0.890 -0.307 0.960 -0.436

0.930 -0.319 0,930 -0.335

0.960 -0.350 0.960 1.245"*

514
Table H-2. Continued.

Flight 217, Wing sweep = 58 °, Time = 11-5-9-000, MINF = 1.221, Camber = 012, ALPT = 5.00, BETA = 0.25, QINF = 602.6,

RNPU = 3.9E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.592 0.000 0.132 0,000 4.018"* 0.010 -0.634

0.060 -0.633 0.020 -0.589 0.020 -0.656 0.020 -0.623

0,110 -0.564 0.040 -0.567 0.060 -0,914"* 0.060 -0.513

0.200 -0.270 0.060 -0.705 0.090 -0.564 0.110 -0.461

0.230 -0.231 0.090 -0.893 0.110 -0.643 0.140 -0.359

0.400 -0.126 0,130 -0.565 0.130 -0.525 0.190 -0.958"*

0.490 -0.199 0,150 -0.542 0.150 -0.419 0.250 -0.274

0.590 -0.172 0.200 -0.466 0.210 -0.369 0.400 -0.175

0.630 -0.191 0.250 -0.223 0.250 -0.208 0.490 -0.219

0.700 -0.197 0.260 -0.189 0.340 -0.505 0.580 -0.134

0.750 -0.290 0.280 -0.193 0.370 -0.235 0.650 -0.177

0.810 -0,289 0.290 -0.185 0,400 -0.152 0.700 -0.157

0.840 -0.286 0.310 -0.230 0.410 1.271 ** 0.750 -0.179

0.900 -0,184 0.320 -0.183 0.430 -0.510 0.800 -0.537

0.960 -0.126 0.340 -0.234 0.440 -0.506 0.830 -0.215

0,350 -0.142"* 0.460 -0.511 0.900 -0.124

0.370 -0.224 0.490 -0.205 0.960 -0.155

0.380 -0.181 0.500 -0.181

0.400 -0.140 0.520 -0.52 l

0.410 -0.176 0.540 -0.173

0.430 -0.273 0,550 -0.373

0.440 -0.144 0,580 -0.148

0,460 -0.170 0.600 -0.181

0.470 -0.235 0.610 -0.187

0,490 -0.172 0.650 1.931"*

0.500 -0.177 0.700 -0.234

0.520 -0.179 0.750 -0.322

0.530 -0.187 0.820 -0.361

0.550 -0.210 0.890 -0.334

0.560 -0.207 0,900 -0.303

0.580 -0.193 0.960 -0.135

0.590 -0.217

0.600 -0.220

0.640 -0.242

0.700 -0.261

0,750 -0.099**

0,820 -0,209

0.870 -0.213

0.930 -0.081

0.960 -0,060

Lower Surface

0.020 -0.069 0.020 0.005 0,020 0.016 0.020 0.163

0.110 -0.110 0.060 0.006 0.060 0,072 0.060 -0.604

0,230 -0.113 0.090 -0319 0,090 1,509"* 0.110 -0.072

0.400 -0.217 0.120 -0.091 0.120 -0.127 0.250 -0.114

0.490 -0.226 0,200 -0.304 0.200 -0.116 0.400 -0.110

0.630 1.887"* 0.260 -0.112 0.250 -0,208 0.490 -0.260

0.750 -0.098 0.400 -0.215 0.400 -0.489 0.580 -0.536

0.850 -0.089 0.490 -0,199 0.490 -0.322 0.650 -0.167

0.900 -0.059 0.580 -0,596 0.580 -0.223 0.750 -0.105

0.960 -0.115 0.640 -0.110 0.650 -0.442 0.830 -0.085

0.750 -0.04 1 0.750 -0.008 0.900 -0.062

0.870 0.026 0.890 0.039 0.960 -0.098

0.930 0.021 0.930 -0.328

0.960 -0.015 0.960 1.228'*

515
Table H-2. Continued.

Flight 217. Wing sweep = 58 °, Time = 11-5-13-500. MINF = 1.222, Camber = 0/2. ALPT = 3.56, BETA = 0.25. QINF = 603.3,

RNPU = 3.9E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.444 0.000 0.219 0.000 4.013"* 0.010 -0.414

0.060 -0.433 0.020 -0.505 0.020 -0.460 0.020 -0.490

0.110 -0.141 0.040 -0.437 0.060 -0.913"* 0.060 -0.404

0.200 -0.103 0.060 -0.462 0.090 -0.393 0.110 -0.305

0.230 -0.045 0.090 -0.403 0.110 -0.338 0.140 -0.260

0.400 -0.077 0.130 -0.240 0.130 -0.257 0.190 -0.957 * *

0.490 -0.106 0.150 -0.170 0.150 -0.225 0.250 -0.197

0.590 -0.137 0.200 -0.130 0.210 -0.221 0.400 -0.094

0.630 -0.154 0.250 -0.098 0.250 -0.094 0.490 -0.050

0.700 -0.163 0.260 -0.089 0.340 -0.077 0.580 -0.052

0.750 -0.238 0.280 -0.110 0.370 -0.106 0.650 -0.098

0.810 -0.230 0.290 -0.114 0.400 -0.077 0.700 -0.101

0.840 -0.244 0.310 -0.108 0.410 1.269"* 0.750 -0.110

0.900 -0.136 0.320 -0.102 0.430 -0.096 0.800 -0.146

0.960 -0.063 0.340 -0.112 0.440 -0.089 0.830 -0.176

0.350 -0.081 ** 0.460 -0.092 0.900 -0.052

0.370 -0.101 0.490 -0.074 0.960 -0.043

0.380 -0.102 0.500 -0.102

0.400 -0.089 0.520 -0.111

0.410 -0.099 0.540 -0.090

0.430 -0.084 0.550 -0.070

0.440 -0.069 0.580 -0.066

0.460 -0.090 0.600 -0.106

0.470 -0.087 0.610 -0.098

0.490 -0.091 0.650 1.929**

0.500 -0.099 0.700 -0.148

0.520 -0.103 0.750 -0.197

0.530 -0.106 0.820 -0.219

0.550 -0.131 0.890 -0.251

0.560 -0.137 0.900 -0.198

0.580 -0.113 0.960 -0.062

0.590 -0.145

0.600 -0.154

0.640 -0.162

0.700 -0.190

0.750 -0.045**

0.820 -0.140

0.870 -0.173

0.930 -0.033

0.960 -0.022

Lower Surface

0.020 -0.038 0.020 0.008 0.020 0.090 0.020 0.173

0.110 -0.114 0.060 0.004 0.060 0.088 0.060 -0.519

0.230 -0.1 04 0.090 -0.093 0.090 1.507** 0.110 -0.012

0.400 -0.193 0.120 -0.075 0.120 -0.109 0.250 -0.037

0.490 -0.191 0.200 -0.062 0.200 -0.084 0.400 -0.086

0.630 1.885"* 0.260 -0.103 0.250 -0.094 0.490 -0.131

0.750 -0.046 0.400 -0.133 0.400 -0.132 0.580 -0.167

0.850 -0.007 0.490 -0.175 0.490 -0.047 0.650 -0.140

0.900 0.026 0.580 -0.218 0.580 -0.206 0.750 -0.129

0.960 0.026 0.640 -0.039 0.650 -0.061 0.830 -0.033

0.750 0.047 0.750 0.019 0.900 0.041

0.870 0.073 0.890 0.068 0.960 -0.098

0.930 0.070 0.930 0.024

0.960 0.046 0.960 1.226**

516
TabLe H-2. Continued.

Flight 217, Wing sweep = 58 °, Time = 11-5-15-000, MINF = 1.224, Camber = 0/2. ALPT = 2.68, BETA = 0.25, QINF = 605.9,

RNPU = 3.9E+06

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.344 0.000 0.253 0.000 3.995"* 0.010 -0.409

0,060 -0.071 0.020 -0.357 0.020 -0.4 t 9 0.020 -0.437

0.110 -0.058 0.040 -0.384 0.060 -0.910"* 0.060 -0.313

0.200 -0.096 0.060 -0.330 0.090 -0.244 0.1 I0 -0.261

0.230 -0.067 0.090 -0.161 0.110 -0.243 0.140 -0.244

0,400 -0.092 0.130 -0.185 0.130 -0.186 0.190 -0.953"*

0.490 -0.113 0.150 -0.099 0.150 -0.195 0.250 -0.172

0.590 -0,144 0.200 -0.101 0.210 -0.201 0,400 -0.063

0.630 -0.160 0,250 -0,092 0.250 -0.065 0,490 -0.045

0,700 -0.163 0.260 -0.075 0.340 -0.069 0.580 -0.035

0.750 -0.235 0.280 -0.089 0.370 -0.084 0.650 -0.075

0.810 -0.229 0.290 -0.101 0.400 -0.081 0.700 -0.075

0.840 -0.233 0.310 -0.087 0.410 1.263"* 0.750 -0.101

0.900 -0.138 0.320 -0.097 0.430 -0.082 0.800 -0,125

0.960 -0.063 0.340 -0.091 0.440 -0.063 0.830 -0.149

0.350 -0.097** 0.460 -0.082 0.900 -0.050

0.370 -0.077 0.490 -0.055 0.960 -0.047

0.380 -0.090 0.500 -0.088

0.400 -0.049 0.520 -0.087

0.410 -0.086 0.540 -0.080

0.430 -0.071 0.550 -0.048

0.440 -0,070 0.580 -0.061

0.460 -0.079 0.600 -0.081

0.470 -0.087 0.610 -0.095

0.490 -0.079 0.650 1.920"*

0.500 -0.092 0.700 -0.152

0.520 -0.092 0.750 -0.162

0.530 -0.097 0.820 -0.206

0,550 -0.121 0.890 -0.246

0.560 -0.121 0.900 -0.188

0.580 -0.107 0.960 -0.065

0.590 -0.136

0.600 -0.138

0.640 -0.153

0.700 -0.171

0.750 -0.047**

0.820 -0.134

0.870 -0.162

0,930 -0.028

0.960 0.008

Lower Surface

0.020 -0.078 0.020 -0.032 0.020 0.070 0.020 0.140

0.110 -0.129 0.060 -0.011 0.060 0.068 0.060 -0.546

0.230 -0.134 0.090 -0.126 0.090 1.500"* 0.110 -0.071

0.400 -0.207 0.120 -0.111 0.120 -0,126 0.250 -0.035

0.490 -0.206 0.200 -0.089 0.200 -0.091 0.400 -0.097

0.630 1.876** 0.260 -0.130 0.250 -0.115 0A90 -0.142

0.750 -0.023 0.400 -0.1 44 0.400 -0.160 0.580 -0.191

0.850 0.012 0.490 -0.198 0.490 -0.058 0.650 -0.148

0.900 0.043 0.580 -0.257 0.580 -0,228 0.750 -0.160

0.960 0.034 0.640 -0.075 0.650 -0.055 0.830 -0.046

0.750 0.039 0.750 -0.005 0.900 0.026

0.870 0.060 0,890 0.067 0.960 -0.042

0.930 0,072 0.930 0.040

0.960 0.047 0.960 1.220"*

517
Table H-2. Continued.

Flight 217, Wing sweep = 58 °, Time = 11-5-17-500, MINF = 1.227, Camber = 0/2, ALPT = 3.56, BETA = 0.34, QINF = 611.8,

RNPU = 4.0E+06

11 = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.444 0.000 0.226 0.000 3.952" * 0.010 -0.407

0.060 -0,459 0.020 -0,476 0.020 -0.463 0.020 -0.458

0.110 -0.167 0,040 -0,433 0,060 -0,906** 0.060 -0.394

0.200 -0.097 0,060 -0.451 0.090 -0.394 0.110 -0.299

0.230 -0.069 0.090 -0.411 0.110 -0,357 0,140 -0.261

0,400 -0,078 0.130 -0,263 0.130 -0.265 0.190 -0.949**

0.490 -0.107 0.150 -0.191 0. ! 50 -0.244 0.250 -0.196

0.590 -0.137 0.200 -0,143 0.210 -0.228 0.400 -0.095

0.630 -0.159 0.250 -0.108 0.250 -0.105 0.490 -0,068

0.700 -0.159 0.260 -0,090 0,340 -0.089 0,580 -0.052

0.750 -0.238 0.280 -0.110 0.370 -0.100 0.650 -0.103

0.8 t 0 -0.250 0.290 -0.100 0.400 -0.086 0,700 -0.090

0,840 -0.236 0.310 -0.099 0.410 1.246 ** 0.750 -0. I 15

0.900 -0.136 0.320 -0.107 0.430 -0.101 0.800 -0.124

0.960 -0,075 0.340 -0.109 0,440 -0.088 0.830 -0.162

0,350 -0.085 ** 0.460 -0.097 0,900 -0.055

0.370 -0,098 0.490 -0.075 0.960 -0.052

0.380 -0.110 0.500 -0.101

0,400 -0.072 0.520 -0.108

0.410 -0.103 0.540 -0.087

0.430 -0.092 0,550 -0.075

0.440 -0.074 0.580 -0.071

0.460 -0,092 0.600 -0.100

0,470 -0,098 0.610 -0.105

0.490 -0.095 0,650 1.896**

0.500 -0.104 0.700 -0.163

0.520 -0.131 0.750 -0.189

0.530 -0.111 0.820 -0.224

0.550 -0.113 0.890 -0.258

0.560 -0.134 0,900 -0.193

0.580 -0. l 18 0.960 -0.065

0.590 -0.138

0.600 -0.153

0.640 -0.167

0.700 -0.184

0,750 -0,050**

0.820 -0,147

0.870 -0.168

0,930 -0,033

0.960 -0.001

Lower Surface

0.020 -0.024 0.020 0,006 0.020 0.083 0.020 0.171

0.110 -0.108 0.060 0.002 0.060 0.084 0.060 -0.519

0.230 -0.115 0.090 -0.095 0.090 1,480"* 0.110 -0,045

0.400 -0. 179 0.120 -0.042 0.120 -0.109 0.250 -0.027

0.490 -0.184 0,200 -0,065 0,200 -0,092 0.400 -0,080

0.630 1.852"* 0.260 -0.100 0.250 -0,098 0,490 -0.121

0,750 -0.057 0.400 -0.138 0.400 -0.136 0,580 -0.171

0,850 -0.016 0.490 -0.183 0,490 -0.053 0.650 -0.144

0.900 0.022 0.580 -0.223 0.580 -0.192 0,750 -0.133

0.960 0.020 0.640 -0.048 0.650 -0,059 0,830 -0.033

0,750 0.047 0.750 0.013 0.900 0,042

0.870 0.071 0.890 0.078 0,960 -0,047

0.930 0.072 0.930 0.047

0.960 0.050 0,960 1.203**

518
Table H-2. Continued.

Flight 217, Wing sweep = 58 °, Time = 11-5-18-500, MINF = 1,227, Camber = 0/2, ALPT = 4.60, BETA = 0.31, QINF = 614.8.

RNPU = 4.0E+06

r 1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 -0.511 0.000 0,200 0.000 3.929 ** 0.010 -0.490

0.060 -0,497 0.020 -0.551 0.020 -0.523 0.020 -0.510

0.110 -0.462 0.040 -0.491 0.060 -0.905"* 0.060 -0.457

0,200 -0.173 0.060 -0.523 0.090 -0.487 0.110 -0.382

0.230 -0.017 0.090 -0.484 0.110 -0.503 0.140 -0.289

0.400 -0.074 0.130 -0.478 0.130 -0.429 0.190 -0.948 **

0.490 -0.074 0.150 -0.460 0.150 -0.316 0.250 -0.216

0.590 -0.127 0.200 -0.328 0,2 l0 -0.307 0.400 -0.122

0,630 -0.144 0.250 -0.142 0.250 -0.154 0.490 -0.1 04

0.700 -0.147 0.260 -0.123 0.340 -0.114 0.580 -0.083

0.750 -0.237 0,280 -0.127 0.370 -0.118 0,650 -0.145

0,810 -0,235 0.290 -0.127 0.400 -0.099 0.700 -0.108

0.840 -0.242 0.310 -0.119 0.410 1.236"* 0,750 -0.126

0.900 -0.142 0.320 -0.127 0.430 -0.146 0.800 -0.132

0.960 -0.133 0.340 -0.125 0.440 -0.111 0.830 -0.188

0.350 -0.096"* 0.460 -0.119 0.900 -0.058

0.370 -0.113 0.490 -0.122 0.960 -0.051

0.380 -0.128 0.500 -0.127

0,400 -0,054 0,520 -0.128

0.410 -0.122 0,540 -0.117

0.430 -0.109 0,550 -0.096

0.440 -0.091 0.580 -0.087

0,460 -0.109 0.600 -0.120

0.470 -0.132 0.610 -0.131

0,490 -0.114 0.650 1.883"*

0.500 -0.117 0.700 -0.180

0.520 -0,126 0.750 -0,208

0.530 -0.127 0.820 -0.245

0.550 -0.151 0.890 -0.277

0.560 -0.151 0.900 -0.196

0.580 -0.147 0.960 -0.087

0.590 -0.158

0.600 -0.163

0.640 -0.185

0.700 -0.203

0.750 -0.051 **

0.820 -0.156

0.870 -0.174

0.930 -0,040

0.960 -0.008

Lower Surface

0.020 -0.017 0.020 0,049 0.020 0.113 0.020 0.207

0.1 l0 -0,075 0.060 0.037 0.060 0.110 0.060 -0.493

0.230 -0.08 t 0.090 -0,047 0.090 1.469"* 0.110 -0.025

0.400 -0.140 0.120 -0.051 0.120 -0.085 0.250 -0.014

0.490 -0.175 0.200 -0.033 0,200 -0,072 0,400 -0.066

0.630 1,840"* 0.260 -0.079 0.250 -0.069 0.490 -0.105

0.750 -0.065 0.400 -0.115 0.400 -0.119 0.580 -0.151

0.850 -0.040 0.490 -0.156 0.490 -0.052 0.650 -0.127

0.900 -0.005 0.580 -0.212 0,580 -0.184 0.750 -0.092

0.960 -0.010 0.640 -0.018 0.650 -0.114 0.830 -0.038

0.750 0.047 0.750 0.035 0.900 0.058

0.870 0.071 0.890 0.085 0.960 -0.050

0,930 0.071 0.930 0.056

0.960 0,041 0.960 1.194"*

519
Table H-2. Continued.

Flight 217, Wing sweep = 58 °, Time = 11-5-19-500, MINF = 1.228, Camber = 0/2, ALPT = 5.85, BETA = 0.28, QINF = 617.9,

RNPU = 4,0E+06

11= 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,684 0.000 0.041 0.000 3.905"* 0.010 -0.682

0.060 -0.681 0.020 -0.726 0.020 -0.711 0.020 -0.702

0.110 -0.680 0.040 -0.686 0.060 -0.904** 0.060 -0.619

0.200 -0.623 0.060 -0.694 0.090 -0.669 0.110 -0.594

0.230 -0.327 0,090 -0.607 0. I 10 -0,706 0.140 -0.479

0.400 -0.209 0.130 -0.655 0.130 -0,594 0.190 -0.947**

0.490 -0.207 0.150 -0.648 0.150 -0,620 0.250 -0.307

0.590 -0.238 0.200 -0.613 0.210 -0.550 0.400 -0,269

0.630 -0.244 0.250 -0.409 0.250 -0.328 0.490 -0.222

0.700 -0.255 0.260 -0.373 0.340 -0.425 0.580 -0.214

0,750 -0.347 0.280 -0.358 0.370 -0.211 0.650 -0.246

0.810 -0.351 0.290 -0.324 0.400 -0.190 0.700 -0.237

0.840 -0.517 0.310 -0.297 0,410 1.226"* 0.750 -0.261

0.900 -0.244 0.320 -0.302 0.430 -0.261 0.800 -0.307

0.960 -0.133 0.340 -0.278 0.440 -0.250 0.830 -0.319

0.350 -0.209** 0.460 -0.259 0.900 -0.061

0.370 -0.250 0.490 -0.232 0.960 -0.112

0.380 -0.206 0.500 -0.263

0.400 -0.215 0.520 -0.210

0.410 -0.256 0.540 -0.257

0.430 -0,245 0.550 -0,239

0,440 -0,230 0.580 -0.183

0.460 -0.407 0.600 -0.263

0.470 -0.258 0.610 -0.274

0.490 -0.193 0,650 1.870**

0.500 -0.252 0.700 -0.314

0.520 -0.262 0.750 -0.356

0.530 -0.265 0.820 -0.392

0.550 -0.286 0.890 -0.438

0.560 -0.288 0.900 -0.342

0.580 -0.276 0.960 -0.236

0.590 -0.236

0.600 -0.300

0.640 -0.319

0.700 -0.340

0,750 -0.165"*

0.820 -0.278

0.870 -0.248

0.930 -0.157

0.960 -0.138

Lower Surface

0.020 -0.087 0.020 -0.016 0.020 0.033 0.020 0.120

0.110 -0.154 0.060 -0.044 0.060 0.021 0.060 -0.587

0.230 -0.162 0.090 -0.138 0.090 1.458"* 0. 110 -0.051

0.400 -0.255 0.120 -0.122 0.120 -0. l 12 0.250 -0.057

0.490 -0.288 0.200 -0.124 0.200 -0.166 0.400 -0.163

0.630 1.827'* 0.260 -0.157 0.250 -0.158 0.490 -0.199

0.750 -0.171 0.400 -0.205 0.400 -0.144 0.580 -0.249

0.850 -0.205 0.490 -0.245 0.490 -0.324 0.650 -0.169

0.900 -0.128 0.580 -0.315 0.580 -0.275 0.750 -0.337

0.960 -0.069 0.640 -0.097 0.650 -0.221 0.830 -0.145

0.750 -0.039 0.750 -0.006 0.900 -0.080

0.870 -0.029 0.890 -0.019 0.960 -0.325

0.930 -0.045 0.930 -0.051

0.960 -0.082 0.960 1.184"*

52O
Table H-2. Cominued.

Flight 217, Wing sweep = 58 °, Time = 11-5-20-500, MINF = 1.226, Camber = 0/2, ALPT = 6.83, BETA = 0.31, QINF = 618.7.

RNPU = 4.0E÷06

rI = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.603 0.000 O. 126 0.000 3.897 * * 0.010 -0.609

0.060 -0.593 0.020 -0.721 0.020 -0.645 0.020 -0.615

O. 110 -0.556 0.040 -0.595 0.060 -0.907** 0.060 -0.546

0.200 -0.541 0.060 -0.600 0.090 -0.595 O.110 -0.518

0.230 -0.491 0.090 -0.577 O.110 -0.618 O.140 -0.424

0.400 -0.166 O.130 -0.578 O.130 -0.576 O. 190 -0.950"*

0.490 -0.101 0.150 -0.573 O.150 -0.557 0.250 -0.272

0.590 -0.111 0.200 -0.539 0.210 -0.548 0.400 -0.173

0.630 -0.118 0.250 -0.359 0.250 -0.282 0.490 -0.217

0.700 -0.137 0.260 -0.325 0.340 -0.169 0.580 -0.086

0.750 -0.219 0.280 -0.330 0.370 -0.173 0.650 -0.137

0.810 -0.217 0.290 -0.306 0.400 -0.139 0.700 -0.118

0.840 -0.224 0.310 -0.285 0.410 1.221 ** 0.750 -0.155

0.900 -0.107 0.320 -0.284 0.430 -0.159 0.800 -0.145

0.960 -0.054 0.340 -0.260 0.440 -0.139 0.830 -0.211

0.350 -0.133"* 0.460 -0.151 0.900 -0.048

0.370 -0.201 0.490 -0.130 0.960 -0.042

0.380 -0.198 0.500 -0.162

0.400 -0.134 0.520 -0.159

0.410 -0.146 0.540 -0.159

0.430 -0.122 0.550 -0.139

0.440 -0.122 0.580 -0.132

0.460 -0.143 0.600 -0.168

0.470 -0.150 0.610 -0.166

0.490 -0.131 0.650 1.864**

0.500 -0. 155 0.700 -0.208

0.520 -0.146 0.750 -0.245

0.530 -0.153 0.820 -0.295

0.550 -0.180 0.890 -0.335

0.560 -0.183 0.900 -0.243

0.580 -0.165 0.960 -0.128

0.590 -0.180

0.600 -0.193

0.640 -0.215

0.700 -0.236

0.750 -0.038**

0.820 -0.149

0.870 -0.098

0.930 -0.039

0.960 -0.029

Lower Surface

0.020 0.071 0.020 O. 129 0.020 O. 182 0.020 0.268

O. 110 0.002 0.060 O. 104 0.060 O. 157 0.060 -0.402

0.230 -0.020 0.090 0.014 0.090 1.453"* O. 110 O. 151

0.400 -0.128 O. 120 0.024 O. 120 -0.029 0.250 0.025

0.490 -0.154 0.200 0.028 0.200 -0.019 0.400 -0.028

0.630 1.821 ** 0.260 -0.006 0.250 -0.013 0.490 -0.056

0.750 -0.048 0.400 -0.063 0.400 -0.061 0.580 -0.108

0.850 -0.028 0.490 -0.093 0.490 -0.327 0.650 -0.086

0.900 -0.003 0.580 -0.178 0.580 -0.134 0.750 -0.052

0.960 0.001 0.640 0.039 0.650 -0.224 0.830 -0.016

0.750 0.094 0.750 0.076 0.900 0.045

0.870 0.098 0.890 0.108 0.960 -0.040

0.930 0.073 0.930 0.086

0.960 0.042 0.960 1.179"*

521
Table H-2. Continued.

Flight 217, Wing sweep = 58 °, Time = 11-5-21-500, MINF = 1.225, Camber = 0/2, ALPT = 7.64, BETA = 0.28, QINF = 618.8,

RNPU = 4.0E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.656 0.000 0.107 0.000 3.893"* 0.010 -0.611

0.060 -0.627 0.020 -0.686 0.020 -0.672 0.020 -0.662

0.110 -0.637 0.040 -0.638 0.060 -0.910 ** 0.060 -0.619

0.200 -0.590 0.060 -0.649 0.090 -0.635 0.110 -0.529

0.230 -0.520 0.090 -0.615 0.110 -0.661 0.140 -0.441

0.400 -0.249 0.130 -0.590 0.130 -0.621 0.190 -0.953"*

0.490 -0.187 0.150 -0.601 0.150 -0.598 0.250 -0.268

0.590 -0.146 0.200 -0.573 0.210 -0.563 0.400 -0.203

0.630 -0.133 0.250 -0.395 0,250 -0.348 0.490 -0.267

0.700 -0.139 0.260 -0.361 0.340 -0.212 0.580 -0.109

0.750 -0.218 0.280 -0.375 0.370 -0.181 0.650 -0.146

0.810 -0.216 0.290 -0.365 0.400 -0.135 0.700 -0.131

0,840 -0.222 0.310 -0.346 0.410 1.218"* 0.750 -0.158

0.900 -0.094 0.320 -0.354 0.430 -0.159 0,800 -0.162

0.960 -0.048 0.340 -0.348 0.440 -0.162 0.830 -0.210

0.350 -0.171 ** 0.460 -0.169 0.900 -0.045

0.370 -0.309 0.490 -0.141 0.960 -0.045

0.380 -0.322 0.500 -0.186

0,400 -0.260 0.520 -0.183

0.410 -0,262 0.540 -0.186

0.430 -0.212 0.550 -0.163

0.440 -0.177 0,580 -0,141

0.460 -0.191 0.600 -0.178

0.470 -0.187 0.610 -0.179

0.490 -0.161 0.650 1.861 **

0.500 -0.153 0.700 -0.215

0.520 -0.1 64 0.750 -0.259

0.530 -0.165 0.820 -0.322

0,550 -0.177 0.890 -0.344

0.560 -0.175 0.900 -0.268

0.580 -0.1 64 0.960 -0.141

0.590 -0.175

0,600 -0.190

0.640 -0,219

0.700 -0.238

0.750 -0.032"*

0.820 -0.121

0.870 -0.067

0.930 -0.040

0.960 -0.037

Lower Surface

0.020 0.094 0,020 0.150 0,020 0.216 0.020 0.296

0.110 0.019 0.060 0.139 0.060 0.196 0.060 -0.363

0.230 0.013 0.090 0,044 0.090 1.450"* 0.110 0.158

0,400 -0.117 0.120 0.058 0.120 0.005 0.250 0.028

0.490 -0.114 0.200 0.065 0.200 0.017 0.400 0.005

0.630 1.818"* 0.260 0.009 0.250 0.012 0.490 -0.037

0.750 -0.039 0.400 -0.036 0.400 -0.038 0.580 -0,091

0.850 -0.015 0.490 -0.085 0.490 -0.035 0.650 -0,060

0.900 0.007 0.580 -0.171 0.580 -0.109 0.750 -0.026

0.960 0.009 0.640 0.068 0.650 -0.227 0.830 0.000

0.750 0.111 0.750 0.091 0.900 0.048

0.870 0.106 0.890 0.123 0.960 -0.026

0.930 0.072 0.930 0.073

0.960 0.035 0.960 1.176"*

522
Table H-2. Continued,

Flight 217. Wing sweep = 58 °, Time = 11-5-22-500, MINF = 1.220, Camber = 0/2. ALPT = 8.44. BETA = 0.34. QINF = 616.2.

RNPU = 4.0E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.708 0.000 0.067 0.000 3.907** 0.010 -0.671

0.060 -0.668 0.020 -0.733 0.020 -0.719 0.020 -0.71 l

0.110 -0.656 0.040 -0.687 0.060 -0.916"* 0.060 -0.662

0.200 -0.626 0.060 -0.684 0.090 -0.671 0. l I 0 -0.541

0.230 -0.385 0.090 -0.663 0.110 -0.699 0.140 -0.470

0.400 -0.318 0.130 -0.653 0.130 -0.658 0.190 -0.959"*

0.490 -0.288 O. 150 -0.649 O. 150 -0.635 0.250 -0.306

0.590 -0.249 0.200 -0.624 0.210 -0.463 0.400 -0.244

0.630 -0.215 0.250 -0.431 0.250 -0.412 0.490 -0.360

0.700 -0.190 0.260 -0.398 0.340 -0.336 0.580 -0. 146

0.750 -0.215 0.280 -0.411 0.370 -0.266 0.650 -0.149

0.810 -0.205 0.290 -0.403 0.400 -0.170 0.700 -0.145

0.840 -0.205 0.310 -0.394 0.410 1.221 ** 0.750 -0.170

0.900 -0.100 0.320 -0.404 0.430 -0.158 0.800 -0.158

0.960 -0.052 0.340 -0.412 0.440 -0.155 0.830 -0.223

0.350 -0.214"* 0.460 -0.177 0.900 -0.061

0.370 -0.385 0.490 -0.143 0.960 -0.037

0.380 -0.410 0.500 -0.187

0.400 -0.352 0.520 -0.200

0.410 -0.378 0.540 -0.182

0.430 -0.344 0.550 -0.172

0.440 -0.312 0.580 -0.175

0.460 -0.322 0.600 -0.193

0.470 -0.308 0.610 -0.202

0.490 -0.283 0.650 1.866**

0.500 -0.263 0.700 -0.262

0.520 -0.264 0.750 -0.298

0.530 -0.241 0.820 -0.386

0.550 -0.228 0.890 -0.374

0.560 -0.232 0.900 -0.272

0.580 -0.207 0.960 -0.14 I

0.590 -0.203

0.600 -0.212

0.640 -0.221

0.700 -0.240

0.750 -0.049**

0.820 -0.110

0.870 -0.071

0.930 -0.039

0.960 -0.039

Lower Surface

0.020 0.119 0.020 0.163 0.020 0.239 0.020 0.338

0.110 0.035 0.060 0.145 0.060 0.201 0.060 -0.377

0.230 0.033 0.090 0.054 0.090 1.453"* 0.110 0.133

0.400 -0.134 0.120 0.089 0.120 0.014 0.250 0.038

0.490 -0.023 0.200 0.085 0.200 0.004 0.400 0.013

0.630 1.823"* 0.260 0.024 0.250 0.042 0.490 -0.025

0.750 -0.051 0.400 -0.016 0.400 -0.025 0.580 -0.084

0.850 -0.026 0.490 -0.093 0.490 -0.041 0.650 -0.059

0.900 0.004 0.580 -0.180 0.580 -0.105 0.750 -0.023

0.960 0.001 0.640 0.071 0.650 -0.231 0.830 -0.017

0.750 0.117 0.750 0.089 0.900 0.035

0.870 0.090 0.890 0.121 0.960 -0.043

0.930 0.054 0.930 0.096

0.960 0.015 0.960 1.178"*

523
Table H-2. Continued.

Flight 217, Wing sweep = 58 °, Time = 11-5-26-500, MINF = 1.195, Camber = 0/2, ALPT = 9.20, BETA = 0.31, QINF = 587.5,

RNPU = 3.8E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.205 0.000 -0.383 0.000 4.103"* 0.010 - 1.158

0.060 - I. 160 0.020 - 1.219 0.020 - 1.185 0.020 - 1.178

0.110 - 1.211 0.040 - 1.163 0.060 -0.956** 0.060 - 1.145

0.200 -0.920 0.060 -1.171 0.090 -1.138 0.110 -0.976

0.230 -0.881 0.090 -1.133 0.110 -1.169 0.140 -0.922

0.400 -0.814 0.130 -1.112 0.130 -1.049 0.190 -1.001"*

0.490 -0.786 0.150 -0.948 0.150 -0.951 0.250 -0.764

0.590 -0.771 0.200 -0.939 0.210 -0.936 0.400 -0.685

0.630 -0.717 0.250 -0.915 0.250 -0.887 0.490 -0.764

0.700 -0.665 0.260 -0.881 0.340 -0.852 0.580 -0.596

0.750 -0.618 0.280 -0.899 0.370 -0.766 0.650 -0.580

0.810 -0.608 0.290 -0.894 0.400 -0.556 0.700 -0.566

0.840 -0.611 0.310 -0.874 0.410 1.285"* 0.750 -0.588

0.900 -0.534 0.320 -0.880 0.430 -0.557 0.800 -0.580

0.960 -0.479 0.340 -0.882 0.440 -0.569 0.830 -0.638

0.350 -0.644** 0.460 -0.586 0.900 -0.473

0.370 -0.850 0.490 -0.561 0.960 -0.468

0.380 -0.884 0.500 -0.610

0.400 -0.830 0.520 -0.613

0.410 -0.856 0.540 -0.616

0.430 -0.843 0.550 -0.592

0.440 -0.792 0.580 -0.613

0.460 -0.834 0.600 -0.632

0.470 -0.833 0.610 -0.637

0.490 -0.800 0.650 1.962"*

0.500 -0.775 0.700 -0.694

0.520 -0.795 0.750 -0.744

0.530 -0.767 0.820 -0.846

0.550 -0.754 0.890 -0.778

0.560 -0.717 0.900 -0.696

0.580 -0.686 0.960 -0.555

0.590 -0.667

0.600 -0.643

0.640 -0.632

0.700 -0.656

0.750 -0.343**

0.820 -0.496

0.870 -0.477

0.930 -0.450

0.960 -0.437

Lower Surface

0.020 -0.276 0.020 -0.227 0.020 -0.145 0.020 -0.071

0. 110 -0.357 0.060 -0.238 0.060 -0.188 0.060 -0.814

0.230 -0.391 0.090 -0.334 0.090 1.529"* 0.110 -0.267

0.400 -0.469 0.120 -0.326 0.120 -0.364 0.250 -0.365

0.490 -0.412 0.200 -0.313 0.200 -0.376 0.400 -0.399

0.630 1.917"* 0.260 -0.378 0.250 -0.356 0.490 -0.410

0.750 -0.453 0.400 -0.444 0.400 -0.434 0.580 -0.471

0.850 -0.445 0.490 -0.514 0.490 -0.458 0.650 -0.457

0.900 -0.399 0.580 -0.452 0.580 -0.517 0.750 -0.441

0.960 -0.410 0.640 -0.318 0.650 -0.465 0.830 -0.416

0.750 -0.292 0.750 -0.310 0.900 -0.358

0.870 -0.340 0.890 -0.288 0.960 -0.448

0.930 -0.347 0.930 -0.302

0.960 -0.384 0.960 1.241 **

524
Table H-2. Continued.

Flight 217, Wing sweep = 58", Time = 11-7-27-500, MINF = 1.185, Camber = 2/1, ALPT = 5.52, BETA = 0.34, QINF = 573.8,

RNPU = 3.8E+06

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP xA. CP

0.020 -0.518 0.000 0.201 0.000 4.208"* 0.010 -0.528

0.060 -0.480 0.020 -0.557 0.020 -0.535 0.020 -0.534

O. 110 -0.451 0.040 -0.476 0.060 -0.972"* 0.060 -0.499

0.200 -0.228 0.060 -0.519 0.090 -0.501 O. 110 -0.432

0.230 -0.151 0.090 -0.495 0.110 -0.533 O. 140 -0.340

0.400 -0.121 0.130 -0.498 0.130 -0.515 0.190 -1.018"*

0.490 -0.130 0.150 -0.513 0.150 -0.501 0.250 -0.189

0.590 -0.161 0.200 -0.457 0.210 -0,331 0.400 -0.140

0.630 -0.175 0.250 -0.192 0.250 -0.157 0.490 -0.137

0.700 -0.169 0.260 -0.166 0.340 -0.141 0.580 -0.095

0.750 -0.202 0.280 -0.178 0.370 -0.151 0.650 -0.138

0.810 -0, 194 0.290 -0.157 0.400 -0.132 0.700 -0.128

0.840 -0.204 0.310 -0.154 0.410 1.323 ** 0.750 -0.146

0.900 -0.098 0.320 -0.169 0.430 -0.150 0.800 -0.158

0.960 -0.070 0.340 -0.162 0.440 -0,148 0.830 -0.206

0.350 -0.090"* 0.460 -0.149 0.900 -0.038

0.370 -0.149 0.490 -0.119 0.960 -0.042

0.380 -0.159 0.500 -0.161

0.400 -0.131 0.520 -0.159

0.410 -0.163 0.540 -0.141

0.430 -0.161 0.550 -0.121

0.440 -0.121 0.580 -0.130

0.460 -0.147 0.600 -0.164

0.470 -0.163 0.610 -0.163

0.490 -0.148 0.650 2.016"*

0.500 -0.160 0.700 -0.207

0.520 -0.154 0.750 -0,229

0.530 -0.167 0.820 -0.265

0.550 -0.202 0.890 -0.261

0.560 -0.191 0.900 -0,176

0.580 -0.172 0.960 -0.082

0.590 -0.192

0.600 -0.193

0.640 -0.217

0.700 -0.233

0.750 -0.040**

0.820 -0.136

0.870 -0.097

0.930 -0.039

0.960 -0.015

Lower Surface

0.020 -0.022 0.020 0.041 0.020 0.093 0.020 O.178

O. 110 -0.054 0.060 0.043 0.060 O. 117 0.060 -0.485

0.230 -0.057 0.090 -0.050 0.090 1.572"* O. 110 0.091

0.400 -0.182 O. 120 -0.021 O. 120 -0.076 0.250 -0.024

0.490 -0.206 0.200 -0.026 0.200 -0.043 0.400 -0.046

0.630 1.969"* 0.260 -0.041 0.250 -0.048 0.490 -0.087

0.750 -0.095 0.400 -0.088 0.400 -0.086 0.580 -0.145

0.850 -0.059 0.490 -0.143 0.490 -0.054 0.650 -0.125

0.900 -0.025 0.580 -0.232 0.580 -0.161 0.750 -0.087

0.960 -0.010 0.640 -0.005 0.650 -0.050 0.830 -0,015

0.750 0.063 0.750 0.042 0.900 0.093

0.870 0.053 0.890 0.055 0.960 -0.045

0.930 0.047 0.930 0.038

0.960 0.029 0.960 1.277"*

525
Table H-2. Continued.

Flight 2t8, Wing sweep = 58 °, Time = 10-23-32-500, MINF = 1.211, Camber = 0/2, ALPT = 4.52, BETA = 0.45, QINF = 587.2,

RNPU = 3.8E+06

1] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.515 0.000 0.220 0.000 4.125" * 0.010 -0.494

0.060 -0.507 0.020 -0.586 0.020 -0.527 0.020 -0,505

0.110 -0.466 0.040 -0.476 0.060 -2.039 ** 0.060 -0.435

0.200 -0.1 04 0.060 -0.530 0.090 -0.481 0.110 -0.323

0.230 -0.028 0.090 -0.482 0.110 -0.513 0.140 -0.274

0.400 -0.047 0.130 -0.470 0.130 -0.386 0.190 -0.975" *

0.490 -0.073 0.150 -0.391 0.150 -0.303 0.250 -0.183

0.590 -0.118 0.200 -0.230 0.210 -0.256 0.400 -0.095

0.630 -0.128 0,250 -0.117 0.250 -0.110 0.490 -0.077

0.700 -0.127 0.260 -0.082 0.340 -0.090 0.580 -0.041

0.750 -0.221 0.280 -0.091 0.370 -0.095 0.650 -0.091

0.810 -0.228 0.290 -0.102 0.400 -0.098 0.700 -0.081

0.840 -0.221 0.310 -0.093 0.410 - 1.045"* 0,750 -0.100

0.900 -0.111 0.320 -0.098 0.430 -0.099 0,800 -0.134

0.960 -0.056 0.340 -0.102 0.440 -0.091 0,830 -0.161

0.350 -0.073"* 0.460 -0.095 0.900 -0,017

0.370 -0.092 0.490 -0.065 0.960 -0.021

0,380 -0.115 0.500 -0.109

0.400 -0.063 0.520 -0.101

0.410 -0.103 0,540 -0.1 04

0.430 -0,087 0.550 -0.074

0.440 -0.063 0.580 -0.063

0.460 -0.101 0.600 -0.107

0.470 -0.096 0.610 -0.109

0.490 -0.095 0.650 1,082"*

0.500 -0.074 0.700 -0,156

0.520 -0.103 0.750 -0.198

0,530 -0.110 0.820 -0.226

0.550 -0.135 0.890 -0.244

0.560 -0.132 0.900 -0.156

0.580 -0.114 0.960 -0.055

0.590 -0.147

0.600 -0.145

0.640 -0.162

0.700 -0.187

0.750 -0.027**

0.820 -0.134

0.870 -0.136

0.930 -0.013

0.960 0.017

Lower Surface

0.020 -0.006 0,020 0.057 0.020 0.127 0.020 0.230

0.1 l0 -0.047 0.060 0.058 0.060 0.130 0.060 -0.495

0.230 -0.049 0.090 -0,034 0.090 0.581 * * 0.110 -0.015

0.400 -0.150 0.120 -0.019 0.120 -0.093 0.250 0.006

0.490 -0.178 0.200 -0.009 0.200 -0.067 0.400 -0.040

0.630 0.914"* 0.260 -0.061 0.250 -0.030 0.490 -0.089

0.750 -0,046 0.400 -0.098 0.400 -0.088 0.580 -0.134

0.850 -0.019 0.490 -0.139 0.490 -0.015 0.650 -0.109

0.900 0.020 0.580 -0.197 0.580 -0.154 0.750 -0.075

0.960 0.020 0.640 0.006 0.650 -0.029 0.830 -0,007

0.750 0.109 0.750 0.058 0.900 0.090

0.870 0.107 0.890 0.107 0.960 -0.027

0.930 0.096 0.930 0.073

0.960 0.072 0.960 - 1.089"*

526
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-23-35-000, MINF = 1.213, Camber = 0/2, ALPT = 3.57, BETA = 0.45, QINF = 588.8,

RNPU = 3.8E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.432 0.000 0.258 0.000 4.115"* 0.010 -0.386

0.060 -0.397 0.020 -0.505 0.020 -0.448 0.020 -0.460

0.110 -0.078 0.040 -0.415 0.060 -2.032** 0.060 -0.351

0.200 -0.078 0.060 -0.466 0.090 -0.353 0.110 -0.267

0.230 -0,044 0.090 -0.377 0.110 -0.311 0.140 -0.225

0.400 -0.056 0.130 -0.215 0.130 -0.236 0.190 -0.971 **

0.490 -0.063 0.150 -0.128 0.150 -0.204 0.250 -0.149

0.590 -0.117 0.200 -0.094 0.210 -0.191 0.400 -0.058

0.630 -0.129 0.250 -0.069 0.250 -0.054 0.490 -0.035

0.700 -0.129 0.260 -0.060 0,340 -0,047 0.580 -0.017

0.750 -0.214 0.280 -0.078 0.370 -0.067 0.650 -0.070

0.810 -0.208 0.290 -0,078 0,400 -0,059 0.700 -0,062

0.840 -0.212 0.310 -0.072 0.410 -1.041"* 0.750 -0.080

0.900 -0.1 04 0.320 -0.072 0.430 -0.068 0.800 -0.1 04

0.960 -0.037 0.340 -0.072 0.440 -0.049 0.830 -0.138

0.350 -0.049** 0.460 -0.066 0.900 -0.027

0.370 -0,063 0.490 -0.025 0.960 -0.020

0.380 -0.083 0.500 -0.073

0.400 -0.027 0.520 -0,067

0.410 -0.079 0.540 -0.061

0.430 -0.065 0.550 -0.044

0.440 -0.013 0.580 -0.063

0.460 -0.067 0.600 -0.070

0.470 -0.055 0,610 -0,079

0.490 -0.064 0,650 1.080"*

0.500 -0.076 0.700 -0.126

0.520 -0.106 0.750 -0.169

0.530 -0.082 0.820 -0.198

0.550 -0.117 0.890 -0.229

0.560 -0.102 0,900 -0.159

0.580 -0.092 0.960 -0.027

0.590 -0.120

0.600 -0.127

0.640 -0.136

0.700 -0.163

0.750 -0.015"*

0,820 -0.110

0.870 -0,135

0.930 0.003

0.960 0.036

Lower Surface

0.020 -0.049 0.020 0.025 0.020 0. I 15 0.020 0.208

O, 110 -0.079 0.060 0,030 0.060 O. 115 0.060 -0.504

0.230 -0.083 0.090 -0.067 0.090 0.580"* O.110 -0.017

0.400 -0. 157 0.120 -0.035 0.120 -0.107 0.250 -0.001

0.490 -0.161 0.200 -0.038 0.200 -0.072 0.400 -0.050

0.630 0.913"* 0.260 -0.078 0.250 -0.061 0.490 -0.096

0.750 -0.014 0.400 -0.105 0.400 -0.104 0.580 -0.137

0.850 0,028 0.490 -0.149 0.490 -0.018 0.650 -0.116

0.900 0.061 0.580 -0.196 0.580 -0.166 0.750 -0.109

0.960 0.058 0.640 -0.013 0.650 -0,039 0.830 0.001

0.750 0.083 0.750 0.043 0,900 0,070

0.870 0.111 0.890 0.106 0.960 -0.012

0.930 0.108 0.930 0.084

0.960 0.084 0.960 - 1.085**

527
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-23-38-500, MINF = 1.218, Camber = 0/2, ALPT = 2.78, BETA = 0.54, QINF = 596.0,

RNPU = 3.9E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.295 0.000 0.302 0.000 4.061"* 0.010 -0.374

0.060 -0.034 0.020 -0.400 0.020 -0.391 0.020 -0.409

O. 110 -0.050 0.040 -0.361 0.060 -2.011 ** 0.060 -0.322

0.200 -0.077 0.060 -0.270 0.090 -0.196 O. 110 -0.227

0.230 -0.034 0.090 -0.136 O.110 -0.224 O. 140 -0.200

0.400 -0.066 O.130 -0.143 O.130 -0.155 O. 190 -0.963 **

0.490 -0.084 O.150 -0.082 O.150 -0.172 0.250 -0.130

0.590 -0.112 0.200 -0.065 0.210 -0.179 0.400 -0.036

0.630 -0.122 0.250 -0.058 0.250 -0.027 0.490 0.000

0.700 -0.139 0.260 -0.035 0.340 -0.024 0.580 0.019

0.750 -0.206 0.280 -0.074 0.370 -0.051 0.650 -0.070

O.810 -0.202 0.290 -0.061 0.400 -0.040 0.700 -0.045

0.840 -0,195 0.310 -0.071 0.410 - 1.032'* 0.750 -0.082

0.900 -0.1 04 0.320 -0.065 0.430 -0.066 0.800 -0.099

0.960 -0.018 0.340 -0.069 0.440 -0.049 0.830 -0.141

0.350 -0.063** 0.460 -0.059 0.900 -0.014

0.370 -0.042 0.490 -0.006 0.960 -0.023

0.380 -0.064 0.500 -0.059

0.400 -0.012 0.520 -0.058

0.410 -0.065 0.540 -0.046

0.430 -0.054 0.550 -0.028

0.440 -0.017 0.580 -0.029

0.460 -0.045 0.600 -0.044

0.470 -0.060 0.610 -0.054

0,490 -0.051 0.650 1.064**

0.500 -0,055 0.700 -0.119

0.520 -0.062 0.750 -0.152

0.530 -0.061 0.820 -0.175

0.550 -0.094 0.890 -0.210

0.560 -0.088 0.900 -0.150

0.580 -0.077 0.960 -0.021

0.590 -0.102

0.600 -0.107

0.640 -0.121

0.700 -0.139

0.750 -0.013"*

0.820 -0.100

0.870 -0.133

0.930 0.010

0.960 0.043

Lower Surface

0.020 -0.059 0.020 0.001 0.020 0.098 0.020 O. 174

0.110 -0.111 0.060 0.006 0.060 0.101 0.060 -0.535

0.230 -0.116 0.090 -0,109 0.090 0.570* * O.110 -0.043

0.400 -0.172 O.120 -0.060 O.120 -0.119 0.250 -0.007

0.490 -0.174 0.200 -0.060 0.200 -0.078 0.400 -0.078

0.630 0.898"* 0.260 -0.117 0.250 -0.081 0.490 -0.102

0.750 0.009 0.400 -0.124 0.400 -0.128 0.580 -0.158

0.850 0.051 0.490 -0.167 0.490 -0.035 0.650 -0.140

0.900 0.082 0.580 -0.219 0.580 -0.200 0.750 -0.124

0.960 0.071 0.640 -0.048 0.650 -0.022 0.830 -0.009

0.750 0.080 0.750 0.013 0.900 0.061

0.870 O. 104 0.890 0.085 0.960 -0.015

0.930 O. 107 0.930 0.080

0.960 0.085 0.960 - 1.075* *

528
Table H-2. Continued.

Flight 218, Wing sweep = 58", Time = 10-23-43-500, MINF = 1.228, Camber = 0/2, ALPT = 6.60, BETA = 0.43, QINF = 620.2,

RNPU = 4.0E+06

r I = 0.93 0.76 0.59 040

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.577 0.000 0,158 0.000 3.881 ** 0.010 -0.567

0.060 -0.553 0.020 -0.717 0.020 -0.6 ! 5 0.020 -0.597

0.110 -0.550 0.040 -0.575 0.060 - 1.955"* 0.060 -0.524

0.200 -0.517 0,060 -0.593 0.090 -0.573 0.110 -0.477

0.230 -0.461 0.090 -0.554 0.110 -0.612 0.140 -0.386

0.400 -0.120 0,130 -0.553 0.130 -0.555 0.190 -0.948"*

0.490 -0.074 0.150 -0.547 0.150 -0.535 0.250 -0.244

0.590 -0,086 0.200 -0.509 0.210 -0.517 0.400 -0.149

0.630 -0.094 0.250 -0.350 0.250 -0.243 0.490 -0.183

0.700 -0.105 0.260 -0.291 0.340 -0.148 0.580 -0.070

0.750 -0.203 0.280 -0.289 0.370 -0.152 0,650 -0.114

0,810 -0.206 0.290 -0.268 0.400 -0.143 0.700 -0.107

0.840 -0.203 0.310 -0.242 0.410 -1.014"* 0.750 -0.131

0.900 -0.092 0.320 -0.246 0.430 -0.134 0.800 -0.134

0.960 -0.042 0.340 -0.209 0.440 -0.120 0.830 -0.183

0.350 -0.116"* 0.460 -0.131 0.900 -0.034

0.370 -0.151 0.490 -0.098 0.960 -0,025

0.380 -0.159 0.500 -0.137

0.400 -0.097 0.520 -0.129

0.410 -0.130 0,540 -0.125

0.430 -0.111 0.550 -0.112

0.440 -0.087 0.580 -0.111

0.460 -0.119 0.600 -0.136

0.470 -0.123 0.610 -0.142

0.490 -0.117 0.650 1.000"*

0.500 -0.102 0.700 -0.182

0.520 -0.132 0.750 -0,228

0,530 -0.131 0,820 -0.268

0.550 -0.164 0.890 -0.315

0.560 -0.147 0.900 -0.205

0.580 -0.147 0.960 -0.112

0.590 -0.164

0.600 -0.172

0.640 -0.189

0,700 -0.210

0.750 -0.019"*

0,820 -0.137

0.870 -0.084

0.930 -0.018

0.960 -0.003

Lower Surface

0.020 0.062 0.020 0.144 0.020 0.198 0.020 0.291

0.110 0.013 0.060 0.119 0.060 0.183 0.060 -0.420

0.230 -0.005 0.090 0.032 0.090 0.525** 0.110 0.161

0.400 -0.112 0.120 0.032 0.120 -0.027 0.250 0.035

0.490 -0.144 0.200 0.04 1 0.200 -0.018 0.400 -0.007

0.630 0.841 ** 0.260 0.001 0.250 -0.001 0.490 -0.042

0.750 -0.029 0.400 -0.048 0,400 -0.04 1 0.580 -0.086

0.850 -0.008 0.490 -0.081 0.490 -0.018 0.650 -0.069

0.900 0.021 0.580 -0.174 0.580 -0.120 0.750 -0.026

0.960 0.018 0.640 0.057 0.650 -0.025 0.830 0.009

0.750 0.107 0.750 0.093 0.900 0.058

0.870 0.114 0.890 0.128 0.960 -0.018

0.930 0.103 0.930 0.097

0.960 0.062 0.960 - 1.056"*

529
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-23-44-500, MINF = 1.227, Camber = 0/2, ALPT = 7.86, BETA = 0.45, QINF = 622.6,

RNPU = 4.0E+06

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.643 0.000 0.132 0.000 3.860* * 0.010 -0.616

0,060 -0.606 0.020 -0.697 0.020 -0.654 0,020 -0.646

O. 110 -0.590 0.040 -0.628 0.060 - 1.953"* 0.060 -0.584

0.200 -0.565 0.060 -0.635 0.090 -0.613 0.110 -0.528

0.230 -0.451 0.090 -0.598 O.110 -0.648 O. 140 -0.427

0.400 -0.232 0.130 -0.590 0.130 -0.607 O. 190 -0.949"*

0.490 -0.187 O.150 -0.588 O.150 -0.577 0.250 -0.269

0.590 -0.146 0.200 -0.553 0.210 -0.569 0.400 -0.180

0.630 -0.113 0.250 -0.389 0.250 -0.328 0.490 -0.260

0.700 -0.113 0.260 -0.340 0.340 -0.205 0.580 -0.071

0.750 -0.192 0.280 -0.355 0.370 -0.162 0.650 -0.117

0.810 -0.197 0.290 -0.341 0.400 -0.102 0.700 -0.103

0.840 -0.183 0.310 -0.328 0.410 - 1.015"* 0.750 -0.132

0.900 -0.062 0.320 -0.333 0.430 -0.150 0.800 -0.135

0.960 -0.021 0.340 -0.328 0.440 -0. t 31 0.830 -0.193

0.350 -0.169** 0.460 -0.144 0.900 -0.023

0.370 -0.294 0.490 -0.115 0.960 -0.030

0.380 -0.318 0.500 -0.155

0.400 -0.252 0.520 -0.153

0.410 -0.267 0.540 -0.149

0.430 -0.220 0.550 -0.121

0.440 -0.190 0.580 -0.127

0.460 -0.184 0.600 -0.156

0.470 -0.180 0.610 -0.156

0.490 -0.152 0.650 0.991 **

0.500 -0.151 0.700 -0.190

0.520 -0.149 0.750 -0.245

0.530 -0.139 0.820 -0.307

0.550 -0.155 0.890 -0.325

0.560 -0.150 0.900 -0.244

0.580 -0.145 0.960 -0.124

0.590 -0.155

0.600 -0.172

0.640 -0.186

0.700 -0.215

0.750 -0.007"*

0.820 -0.097

0.870 -0.044

0.930 -0.020

0.960 -0.010

Lower Surface

0.020 O. 110 0.020 O. 184 0.020 0.244 0.020 0.340

O. 110 0.056 0.060 0.167 0.060 0.223 0.060 -0.325

0.230 0.045 0.090 0.074 0.090 0.518"* 0.110 O. 189

0.400 -0.087 O. 120 0.076 O. 120 0.010 0.250 0.059

0.490 -0.099 0.200 0.095 0.200 0.032 0.400 0.033

0.630 0.832** 0.260 0.044 0.250 0.049 0.490 -0.001

0.750 -0.002 0.400 -0.010 0.400 -0.003 0.580 -0.053

0.850 0.010 0.490 -0.061 0.490 -0.006 0.650 -0.035

0.900 0.045 0.580 -0.147 0.580 -0.084 0.750 -0.004

0.960 0.036 0.640 0.095 0.650 -0.034 0.830 0.021

0.750 0.142 0.750 O, 119 0.900 0.072

0.870 O. 127 0.890 O. 147 0.960 -0.006

0.930 0.109 0.930 0.119

0.960 0.062 0.960 - 1.057"*

530
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-23-45-000, MINF = 1.226, Camber = 0/2, ALPT = 8.42, BETA = 0.45, QINF = 622.9,

RNPU = 4.0E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.690 0.000 0.109 0,000 3.856"* 0.010 -0.659

0.060 -0.641 0.020 -0.728 0.020 -0.686 0.020 -0.678

O. 110 -0.624 0.040 -0.655 0.060 - 1.954 ** 0.060 -0.657

0.200 -0.601 0.060 -0.677 0.090 -0.645 0.110 -0.526

0.230 -0.481 0.090 -0.631 0. 110 -0.686 0.140 -0.448

0.400 -0.286 0.130 -0.618 0.130 -0.642 0.190 -0.951 **

0.490 -0.249 0.150 -0.619 0.150 -0.614 0.250 -0.281

0.590 -0.220 0.200 -0.590 0.210 -0,497 0,400 -0.213

0.630 -0.188 0.250 -0.414 0.250 -0.372 0.490 -0.331

0.700 -0.156 0.260 -0.379 0.340 -0.304 0.580 -0.099

0.750 -0.186 0.280 -0.393 0.370 -0.235 0.650 -0.125

0.810 -0.182 0.290 -0.381 0,400 -0.151 0.700 -0.113

0,840 -0,174 0.310 -0.369 0.410 -1.017"* 0.750 -0.141

0.900 -0.077 0.320 -0.368 0.430 -0.146 0.800 -0.148

0.960 -0.034 0.340 -0.375 0.440 -0.139 0.830 -0.191

0.350 -0.184"* 0.460 -0.153 0.900 -0.032

0.370 -0.345 0.490 -0.117 0.960 -0.032

0.380 -0.379 0.500 -0.165

0.400 -0.318 0.520 -0.162

0.410 -0.348 0.540 -0.162

0.430 -0.316 0.550 -0.140

0.440 -0.275 0,580 -0.148

0.460 -0.300 0.600 -0.171

0.470 -0.292 0.610 -0.169

0.490 -0.247 0,650 0.988"*

0.500 -0.245 0.700 -0.221

0.520 -0.229 0.750 -0,272

0.530 -0.208 0.820 -0.357

0.550 -0.202 0.890 -0.352

0.560 -0.183 0.900 -0.254

0.580 -0.167 0.960 -0.118

0.590 -0.180

0.600 -0.175

0.640 -0. 197

0.700 -0.222

0.750 -0.018"*

0.820 -0.088

0.870 -0.044

0.930 -0,022

0.960 -0,014

Lower Surface

0.020 0.102 0.020 0.185 0.020 0.250 0.020 0.364

0.110 0.063 0.060 0.185 0.060 0.223 0.060 -0.320

0.230 0.060 0.090 0.081 0,090 0,515"* 0.110 0.176

0,400 -0.093 0.120 0.077 0.120 0.022 0.250 0.062

0,490 -0.030 0.200 0.109 0.200 0.026 0.400 0.038

0.630 0,829** 0.260 0.042 0.250 0.067 0.490 0.004

0.750 -0.024 0.400 0,001 0,400 -0.002 0.580 -0.051

0.850 0,004 0.490 -0.068 0.490 -0.019 0,650 -0,028

0.900 0.039 0,580 -0.152 0.580 -0.087 0.750 -0.008

0.960 0,028 0.640 0,096 0.650 -0.026 0.830 0.019

0.750 0.142 0.750 0.113 0.900 0.065

0.870 0.120 0.890 0.144 0.960 -0.015

0.930 0.087 0.930 0.117

0.960 0.047 0.960 - 1.059"*

531
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-23-46-000, MINF = 1.222, Camber = 0/2, ALPT = 9.47, BETA = 0.45, QINF : 621.6,

RNPU = 4.0E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.740 0.000 0.065 0.000 3.861 ** 0.010 -0,704

0.060 -0.680 0.020 -0.767 0.020 -0.724 0.020 -0.725

O. 110 -0,708 0.040 -0.697 0.060 - 1.962"* 0.060 -0.689

0.200 -0.491 0.060 -0.719 0.090 -0.682 O. 110 -0.576

0.230 -0.406 0.090 -0.676 O. 110 -0.723 O. 140 -0.489

0.400 -0.357 O. 130 -0.665 O. 130 -0.686 O. 190 -0.957" *

0.490 -0.334 O.150 -0.660 O.150 -0.561 0.250 -0.360

0.590 -0.318 0.200 -0.555 0.210 -0.495 0.400 -0.251

0.630 -0.273 0.250 -0.456 0.250 -0.432 0.490 -0.333

0.700 -0.234 0.260 -0.423 0.340 -0,438 0.580 -0.175

0.750 -0.205 0.280 -0.450 0.370 -0.404 0.650 -0.148

0.810 -0.199 0.290 -0.438 0.400 -0.268 0.700 -0.135

0.840 -0.197 0.310 -0.424 0.410 - 1.023"* 0.750 -0.148

0.900 -0.111 0.320 -0.429 0.430 -0.127 0.800 -0.155

0.960 -0.065 0.340 -0.433 0.440 -0.117 0.830 -0.201

0.350 -0.215"* 0.460 -0.139 0.900 -0.050

0.370 -0.404 0.490 -0.127 0.960 -0.041

0.380 -0.445 0.500 -0.172

0.400 -0.360 0.520 -0.183

0.410 -0.426 0.540 -0.179

0.430 -0.410 0.550 -0.160

0.440 -0.373 0.580 -0.162

0.460 -0.397 0.600 -0.194

0.470 -0.397 0.610 -0.199

0.490 -0.368 0.650 0.986**

0_500 -0.374 0.700 -0.254

0.520 -0.375 0.750 -0.307

0.530 -0.349 0.820 -0.409

0,550 -0.344 0.890 -0.354

0.560 -0.328 0.900 -0.273

0.580 -0.306 0.960 -0.135

0.590 -0.300

0.600 -0.259

0.640 -0.166

0.700 -0.201

0.750 -0.028"*

0.820 -0.071

0.870 -0.037

0.930 -0.024

0.960 -0.010

Lower Surface

0.020 O.142 0.020 0.202 0.020 0.259 0.020 0.379

0.110 0.091 0.060 0.203 0.060 0.226 0.060 -0.338

0.230 0.063 0.090 0.124 0.090 0.513"* 0.110 0.186

0.400 -0.078 O. 120 O.129 O. 120 0.074 0.250 0.080

0.490 0.025 0.200 O. 122 0.200 0.037 0.400 0.049

0.630 0.828** 0.260 0.056 0.250 0.092 0.490 0.026

0.750 -0.019 0.400 0.009 0.400 0.013 0.580 -0.031

0.850 0.009 0.490 -0.066 0.490 -0.026 0.650 -0.016

0.900 0.038 0.580 -0.141 0.580 -0.071 0.750 0.014

0.960 0.036 0.640 O. 109 0.650 -0.040 0.830 0.019

0.750 O. t 48 0.750 O. 121 0.900 0.072

0.870 O. 104 0.890 O. 152 0.960 -0.020

0.930 0.079 0.930 0.118

0.960 0.032 0.960 - 1.065"*

532
Table H-2. Continued,

Flight 218, Wing sweep = 58 _', Time = 10-23-47-000, MINF = 1.216, Camber = 0/2, ALPT = 10.5t, BETA = 0.48, QINF = 615.9,

RNPU = 4.0E+06

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.786 0.000 0,022 0.000 3.895 * * 0.010 -0.736

0.060 -0.740 0.020 -0.828 0.020 -0.759 0.020 -0.735

0.110 -0.583 0.040 -0.742 0.060 - 1.981 ** 0.060 -0.734

0.200 -0.528 0.060 -0.764 0.090 -0.722 0.110 -0.586

0.230 -0.487 0.090 -0.719 0.110 -0,768 0.140 -0.567

0.400 -0.418 0.130 -0.627 0.130 -0.593 0.190 -0.967" *

0.490 -0.386 0.150 -0.550 0.150 -0.546 0.250 -0,399

0.590 -0.381 0.200 -0.544 0.210 -0.548 0.400 -0.279

0.630 -0.338 0.250 -0.524 0.250 -0.490 0.490 -0.445

0.700 -0.287 0.260 -0.485 0.340 -0.517 0.580 -0.249

0,750 -0.252 0.280 -0.505 0.370 -0.515 0.650 -0.184

0.810 -0.255 0.290 -0.497 0,400 -0.379 0.700 -0.161

0.840 -0.253 0.310 -0.478 0.410 - 1.033"* 0.750 -0.155

0.900 -0.175 0,320 -0.482 0.430 -0.158 0.800 -0.158

0.960 -0.094 0.340 -0.492 0.440 -0.144 0.830 -0.194

0.350 -0,239"* 0.460 -0.165 0.900 -0.045

0.370 -0.466 0.490 -0.177 0.960 -0.050

0.380 -0,509 0.500 -0.197

0.400 -0.458 0.520 -0.210

0.410 -0.487 0.540 -0.202

0.430 -0.488 0.550 -0.184

0.440 -0.440 0.580 -0.189

0,460 -0.482 0.600 -0.222

0.470 -0.475 0.610 -0.229

0.490 -0.453 0.650 0.994"*

0.500 -0,444 0.700 -0.292

0.520 -0.462 0.750 -0.344

0.530 -0.450 0,820 -0.437

0.550 -0.458 0.890 -0.304

0,560 -0.448 0.900 -0.291

0.580 -0.441 0.960 -0.186

0.590 -0.432

0.600 -0,409

0.640 -0.181

0.700 -0.209

0.750 -0.035**

0,820 -0.093

0.870 -0.033

0,930 -0.041

0.960 -0.026

Lower Surface

0.020 0.159 0.020 0.255 0.020 0.321 0.020 0.387

0.110 0.103 0.060 0.225 0.060 0.291 0.060 -0.335

0.230 0.073 0.090 0.131 0.090 0.516"* 0.1 I0 0.159

0.400 -0.020 0.120 0.149 0.120 0.083 0.250 0.095

0.490 0.056 0,200 0.152 0.200 0.080 0.400 0.070

0.630 0.834"* 0.260 0.083 0.250 0.117 0.490 0,060

0.750 -0.015 0.400 0.011 0.400 0.032 0.580 -0.010

0.850 0.001 0.490 -0.067 0.490 -0.024 0.650 0.006

0,900 0.039 0.580 -0.020 0.580 -0.063 0.750 0.021

0.960 0.036 0.640 0.127 0.650 -0.04 1 0.830 0.031

0,750 0.145 0.750 0.139 0.900 0.082

0.870 0.114 0.890 0.156 0.960 -0,017

0.930 0.075 0.930 0.125

0.960 0.029 0.960 - 1.076**

533
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-23-48-000, MINF = 1.206, Camber = 0/2, ALPT = 11.26. BETA = 0.51, QINF = 606.1,

RNPU = 4.0E+06

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.776 0.000 -0.024 0.000 3.958** 0.010 -0.772

0.060 -0.623 0.020 -0.791 0.020 -0.784 0.020 -0.806

0.110 -0.663 0.040 -0,670 0.060 -2.013"* 0.060 -0.768

0.200 -0.533 0.060 -0.635 0.090 -0.627 O. 110 -0.634

0.230 -0.491 0.090 -0.591 O. 110 -0.654 O.140 -0.617

0.400 -0.477 0.130 -0.589 0.130 -0.611 0.190 -0.983"*

0.490 -0.425 0.150 -0.588 0.150 -0.601 0.250 -0.395

0.590 -0.424 0.200 -0.582 0.210 -0.599 0.400 -0.331

0.630 -0.382 0.250 -0.592 0.250 -0.519 0.490 -0.512

0.700 -0.366 0.260 -0.552 0.340 -0.551 0.580 -0.288

0.750 -0.329 0.280 -0.579 0.370 -0.536 0.650 -0.199

0.810 -0.312 0.290 -0.566 0.400 -0.437 0.700 -0.171

0.840 -0.323 0.310 -0.548 0.410 - 1.050** 0.750 -0.150

0.900 -0.215 0.320 -0.552 0.430 -0.273 0.800 -0.161

0.960 -0.127 0.340 -0.557 0.440 -0.235 0.830 -0.189

0.350 -0.249** 0.460 -0.231 0.900 -0.052

0.370 -0.519 0.490 -0.191 0.960 -0.049

0.380 -0.567 0.500 -0.229

0.400 -0.505 0.520 -0.227

0.410 -0.539 0.540 -0.229

0.430 -0.529 0.550 -0.204

0.440 -0.493 0.580 -0.220

0.460 -0.530 0.600 -0.248

0.470 -0.524 0.610 -0.252

0.490 -0,496 0.650 1.010"*

0.500 -0.515 0.700 -0.327

0.520 -0.504 0.750 -0.371

0.530 -0.497 0.820 -0.482

0.550 -0.511 0.890 -0.298

0.560 -0.501 0.900 -0.298

0.580 -0.484 0.960 -0.204

0.590 -0.484

0.600 -0.470

0.640 -0.272

0.700 -0.220

0.750 -0.027**

0.820 -0.099

0.870 -0.030

0.930 -0.046

0.960 -0.046

Lower Surface

0.020 O. 167 0.020 0.277 0.020 0.353 0.020 0.376

O. 110 O. 118 0.060 0.245 0.060 0.319 0.060 -0.330

0.230 0.093 0.090 O.160 0.090 0.524"* O.110 0.285

0.400 0.026 O. 120 O.184 O. 120 O. 130 0.250 O. 120

0.490 0.079 0.200 O. 190 0.200 O. 109 0.400 O. 103

0.630 0.848"* 0.260 O. 110 0.250 O. 158 0.490 0.088

0.750 -0.006 0.400 0.019 0.400 0.056 0.580 0.021

0.850 0.004 0.490 -0.044 0.490 -0.017 0.650 0.032

0.900 0.043 0.580 0.052 0.580 -0.060 0.750 0.047

0.960 0.027 0.640 O. 153 0.650 -0.035 0.830 0.056

0.750 O.163 0.750 O. 163 0.900 O. 108

0.870 O. 124 0.890 O. 169 0.960 -0.002

0.930 0.091 0.930 O. 161

0.960 0.044 0.960 - 1.093" *

534
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-14-000, MINF = 1.214, Camber = 2/t, ALPT = 5.12, BETA = 0.37, QINF = 599.3,

RNPU = 3,9E+06

1"1= 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.426 0.000 0.244 0.000 4.027'* 0.0 l0 -0,449

0.060 -0.358 0.020 -0.465 0.020 -0.468 0,020 -0.484

0,110 -0.379 0,000 -0.408 0.060 - 1.555** 0.060 -0.426

0.200 -0.198 0.060 -0.455 0.090 -0.430 0.110 -0.393

0.230 -0.095 0.090 -0.410 0,110 -0.460 0,140 -0.309

0.400 -0.081 0.130 -0,431 0.130 -0.431 0.190 -0.969"*

0,490 -0.075 0.150 -0.442 0.150 -0.443 0.250 -0.192

0.590 -0.110 0.200 -0,423 0.210 °0.333 0.400 -0.096

0.630 -0,116 0.250 -0.160 0.250 -0.137 0.490 -0.088

0.700 -0.114 0.260 -0.128 0.340 -0.096 0.580 -0.055

0.750 -0.200 0.280 -0,137 0.370 -0.116 0.650 -0.104

0.810 -0.183 0.290 -0.113 0.400 -0.085 0.700 -0.089

0.840 -0.183 0.3 l0 -0.122 0,410 - 1,467** 0.750 -0.101

0.900 -0.080 0.320 -0.122 0.430 -0.112 0.800 -0,127

0.960 -0.037 0.340 -0.116 0.440 -0.097 0.830 -0.166

0.350 -0.061 ** 0.460 -0.109 0.900 -0.016

0.370 -0.094 0.490 -0.022 0.960 -0.024

0.380 -0.124 0.500 -0.106

0.400 -0.067 0.520 -0.096

0.410 -0.120 0.540 -0.108

0.430 -0.102 0.550 -0.084

0.440 -0.072 0.580 -0,082

0.460 -0.113 0.600 -0.099

0.470 -0,102 0.610 -0.098

0,490 -0.112 0.650 3.342" *

0.500 -0.094 0.700 -0.165

0.520 -0.124 0.750 -0.194

0.530 -0.118 0.820 -0.233

0.550 -0.135 0.890 -0.254

0.560 -0.142 0.900 -0.153

0,580 -0.124 0.960 -0.053

0.590 -0.142

0.600 -0.159

0.640 -0.175

0.700 -0.190

0.750 -0.010"*

0.820 -0.122

0,870 -0.111

0.930 -0.014

0,960 0.013

Lower Surface

0.020 -0.010 0.020 0.044 0.020 0.1 l0 0.020 0,211

0,110 -0.002 0.060 0,055 0.060 0.149 0.060 -0.485

0.230 -0.083 0.090 -0.028 0.090 1.806** 0.110 -0.013

0.400 -0.123 0.120 -0.009 0. | 20 -0.082 0.250 0.028

0.490 -0.144 0.200 -0.018 0,200 -0,041 0.400 -0.024

0.630 1.388 ** 0,260 -0.034 0.250 -0.031 0.490 -0.065

0.750 -0.005 0.400 -0.084 0.400 -0.079 0.580 -0,122

0.850 -0.028 0.490 -0.123 0.490 -0.021 0,650 -0.103

0.900 0.009 0.580 -0.184 0.580 -0.149 0.750 -0.088

0.960 0.012 0.640 0.009 0.650 -0.016 0.830 0.008

0.750 0.089 0,750 0.060 0.900 0.097

0.870 0.121 0.890 0.102 0.960 -0.023

0.930 0.094 0.930 0.075

0.960 0.071 0.960 -1.510"*

535
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-26-000, MINF = 1.215, Camber = 2/1, ALPT = 5.12, BETA = 0.37, QINF = 604.3,

RNPU = 3.9E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x./c CP x/c CP x/c CP

0,020 -0,434 0.000 0.243 0.000 3.987"* 0.010 -0.456

0.060 -0.408 0.020 -0.491 0.020 -0.465 0.020 -0.487

0.110 -0,387 0.040 -0.416 0.060 - 1.960** 0.060 -0.397

0.200 -0.219 0.060 -0.462 0.090 -0.432 0.110 -0.401

0.230 -0.101 0.090 -0.422 O. 110 -0.472 O. 140 -0.298

0.400 -0.081 O. 130 -0.437 O. 130 -0.434 O.t 90 -0.968"*

0.490 -0.086 O. 150 -0.448 O.150 -0.461 0.250 -0.184

0.590 -0.116 0.200 -0.423 0.210 -0.335 0.400 -0.096

0.630 -0.126 0.250 -0.179 0.250 -0.140 0.490 -0.083

0.700 -0.120 0.260 -0.120 0.340 -0.096 0.580 -0.066

0.750 -0.194 0.280 -0.140 0.370 -0.112 0.650 -0,098

0.810 -0.179 0.290 -0.124 0,400 -0.121 0.700 -0,085

0.840 -0.194 0.310 -0.116 0.410 -1.462"* 0.750 -0.108

0.900 -0.094 0.320 -0.109 0.430 -0.108 0.800 -0.130

0.960 -0.044 0.340 -0.116 0.440 -0.102 0.830 -0.165

0.350 -0.071 ** 0.460 -0.101 0,900 -0.017

0.370 -0.1 04 0.490 -0.078 0.960 -0.028

0.380 -0.115 0.500 -0.121

0.400 -0.077 0.520 -0.111

0.410 -0.125 0.540 -0.108

0.430 -0.102 0,550 -0.090

0.440 -0.089 0,580 -0.087

0.460 -0.105 0,600 -0.112

0.470 -0.096 0.610 -0.115

0.490 -0.109 0.650 3.307 * *

0.500 -0.120 0.700 -0.166

0.520 -0.127 0.750 -0.203

0.530 -0.123 0.820 -0.228

0.550 -0.145 0.890 -0.251

0.560 -0.133 0.900 -0.159

0.580 -0.123 0.960 -0.065

0.590 -0.167

0.600 -0.163

0.640 -0.177

0.700 -0.191

0.750 -0.021 **

0.820 -0.125

0.870 -0.109

0.930 -0.014

0.960 0.009

Lower Surface

0.020 -0.021 0.020 0.060 0.020 0.112 0.020 0.201

0.110 -0.028 0.060 0,060 0.060 0.130 0.060 -0.488

0.230 -0.079 0.090 -0.031 0,090 1.784"* 0.110 -0.024

0.400 -0.129 0.120 -0.013 0.120 -0.074 0.250 0.017

0.490 -0.161 0.200 -0.016 0.200 -0.035 0.400 -0.035

0.630 1.369"* 0.260 -0.037 0.250 -0.031 0.490 -0.076

0.750 -0.052 0.400 -0.084 0.400 -0.079 0.580 -0.125

0.850 -0,026 0.490 -0.115 0.490 -0.014 0.650 -0,099

0.900 0.012 0.580 -0.185 0.580 -0.144 0.750 -0.078

0.960 0.015 0.640 0.002 0.650 -0.018 0.830 -0.003

0.750 0.078 0,750 0,052 0.900 0.095

0,870 0.086 0.890 0.092 0.960 -0.009

0.930 0.081 0.930 0.078

0.960 0.059 0.960 - 1.505"*

536
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-29-500, MINF = 1.217. Camber = I/2, ALPT = 3.55, BETA = 0.37, QINF = 607.7.

RNPU = 4.0E+06

i"1= 0.93 0.76 0.59 0,40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0,020 -0.249 0.000 0.289 0.000 3.963"* 0.010 -0.376

0,060 -0,262 0,020 -0.371 0.020 -0.382 0,020 -0.439

0,110 -0.061 0.040 -0.309 0.060 - 1.951 ** 0.060 -0.353

0.200 -0.103 0.060 -0.363 0.090 -0.353 0.110 -0.258

0,230 -0,059 0.090 -0.215 0.110 -0.281 0.140 -0.254

0,400 -0.075 0.130 -0,233 0.130 -0.275 0.190 -0.965"*

0.490 -0.085 0.150 -0.211 0.150 -0.261 0,250 -0.154

0.590 -0.122 0.200 -0.127 0.210 -0.215 0.400 -0.059

0.630 -0.144 0.250 -0.095 0.250 -0,073 0.490 -0.036

0.700 -0.145 0.260 -0.078 0,340 -0,067 0.580 -0.034

0.750 -0,222 0.280 -0,083 0.370 -0.082 0.650 -0,069

0.810 -0.215 0.290 -0.098 0.400 -0.064 0.700 -0.073

0.840 -0.219 0.310 -0.080 0.410 -1.456"* 0.750 -0,095

0.900 -0.106 0.320 -0.081 0.430 -0,072 0.800 -0.118

0.960 -0,042 0.340 -0.090 0.440 -0.071 0.830 -0.151

0.350 -0.066** 0,460 -0.077 0,900 -0.018

0.370 -0.067 0.490 -0.042 0,960 -0,029

0.380 -0,084 0.500 -0,085

0,400 -0,045 0,520 -0,076

0.410 -0,080 0.540 -0.079

0,430 -0,068 0.550 -0.042

0.440 -0.035 0.580 -0.045

0,460 -0.068 0.600 -0.067

0,470 -0.078 0.610 -0,076

0,490 -0.067 0.650 3,287**

0.500 -0.071 0,700 -0.142

0.520 -0.087 0.750 -0.168

0.530 -0,084 0.820 -0.203

0.550 -0.118 0.890 -0.239

0,560 -0.1 l I 0.900 -0.154

0,580 -0.102 0,960 -0.043

0,590 -0.126

0,600 -0.121

0,640 -0.1 40

0.700 -0.168

0.750 -0.015"*

0.820 -0.115

0.87O -0.148

0.930 -0,003

0.960 0.030

Lower Surface

0.020 -0.089 0.020 -0.016 0.020 0.070 0.020 0.162

0.110 -0.100 0.060 0.024 0,060 0.096 0.060 -0.504

0.230 -0.120 0,090 -0.085 0,090 1.772"* 0.110 -0,049

0.400 -0.158 0.120 -0.069 0.120 -0.115 0.250 -0,004

0.490 -0.163 0.200 -0,052 0,200 -0.056 0.400 -0,066

0.630 1.359"* 0.260 -0,089 0.250 -0.080 0.490 -0.1 l0

0.750 -0.003 0.400 -0.115 0.400 -0.114 0.580 -0.161

0.850 0,026 0.490 -0.154 0.490 -0,030 0.650 -0.126

0.900 0,063 0,580 -0.198 0.580 -0.178 0.750 -0.139

0,960 0.053 0.640 -0.030 0,650 -0,030 0.830 -0.012

0,750 0.068 0.750 0.039 0.900 0.067

0.870 0,100 0.890 0.101 0.960 -0.025

0,930 0,098 0,930 0,077

0.960 0,079 0.960 - 1,499"*

537
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-32-500, MINF = 1.222, Camber = 0/3, ALPT = 2.56, BETA = 0.43, QINF -- 615.5,

RNPU = 4.0E+06

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 0.027 0.000 0.317 0.000 3.908 ** 0.010 -0.352

0.060 -0.016 0.020 -0.320 0.020 -0.213 0.020 -0.282

0.110 -0.001 0.040 -0.172 0.060 - 1.931 ** 0.060 -0.269

0.200 -0,055 0.060 -0.179 0.090 -0.167 0.110 -0.208

0.230 -0.017 0.090 -0.128 0.110 -0.186 0.140 -0.209

0.400 -0.062 0.130 -0.101 0.130 -0.172 0.190 -0.957"*

0.490 -0.108 0.150 -0,063 0.150 -0.172 0.250 -0.133

0.590 -0.114 0.200 -0.064 0.210 -0.149 0.400 -0.018

0.630 -0.126 0.250 -0.058 0.250 -0.013 0.490 0.000

0.700 -0.144 0.260 -0.045 0.340 -0.031 0.580 0.000

0.750 -0.262 0.280 -0.061 0.370 -0.035 0.650 -0.057

0.810 -0.259 0.290 -0.066 0.400 -0.025 0.700 -0.052

0.840 -0.255 0.310 -0.056 0.410 - 1.442"* 0.750 -0.074

0.900 -0.109 0.320 -0.049 0.430 -0.044 0.800 -0.094

0.960 -0.043 0,340 -0.057 0.440 -0.040 0.830 -0.114

0.350 -0.071 ** 0.460 -0.037 0.900 -0.008

0.370 -0.033 0.490 0.000 0.960 -0.024

0.380 -0.052 0.500 -0.050

0.400 -0.009 0.520 -0.041

0.410 -0.049 0.540 -0.049

0.430 -0.030 0.550 -0.029

0.440 -0.011 0.580 -0.025

0.460 -0.055 0.600 -0.040

0.470 -0.043 0.610 -0.040

0.490 -0.047 0.650 3.240**

0.500 -0.043 0.700 -0.108

0.520 -0.062 0,750 -0.145

0.530 -0.056 0.820 -0.198

0,550 -0.093 0.890 -0.201

0.560 -0.076 0.900 -0.127

0.580 -0.066 0.960 -0.016

0.590 -0,094

0.600 -0.096

0.640 -0.126

0,700 -0.154

0.750 -0.020**

0.820 -0. I 18

0.870 -0.173

0.930 0.005

0.960 0.033

Lower Surface

0,020 -0.098 0.020 -0.038 0.020 0.014 0.020 0.147

0.110 -0.137 0.060 -0.002 0.060 0.090 0.060 -0.526

0.230 -0.136 0.090 -0.112 0.090 1.745 ** 0. I 10 -0.049

0.400 -0.173 0,120 -0.101 0,120 -0.121 0.250 -0.011

0.490 -0.177 0,200 -0.055 0.200 -0.066 0.400 -0.084

0.630 1.337"* 0.260 -0.111 0.250 -0.088 0.490 -0.111

0.750 0.044 0.400 -0.131 0.400 -0.132 0.580 -0.178

0.850 0.078 0.490 -0.186 0.490 -0.021 0.650 -0.127

0.900 0.105 0.580 -0.231 0.580 -0.209 0.750 -0.150

0.960 0.073 0.640 0.003 0,650 -0.017 0.830 -0.011

0.750 0,094 0.750 0.047 0.900 0.056

0.870 0.112 0.890 0.116 0.960 -0.008

0.930 0.118 0.930 0.087

0.960 0.095 0.960 -1.485"*

538
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-36-500, MINF = 1.235, Camber = 1/3, ALPT = 3.80, BETA = 0.31, QINF = 641.9,

RNPU = 4.2E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.380 0.000 0.268 0.000 3.728** 0.010 -0.376

0.060 -0.359 0.020 -0.450 0.020 -0,402 0.020 -0.441

0.110 -0.165 0.040 -0.377 0.060 - 1.870"* 0.060 -0.374

0.200 -0,080 0.060 -0.419 0.090 -0.330 0.110 -0.282

0.230 -0.035 0.090 -0,347 0.110 -0.361 0.140 -0.244

0.400 -0.060 0.130 -0.316 0.130 -0.276 0.190 -0.937 **

0.490 -0.070 0.150 -0.246 0.150 -0.251 0.250 -0.156

0.590 -0.095 0,200 -0.184 0.210 -0.253 0.400 -0.079

0.630 -0.129 0.250 -0.100 0.250 -0.103 0.490 -0.041

0.700 -0.136 0.260 -0.074 0.340 -0.063 0.580 -0.033

0.750 -0.248 0,280 -0.093 0.370 -0.078 0.650 -0.079

0.810 -0.244 0.290 -0.089 0.400 -0.064 0,700 -0.063

0.840 -0.242 0.310 -0.083 0.410 -1.402** 0.750 -0,090

0.900 -0.138 0.320 -0.089 0.430 -0.075 0.800 -0.095

0,960 -0.060 0.340 -0.082 0.440 -0.063 0.830 -0.152

0.350 -0.072"* 0.460 -0.074 0.900 -0.034

0.370 -0.072 0.490 -0,064 0.960 -0.012

0.380 -0.089 0.500 -0.077

0,400 -0.012 0.520 -0.066

0.410 -0.085 0.540 -0.075

0.430 -0.060 0,550 -0.050

0.440 -0.044 0.580 -0.043

0.460 -0.071 0.600 -0.074

0.470 -0.084 0.610 -0.073

0.490 -0.073 0.650 3.088**

0.500 -0.080 0.700 -0.139

0.520 -0.085 0.750 -0.176

0.530 -0.086 0.820 -0.217

0.550 -0.112 0.890 -0.227

0.560 -0.097 0,900 -0.153

0.580 -0.094 0.960 -0.046

0.590 -0.117

0,600 -0.121

0.640 -0.1 44

0.700 -0.166

0.750 -0.023**

0.820 -0.133

0.870 -0+185

0,930 -0.024

0.960 0.012

Lower Surface

0.020 -0.062 0.020 0.020 0.020 0.089 0.020 0.181

0. l 10 -0.091 0.060 0.018 0.060 0.083 0.060 -0.476

0.230 -0.112 0.090 -0.077 0.090 1.654"* 0.110 0.000

0.400 -0.178 0.120 -0,050 0.120 -0.101 0.250 0.000

0.490 -0.166 0,200 -0.050 0.200 -0.04 1 0.400 -0.059

0.630 |.264"* 0.260 -0,081 0.250 -0.072 0.490 -0.101

0.750 -0.027 0.400 -0.109 0.400 -0.113 0.580 -0.148

0,850 0.022 0.490 -0.161 0.490 -0,029 0.650 -0.120

0.900 0,056 0.580 -0.202 0.580 -0.175 0.750 -0.123

0.960 0.040 0,640 0.000 0.650 -0.035 0.830 -0.020

0,750 0.091 0.750 0.051 0.900 0.073

0.870 0.105 0.890 0.123 0.960 -0.024

0.930 0.096 0.930 0.092

0.960 0.076 0.960 - 1.442"*

539
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-37-000, MINF = 1.237, Camber = 1/3, ALPT = 4.71, BETA = 0.37, QINF = 646.5,

RNPU = 4.2E+06

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.422 0.000 0.260 0.000 3.699 ** 0.010 -0.441

0.060 -0.378 0.020 -0.486 0.020 -0.437 0.020 -0.460

0.110 -0.377 0.040 -0.404 0.060 - 1.860"* 0.060 -0.397

0.200 -0.179 0.060 -0.445 0.090 -0.415 0.110 -0.353

0.230 -0.073 0.090 -0.411 0.110 -0.433 0.140 -0.278

0.400 -0.063 0.130 -0.410 0.130 -0.381 0.190 -0.933"*

0.490 -0.053 0,150 -0.405 0,150 -0,348 0.250 -0.200

0.590 -0.086 0,200 -0.366 0.210 -0.311 0.400 -0.104

0.630 -0.097 0.250 -0.139 0.250 -0.143 0.490 -0.070

0.700 -0.106 0.260 -0.108 0.340 -0.084 0.580 -0.058

0.750 -0.211 0.280 -0.111 0.370 -0.093 0.650 -0.092

0.810 -0.209 0.290 -0.103 0.400 -0.074 0.700 -0.083

0.840 -0.213 0.310 -0.091 0.410 - 1.395"* 0.750 -0.086

0.900 -0.134 0.320 -0.108 0.430 -0,095 0.800 -0.104

0.960 -0.041 0.340 -0.089 0.440 -0.081 0.830 -0.159

0.350 -0.063 ** 0.460 -0.080 0.900 -0.015

0.370 -0.077 0.490 -0.043 0.960 -0.024

0.380 -0.094 0.500 -0.079

0.400 -0.054 0.520 -0.084

0.410 -0.087 0.540 -0.087

0.430 -0.084 0.550 -0.066

0.440 -0.078 0.580 -0.057

0.460 -0.077 0.600 -0.082

0.470 -0.082 0.610 -0.100

0.490 -0.079 0.650 3,063"*

0.500 -0.076 0,700 -0.143

0.520 -0.096 0.750 -0.177

0.530 -0,088 0.820 -0,232

0.550 -0.119 0.890 -0,228

0.560 -0,I12 0.900 -0.146

0.580 -0.112 0,960 -0.054

0.590 -0.136

0.600 -0.128

0.640 -0.149

0.700 -0.165

0,750 -0.011"*

0.820 -0.121

0.870 -0.166

0.930 -0.020

0.960 0.023

Lower Surface

0.020 -0.002 0.020 0.079 0.020 0.138 0.020 0.226

0.110 -0.040 0.060 0.054 0.060 0.129 0.060 -0.438

0.230 -0.078 0.090 -0.015 0.090 1.640"* 0.110 -0.005

0.400 -0. I 18 0.120 -0.024 0.120 -0.065 0.250 0.027

0.490 -0.136 0.200 -0.0199 0.200 -0.009 0.400 -0.025

0.630 1.252** 0.260 -0.057 0.250 -0.035 0.490 -0.064

0,750 -0.014 0.400 -0.074 0.400 -0.071 0.580 -0.128

0.850 0.010 0.490 -0.118 0.490 -0.012 0.650 -0.088

0.900 0,030 0.580 -0.167 0.580 -0.160 0.750 -0.087

0.960 0.015 0.640 0.027 0.650 -0.035 0.830 0.002

0.750 0.090 0.750 0.079 0.900 0.066

0.870 0.110 0.890 0,139 0.960 -0.023

0.930 0.099 0.930 0,105

0,960 0.076 0.960 - 1.435" *

540
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-37-500, MINF = 1.238, Camber = 1/2, ALPT = 5.82, BETA = 0.37, QINF = 649.7,

RNPU = 4.2E+06

q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.465 0.000 0.241 0.000 3.677"* 0.010 -0.471

0.060 -0.443 0,020 -0.533 0.020 -0.484 0.020 -0.500

0.! 10 -0,429 0.040 -0.444 0.060 -1.854** 0.060 -0.440

0.200 -0.455 0.060 -0.483 0.090 -0.463 O. 110 -0.430

0.230 -0.394 0.090 -0.449 O.110 -0,502 O. 140 -0.327

0.400 -0.068 O. 130 -0.462 O.130 -0.469 O. 190 -0.932"*

0.490 -0.055 O.150 -0.466 O.150 -0.449 0.250 -0.222

0.590 -0.087 0.200 -0.440 0.210 -0.439 0.400 -0.121

0.630 -0.087 0.250 -0.305 0.250 -0.207 0.490 -0.119

0.700 -0.097 0.260 -0.234 0.340 -0.116 0.580 -0.055

0.750 -0.184 0.280 -0.216 0.370 -0.122 0.650 -0.090

0.810 -0.178 0.290 -0.184 0.400 -0.094 0.700 -0.080

0.840 -0.182 0.310 -0.157 0.410 - 1.39 l ** 0.750 -0.103

0.900 -0.088 0.320 -0.157 0.430 -0.103 0.800 -0.1 O0

0.960 -0.033 0,340 -0.134 0.440 -0.094 0.830 -0.163

0.350 -0.072** 0.460 -0.103 0.900 -0.021

0370 -0.102 0.490 -0.072 0.960 -0.028

0.380 -0.119 0.500 -0.106

0.400 -0.081 0.520 -0.096

0.410 -0.108 0.540 -0.099

0.430 -0.089 0.550 -0.079

0.440 -0.073 0.580 -0.078

0.460 -0.096 0.600 -0.107

0.470 -0.103 0.610 -0.115

0.490 -0.093 0.650 3.044**

0.500 -0.101 0.700 -0,155

0.520 -0.107 0250 -0.199

0.530 -0.107 0.820 -0.230

0.550 -0.136 0.890 -0,281

0.560 -0.131 0.900 -0.182

0.580 -0.123 0.960 -0.079

0.590 -0.144

0.600 -0.145

0.640 -0.167

0.700 -0.182

0,750 -0.003**

0.820 -O.114

0.870 -0.117

0.930 -0.004

0.960 0.006

Lower Surface

0.020 0.005 0.020 O. 119 0.020 O. 158 0.020 0.254

O. l 10 -0.005 0.060 O. 1O0 0.060 O. 175 0.060 -0.426

0.230 -0.052 0.090 0.002 0.090 1.628" * O.110 -0.002

0.400 -0.089 O. 120 0.019 O. 120 -0.034 0.250 0.045

0.490 -0.120 0.200 0.018 0.200 0.002 0.400 -0.007

0.630 1.242"* 0.260 -0.001 0.250 0.004 0.490 -0.046

0.750 -0.004 0.400 -0,051 0.400 -0.04 1 0.580 -0.095

0.850 0.003 0.490 -0.092 0.490 -0.006 0.650 -0.074

0.900 0.037 0.580 -0.171 0.580 -0.120 0.750 -0.043

0.960 0.033 0.640 0.035 0.650 -0.012 0.830 0.012

0,750 O. 106 0.750 0.084 0.900 0.065

0.870 O. 142 0.890 O. 133 0.960 -0.017

0.930 O. 111 0.930 O. 104

0.960 0.085 0.960 -1.432'*

541
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-38-000, MINF = 1.238, Camber = 2/1, ALPT = 6.70, BETA = 0.43, QINF = 651.6,

RNPU = 4.2E+06

lq = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.486 0.000 0.227 0.000 3.663"* 0,010 -0.502

0.060 -0.467 0.020 -0.631 0.020 -0.507 0.020 -0.540

0.110 -0.468 0.040 -0.458 0.060 -1.852"* 0.060 -0.506

0.200 -0.504 0.060 -0.514 0.090 -0.499 O. 110 -0.482

0.230 -0.447 0.090 -0.476 O. 110 -0.549 O. 140 -0.424

0.400 -0.157 O. 130 -0.491 O.130 -0.520 O. 190 -0.933 * *

0.490 -0.089 0.150 -0.507 0.150 -0,516 0,250 -0.234

0.590 -0.099 0.200 -0.491 0.210 -0.513 0.400 -0.143

0,630 -0.086 0.250 -0.517 0.250 -0.281 0.490 -0.175

0.700 -0,092 0,260 -0.440 0.340 -0.147 0.580 -0.063

0.750 -0.149 0,280 -0.327 0.370 -0.154 0.650 -0.100

0.810 -0.151 0.290 -0.283 0.400 -0.131 0.700 -0.092

0.840 -0,140 0.310 -0.260 0.410 - 1.390"* 0.750 -0.126

0.900 -0,068 0.320 -0.262 0.430 -0.127 0. 800 -0.113

0.960 -0.020 0.340 -0,239 0.440 -0.117 0.830 -0,178

0.350 -0.100"* 0.460 -0.128 0,900 -0.024

0.370 -0.178 0.490 -0.096 0.960 -0,009

0,380 -0.187 0,500 -0.134

0,400 -0.125 0,520 -0.127

0,410 -0.151 0.540 -0,130

0.430 -0,124 0,550 -0.1 04

0.440 -0.097 0.580 -0.109

0,460 -0.126 0.600 -0.125

0.470 -0.135 0.610 -0.130

0.490 -0.118 0.650 3.032**

0.500 -0.124 0,700 -0.176

0.520 -0.132 0.750 -0.215

0,530 -0.129 0.820 -0.237

0.550 -0.160 0.890 -0.273

0.560 -0.143 0.900 -0.196

0.580 -0.144 0,960 -0.098

0.590 -0.159

0.600 -0.163

0.640 -0,181

0,700 -0.195

0.750 -0.006"*

0.820 -0.101

0.870 -0,070

0,930 -0,014

0.960 0.004

Lower Surface

0.020 0,049 0.020 0.141 0,020 0.169 0.020 0,265

0.110 0.012 0.060 0.112 0.060 0.183 0,060 -0.425

0.230 -0.026 0,090 0,028 0.090 1.620* * 0.110 0.147

0,400 -0.090 0.120 0.042 0.120 -0.018 0.250 0.052

0.490 -0.115 0,200 0,048 0.200 0.017 0,400 0.005

0.630 1.235** 0.260 0.023 0.250 0.009 0,490 -0.032

0.750 -0.023 0,400 -0.029 0,400 -0.019 0.580 -0.082

0.850 -0.022 0.490 -0.063 0,490 -0.009 0.650 -0.060

0,900 0.019 0.580 -0.154 0.580 -0.110 0.750 -0.021

0.960 0.022 0,640 0.021 0.650 -0.015 0.830 0.010

0.750 0.091 0.750 0.083 0.900 0.069

0,870 0.092 0,890 0.111 0.960 -0,004

0.930 0,088 0,930 0.080

0,960 0.059 0,960 - 1.431 **

542
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-38-500, MINF = 1.237, Camber = 3/0, ALPT = 7.54, BETA = 0.45, QINF = 653.3,

RNPU = 4.2E+06

= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.514 0.000 0.201 0.000 3.650** 0.010 -0.529

0.060 -0.490 0.020 -0.580 0.020 -0.520 0.020 -0.566

O.110 -0.512 0.040 -0.480 0.060 - 1.851 * * 0.060 -0.559

0.200 -0.541 0.060 -0.523 0,090 -0.520 0.110 -0.529

0.230 -0.488 0.090 -0,499 0.110 -0.572 0.140 -0.469

0.400 -0.250 O. 130 -0.511 O. 130 -0,557 O. 190 -0.933"*

0.490 -0.186 O. 150 -0.544 O. 150 -0.561 0.250 -0.240

0.590 -0.133 0.200 -0.532 0.210 -0.558 0.400 -0.181

0.630 -0.110 0.250 -0.557 0.250 -0,335 0,490 -0.247

0.700 -0.100 0.260 -0,507 0.340 -0.232 0.580 -0.087

0.750 -0.116 0.280 -0.382 0.370 -0.193 0.650 -0.116

0.810 -0.112 0.290 -0.346 0.400 -0.151 0.700 -0.116

0.840 -0.109 0.310 -0.326 0.410 -1.390"* 0.750 -0.139

0.900 -0.041 0.320 -0.326 0.430 -0.154 0.800 -0.132

0.960 -0.013 0.340 -0.320 0.440 -0.142 0.830 -0.183

0.350 -0.118"* 0.460 -0.152 0.900 -0.027

0.370 -0.281 0.490 -0.109 0.960 -0.012

0.380 -0.308 0.500 -0.163

0.400 -0.248 0.520 -0.145

0.4 lO -0.269 0.540 -0.148

0.430 -0.223 0.550 -0.126

0.440 -0.181 0.580 -0.148

0.460 -0.200 0.600 -0.159

0.470 -0.180 0.610 -0.151

0.490 -0.166 0.650 3.021 **

0.500 -0.157 0.700 -0.186

0.520 -0.163 0.750 -0.230

0.530 -0.150 0.820 -0.253

0.550 -0.171 0.890 -0.261

0.560 -0.165 0.900 -0.231

0.580 -0.156 0.960 -0.1 l 1

0.590 -0.175

0.600 -0.17 3

0.640 -0.189

0.700 -0.200

0.750 -0.010"*

0.820 -0.085

0.870 -0.055

0.930 -0.019

0.960 -0.003

Lower Surface

0.020 0.073 0.020 O. 160 0.020 O. 172 0.020 0.269

0.110 0.033 0.060 0.151 0.060 0.197 0.060 -0.373

0.230 0.063 0.090 0.043 0.090 1.612"* O. 110 O. 168

0.400 -0.083 O.120 0.068 O. 120 -0.007 0.250 0.059

0.490 -0.125 0.200 0.063 0.200 0.046 0.400 0.019

0.630 1.228"* 0.260 0.038 0.250 0.032 0.490 -0.018

0.750 -0.052 0.400 -0.013 0.400 -0.007 0.580 -0.069

0.850 -0.036 0.490 -0.056 0.490 0.001 0.650 -0.055

0.900 -0.003 0.580 -0. 150 0.580 -0.086 0.750 -0.011

0.960 0.016 0.640 0.013 0.650 -0.022 0.830 0.028

0.750 0.080 0.750 0.073 0.900 0.074

0.870 0.071 0.890 0.077 0.960 -0.009

0.930 0.066 0.930 0.063

0.960 0.037 0,960 - 1.430**

543
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-39-500, MINF = 1.235, Camber = 5/-1, ALPT = 8.70, BETA = 0.43, QINF = 655.6,

RNPU = 4.2E÷06

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0,507 0.000 0.209 0.000 3.631 ** 0.010 -0.527

0.060 -0.476 0.020 -0.583 0.020 -0.525 0.020 -0.556

0.110 -0.391 0.040 -0.451 0.060 - 1.850"* 0.060 -0.583

0.200 -0.583 0.060 -0.520 0.090 -0.543 0.110 -0.542

0.230 -0.537 0.090 -0.500 0.110 -0.600 0.140 -0.478

0.400 -0.317 0.130 -0.526 0.130 -0.602 0.190 -0.936 **

0.490 -0.279 0.150 -0,575 0.150 -0,605 0.250 -0.325

0.590 -0.240 0.200 -0.574 0.210 -0.595 0.400 -0.225

0.630 -0.194 0.250 -0.439 0.250 -0.387 0.490 -0.351

0.700 -0.156 0.260 -0.391 0.340 -0.393 0.580 -0.139

0.750 -0.105 0.280 -0.408 0.370 -0.390 0,650 -0.134

0.810 -0.111 0.290 -0.397 0.400 -0.306 0.700 -0.116

0.840 -0.094 0.310 -0.383 0.410 -1.391"* 0.750 -0.141

0.900 -0.039 0.320 -0.388 0.430 -0.170 0.800 -0.141

0.960 -0.023 0.340 -0.388 0.440 -0.119 0.830 -0.192

0.350 -0.116"* 0.460 -0.125 0.900 -0.028

0.370 -0.364 0.490 -0.108 0.960 -0.024

0.380 -0.406 0.500 -0.1 64

0.400 -0.361 0.520 -0.166

0.410 -0.378 0.540 -0.169

0.430 -0.356 0.550 -0.149

0.440 -0.321 0.580 -0.15 l

0.460 -0.348 0.600 -0. 178

0.470 -0.339 0.610 -0.178

0.490 -0.312 0.650 3.004"*

0.500 -0.300 0.700 -0.225

0.520 -0.311 0.750 -0.262

0.530 -0.291 0.820 -0.329

0.550 -0.267 0.890 -0.273

0.560 -0.275 0.900 -0.222

0.580 -0.262 0.960 -0.105

0.590 -0.264

0.600 -0.262

0.640 -0.184

0,700 -0.206

0.750 -0.004**

0.820 -0.071

0.870 -0.011

0.930 -0.024

0,960 -0.015

Lower Surface

0.020 0.080 0.020 0.182 0.020 0.194 0.020 0.301

0.110 0.066 0.060 0.170 0.060 0.212 0.060 -0.342

0.230 0.127 0.090 0.087 0.090 1.601 ** 0.110 0.143

0.400 -0.079 0.120 0.100 0.120 0,020 0.250 0.077

0.490 -0.090 0.200 0.136 0,200 0.125 0.400 0.042

0.630 1.218"* 0.260 0.063 0.250 0.083 0,490 0.003

0.750 -0.059 0.400 0,026 0.400 0.001 0.580 -0.048

0.850 -0.055 0.490 -0.050 0.490 -0.008 0.650 -0.029

0.900 -0.007 0.580 -0.137 0.580 -0.082 0.750 0.005

0.960 0.020 0.640 0.032 0.650 -0.021 0.830 0.023

0.750 0.104 0.750 0.070 0.900 0.084

0.870 0.062 0.890 0.068 0.960 0.001

0.930 0.04 1 0.930 0.060

0.960 0.012 0.960 -1.431 **

544
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-40-500, MINF = 1.231, Camber = 7/-1, ALPT = 9.74, BETA = 0.43, QINF = 654.0,

RNPU = 4.2E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.476 0.000 0.238 0.000 3.636"* 0.010 -0.536

0.060 -0.453 0.020 -0.531 0.020 -0.494 0.020 -0.558

0.110 -0.476 0.040 -0,426 0.060 - 1.859"* 0.060 -0.597

0.200 -0.610 0.060 -0.486 0.090 -0.545 0.110 -0.546

0.230 -0.568 0.090 -0.501 0.1 I 0 -0.603 0.140 -0.555

0.400 -0.373 0.130 -0,544 0.130 -0.625 0.190 -0.942"*

0.490 -0,325 0.150 -0.597 0.150 -0.644 0.250 -0.401

0,590 -0.306 0.200 -0.611 0.210 -0.501 0.400 -0.252

0.630 -0.252 0.250 -0.464 0,250 -0.435 0.490 -0,360

0.700 -0.203 0.260 -0.430 0.340 -0.480 0.580 -0.187

0.750 -0.178 0.280 -0.452 0,370 -0,494 0.650 -0.154

0.810 -0.177 0.290 -0,448 0.400 -0.385 0.700 -0.136

0.840 -0.167 0.310 -0.436 0.410 - 1.399"* 0.750 -0.152

0.900 -0.095 0,320 -0.437 0.430 -0.215 0.800 -0.142

0.960 -0.065 0,340 -0.443 0.440 -0.135 0,830 -0.194

0.350 -0.122"* 0.460 -0.145 0.900 -0.032

0.370 -0.414 0.490 -0.133 0.960 -0,025

0,380 -0.453 0.500 -0.178

0,400 -0.396 0,520 -0.186

0.410 -0.432 0,540 -0.179

0.430 -0.417 0.550 -0.176

0.440 -0,394 0,580 -0.187

0.460 -0.416 0.600 -0.208

0,470 -0,406 0.610 -0,204

0.490 -0.392 0.650 3.008"*

0.500 -0.393 0.700 -0.246

0.520 -0.394 0.750 -0.293

0.530 -0.384 0.820 -0.374

0.550 -0.394 0.890 -0.287

0.560 -0.391 0.900 -0.25 l

0.580 -0.383 0.960 -0.134

0,590 -0.380

0,600 -0.367

O.640 -0.223

0.700 -0.194

0.750 -0.008"*

0.820 -0,097

0.870 -0.016

0.930 -0.039

0.960 -0.023

Lower Surface

0.020 0.090 0,020 0.183 0.020 0.215 0.020 0.288

0.110 0,086 0.060 0.199 0.060 0.227 0.060 -0.363

0,230 0.132 0.090 0,109 0.090 1.601"* 0.110 0,133

0.400 -0.053 0.120 0.127 0.120 0.071 0.250 0.107

0.490 -0.003 0,200 0.131 0.200 0.110 0.400 0,072

0.630 1.217"* 0.260 0.099 0,250 0.120 0.490 0.037

0.750 -0,064 0.400 0,036 0.400 0.035 0.580 -0.023

0.850 -0.060 0.490 -0.045 0.490 0.001 0.650 -0.002

0.900 -0,008 0.580 -0.122 0.580 -0.052 0.750 0.024

0.960 0.010 0.640 0.056 0.650 -0.016 0.830 0.037

0.750 0.117 0.750 0.086 0.900 0.089

0.870 0.071 0.890 0.084 0.960 -0.004

0.930 0.029 0.930 0.073

0.960 -0.003 0.960 -1.439"*

545
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-41-000, MINF = 1.228, Camber = 9/-1, ALPT = 10.14, BETA = 0.34, QINF = 651.8,

RNPU = 4.2E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.430 0.000 0.249 0.000 3.647"* 0.010 -0.500

0.060 -0.386 0.020 -0.448 0.020 -0.456 0.020 -0.529

0.110 -0.454 0.040 -0.371 0.060 - 1.866** 0.060 -0.604

0.200 -0.650 0.060 -0.446 0.090 -0.531 0.110 -0.568

0.230 -0.584 0.090 -0.489 0.110 -0.605 0.140 -0.550

0.400 -0.400 0.130 -0.545 0.130 -0.644 0.190 -0.947" *

0.490 -0.348 O. 150 -0.614 O. 150 -0.619 0.250 -0.413

0.590 -0.332 0.200 -0.634 0.210 -0.506 0.400 -0.277

0.630 -0.270 0.250 -0.485 0.250 -0.467 0.490 -0.434

0.700 -0.224 0.260 -0.439 0.340 -0.514 0.580 -0.231

0.750 -0.208 0.280 -0.467 0.370 -0.508 0.650 -0.165

0.810 -0.196 0.290 -0.470 0.400 -0.445 0.700 -0.143

0.840 -0.192 0.310 -0.460 0.410 -1.405"* 0.750 -0.151

0.900 -0.148 0.320 -0.466 0.430 -0.252 0.800 -0.153

0.960 -0.103 0.340 -0.478 0.440 -0.181 0.830 -0.189

0.350 -0.159** 0.460 -0.178 0.900 -0.033

0.370 -0.443 0.490 -0.169 0.960 -0.037

0.380 -0.481 0.500 -0.197

0.400 -0.405 0.520 -0.218

0.410 -0.456 0.540 -0.213

0.430 -0.445 0.550 -0.20 l

0.440 -0.411 0.580 -0.204

0.460 -0.448 0.600 -0.233

0.470 -0.445 0.610 -0.235

0.490 -0.416 0.650 3.017"*

0.500 -0.429 0.700 -0.290

0.520 -0.428 0.750 -0.323

0.530 -0.426 0.820 -0.392

0.550 -0.462 0.890 -0.289

0.560 -0.428 0.900 -0.270

0.580 -0.423 0.960 -0.157

0.590 -0,428

0.600 -0.415

0.640 -0.288

0.700 -0.243

0.750 -0.013"*

0.820 -0.109

0.870 -0.026

0.930 -0,039

0.960 -0.036

Lower Surface

0.020 0.083 0.020 O. 179 0.020 0.204 0.020 0.261

O. 110 0.088 0.060 O. 197 0.060 0.232 0.060 -0.385

0.230 0.099 0.090 O.107 0.090 1.605"* O. 110 O. 125

0.400 -0.046 O. 120 O. 146 O. 120 0.067 0.250 O. 121

0.490 0.004 0.200 0.099 0.200 0.091 0.400 0.074

0.630 1.220* * 0.260 O. 117 0.250 O. 116 0.490 0.040

0.750 -0.068 0.400 0.032 0.400 0.040 0.580 -0.012

0.850 -0.063 0.490 -0.050 0.490 -0.013 0.650 -0.006

0.900 -0.014 0.580 -0.117 0.580 -0.054 0.750 0.020

0.960 -0.002 0.640 0.062 0.650 -0.017 0.830 0.038

0.750 O. 110 0.750 0.092 0.900 0.086

0.870 0.061 0.890 0.076 0.960 -0.009

0.930 0.021 0.930 0.072

0.960 -0.009 0.960 -1.445**

546
TabLe H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-26-42-500, MINF = 1.216, Camber = 12/-1, ALPT = l 1.03, BETA = 0.34, QINF = 639.0,

RNPU = 4.2E+06

•q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.138 0.000 0.330 0.000 3.719"* 0,010 -0.430

0.060 -0.324 0,020 -0,250 0.020 -0.268 0,020 -0.469

0.110 -0,466 0.040 -0.197 0.060 - 1.905" * 0,060 -0.565

0.200 -0,530 0.060 -0,394 0.090 -0,528 0.110 -0,581

0,230 -0.507 0.090 -0.483 0.110 -0.618 0.140 -0.565

0.400 -0.454 0.130 -0,559 0.130 -0,668 0.190 -0.967"*

0.490 -0.364 0.150 -0.652 0.150 -0.519 0.250 -0.429

0.590 -0.322 0.200 -0.517 0.210 -0.522 0.400 -0,358

0.630 -0,293 0,250 -0.511 0.250 -0.491 0,490 -0,458

0.700 -0.251 0.260 -0.477 0,340 -0.540 0.580 -0.291

0,750 -0.228 0.280 -0.505 0.370 -0.537 0.650 -0.208

0.810 -0.231 0.290 -0.509 0.400 -0.455 0,700 -0.174

0,840 -0.253 0.310 -0.496 0.410 - 1.434"* 0.750 -0.144

0,900 -0,209 0,320 -0.504 0.430 -0,346 0.800 -0.1 64

0.960 -0.179 0.340 -0.511 0.440 -0.293 0.830 -0.192

0.350 -0.204"* 0.460 -0.277 0.900 -0.034

0.370 -0,472 0.490 -0.220 0.960 -0.048

0.380 -0.516 0,500 -0.256

0.400 -0.452 0.520 -0.243

0.410 -0.486 0,540 -0.257

0.430 -0.492 0.550 -0.249

0,440 -0,436 0.580 -0.255

0.460 -0.481 0,600 -0.280

0.470 -0,470 0.610 -0.281

0.490 -0.449 0.650 3,076"*

0.500 -0,457 0.700 -0.340

0,520 -0.463 0,750 -0.417

0.530 -0,452 0.820 -0,455

0.550 -0.460 0,890 -0.305

0.560 -0.455 0,900 -0.271

0,580 -0.451 0,960 -0,167

0.590 -0.439

0.600 -0.441

0.640 -0,327

0,700 -0.290

0.750 -0.014"*

0.820 -0.087

0.870 -0,024

0.930 -0.044

0,960 -0,044

Lower Surface

0,020 0.082 0,020 0.170 0.020 0.201 0.020 0.197

0.110 0,095 0,060 0.209 0.060 0.245 0.060 -0.415

0,230 0.045 0.090 0.136 0.090 1.636** 0.110 0.178

0.400 0.062 0,120 0.189 0.120 0.107 0,250 0.134

0.490 0,000 0,200 0.040 0.200 0.025 0,400 0,075

0,630 1.243"* 0.260 0.136 0,250 0.160 0,490 0.047

0,750 -0.054 0.400 0.038 0,400 0,065 0.580 0,006

0,850 -0,036 0.490 -0,022 0.490 -0.001 0.650 0.024

0,900 -0,022 0,580 0.025 0.580 -0.052 0.750 0.043

0.960 -0.015 0.640 0.059 0.650 -0.035 0,830 0.064

0,750 0.1 04 0,750 0.1 04 0.900 0.108

0,870 0.065 0.890 0.090 0,960 0.001

0.930 0.019 0.930 0.056

0,960 -0.017 0,960 - 1.475"*

547
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-28-24-000, MINF = 1.197, Camber = 4/-1, ALPT = 7.55, BETA = 0.51, QINF = 565.8,

RNPU = 3.7E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.527 0.000 0.222 0.000 4.295"* 0.010 -0.528

0.060 -0.475 0.020 -0.577 0.020 -0.535 0.020 -0.543

0.110 -0.519 0.040 -0.453 0.060 -2.056** 0.060 -0.570

0.200 -0.585 0.060 -0.524 0.090 -0.521 0.110 -0.514

0.230 -0.503 0.090 -0.497 0.110 -0.602 0.140 -0.464

0.400 -0.251 0.130 -0.539 0.130 -0.583 0.190 -0.997"*

0.490 -0.186 0.150 -0.564 0.150 -0.597 0.250 -0.227

0.590 -0.155 0.200 -0.569 0.210 -0.585 0.400 -0.200

0.630 -0.128 0.250 -0.403 0.250 -0.344 0.490 -0.253

0.700 -0.090 0.260 -0.368 0.340 -0.235 0.580 -0.085

0.750 -0.068 0.280 -0.377 0.370 -0.180 0.650 -0.129

0.810 -0.064 0.290 -0.370 0.400 -0.130 0.700 -0.120

0.840 -0.056 0.310 -0.356 0.410 - 1.525"* 0.750 -0.136

0.900 -0.036 0.320 -0.369 0.430 -0.148 0.800 -0.158

0.960 -0.014 0.340 -0.351 0.440 -0.137 0.830 -0.187

0.350 -0.118 * * 0.460 -0.163 0.900 -0.019

0.370 -0.310 0.490 -0.108 0.960 -0.008

0.380 -0.333 0.500 -0.176

0.400 -0.251 0.520 -0.166

0.410 -0.265 0.540 -0.177

0.430 -0.226 0.550 -0.140

0.440 -0.166 0.580 -0.155

0.460 -0.216 0.600 -0.183

0.470 -0.195 0.610 -0.177

0.490 -0.178 0.650 3.569"*

0.500 -0.181 0.700 -0.170

0.520 -0.179 0.750 -0.246

0.530 -0.170 0.820 -0.260

0.550 -0.185 0.890 -0.242

0.560 -0.189 0.900 -0.216

0.580 -0.186 0.960 -0.063

0.590 -0.194

0.600 -0.203

0.640 -0.201

0.700 -0.217

0.750 -0.013"*

0.820 -0.073

0.870 -0.054

0.930 -0.016

0.960 -0.001

Lower Surface

0.020 0.063 0.020 O. 106 0.020 0.196 0.020 0.277

0.110 0.036 0.060 0.132 0.060 0.184 0.060 -0.437

0.230 0.116 0.090 0.046 0.090 1.942"* 0.110 0.081

0.400 -0.116 0.120 0.090 0.120 -0.005 0.250 0.053

0.490 -0.06d. 0.200 0.122 0.200 0.098 0.400 0.016

0.630 1.499** 0.260 0.039 0.250 0.055 0.490 -0.007

0.750 -0.082 0.400 -0.003 0.400 -0.020 0.580 -0.064

0.850 -0.048 0.490 -0.080 0.490 0.003 0.650 -0.048

0.900 -0.025 0.580 -0.170 0.580 -0.082 0.750 -0.014

0.960 0.011 0.640 0.011 0.650 -0.009 0.830 0.039

0.750 0.098 0.750 0.056 0.900 0.121

0.870 0.061 0.890 0.057 0.960 -0.001

0.930 0.033 0.930 0.039

0.960 0.020 0.960 - 1.571 **

548
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-30-25-000, MINF = 1,218, Camber = 0/2, ALPT = 7.49. BETA = 0,43, QINF = 572.7,

RNPU = 3.7E+06

"q= 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.658 0.000 0.122 0.000 4.265"* 0.010 -0.621

0,060 -0.618 0.020 -0.692 0.020 -0.663 0.020 -0.645

0,110 -0.618 0.040 -0.633 0.060 -2.092** 0,060 -0.597

0.200 -0.581 0.060 -0.640 0.090 -0.620 0.110 -0.521

0.230 -0.465 0.090 -0,589 0.110 -0.662 0.140 -0.407

0.400 -0.221 0.130 -0.599 0.130 -0.610 0.190 -0.964"*

0.490 -0.157 0.150 -0.594 0.150 -0.588 0.250 -0.258

0.590 -0.118 0.200 -0.570 0.2 l0 -0.575 0.400 -0.173

0.630 -0.108 0.250 -0.383 0.250 -0.317 0,490 -0.251

0.700 -0.107 0.260 -0.333 0.340 -0.166 0.580 -0.091

0,750 -0.204 0.280 -0.366 0.370 -0.173 0.650 -0.125

0.810 -0,205 0.290 -0.342 0.400 -0.136 0.700 -0. I 15

0.840 -0.208 0.310 -0,337 0.410 - 1.485** 0.750 -0.135

0.900 -0.084 0.320 -0.340 0.430 -0.154 0.800 -0.150

0.960 -0.033 0.340 -0.329 0.440 -0.143 0.830 -0.183

0.350 -0.186"* 0.460 -0.147 0.900 -0.036

0.370 -0.278 0.490 -0, l 31 0.960 -0.027

0.380 -0.289 0.500 -0.172

0.400 -0.167 0.520 -0.162

0.410 -0.228 0.540 -0.161

0.430 -0.172 0.550 -0.124

0.440 -0,149 0.580 -0.126

0.460 -0.164 0.600 -0.157

0.470 -0.151 0.610 -0.165

0.490 -0.139 0.650 3.547**

0.500 -0.149 0.700 -0.203

0.520 -0.151 0.750 -0.255

0.530 -0.139 0.820 -0.305

0.550 -0.170 0,890 -0.337

0.560 -0.167 0.900 -0,246

0.580 -0.178 0.960 -0.129

0,590 -0.172

0.600 -0.188

0.640 -0.202

0.700 -0.236

0.750 -0.019"*

0,820 -0.123

0.870 -0,072

0.930 -0,035

0.960 -0.012

Lower Surface

0.020 0.084 0.020 0.150 0.020 0.219 0.020 0314

0.110 0.034 0.060 0.135 0.060 0,194 0.060 -0.394

0.230 0.024 0.090 0.052 0.090 1.940 ** 0.110 0.181

0.400 -0,116 0.120 0,061 0.120 0.003 0.250 0,052

0.490 -0,102 0.200 0,073 0.200 0.015 0.400 0,005

0.630 1.502" * 0.260 0.030 0,250 0.023 0.490 -0.011

0.750 -0.030 0.400 -0.029 0.400 -0.011 0.580 -0.065

0.850 -0.015 0.490 -0.082 0.490 -0.022 0.650 -0,059

0.900 0.018 0.580 -0.177 0.580 -0.101 0.750 -0.028

0,960 0.015 0,640 0.072 0.650 -0.026 0.830 0.018

0.750 0.127 0.750 0.096 0.900 0.076

0.870 0.100 0.890 0.127 0.960 -0.012

0.930 0.080 0.930 0.1 04

0.960 0.044 0.960 - 1.107 **

549
Table H-2. Continued.

Flight 218, Wing sweep = 58 °, Time = 10-30-33-000, MINF = 1.220, Camber = 0/2, ALPT = 8.31, BETA = 0.37, QINF = 575.5,

RNPU = 3.7E+06

lq = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.687 0.000 0.089 0.000 4.244"* 0.010 -0.658

0.060 -0.641 0.020 -0.737 0.020 -0.673 0.020 -0.669

0.110 -0.634 0.040 -0.656 0.060 -2.081 ** 0.060 -0.623

0.200 -0.600 0.060 -0.674 0.090 -0.644 0.110 -0.5 l0

0.230 -0.394 0.090 -0.634 0.110 -0.677 0.1 40 -0.455

0.400 -0.286 0.130 -0.640 0.130 -0.639 0.190 -0.959 **

0.490 -0.243 0.150 -0.627 0.150 -0.615 0.250 -0.278

0.590 -0.211 0.200 -0.598 0.210 -0.468 0.400 -0.212

0.630 -0.181 0.250 -0.417 0.250 -0.372 0.490 -0.312

0.700 -0.148 0.260 -0.377 0.340 -0.295 0.580 -0.103

0.750 -0. t 85 0.280 -0.392 0.370 -0.234 0.650 -0.121

0.810 -0.182 0.290 -0.382 0.400 -0.1 44 0.700 -0,122

0.840 -0.173 0.310 -0.367 0.410 -1.478"* 0.750 -0.138

0.900 -0.071 0.320 -0.374 0.430 -0.150 0.800 -0.138

0.960 -0.025 0.340 -0.385 0.440 -0.135 0.830 -0.195

0.350 -0.185"* 0.460 -0.143 0.900 -0.027

0.370 -0,355 0.490 -0.111 0.960 -0.009

0.380 -0.382 0.500 -0.165

0.400 -0.333 0.520 -0.171

0.410 -0.353 0.540 -0.171

0.430 -0.324 0.550 -0.139

0.440 -0.283 0.580 -0.133

0.460 -0.294 0.600 -0.171

0.470 -0.288 0.610 -0.168

0.490 -0.257 0.650 3.530**

0.500 -0.237 0.700 -0.224

0.520 -0.225 0.750 -0.277

0.530 -0.203 0.820 -0.362

0.550 -0.203 0.890 -0.345

0.560 -0.190 0.900 -0.250

0.580 -0.169 0.960 -0.107

0.590 -0.178

0.600 -0.173

0,640 -0.199

0.700 -0.218

0.750 -0.006"*

0.820 -0.082

0.870 -0.042

0.930 -0.017

0.960 -0.021

Lower Surface

0.020 0.109 0.020 0.168 0.020 0.245 0.020 0.360

0.110 0.060 0.060 0.175 0.060 0,225 0.060 -0.373

0.230 0.053 0.090 0.079 0.090 1.931 ** 0. l 10 0.170

0.400 -0.093 0.120 0.101 0.120 0.026 0.250 0.054

0.490 0.003 0.200 0.103 0.200 0.037 0.400 0,032

0.630 1.495** 0.260 0.031 0.250 0,072 0.490 -0.003

0.750 -0.025 0.400 0,018 0.400 0.004 0.580 -0.049

0.850 0.002 0.490 -0.067 0.490 -0.009 0.650 -0.032

0.900 0.031 0.580 -0.161 0.580 -0.063 0.750 0.001

0.960 0.036 0.640 0.100 0.650 -0.015 0.830 0.018

0.750 0.151 0.750 0.126 0.900 0.083

0.870 0.111 0.890 0.142 0.960 -0.010

0.930 0.091 0.930 0.115

0.960 0.051 0.960 - 1.102 * *

550
Table H-2. Continued.

Flight 222, Wing sweep = 58", Time = 11-35-51-500, MINF = 1.395, Camber = 0/2, ALPT = 4.24, BETA = 0.43, QINF = 790.9,

RNPU = 4.9E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x,/c CP

0.020 -0.287 0,000 0,297 0.000 1.305"* 0.010 -0.335

0.060 -0.295 0.020 -0.301 0,020 -0.281 0.020 -0.359

0. 110 -0.287 0.040 -0.285 0.060 -1.526** 0.060 -0.333

0.200 -0.265 0.060 -0.332 0.090 -0,333 0.110 -0.318

0.230 -0.233 0,090 -0.296 0.110 -0.349 0.140 -0.294

0.400 -0.119 0.130 -0.303 0.130 -0.299 0.190 -0.734"*

0.490 -0.076 0. 150 -0.299 0.150 -0.295 0.250 -0.201

0.590 -0.073 0.200 -0,267 0.210 -0.297 0.400 -0.137

0.630 -0.058 0.250 -0.285 0,250 -0.219 0.490 -0.101

0.700 -0.095 0.260 -0.266 0.340 -0.199 0.580 -0.070

0.750 -0.142 0.280 -0.272 0.370 -0.162 0,650 -0.093

0.8 l0 -0. 138 0.290 -0.252 0.400 -0.141 0.700 -0.082

0.840 -0.135 0.310 -0.219 0.410 -0.159 ** 0.750 -0,097

0.900 -0.248 0.320 -0,220 0.430 -0.128 0.800 -0.105

0.960 -0.121 0.340 -0.218 0.440 -0.112 0.830 -0.138

0.350 -0.133"* 0.460 -0.119 0.900 -0.047

0.370 -0.180 0,490 -0.074 0.960 -0.042

0,380 -0.171 0.500 -0.115

0.400 -0.114 0.520 -0.101

0.410 -0.133 0.540 -0.098

0.430 -0.108 0.550 -0,076

0.440 -0,080 0.580 -0.079

0.460 -0.109 0.600 -0.086

0.470 -0.090 0.610 -0.083

0.490 -0.092 0.650 0.785"*

0.500 -0.093 0.700 -0.126

0.520 -0.088 0.750 -0.144

0.530 -0.085 0.820 -0.168

0.550 -0.102 0.890 -0.240

0.560 -0.094 0.900 -0.234

0.580 -0.083 0.960 -0.093

0.590 -0.101

0,600 -0.1 04

0.640 -0.127

0.700 -0.130

0.750 -0.043"*

0.820 -0.097

0.870 -0.122

0.930 -0.216

0.960 -0.089

Lower Surface

0.020 0.000 0.020 0.037 0.020 0.048 0.020 0.193

0. l 10 -0.050 0.060 0.080 0.060 0.039 0.060 0.676" *

0.230 -0.055 0.090 -0.016 0.090 0.405* * 0.1 l0 -0.037

0.400 -0.098 0.120 -0.011 0.120 -0.138 0.250 -0.048

0.490 -0.110 0.200 0.000 0.200 -0,045 0.400 -0.028

0.630 0.698** 0.260 -0.057 0,250 -0.025 0.490 -0.078

0.750 -0.028 0.400 -0.081 0.400 -0,072 0.580 -0.102

0,850 -0.013 0,490 -0.122 0.490 -0.044 0.650 -0.088

0.900 0.011 0.580 -0.165 0.580 -0.142 0.750 -0.096

0.960 0.009 0.640 -0.177 0,650 -0.050 0.830 -0.030

0.750 0.055 0,750 -0.037 0.900 0.024

0.870 0.068 0.890 0.119 0.960 -0.041

0.930 0.059 0.930 0.107

0,960 0.023 0.960 -0.821 **

551
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-36-0-000, MINF = 1.395, Camber = 0/2, ALPT = 3.56, BETA = 0.45, QINF = 789.7,

RNPU = 4.9E+06

rl = 0.93 0.76 0.59 0A0

Upper Surface

x./c CP x./c CP x/c CP x/c CP

0.020 -0.262 0.000 0.306 0.000 1,308"* 0.010 -0.275

0.060 -0.255 0.020 -0.271 0.020 -0.268 0.020 -0.356

O. 110 -0.312 0.040 -0.253 0.060 - 1.527"* 0.060 -0.301

0.200 -0.226 0.060 -0.284 0.090 -0.308 O. 110 -0.280

0.230 -0.204 0.090 -0.263 O. 110 -0.311 O. 140 -0.246

0.400 -0.078 O. 130 -0.283 O. 130 -0.258 O. 190 -0.734**

0.490 -0.062 O. 150 -0.262 O. 150 -0.250 0.250 -0.206

0.590 -0.063 0.200 -0.221 0.210 -0.263 0.400 -0.114

0.630 -0.053 0.250 -0.232 0.250 -0.187 0.490 -0.085

0.700 -0.089 0.260 -0.198 0.340 -0.164 0.580 -0.059

0.750 -0.136 0.280 -0.205 0.370 -0.135 0.650 -0.085

0.810 -0.134 0.290 -0.205 0.400 -0.106 0.700 -0.069

0.840 -0.135 0.310 -0.194 0.410 -0.158"* 0.750 -0.088

0.900 -0.248 0.320 -0.202 0.430 -0.110 0.800 -0.090

0.960 -0.126 0.340 -0.196 0.440 -0.095 0.830 -0.127

0.350 -0.124 ** 0.460 -0.101 0.900 -0.046

0.370 -0.131 0.490 -0.064 0.960 -0.039

0.380 -0.130 0.500 -0.096

0.400 -0.080 0.520 -0.087

0.410 -0.110 0.540 -0.081

0.430 -0.057 0.550 -0.061

0.440 -0.066 0.580 -0.045

0.460 -0.090 0.600 -0.071

0.470 -0.081 0.610 -0.067

0.490 -0.074 0.650 0.788**

0.500 -0.080 0.700 -0.121

0.520 -0.072 0.750 -0.130

0.530 -0.070 0.820 -0.156

0.550 -0.081 0.890 -0.233

0.560 -0.081 0.900 -0.237

0.580 -0.059 0.960 -0.087

0.590 -O.O87

0.600 -0.090

0.640 -0.116

0.700 -0.119

0.750 -0.043**

0.820 -0.099

0.870 -0.117

0.930 -0.207

0.960 -0.099

Lower Surface

0.020 0.017 0.020 -0.008 0.020 0.025 0.020 O. 174

O. 110 -0,064 0.060 0.008 0.060 0.025 0.060 0.678 **

0.230 -0.075 0.090 -0.057 0.090 0.407"* O.110 -0.051

0.400 -0,103 O. 120 -0.007 O.120 -0.143 0.250 -0.064

0.490 -0.117 0.200 -0.015 0.200 -0.067 0.400 -0.032

0.630 0.701 ** 0.260 -0.062 0.250 -0.030 0.490 -0.086

0.750 -0.041 0.400 -0.090 0.400 -0.075 0.580 -0.107

0.850 -0.016 0.490 -0.128 0.490 -0.044 0.650 -0,092

0.900 0.007 0.580 -0.170 0,580 -0.158 0.750 -0.120

0.960 0.014 0.640 -0.189 0.650 -0.049 0.830 -0.030

0.750 0.049 0.750 -0.041 0.900 0.046

0.870 0.083 0.890 O. 115 0.960 -0.040

0.930 0.059 0.930 O. 102

0.960 0.025 0.960 -0. 821 **

552
Table H-2. Continued.

Flighl 222, Wing sweep = 58 °, Time = 11-36-3-500, MINF = 1.399, Camber = 0/2, ALPT = 2.43, BETA = 0.48, QINF = 795.4,

RNPU = 5.0E+06

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.145 0.000 -0.766 0.000 1.298"* 0.010 -0.262

0.060 -0.159 0.020 3.229 0.020 -0.217 0.020 -0.302

0.110 -0.207 0.040 -0.160 0,060 -1.517"* 0.060 -0.260

0.200 -0.145 0,060 2.040 0.090 -0.236 0.110 -0.234

0.230 -0.158 0.090 -0.207 0.110 -0.251 0.140 -0.191

0.400 -0.048 0.130 -0.206 0.130 -0.197 0.190 -0.730**

0.490 -0.045 0.150 -0.188 0.150 -0.183 0.250 -0,179

0.590 -0.065 0.200 -0.142 0.210 -0.197 0.400 -0.091

0,630 -0.052 0.250 -0.179 0.250 -0.160 0.490 -0.058

0.700 -0.091 0.260 -0.167 0.340 -0.129 0.580 -0.048

0.750 -0.138 0.280 -0.175 0.370 -0.108 0.650 -0.070

0.810 -0.301 0.290 -0.185 0.400 -0.098 0.700 -0,050

0.840 -0.749 0.310 -0.166 0.410 -0.158"* 0.750 -0.075

0.900 -0.247 0.320 -0.158 0.430 -0,088 0.800 -0.072

0.960 -0.129 0.340 -0. 130 0,440 -0.072 0.830 -0. I 10

0.350 -0.108"* 0.460 -0.081 0.900 -0.047

0.370 -0.088 0.490 -0.037 0.960 -0.038

0,380 -0.094 0.500 -0.072

0.400 -0.027 0.520 -0.069

0.410 -0.084 0.540 -0.061

0.430 -0.064 0.550 -0,039

0.440 -0.043 0,580 -0.033

0,460 -0.066 0.600 -0.054

0.470 -0.060 0.610 -0.042

0.490 -0.055 0.650 0.781 **

0.500 -0.051 0.700 -0.099

0.520 1.396 0.750 -0.117

0.530 -0.048 0,820 -0.139

0.550 1.572 0.890 -0.224

0.560 -0.065 0,900 -0.223

0.580 -0.055 0.960 -0.087

0.590 -0.072

0.600 -0.061

0.640 -0.105

0.700 -0.104

0.750 -0.047**

0.820 -0.094

0.870 -0.110

0.930 -0.207

0.960 -0.110

Lower Surface

0.020 -0.075 0.020 -0.071 0.020 -0.008 0.020 0.139

0.110 0.478 0.060 -0.010 0.060 -0.001 0.060 0.672* *

0.230 -0.090 0.090 -0.108 0.090 0.402** 0.110 -0.067

0.400 -0.125 0.120 -0.732 0.120 -0.160 0.250 -0.149

0.490 -0.135 0.200 -0.020 0.200 0.399 0.400 -0.050

0.630 0.694"* 0,260 -0,073 0.250 -0.094 0,490 -0.100

0.750 -0.065 0.400 -0.108 0.400 0.708 0,580 -0.126

0.850 -0.026 0.490 -0.144 0.490 -0.050 0.650 -0.112

0.900 0.000 0.580 -0.183 0,580 -0.163 0.750 -0.149

0,960 0.017 0.640 -0.201 0.650 -0.055 0.830 -0.04 1

0.750 0.024 0.750 -0.042 0.900 0.028

0.870 0.046 0.890 0.099 0.960 -0.04 1

0,930 0,099 0.930 0.086

0.960 -0.596 0,960 -0.816**

553
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = l 1-36-6-000, MINF = 1.403, Camber = 0/2, ALPT = 2.48, BETA = 0.48, QINF = 805.4,

RNPU = 5.0E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.139 0.000 0.325 0.000 1.277" * 0.010 -0.258

0.060 -0.180 0.020 -0.216 0.020 -0.210 0.020 -0.297

0.110 -0.225 0.040 -0.158 0.060 - 1.503 ** 0.060 -0.248

0.200 -0.138 0.060 -0.233 0.090 -0.236 0.110 -0.230

0.230 -0.148 0.090 -0.203 0.110 -0.247 0.140 -0.201

0.400 -0.046 0.130 -0.212 0.130 -0.196 0.190 -0.726" *

0.490 -0.046 0.150 -0.184 0.150 -0.179 0.250 -0.176

0.590 -0.062 0.200 -0.141 0.210 -0.196 0.400 -0.089

0.630 -0.055 0.250 -0.175 0.250 -0.157 0.490 -0.056

0.700 -0.091 0.260 -0.164 0.340 -0.132 0.580 -0.035

0.750 -0.134 0.280 -0.179 0.370 -0.100 0.650 -0.068

0.810 -0.134 0.290 -0.182 0.400 -0.082 0.700 -0.052

0.840 -0.136 0.310 -0.166 0.410 -0.161 * * 0.750 -0.075

0.900 -0.244 0.320 -0.164 0.430 -0.085 0.800 -0.065

0.960 -0.128 0.340 -0.131 0.440 -0.072 0.830 -0.107

0.350 -0.106** 0.460 -0.079 0.900 -0.04 1

0.370 -0.087 0.490 -0.038 0.960 -0.038

0.380 -0.093 0.500 -0.070

0.400 -0.050 0.520 -0.064

0.410 -0.082 0.540 -0.060

0.430 -0.062 0.550 -0.042

0.440 -0.042 0.580 -0.031

0.460 -0.066 0.600 -0.052

0.470 -0.058 0.610 -0.04 1

0.490 -0.052 0.650 0.767**

0.500 -0.054 0.700 -0.112

0.520 -0.050 0.750 -0.114

0.530 -0.047 0.820 -0.136

0.550 -0.059 0.890 -0.221

0.560 -0.063 0.900 -0.223

0.580 -0.053 0.960 -0.087

0.590 -0.069

0.600 -0.072

0.640 -0.104

0.700 -0.103

0.750 -0.045"*

0.820 -0.094

0.870 -0.109

0.930 -0.199

0.960 -0.117

Lower Surface

0.020 -0.066 0.020 -0.064 0.020 -0.022 0.020 0.143

0.110 -0.066 0.060 -0.031 0.060 -0.003 0.060 0.659**

0.230 -0.085 0.090 -0.106 0.090 0.393" * 0.110 -0.065

0.400 -0.127 0.120 -0.126 0.120 -0.156 0.250 -0.161

0.490 -0.132 0.200 -0.015 0.200 -0.138 0.400 -0.045

0.630 0.681 ** 0.260 -0.074 0.250 -0.105 0.490 -0.098

0.750 -0.063 0.400 -0.1 04 0.400 -0.088 0.580 -0.123

0.850 -0.023 0.490 -0.140 0.490 -0.049 0.650 -0.113

0.900 0.005 0.580 -0.179 0.580 -0.160 0.750 -0.146

0.960 0.018 0.640 -0.197 0.650 -0.054 0.830 -0.039

0.750 0.031 0.750 -0.035 0.900 0.030

0.870 0.054 0.890 0.102 0.960 -0.039

0.930 0.059 0.930 0.089

0.960 0.031 0.960 -0.811 **

554
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-36-9-000, MINF = 1.408, Camber = 0/2, ALPT = 3.65, BETA = 0.45, QINF = 822.3,

RNPU = 5.1E+06

r I = 0,93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 -0.228 0.000 0,312 0.000 1.241 ** 0.010 -0.272

0.060 -0.241 0.020 -0.246 0.020 -0.266 0.020 -0.340

0,110 -0.232 0.040 -0.247 0,060 - 1.482"* 0.060 -0.288

0.200 -0.226 0.060 -0.284 0.090 -0.273 O. 110 -0.282

0.230 -0.195 0,090 -0.261 0.110 -0.307 0.140 -0.248

0.400 -0.091 0.130 -0.266 0.130 -0.256 0.190 -0.721 **

0.490 -0.067 O. 150 -0.260 O. 150 -0.252 0.250 -0.197

0.590 -0.063 0.200 -0.224 0.210 -0.264 0.400 -0.117

0.630 -0.049 0.250 -0.245 0.250 -0.193 0.490 -0.085

0.700 -0.092 0.260 -0.224 0.340 -0.173 0.580 -0.058

0.750 -0.132 0.280 -0,203 0.370 -0,140 0.650 -0.08 [

0.810 -0.131 0.290 -0.200 0.400 -0.112 0.700 -0.070

0.840 -0.127 0.310 -0.192 0.410 -0.168"* 0.750 -0.092

0.900 -0.238 0.320 -0.193 0.430 -0.110 0.800 -0.073

0.960 -0,133 0.340 -0.198 0.440 -0.091 0.830 -0.121

0.350 -0.132' * 0.460 -0.101 0.900 -0.043

0.370 -0.156 0.490 -0.056 0.960 -0.038

0.380 -0.144 0.500 -0.092

0.400 -0.092 0.520 -0.089

0.410 -0.114 0.540 -0.082

0.430 -0.090 0.550 -0.063

0.440 -0.067 0.580 -0.042

0.460 -0.095 0.600 -0,073

0.470 -0.082 0.610 -0,064

0.490 -0.073 0.650 0,741 **

0.500 -0.054 0.700 -0.112

0.520 -0.077 0.750 -0.129

0.530 -0.068 0.820 -0.149

0.550 -0.083 0.890 -0.229

0.560 -0.079 0.900 -0.235

0.580 -0.068 0.960 -0.087

0.590 -0.086

0.600 -0.088

0.640 -0.117

0.700 -0.118

0.750 -0.041"*

0.820 -0.089

0.870 -0.110

0.930 -0.207

0.960 -0.116

Lower Surface

0.020 0.039 0.020 0.008 0.020 0.033 0.020 O. 185

O. 110 -0.056 0.060 0.013 0.060 0.022 0.060 0.635"*

0.230 -0.066 0,090 -0.050 0.090 0.375** 0.110 -0.048

0.400 -0.099 0.120 -0.001 0.120 -0.134 0.250 -0.061

0.490 -0.109 0.200 -0.005 0.200 -0.059 0.400 -0.033

0.630 0,663"* 0,260 -0.051 0.250 -0.020 0.490 -0.079

0.750 -0.038 0.400 -0.083 0.400 -0.064 0.580 -0.102

0.850 -0.016 0.490 -0.122 0.490 -0.042 0,650 -0.09 l

0.900 0.011 0.580 -0.160 0.580 -0.151 0.750 -0.108

0.960 0.017 0.640 -0.176 0,650 -0.047 0.830 -0.031

0.750 0.049 0.750 -0.039 0.900 0.047

0.870 0.074 0.890 O. 122 0.960 -0.048

0.930 0.064 0,930 O. 107

0.960 0.027 0.960 -0.793"*

555
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = l 1-36-10-500, MINF = 1.410, Camber = 0/2, ALPT = 5.41, BETA = 0.45, QINF = 832.6,

RNPU = 5.2E+06, CNWP = 0.1637

1"1-- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.336 0.000 0.288 0.000 1.2 l 8"* 0.010 -0.365

0.060 -0.319 0.020 -0.369 0.020 -0.333 0.020 -0.373

0.110 -0.379 0.040 -0.315 0.060 - 1.455"* 0.060 -0.364

0.200 0.103 0.060 -0.349 0.090 -0.370 0.110 -0.367

0.230 -0.289 0.090 -0.332 0.110 -0.397 0.140 -0.370

0.400 -0.275 0.130 -0.336 0.130 -0.730 0.190 -0.719 * *

0.490 -0.114 0.150 -0.330 0.150 -0.332 0.250 -0.256

0.590 -0.082 0.200 -0.304 0.210 -0.330 0.400 0.570

0.630 -0.062 0.250 -0.330 0.250 -0.307 0.490 -0.134

0.700 -0.095 0.260 -0.313 0.340 -0.232 0.580 -0.097

0.750 -0.140 0.280 -0.319 0.370 -0.199 0.650 -0.112

0.810 -0.136 0.290 -0.313 0.400 -0.163 0.700 -0.095

0.840 -0.133 0.310 -0,301 0.410 -0.173"* 0.750 -0.103

0.900 -0.244 0.320 -0.302 0.430 -0.154 0.800 -0.091

0.960 -0.110 0.340 -0.304 0.440 -0.138 0.830 -0.142

0.350 -0.163 * * 0.460 -0.140 0.900 -0.050

0.370 -0.268 0.490 -0.103 0.960 -0.045

0.380 -0.253 0.500 -0.127

0.400 -0.174 0.520 -0.121

0.410 -0.188 0.540 -0.117

0.430 -0.151 0.550 -0.093

0.440 -0.125 0.580 -0.082

0.460 -0.141 0.600 -0.789

0.470 -0.131 0.610 -0.098

0.490 0.382 0.650 0.725**

0.500 -0.120 0.700 -0.129

0.520 -0.111 0.750 -0.158

0.530 -0.106 0.820 -0.180

0.550 -0.128 0.890 -0.243

0.560 -0.115 0.900 -0.229

0.580 0.554 0.960 -0,096

0.590 -0.120

0.600 -0,116

0.640 -0.326

0.700 -0.138

0.750 -0.034**

0.820 -0.091

0.870 -0.117

0.930 -0.189

0.960 -0.065

Lower Surface

0.020 0.065 0.020 0.133 0.020 0.096 0.020 0.230

0.110 -0.026 0.060 0.103 0.060 0.075 0.060 0.621 **

0.230 -0.025 0.090 0.007 0.090 0.363"* 0.110 -0.015

0.400 -0.071 0.120 0.003 0.120 -0.042 0.250 -0.028

0.490 -0.079 0.200 0.020 0.200 0.024 0.400 -0.011

0.630 0.648"* 0.260 -0.033 0.250 -0.006 0.490 -0.061

0.750 -0.015 0.400 -0.054 0.400 -0.052 0.580 -0.082

0.850 0.003 0.490 -0.097 0.490 -0.033 0.650 -0.071

0.900 0.025 0.580 -0.146 0.580 -0.129 0.750 -0.048

0.960 0.022 0.640 -0.143 0.650 -0.042 0.830 0.376

0.750 0.070 0.750 -0.040 0.900 0.020

0.870 0.106 0.890 0.129 0.960 -0.078

0.930 0.074 0.930 0.117

0.960 0.034 0.960 -0.791 **

CN = 0.t46 0.177 0.203 0.082

556
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-36-13-000, MINF = 1.405, Camber = 0/2, ALPT = 7.58, BETA = 0.45, QINF = 836.9,

RNPU = 5.2E+06

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.420 0.000 0.217 0.000 1.203"* 0.010 -0.447

0.060 -0.407 0.020 -0.47 l 0.020 -0,424 0.020 -0,470

0.110 -0.398 0.040 -0.419 0.060 - 1.456" * 0.060 -0.449

0.200 -0.391 0.060 -0.428 0.090 -0.422 0. l I 0 -0.444

0.230 -0.296 0.090 -0.420 0.110 -0.468 0.140 -0.444

0.400 -0.353 0.130 -0.419 0.130 -0.436 0.190 -0.724**

0.490 -0.333 0.150 -0.414 0.150 -0.424 0.250 -0.294

0.590 -0.160 0.200 -0.386 0.210 -0.424 0.400 -0.196

0.630 -0.131 0.250 -0.414 0.250 -0.400 0.490 -0.257

0,700 -0.132 0.260 -0.394 0.340 -0.275 0.580 -0.109

0.750 -0.168 0.280 -0.404 0.370 -0.252 0.650 -0.133

0.810 -0.160 0.290 -0.395 0.400 -0.216 0.700 -0.116

0.840 -0. 156 0.310 -0.391 0,410 -0.181 ** 0.750 -0.130

0.900 -0.148 0.320 -0.392 0.430 -0.211 0.800 -0.112

0.960 -0,057 0.340 -0.400 0,440 -0.187 0.830 -0.170

0.350 -0.203"* 0.460 -0.192 0.900 -0,049

0.370 -0.378 0.490 -0.160 0.960 -0.051

0.380 -0.414 0.500 -0.172

0.400 -0.355 0.520 -0,171

0.410 -0.361 0.540 -0.159

0.430 -0.263 0.550 -0.139

0.440 -0.231 0.580 -0.122

0.460 -0.241 0.600 -0.159

0.470 -0.221 0.610 -0.150

0.490 -0,207 0.650 0.712"*

0.500 -0,177 0.700 -0.161

0.520 -0.200 0.750 -0.199

0.530 -0.181 0.820 -0.223

0.550 -0.191 0.890 -0.285

0.560 -0.179 0,900 -0.274

0.580 -0.170 0.960 -0.155

0,590 -0.176

0.600 -0.171

0.640 -0.164

0.700 -0.186

0.750 -0.043**

0.820 -0.107

0.870 -0.117

0,930 -0.077

0.960 -0.047

Lower Surface

0.020 0.123 0,020 0.175 0.020 0.198 0.020 0.274

0.110 0.022 0.060 0.140 0.060 0.175 0.060 0.635' *

0.230 0.020 0.090 0,052 0.090 0.352** 0.110 0.070

0,400 -0.031 O. 120 0.057 0.120 0.023 0.250 0.005

0.490 -0.041 0.200 0,052 0.200 0.031 0.400 0.022

0.630 0.635** 0.260 0.004 0.250 0.023 0.490 -0.027

0.750 0.013 0.400 -0.021 0.400 -0.022 0.580 -0.057

0.850 0.016 0.490 -0.067 0.490 -0.04 1 0.650 -0.044

0.900 0.050 0.580 -0.121 0.580 -0.101 0.750 -0.027

0.960 0.020 0.640 -0.091 0.650 -0.049 0.830 0.003

0.750 0.099 0.750 -0.038 0.900 0.031

0.870 0.093 0,890 0.143 0.960 -0.035

0.930 0.079 0.930 0.113

0.960 0.034 0.960 -0.796**

557
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-36-14-000, M1NF -- 1.400, Camber = 0/2, ALPT = 8.35, BETA = 0.45, QINF = 833.5,

RNPU = 5.2E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0,020 -0.438 0.000 0.199 0.000 1.207 ** 0.010 -0.471

0.060 -0.432 0,020 -0,507 0.020 -0,466 0.020 -0.493

0.110 -0.427 0.040 -0.449 0.060 -1.464** 0,060 -0,477

0.200 -0.417 0.060 -0.465 0.090 -0,468 0.110 -0,470

0.230 -0.384 0,090 -0.450 0. 110 -0.496 0.140 -0,469

0,400 -0.377 0.130 -0.446 0.130 -0.460 0.190 -0.729* *

0.490 -0.350 0.150 -0,443 0.150 -0,448 0.250 -0.312

0.590 -0.198 0.200 -0.415 0,210 -0.449 0,400 -0.213

0,630 -0.169 0.250 -0.441 0.250 -0.429 0.490 -0,292

0,700 -0.1 64 0,260 -0.419 0.340 -0.291 0.580 -0.124

0.750 -0.198 0.280 -0.432 0.370 -0.271 0,650 -0.132

0.810 -0.185 0.290 -0,425 0.400 -0.258 0.700 -0,118

0.840 -0.183 0,310 -0.417 0.410 -0.183"* 0,750 -0,129

0.900 -0.102 0.320 -0.418 0.430 -0,256 0,800 -0.119

0,960 -0.062 0.340 -0.426 0.440 -0.239 0.830 -0.177

0,350 -0.211 ** 0,460 -0.239 0,900 -0,058

0.370 -0.408 0.490 -0.219 0.960 -0.053

0.380 -0,439 0,500 -0,210

0.400 -0.320 0,520 -0.197

0,410 -0.310 0.540 -0.181

0,430 -0.271 0,550 -0.158

0.440 -0.246 0,580 -0.117

0.460 -0.264 0.600 -0.157

0.470 -0,252 0.610 -0.148

0,490 -0,240 0.650 0.735**

0.500 -0,238 0.700 -0.170

0.520 -0.233 0.750 -0.204

0,530 -0.226 0.820 -0.258

0.550 -0.235 0.890 -0.303

0.560 -0.228 0.900 -0.298

0.580 -0.218 0.960 -0.172

0.590 -0,226

0.600 -0.215

0.640 -0.189

0.700 -0.213

0.750 -0.046**

0.820 -0.108

0.870 -0,098

0.930 -0.109

0.960 -0.071

Lower Surface

0.020 0.132 0.020 0.185 0.020 0.214 0.020 0.305

0.110 0.037 0.060 0.148 0.060 0.221 0.060 0.636**

0.230 0.031 0.090 0.063 0,090 0,379** 0.110 0.086

0.400 -0.008 0.120 0.066 0.120 0.028 0.250 0,060

0.490 -0.024 0.200 0.069 0,200 0,027 0.400 0,029

0.630 0.636** 0.260 0.021 0.250 0,029 0,490 -0,015

0.750 0.019 0,400 -0.012 0,400 -0.015 0.580 -0.048

0.850 0.02 t 0,490 -0.062 0.490 -0.045 0,650 -0.032

0.900 0.058 0.580 -0.112 0.580 -0.095 0,750 -0,020

0,960 0.018 0.640 -0.085 0,650 -0,053 0,830 0,008

0.750 0.101 0,750 -0.045 0.900 0.033

0,870 0.100 0.890 0.155 0,960 -0,039

0.930 0.079 0.930 0.120

0.960 0.032 0,960 -0.800**

558
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-36-16-000, MINF = 1.385, Camber = 0/2, ALPT = 8.95, BETA = 0.40, QINF = 816.0,

RNPU = 5.1E+06

1] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0,470 0.000 0.164 0.000 1.232** 0.010 -0,495

0.060 -0.472 0.020 °0,544 0.020 -0,509 0.020 -0.525

0. I 10 -0.463 0.040 -0,486 0,060 - 1.495"* 0.060 -0.501

0,200 -0,450 0.060 -0.503 0,090 -0,496 0.110 -0.490

0.230 -0.425 0,090 -0.481 0.110 -0,529 0,140 -0.498

0.400 -0.413 0.130 -0,478 0.130 -0.493 0.190 -0,744 **

0,490 -0.321 0.150 -0,479 0.150 -0,482 0.250 -0.335

0,590 -0.231 0.200 -0.450 0.210 -0.482 0,400 -0.231

0.630 -0.202 0,250 -0.470 0.250 -0,460 0.490 -0,346

0.700 -0,203 0.260 -0,451 0.340 -0.319 0.580 -0.159

0.750 -0.228 0.280 -0,463 0.370 -0.326 0.650 -0,140

0.810 -0,216 0.290 -0.459 0.400 -0,299 0.700 -0.119

0.840 -0.206 0,310 -0,449 0.410 -0.187"* 0.750 -0.135

0.900 -0.119 0.320 -0.451 0.430 -0,289 0,800 -0.128

0.960 -0.095 0.340 -0.458 0,440 -0.273 0,830 -0.183

0.350 -0.221 * * 0.460 -0,276 0.900 -0,063

0.370 -0,358 0.490 -0.232 0.960 -0.058

0,380 -0,344 0.500 -0,227

0,400 -0.316 0.520 -0.213

0.410 -0.3 l I 0,540 -0.186

0.430 -0,287 0.550 -0.149

0.440 -0.270 0.580 -0.151

0.460 -0.284 0.600 -0.160

0.470 -0.287 0.610 -0.152

0,490 -0.276 0,650 0.745"*

0,500 -0.26t 0.700 -0.191

0.520 -0.281 0.750 -0.227

0.530 -0.261 0.820 -0,272

0.550 -0.282 0.890 -0.315

0,560 -0,280 0,900 -0.318

0.580 -0,275 0.960 -0_184

0,590 -0.270

0.600 -0.262

0,640 -0.227

0.700 -0,246

0,750 -0,051 **

0.820 -0.112

0,870 -0,086

0,930 -0.133

0.960 -0.095

Lower Surface

0,020 0.153 0,020 0.188 0.020 0.236 0,020 0.308

0.110 0.044 0.060 0.159 0.060 0.215 0,060 0,639 **

0.230 0.043 0.090 0.073 0.090 0.381 ** O. 110 0.097

0.400 -0.028 O. 120 0.083 O.120 0.023 O.250 O. 1O0

0.490 -0.037 0.200 0.075 0.200 0.022 0.400 0.034

0.630 0.650'* 0.260 0.034 0.250 0.036 0.490 -0.558

0.750 0.012 0.400 -0.004 0.400 -0.003 0.580 -0.043

0.850 0.024 0.490 -0.052 0.490 -0.048 0.650 -0.033

0.900 0.055 0,580 -0.106 0.580 -0,084 0.750 -0.012

0.960 0,014 0.640 -0.084 0.650 -0.057 0.830 0.014

0,750 0.107 0.750 -0.052 0,900 0.038

0,870 0.097 0.890 0.158 0,960 -0.033

0,930 0.075 0.930 0.117

0,960 0.027 0,960 -0.818**

559
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 1142-6-000, MINF = 1.403. Camber = 1/2, ALPT = 4.20, BETA = 0.40, QINF = 786.1,

RNPU = 4.9E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.242 0.000 0.313 0.000 1.337"* 0.010 -0.295

0.060 -0.249 0.020 -0.257 0.020 -0.275 0.020 -0.351

0.110 -0.247 0.040 -0.249 0.060 - 1.505"* 0.060 -0.318

0.200 -0.260 0.060 -0.285 0.090 -0.309 0.110 -0.310

0.230 -0.246 0.090 -0.264 0.110 -0.322 0.140 -0.287

0,400 -0.144 0.130 -0.281 0.130 -0.281 0.190 -0.726" *

0.490 -0.080 0.150 -0.283 0.150 -0.283 0.250 -0.233

0.590 -0.076 0,200 -0.261 0.210 -0,294 0.400 -0.136

0.630 -0.058 0.250 -0.286 0,250 -0.221 0.490 -0.100

0.700 -0.099 0.260 -0.271 0.340 -0.210 0.580 -0.069

0,750 -0.150 0.280 -0.275 0.370 -0.168 0.650 -0.088

0.810 -0.148 0.290 -0.265 0.400 -0.134 0.700 -0.081

0.840 -0.1 44 0.310 -0.231 0.410 -0.147 * * 0.750 -0.105

0.900 -0.261 0.320 -0.231 0.430 -0.133 0.800 -0,087

0.960 -0.126 0.340 -0.222 0.440 -0.115 0.830 -0.134

0.350 -0.136 ** 0.460 -0.118 0.900 -0.045

0.370 -0.192 0.490 -0.070 0.960 -0.040

0.380 -0.191 0.500 -0.110

0,400 -0.134 0.520 -0.106

0.410 -0.141 0.540 -0.097

0.430 -0.112 0.550 -0.073

0.440 -0.089 0.580 -0.051

0.460 -0.113 0.600 -0,085

0.470 -0.1 04 0.610 -0.077

0.490 -0,093 0.650 0.820**

0.500 -0.090 0,700 -0.128

0.520 -0.098 0.750 -0.139

0.530 -0.085 0.820 -0.169

0.550 -0,098 0.890 -0.245

0.560 -0.090 0.900 -0.238

0.580 -0.082 0.960 -0.091

0.590 -0.097

0.600 -0.103

0.640 -0.126

0.700 -0.131

0.750 -0.046**

0.820 -0.100

0.870 -0.128

0.930 -0.223

0.960 -0.093

Lower Surface

0.020 0.021 0.020 0.014 0.020 0.026 0.020 0.175

0.110 -0.051 0.060 0.037 0.060 0.025 0.060 0.710"*

0.230 -0.097 0.090 -0.008 0.090 0.443** 0.110 -0.035

0.400 -0.095 0.120 -0.009 0.120 -0.114 0.250 -0,046

0.490 -0.100 0.200 -0.001 0.200 -0,025 0.400 -0,026

0.630 0.721 ** 0.260 -0,048 0.250 -0,021 0.490 -0.080

0.750 -0.035 0.400 -0,083 0.400 -0.071 0.580 -0. I 01

0.850 -0.007 0.490 -0.120 0.490 -0.046 0.650 -0.078

0.900 0.012 0.580 -0.1 64 0.580 -0.1 44 0.750 -0.113

0.960 0.011 0,640 -0.180 0.650 -0,052 0.830 -0.030

0.750 0.054 0.750 -0.034 0.900 0.024

0.870 0.077 0.890 0.126 0.960 -0.042

0.930 0.059 0.930 0.112

0.960 0.027 0,960 -0,802"*

560
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 1t-42-18-000, MINF = 1.404, Camber = 1/2, ALP'I" = 3.93, BETA = 0.43, QINF = 785.5,

RNPU = 4.9E+06

_1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 -0.177 0.000 0.312 0,000 1.340"* 0,010 -0.262

0.060 -0.208 0.020 -0.234 0.020 -0.256 0.020 -0.342

0.110 -0,233 0.040 -0.230 0.060 - 1.505"* 0.060 -0.300

0.200 -0.245 0.060 -0.266 0.090 -0.292 0.110 -0.294

0.230 -0.245 0,090 -0.249 0.110 -0.303 0.140 -0.272

0.400 -0.122 0.130 -0.267 0.130 -0.271 0.190 -0.725" *

0.490 -0.078 0.150 -0.269 0.150 -0,265 0.250 -0.215

0.590 -0.071 0.200 -0.247 0.210 -0.282 0.400 -0.126

0.630 -0.055 0.250 -0.275 0.250 -0.214 0.490 -0.091

0.700 -0.097 0.260 -0.257 0,340 -0.197 0.580 -0.058

0.750 -0.147 0.280 -0.258 0.370 -0.148 0.650 -0,087

0.810 -0.141 0,290 -0.224 0.400 -0.121 0.700 -0.071

0.840 -0.143 0.310 -0.211 0.410 -0.146"* 0.750 -0.098

0.900 -0.259 0.320 -0.211 0.430 -0.120 0.800 -0.083

0.960 -0.124 0.340 -0.213 0.440 -0.106 0.830 -0.129

0.350 -0.126"* 0.460 -0.111 0.900 -0.044

0.370 -0.181 0,490 -0,086 0.960 -0.039

0.380 -0.172 0.500 -0.107

0.400 -0.112 0.520 -0.099

0.410 -0.130 0.540 -0.085

0.430 -0.1 04 0,550 -0.069

0.440 -0,083 0,580 -0.056

0.460 -0.102 0.600 -0.079

0.470 -0.092 0.610 -0.071

0.490 -0.084 0.650 0.822**

0,500 -0.082 0.700 -0,120

0.520 -0.082 0.750 -0.133

0,530 -0,077 0.820 -0.161

0.550 -0.093 0.890 -0.240

0.560 -0.089 0.900 -0,235

0.580 -0.078 0.960 -0.089

0.590 -0.094

0.600 -0.096

0.640 -0.121

0.700 -0.125

0.750 -0.044"*

0.820 -0,096

0.870 -0.125

0.930 -0.223

0.960 -0.094

Lower Surface

0.020 0.019 0.020 -0.025 0.020 0.016 0.020 0.171

0.110 -0.060 0.060 0.035 0.060 0.022 0.060 0.712**

0.230 -0.106 0.090 -0.042 0.090 0.445 ** 0.110 -0.049

0.400 -0.101 0.120 -0.005 0.120 -0.116 0.250 -0.055

0.490 -0.108 0.200 -0.005 0.200 -0.036 0.400 -0.028

0,630 0.723** 0.260 -0.049 0.250 -0.028 0.490 -0.078

0,750 -0.038 0.400 -0.085 0.400 -0.071 0.580 -0.107

0.850 -0.012 0.490 -0.118 0.490 -0.045 0.650 -0.085

0.900 0.012 0.580 -0.163 0.580 -0.148 0,750 -0.115

0.960 0.012 0.640 -0.182 0.650 -0,050 0.830 -0.035

0.750 0.052 0.750 -0.031 0.900 0.035

0.870 0.075 0.890 0.125 0,960 -0.038

0.930 0.066 0.930 0.110

0.960 0.027 0.960 -0.801 **

561
Table H-2. Continued.

Hight 222, Wing sweep = 58 °, Time = I 1-42-26-500, MINF = 1.406, Camber = 0/3, ALPT = 3.51, BETA = 0.43, QINF = 788.3,

RNPU = 4.9E+06

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.155 0.000 0.318 0.000 1.335"* 0.010 -0.261

0.060 -0.197 0.020 -0.198 0.020 -0.240 0.020 -0.333

O. 1 lO -0.219 0.040 -0.214 0.060 -1.500** 0.060 -0.283

0.200 -0.215 0.060 -0.254 0.090 -0.283 O. 110 -0.27 l

0.230 -0.216 0.090 -0.232 0.110 -0.271 O. 140 -0.231

0.400 -0.088 O.130 -0.244 O.130 -0.252 O. 190 -0.722 **

0.490 -0.059 O.150 -0.247 O.150 -0.242 0.250 -0.199

0.590 -0.068 0.200 -0.215 0.210 -0.256 0.400 -0.113

0.630 -0.051 0.250 -0.245 0.250 -0.194 0.490 -0.080

0.700 -0.095 0.260 -0.209 0.340 -0.179 0.580 -0.049

0.750 -0.149 0.280 -0.204 0.370 -0.142 0.650 -0.081

0.810 -0.127 0.290 -0.204 0.400 -0.110 0.700 -0.063

0.840 -0.145 0.310 -0.196 0.410 -0.145"* 0.750 -0.097

0.900 -0.263 0.320 -0.197 0.430 -0.120 0.800 -0.080

0.960 -0.124 0.340 -0.208 0.440 -0.097 0.830 -0.121

0.350 -0.126** 0.460 -0. I O0 0.900 -0.044

0.370 -0.154 0.490 -0.054 0.960 -0.036

0.380 -0.142 0.500 -0.091

0.400 -0.086 0.520 -0.085

0.410 -0.113 0.540 -0.080

0.430 -0.088 0.550 -0.055

0.440 -0.070 0.580 -0.043

0.460 -0.088 0.600 -0.075

0.470 -0.087 0.610 -0.060

0.490 -0.074 0.650 0.819"*

0.500 -0.069 0.700 -0.112

0.520 -0.070 0.750 -0.124

0.530 -0.067 0.820 -0.156

0.550 -0.082 0.890 -0.238

0,560 -0.079 0.900 -0.232

0.580 -0.065 0.960 -0.085

0.590 -0.083

0.600 -0.088

0.640 -0.118

0.700 -0.119

0.750 -0.044**

0.820 -O.093

0.870 -0.124

0.930 -0.224

0.960 -0.097

Lower Surface

0.020 0.007 0.020 -0.034 0.020 0.007 0.020 O. 163

O. 110 -0.071 0.060 -0.007 0.060 0.017 0.060 0.709 **

0.230 -0.105 0.090 -0.079 0.090 0.443** O. 110 -0.057

0.400 -0.105 O. 120 -0.016 O. 120 -0.112 0.250 -0.082

0.490 -0.127 0.200 -0.008 0.200 -0.062 0.400 -0.039

0.630 0.721 ** 0.260 -0.052 0.250 -0.028 0.490 -0.084

0.750 -0.038 0.400 -0.093 0.400 -0.073 0.580 -0.118

0.850 -0.010 0.490 -0.126 0.490 -0.046 0.650 -0.085

0.900 0.013 0.580 -0.167 0.580 -0.150 0.750 -0.133

0.960 0.017 0.640 -0.187 0.650 -0.053 0.830 -0.035

0.750 0.049 0,750 -0.032 0.900 0.053

0.870 0.075 0.890 O.123 0.960 -0.043

0.930 0.070 0.930 O. 107

0.960 0.032 0.960 -0.798**

562
Table H-2. Continued,

Flight 222, Wing sweep = 58 °, Time = 11-42-29-500, MINF = 1.409, Camber = 0/3, ALPT = 2,38, BETA = 0.45, QINF = 792.6,

RNPU = 4.9E+06

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.122 0.000 0.324 0.000 1.327"* O.OlO -0.247

0,060 -0.162 0.020 -0.161 0.020 -0.200 0.020 -0.277

0.110 -0.161 0.040 -0.161 0.060 -1.492"* 0.060 -0.243

0.200 -0.134 0.060 -0.218 0.090 -0.225 0.110 -0.211

0.230 -0.174 0.090 -0.192 0A 10 -0.224 0.140 -0.164

0.400 -0.044 0.130 -0.184 0.130 -0.184 0.190 -0,719"*

0.490 -0.034 0.150 -0.171 0.150 -0.168 0.250 -0.177

0.590 -0.054 0.200 -0.124 0.210 -0.192 0.400 -0.091

0.630 -0.057 0.250 -0.166 0.250 -0.161 0.490 -0.052

0.700 -0.096 0.260 -0.159 0.340 -0.130 0.580 -0.030

0.750 -0. 168 0.280 -0.175 0.370 -0.103 0.650 -0.068

0.810 -0.160 0.290 -0.180 0.400 -0.082 0,700 -0.052

0.840 -0.168 0.310 -0,165 0.410 -0.145"* 0.750 -0.075

0.900 -0.286 0.320 -0.159 0.430 -0.086 0.800 -0.064

0.960 -0.113 0.340 -0.127 0.440 -0.074 0.830 -0.108

0.350 -0.112"* 0.460 -0.077 0.900 -0.04 1

0.370 -0.087 0.490 -0.037 0.960 -0.039

0.380 -0.091 0.500 -0.063

0.400 -0.049 0.520 -0.060

0.410 -0.075 0.540 -0.059

0.430 -0.052 0.550 -0.031

0.440 -0.044 0.580 -0.025

0.460 -0.056 0.600 -0.046

0.470 -0.060 0.610 -0.045

0.490 -0.051 0.650 0.814"*

0.500 -0.044 0.700 -0.099

0.520 -0.047 0.750 -0.112

0.530 -0.040 0.820 -0.147

0.550 -0.062 0.890 -0.245

0.560 -0.055 0.900 -0.222

0.580 -0.044 0.960 -0.079

0.590 -0.063

0.600 -0.057

0.640 -0.102

0.700 -0.105

0,750 -0.038"*

0.820 -0.096

0.870 -0.134

0.930 -0.240

0.960 -0.092

Lower Surface

0.020 -0.066 0.020 -0.090 0.020 -0.033 0.020 O. 138

O.110 -0,148 0.060 -0.038 0.060 -0.003 0.060 0.705"*

0.230 -0.09 l 0.090 -0. 110 0.090 0.440** O. 110 -0.057

0.400 -0.126 O. 120 -0.133 O. 120 -0.135 0.250 -0.187

0.490 -0.135 0.200 -0.055 0.200 -0. 139 0.400 -0.047

0.630 0.716 ** 0.260 -0.066 0,250 -0.125 0.490 -0.104

0.750 -0.047 0.400 -0.109 0.400 -0.092 0.580 -0,131

0.850 -0.007 0.490 -0.147 0.490 -0.045 0.650 -0.102

0.900 0.019 0.580 -0.180 0.580 -0.167 0.750 -0.165

0.960 0.015 0.640 -0.204 0.650 -0.048 0.830 -0.048

0.750 0.043 0.750 -0.034 0.900 0.026

0.870 0.070 0.890 O. 138 0.960 -0.044

0.930 0.081 0.930 0.114

0.960 0.037 0.960 -0.794'*

563
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-42-30-500, MINF = 1.411, Camber = 0/3, ALPT = 2.38, BETA = 0.45, QINF = 795.2,

RNPU = 4.9E+06

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.I 17 0,000 0.329 0.000 1.322"* 0.010 -0.255

0.060 -0.162 0.020 -0.185 0.020 -0.194 0.020 -0.279

0.110 -0.160 0.040 -0,153 0.060 - 1.488" * 0.060 -0.237

0.200 -0.133 0.060 -0.218 0,090 -0.233 0.110 -0,205

0.230 -0.147 0.090 -0.187 0.110 -0.220 0.140 -0,137

0.400 -0.035 0.130 -0.174 0.130 -0.179 0,190 -0.718"*

0.490 -0.041 0.150 -0.161 0.150 -0.153 0,250 -0.169

0.590 -0,055 0.200 -0.122 0.210 -0.183 0.400 -0.086

0.630 -0.048 0.250 -0.167 0.250 -0.155 0.490 -0.050

0.700 -0.093 0.260 -0.160 0.340 -0.128 0.580 -0.025

0.750 -0.167 0.280 -0.170 0.370 -0.098 0.650 -0.063

0.810 -0.164 0.290 -0.173 0.400 -0,077 0.700 -0.053

0.840 -0.168 0.310 -0.156 0.410 -0.146* * 0.750 -0.073

0.900 -0.293 0.320 -0.153 0.430 -0.080 0.800 -0.062

0.960 -0.111 0.340 -0.127 0.440 -0.069 0.830 -0.103

0.350 -0.107 ** 0.460 -0.072 0,900 -0.039

0.370 -0.081 0.490 -0.038 0.960 -0.034

0.380 -0.088 0.500 -0.068

0.400 -0.032 0.520 -0.061

0.410 -0.076 0.540 -0.054

0.430 -0.057 0.550 -0,032

0.440 -0.051 0,580 -0.025

0,460 -0.057 0.600 -0.044

0.470 -0.058 0.610 -0.040

0.490 -0,045 0.650 0.811 **

0.500 -0.044 0.700 -0.091

0.520 -0.060 0.750 -0.105

0.530 -0.040 0.820 -0.152

0.550 -0.050 0.890 -0.242

0.560 -0.056 0.900 -0.224

0.580 -0.048 0,960 -0.075

0.590 -0.064

0.600 -0.063

0.640 -0.097

0.700 -0.100

0,750 -0.038"*

0.820 -0.094

0.870 -0.130

0.930 -0.234

0.960 -0.085

Lower Surface

0.020 -0.091 0,020 -0.081 0.020 -0.022 0.020 0.137

0.110 -0.150 0.060 -0,034 0.060 -0.009 0.060 0.702**

0.230 -0.083 0.090 -0.104 0.090 0.438** 0.110 -0,060

0,400 -0.127 0.120 -0.125 0.120 -0.130 0.250 -0.184

0.490 -0.136 0.200 -0.067 0.200 -0.136 0.400 -0.054

0.630 0.713"* 0.260 -0.069 0,250 -0.119 0.490 -0.099

0.750 -0.036 0.400 -0.105 0.400 -0.087 0.580 -0.130

0.850 -0.001 0,490 -0.143 0.490 -0.046 0.650 -0.097

0.900 0.024 0.580 -0.181 0.580 -0.161 0.750 -0.160

0.960 0.018 0.640 -0.198 0.650 -0.049 0.830 -0.043

0.750 0.042 0.750 -0.029 0.900 0.030

0.870 0.071 0.890 0.137 0.960 -0.033

0.930 0.080 0.930 0.122

0.960 0.047 0,960 -0,793**

564
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-42-32-500, MINF = 1.411, Camber = 0/3, ALPT = 4.74, BETA = 0.40, QINF = 800.8,

RNPU = 5.0E+06

T1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.273 0.000 0.295 0.000 1.307"* 0.010 -0.321

0.060 -0,269 0.020 -0.260 0.020 -0.285 0,020 -0.360

0.110 -0.268 0.040 -0.272 0.060 -1.483** 0.060 -0.343

0.200 -0.274 0.060 -0.309 0.090 -0.331 0.110 -0.330

0.230 -0.263 0.090 -0.285 0.110 -0.343 0.140 -0.315

0.400 -0.209 0.130 -0.298 0.130 -0.312 0.190 -0.718"*

0.490 -0.094 0.150 -0.302 0.150 -0.290 0.250 -0.244

0.590 -0.084 0,200 -0.275 0.210 -0.306 0.400 -0.149

0.630 -0.057 0.250 -0.299 0.250 -0.263 0.490 -0.115

0.700 -0.100 0.260 -0.284 0.340 -0.223 0.580 -0.077

0.750 -0.157 0.280 -0.290 0.370 -0.188 0.650 -0.098

0.810 -0.148 0.290 -0.287 0.400 -0.154 0.700 -0.091

0.840 -0.153 0.310 -0.273 0.410 -0.150"* 0,750 -0.111

0.900 -0.272 0.320 -0.273 0.430 -0.142 0.800 -0.083

0.960 -0.121 0.340 -0.254 0.440 -0.128 0.830 -0.141

0.350 -0.139"* 0.460 -0.131 0.900 -0.045

0.370 -0.210 0.490 -0.083 0,960 -0.040

0.380 -0.217 0.500 -0.119

0.400 -0.164 0,520 -0A 17

0.410 -0.169 0.540 -0.105

0.430 -0.131 0.550 -0,083

0.440 -0.114 0.580 -0.050

0.460 -0.124 0.600 -0.092

0.470 -0.116 0.610 -0.086

0.490 -0.104 0.650 0.800"*

0.500 -0.1 04 0,700 -0.128

0.520 -0.091 0.750 -0.1 44

0.530 -0.094 0.820 -0.174

0.550 -0.096 0.890 -0.251

0.560 -0.105 0.900 -0.223

0.580 -0.090 0.960 -0.092

0,590 -0.122

0,600 -& 107

0.640 -0.130

0.700 -0.136

0.750 -0.044**

0,820 -0.097

0.870 -0.132

0.930 -0,226

0.960 -0,076

Lower Surface

0.020 0.036 0,020 0.039 0.020 0.055 0.020 0.195

0.110 -0.046 0.060 0.070 0.060 0.040 0.060 0.691 **

0.230 -0.072 0.090 -0.002 0.090 0.429"* 0.110 -0.031

0.400 -0.089 0.120 -0.001 0.120 -0.099 0.250 -0.043

0.490 -0.101 0.200 0.012 0.200 -0.015 0.400 -0.022

0.630 0.703"* 0.260 -0.041 0.250 -0.019 0.490 -0.070

0.750 -0,024 0.400 -0.074 0.400 -0.066 0.580 -0.097

0.850 -0.002 0.490 -0.112 0.490 -0.043 0,650 -0.078

0.900 0.020 0.580 -0. 158 0.580 -0.136 0.750 -0.093

0,960 0.011 0.640 -0.169 0.650 -0.051 0.830 -0.029

0.750 0.062 0.750 -0.032 0.900 0.017

0.870 0.072 0.890 0.136 0.960 -0.039

0.930 0.068 0.930 0.121

0.960 0.030 0.960 -0.793"*

565
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-42-34-000, MINF -- 1.408, Camber = 1/1, ALPT = 6.44, BETA -- 0.43, QINF -- 802.3,

RNPU = 5.0E+06

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.331 0.000 0.279 0.000 1.301"* 0.010 -0,369

0.060 -0.311 0.020 -0.373 0.020 -0.328 0.020 -0.423

O. 110 -0.313 0.040 -0.312 0.060 - 1.485"* 0.060 -0.382

0.200 -0.347 0.060 -0.348 0.090 -0.378 O. 110 -0.385

0.230 -0.283 0.090 -0.338 O. 110 -0.396 O. 140 -0.408

0.400 -0.325 O. 130 -0.342 O.130 -0.379 O. 190 -0.721 **

0.490 -0.285 O. 150 -0.358 O. 150 -0.383 0.250 -0.268

0.590 -0.126 0.200 -0.342 0.210 -0.381 0.400 -0.179

0.630 -0.098 0.250 -0.377 0.250 -0.361 0.490 -0.182

0.700 -0.116 0.260 -0.361 0.340 -0.277 0.580 -0.113

0.750 -0.135 0.280 -0.367 0.370 -0.239 0.650 -0.129

0.810 -0.128 0.290 -0.364 0.400 -0.199 0.700 -0.115

0.840 -0.126 0.310 -0.353 0.410 -0.154"* 0.750 -0.118

0.900 -0.213 0,320 -0.354 0.430 -0.191 0.800 -0.097

0.960 -0.082 0.340 -0.364 0.440 -0.171 0.830 -0.161

0.350 -0.174 * * 0.460 -0.169 0.900 -0.043

0.370 -0.346 0.490 -0.126 0.960 -0.034

0.380 -0.374 0.500 -0.154

0.400 -0.321 0.520 -0.142

0.410 -0.318 0.540 -0.139

0.430 -0.224 0.550 -0.115

0.440 -0.198 0.580 -0.102

0.460 -0.201 0.600 -0.130

0.470 -0.184 0.610 -0.119

0.490 -0.1 64 0.650 0.794**

0.500 -0.163 0.700 -0.152

0.520 -0.156 0.750 -0.172

0.530 -0.142 0.820 -0.187

0.550 -0.153 0.890 -0.234

0.560 -0.151 0.900 -0.223

0.580 -0.133 0.960 -0.107

0.590 -0.143

0.600 -0.146

0.640 -0.153

0.700 -0.160

0.750 -0.035"*

0.820 -0.096

0.870 -0.113

0.930 -0.126

0.960 -0.051

Lower Surface

0.020 0.070 0.020 O. 117 0.020 0.096 0.020 0.215

O. 110 -0.004 0.060 O. 107 0.060 O. 135 0.060 0.686**

0.230 -0.056 0.090 0,021 0.090 0.424** O. 110 0.002

0.400 -0.032 O. 120 0.032 O. 120 -0.003 0.250 -0.029

0.490 -0.069 0.200 0.017 0.200 0.050 0.400 0.004

0.630 0.697 ** 0.260 -0.001 0.250 0.008 0.490 -0.043

0.750 -0.032 0.400 -0.039 0.400 -0.040 0.580 -0.079

0.850 -0.018 0.490 -0.083 0.490 -0.031 0.650 -0.058

0.900 0.004 0.580 -0.138 0.580 -0.118 0.750 -0.048

0.960 0.008 0.640 -0.132 0.650 -0.041 0.830 -0.010

0.750 0.075 0.750 -0.025 0.900 0.027

0.870 0.065 0.890 O.110 0.960 -0.032

0.930 0.052 0.930 0.091

0.960 0.015 0.960 -0.795"*

566
Table H-2. Continued,

Flight 222, Wing sweep = 58", Time = 11-42-35-000, MINF = 1.405, Camber = 2/0, ALPT = 7.35, BETA = 0.43, QINF = 800.8,

RNPU = 5,0E+06

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.358 0.000 0,262 0.000 1.301 ** 0.010 -0.387

0.060 -0.331 0.020 -0.411 0.020 -0,352 0.020 -0.434

0.110 -0,350 0.040 -0.337 0.060 - 1.489"* 0.060 -0.432

0.200 -0.388 0.060 -0.379 0.090 -0.415 0.110 -0.435

0.230 -0.354 0.090 -0.363 0.110 -0.429 0.140 -0.445

0.400 -0.367 0.130 -0.381 0.130 -0.407 0.190 -0.724 * *

0.490 -0.346 0.150 -0.395 0.150 -0.411 0.250 -0.297

0.590 -0.175 0.200 -0.383 0.210 -0.422 0.400 -0.202

0.630 -0.146 0.250 -0.4 l 8 0.250 -0.407 0.490 -0.234

0,700 -0.139 0.260 -0.399 0.340 -0.308 0.580 -0.123

0.750 -0.132 0.280 -0.406 0.370 -0.265 0.650 -0.131

0.810 -0.119 0.290 -0.406 0.400 -0.234 0.700 -0.117

0.840 -0.115 0.310 -0.394 0.410 -0.156"* 0.750 -0.131

0.900 -0.140 0.320 -0.396 0.430 -0.227 0,800 -0.109

0,960 -0.047 0.340 -0.403 0.440 -0.206 0.830 -0.168

0.350 -0.172"* 0.460 -0.202 0,900 -0,037

0.370 -0.384 0.490 -0.162 0.960 -0.038

0.380 -0.421 0.500 -0.180

0,400 -0.348 0.520 -0.169

0.410 -0.403 0.540 -0.156

0.430 -0.325 0.550 -0.132

0.440 -0,286 0.580 -0.130

0.460 -0.260 0,600 -0.145

0.470 -0.249 0.610 -0.141

0.490 -0.222 0.650 0.793**

0.500 -0.216 0.700 -0.166

0.520 -0.211 0.750 -0.182

0.530 -0.194 0.820 -0.197

0.550 -0.203 0.890 -0.238

0,560 -0.190 0.900 -0.219

0.580 -0.185 0.960 -0.126

0.590 -0.187

0.600 -0.175

0.640 -0.167

0.700 -0.181

0,750 -0.037**

0.820 -0.089

0.870 -0.098

0.930 -0.108

0,960 -0.059

Lower Surface

0.020 0.088 0.020 0.143 0.020 0.170 0.020 0.223

0.110 0.014 0.060 0.126 0.060 0.168 0.060 0.685**

0.230 -0.019 0.090 0.040 0.090 0.423** 0.110 0.038

0.400 -0.038 0.120 0.053 0.120 0.037 0.250 -0.006

0.490 -0.055 0.200 0.044 0.200 0.048 0_400 0.025

0.630 0.696** 0.260 0.012 0.250 0.026 0.490 -0.03 I

0.750 -0.039 0.400 -0.024 0.400 -0,022 0.580 -0.060

0,850 -0.029 0.490 -0.064 0.490 -0.027 0.650 -0.052

0.900 -0.010 0.580 -0.126 0.580 -0.106 0.750 -0.039

0.960 0,002 0.640 -0.109 0.650 -0.040 0.830 0.004

0.750 0.064 0.750 -0.027 0.900 0.038

0.870 0.056 0.890 0.085 0.960 -0.029

0.930 0.035 0,930 0.067

0.960 -0.002 0.960 -0.799**

567
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-42-36-500, MINF = 1.397, Camber = 3/-1, ALPT = 8.55, BETA = 0.45, QINF = 793.3,

RNPU = 4.9E+06

lq = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.365 0.000 0.254 0.000 1.312"* 0.010 -0.399

0.060 -0.349 0.020 -0,437 0.020 -0.374 0.020 -0.423

0.110 -0.380 0.040 -0.349 0.060 - 1.505 ** 0.060 -0.461

0.200 -0.43 ! 0.060 -0.378 0.090 -0.420 0.110 -0.459

0.230 -0.429 0.090 -0.384 0.1 l0 -0.454 0.140 -0.496

0.400 -0,406 0.130 -0.408 0.130 -0.451 0.190 -0.732" *

0.490 -0.384 0.150 -0.434 0.150 -0.457 0.250 -0.322

0.590 -0.256 0.200 -0.428 0.210 -0.466 0.400 -0.242

0,630 -0.205 0.250 -0.461 0.250 -0.454 0.490 -0.340

0.700 -0.182 0.260 -0.442 0.340 -0.335 0.580 -0.145

0.750 -0.166 0.280 -0.450 0.370 -0.328 0.650 -0.141

0,810 -0.146 0.290 -0.447 0.400 -0.305 0.700 -0.127

0.840 -0,139 0.310 -0.438 0.410 -0.159 * * 0.750 -0.136

0.900 -0.086 0.320 -0.44 1 0.430 -0.315 0.800 -0.118

0.960 -0.056 0.340 -0.449 0.440 -0.297 0.830 -0.180

0.350 -0.143"* 0.460 -0.300 0.900 -0.041

0.370 -0.430 0.490 -0.248 0.960 -0.036

0.380 -0.469 0.500 -0.254

0.400 -0.415 0.520 -0.229

0.410 -0.384 0,540 -0.190

0.430 -0.308 0.550 -0.145

0.440 -0,288 0.580 -0.120

0.460 -0.301 0.600 -0.149

0.470 -0.292 0.610 -0.144

0,490 -0.276 0.650 0.800**

0.500 -0.279 0.700 -0.192

0.520 -0.275 0.750 -0.191

0.530 -0.268 0.820 -0.211

0.550 -0.278 0.890 -0.273

0.560 -0.277 0.900 -0,266

0.580 -0.269 0.960 -0.171

0.590 -0.273

0.600 -0.280

0.640 -0.224

0.700 -0.234

0.750 -0.036"*

0.820 -0.098

0.870 -0.077

0.930 -0,115

0,960 -0.087

Lower Surface

0.020 0.107 0.020 0.154 0.020 0.194 0.020 0.251

0.110 0.038 0.060 0.147 0.060 0.194 0.060 0.691"*

0.230 0.089 0.090 0.062 0.090 0.426"* 0.110 0.061

0.400 -0.012 0.120 0.080 0.120 0.043 0.250 0.080

0,490 -0.034 0.200 0.084 0.200 0.085 0.400 0,044

0.630 0.702"* 0.260 0.044 0.250 0.043 0.490 -0.012

0.750 -0.035 0.400 -0.001 0.400 -0.006 0.580 -0.045

0.850 -0.034 0.490 -0.050 0.490 -0.028 0.650 -0.034

0.900 -0.009 0.580 -0.108 0.580 -0,086 0.750 -0,022

0.960 -0.007 0.640 -0.093 0.650 -0.036 0.830 0.019

0.750 0.073 0.750 -0.028 0,900 0.044

0.870 0,042 0.890 0.079 0.960 -0.028

0.930 0.029 0.930 0.059

0.960 -0.011 0.960 -0,807**

568
Table H-2. Continued.

Flight 222, Wing sweep = 58 °, Time = 11-42-38-000, MINF = 1.387, Camber = 5/-1, ALPT = 9.32, BETA = 0.45, QINF = 779.3,

RNPU = 4.9E+06

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.366 0.000 0.254 0.000 1.339"* 0.010 -0.410

0.060 -0.351 0.020 -0.404 0.020 -0.381 0.020 -0.442

O. 110 -0.377 0.040 -0.348 0.060 - 1.529"* 0.060 -0.472

0.200 -0.456 0.060 -0.394 0.090 -0.431 O.110 -0.486

0.230 -0.432 0.090 -0,398 O. 110 -0.469 O. 140 -0.522

0.400 -0.445 O. 130 -0.423 O. 130 -0.478 O. 190 -0.743" *

0.490 -0.405 O. 150 -0.457 O.150 -0,488 0.250 -0.347

0.590 -0.271 0.200 -0.458 0.210 -0.495 0.400 -0.263

0.630 -0.223 0.250 -0.498 0.250 -0.492 0.490 -0.357

0.700 -0.207 0.260 -0.473 0.340 -0.373 0.580 -0.195

0.750 -0.193 0.280 -0.481 0.370 -0.367 0.650 -0.151

0.810 -0.169 0.290 -0.475 0.400 -0.370 0,700 -0.128

0.840 -0.161 0.310 -0.467 0.410 -0.159'* 0.750 -0.135

0.900 -0. 102 0.320 -0.468 0.430 -0.399 0.800 -0.119

0,960 -0.088 0.340 -0,478 0.440 -0.377 0.830 -0.179

0.350 -0,134** 0.460 -0.383 0.900 -0.042

0.370 -0.457 0.490 -0.339 0.960 -0.037

0.380 -0.424 0.500 -0.337

0.400 -0.324 0.520 -0.281

0.410 -0.351 0.540 -0.183

0.430 -0.330 0.550 -0.128

0.440 -0.309 0.580 -0.105

0.460 -0.332 0.600 -0.163

0.470 -0.328 0.610 -0.165

0.490 -0.313 0.650 0.817"*

0.500 -0,318 0.700 -0.210

0.520 -0.331 0.750 -0.214

0.530 -0.315 0.820 -0.241

0.550 -0.311 0.890 -0.275

0.560 -0.319 0.900 -0.305

0.580 -0.318 0.960 -0.200

0.590 -0.322

0.600 -0.315

0.640 -0.279

0.700 -0.297

0.750 -0.037**

0.820 -0.155

0.870 -0.147

0.930 -0.074

0.960 -0.065

Lower Surface

0.020 O. 126 0.020 O. 156 0,020 0.195 0.020 0.254

O. 110 0.056 0.060 O. 162 0.060 0,205 0.060 0.706' *

0.230 O. 104 0.090 0.083 0.090 0.436"* O. 110 0.059

0.400 -0.003 O. 120 0.097 O. 120 0.064 0.250 O.101

0.490 -0.009 0.200 O. 110 0.200 0.099 0.400 0.054

0.630 0.717'* 0,260 0,061 0.250 0.059 0.490 0.001

0.750 -0.036 0.400 0.007 0.400 0.013 0.580 -0.033

0.850 -0.034 0.490 -0.033 0.490 -0.032 0.650 -0.020

0.900 -0.002 0.580 -0.102 0.580 -0.077 0.750 -0.015

0.960 -0.018 0.640 -0.092 0.650 -0.040 0.830 0.029

0,750 0.071 0.750 -0.037 0.900 0.051

0.870 0.027 0.890 0.085 0.960 -0,023

0.930 0.026 0.930 0.057

0,960 -0.012 0.960 -0.819"*

569
Table H-2. Concluded.

Flight 222, Wing sweep = 58 °, Time = 11-42-40-000, MINF = 1.369, Camber = 5/-1, ALPT = 9.50, BETA = 0.48, QINF = 750.7,

RNPU = 4.7E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP .r./c CP

0.020 -0.355 0.000 0.246 0.000 1.398"* 0.010 -0.412

0.060 -0.314 0.020 -0.399 0.020 -0.380 0.020 -0.460

0.110 -0.396 0.040 -0.353 0.060 - 1.579"* 0.060 -0.491

0.200 -0.482 0.060 -0.388 0.090 -0.449 0.110 -0.514

0.230 -0.458 0.090 -0.407 0. l 10 -0.492 0.140 -0.552

0.400 -0.462 0.130 -0.44 1 0.130 -0.491 0.190 -0.763"*

0.490 -0.330 0.150 -0.479 0.150 -0,492 0.250 -0.364

0.590 -0.281 0,200 -0.477 0.210 -0.518 0.400 -0.265

0.630 -0.232 0.250 -0.520 0.250 -0.434 0.490 -0.357

0.700 -0.227 0.260 -0.492 0.340 -0.390 0.580 -0.202

0.750 -0.210 0.280 -0.506 0.370 -0.397 0.650 -0.162

0.810 -0.181 0.290 -0.502 0.400 -0.385 0.700 -0.133

0.840 -0.180 0.310 -0.488 0.410 -0.157" * 0.750 -0.147

0.900 -0.124 0.320 -0.491 0.430 -0.418 0.800 -0.130

0.960 -0.103 0.340 -0.462 0.440 -0.403 0.830 -0.188

0.350 -0.125'* 0.460 -0.410 0.900 -0.036

0.370 -0.354 0.490 -0.353 0.960 -0.048

0.380 -0.375 0.500 -0.320

0.400 -0.320 0.520 -0.241

0.410 -0.356 0.540 -0.158

0.430 -0.347 0.550 -0.135

0.440 -0.322 0.580 -0.153

0.460 -0.349 0.600 -0.178

0.470 -0.345 0.610 -0.175

0.490 -0.339 0.650 0.856**

0.500 -0.342 0.700 -0.220

0.520 -0.344 0.750 -0.239

0.530 -0.337 0.820 -0.300

0.550 -0.332 0.890 -0.286

0.560 -0.339 0.900 -0.307

0.580 -0.342 0.960 -0.192

0.590 -0.349

0.600 -0.344

0.640 -0.309

0.700 -0.335

0.750 -0.034**

0.820 -0.204

0.870 -0.157

0.930 -0.065

0.960 -0.056

Lower Surface

0.020 0.105 0.020 0.135 0.020 0.180 0.020 0.243

0.110 0.055 0.060 0.161 0.060 0.187 0.060 0.741"*

0.230 0.098 0.090 0.076 0.090 0.461 ** 0.110 0.035

0.400 -0.015 0.120 0.087 0.120 0.050 0.250 0.085

0.490 -0.034 0.200 0.106 0.200 0.100 0.400 0.054

0.630 0.753** 0.260 0.066 0.250 0.067 0,490 0.000

0.750 -0.044 0.400 0.004 0.400 0.006 0.580 -0.026

0.850 -0.029 0.490 -0.043 0.490 -0.025 0.650 -0.022

0.900 -0.016 0.580 -0.086 0.580 -0.064 0.750 -0.019

0.960 -0.026 0.640 -0.112 0.650 -0.039 0.830 0.019

0.750 0.061 0.750 -0.030 0.900 0,054

0.870 0.045 0.890 0.079 0.960 -0.035

0.930 0.018 0.930 0.052

0.960 0.006 0.960 -0.842'*

570
APPENDIX I

Wing Pressure Coefficients for Dynamic Pressures From

80 to 300 lb/ft 2 and Mach Numbers From 0.28 to 0.59.

Leading-edge wing sweep is 26 ° unless otherwise indicated at flight number. Table I-1 contains a summary of

the data listing in table I-2. The asterisks (*) in table 1-2 indicate invalid values. Camber is _)LE/TE"Refer to

Nomenclature for definitions.

Table I-1. Summary of data.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

216 9-1-1-000 0.499 0/2 6.00 0.37 299.9 3.6E+06 0.2065

216 9-1-30-000 0.500 0/2 6.30 0.34 300.8 3.6E+06 0.2135

216 9-1-47-000 0.496 0/2 7.06 -0.41 295.1 3.6E+06 0.2285

216 9-2-1-500 0.500 0/2 8.07 0.25 297.4 3.6E+06 0.2661

216 9-3-38-000 0.497 0/2 3.98 0.48 293.0 3.5E+06 0.1361

216 9-5-50-500 0.502 10/2 6.22 0.45 304.1 3.6E+06 0.2446

216 9-6-12-000 0.500 10/2 8.02 0.95 302.4 3.6E+06 0.3026

216 9-7-33-500 0.505 10/2 3.44 0.66 303.3 3.6E+06 0.1656

216 9-10-16-500 0.499 10/10 4.02 0.37 299.6 3.6E+06 0.3256

216 9-10-54-000 0.497 10/11 4.06 -0.04 297.6 3.6E+06 0.3149

216 9-11-16-000 0.507 10/10 8.00 0.05 307.2 3.6E+06 0.4295

216 9-11-52-500 0.498 10/10 3.13 0.57 298.6 3.6E+06 0.2945

192 10-44-34-000 0.506 5/10 11.09 0.05 123.6 1.5E+06 0.5703

192 10-51-35-500 0.508 0/10 12.22 0.76 134.1 1.6E+06 0.3622

192 11-13-15-500 0.497 10/16 10.03 -0.72 118.0 1.4E+06 0.5683

2011 9-54-1-000 0.519 15/10 3.93 0.83 276.0 3.2E+06 0.3442

2011 9-54-22-000 0.508 15/10 4.00 0.86 273.4 3.2E+06 0.3278

2011 9-55-2-500 0.407 20/18 4.05 1.12 189.8 2.7E+06 0.4625

2011 9-55-27-000 0.368 20/17 5.12 0.89 161.9 2.6E+06 0.4656

2011 9-55-44-500 0.345 20/17 6.02 0.63 145.7 2.4E+06 0.5411

2011 9-56-4-500 0.315 20/18 7.26 0.66 124.2 2.3E+06 0.6770

2011 9-56-37-500 0.289 20/17 7.93 0.89 107.3 2.1E+06 0.7357

2011 9-57-0-000 0.279 20/17 9.10 0.95 101.4 2.1E+06 0.8558

2011 9-58-22-500 0.268 20/17 9.90 1.32 97.7 2.1E+06 0.9262

2011 9-52-31-000 0.592 15/10 3.01 0.89 309.7 3.2E+06 0.2814

2011 9-54-25-500 0.496 15/9 4.02 1.21 262.9 3.2E+06 0.3380

2011 9-54-29-500 0.484 15/10 5.03 0.86 251.8 3.1E+06 0.3694

2011 9-55-45-500 0.344 20/17 6.03 0.63 144.5 2.4E+06 0.5245

lWing sweep of 9 ° 2Wing sweep of 16°

571
TableI-1.Concluded.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

2011 9-56-19-500 0.289 20/18 8.02 0.74 105.5 2.1E+06 0.6455

2011 9-56-58-000 0.280 20/18 8.98 1.35 101.7 2.1E+06 0.8802

2222 12-20-11-500 0.306 20/18 10.03 1.03 95.6 1.8E+06 0.6852

2222 12-20-15-000 0.304 20/18 9.97 0.72 94.6 1.8E+06 0.6993

2222 12-21-25-000 0.295 20/18 10.05 1.21 89.3 1.7E+06 0.6392

2222 12-22-23-000 0.285 20/18 11.58 0.83 83.3 1.7E+06 0.7351

IWing sweep of 9 ° 2Wing sweep of 16°

572
Table I-2. Listing of data.

Flight 216, Wing sweep = 26 °, Time = 9-1-1-000, MINF = 0.499, Camber = 0/2, ALP'I" = 6.00, BETA = 0.37, QINF = 299.9,

RNPU = 3.6E+06, CNWP = 0.2065

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x,/c CP

0.020 -0.461 0.000 0.629 0.000 0.393"* 0.010 - 1.496

0.060 -0.308 0.020 -0.821 0.020 - 1.050 0.020 - 1.047

0.110 -0.286 0.040 -0.515 0.060 -0.356"* 0.060 -0.791

0.200 -0.244 0.060 -0.546 0.090 -0.535 0.110 -0.595

0.230 -0.270 0.090 -0.422 0.110 -0.510 0.140 -0.566

0.400 -0.210 0.130 -0.414 0.130 -5.742 ** 0.190 -5.742 * *

0.490 -0.189 0.150 -0.379 0.150 -0.452 0.250 -0.450

0.590 -0.214 0.200 -0.361 0.210 -0.467 0.400 -0.385

0.630 -0.214 0.250 -0.331 0.250 -0.408 0.490 -0.312

0.700 -0.229 0.260 -0.335 0.340 -0.382 0.580 -0.291

0.750 -0.221 0.280 -0.329 0.370 -0.369 0.650 -0.347

0.810 -0.190 0.290 -0.320 0.400 -0.312 0.700 -0.305

0.840 -0.218 0.310 -0.306 0.410 - 1.240"* 0.750 -0.315

0.900 -0.150 0.320 -0.327 0.430 -0.346 0.800 -0.289

0.960 -0.041 0.340 -0.310 0.440 -0.332 0.830 -0.279

0.350 -0.156"* 0.460 -0.326 0.900 -0.192

0.370 -0.303 0.490 -0.310 0.960 -0.036

0.380 -0.315 0.500 -0.311

0.400 -0.279 0.520 -0.335

0_410 -0.288 0.540 -0.314

0.430 -0.266 0.550 -0.294

0.440 -0.264 0.580 -0.300

0.460 -0.257 0.600 -0.305

0.470 -0.300 0.610 -0.302

0.490 -0.290 0.650 -0.383

0.500 -0.288 0.700 -0.321

0.520 -0.258 0.750 -0.306

0.530 -0.268 0.820 -0.293

0.550 -0.294 0.890 -0. 150

0.560 -0.304 0.900 -0.133

0.580 -0.259 0.960 -0.011

0.590 -0.281

0.600 -0.267

0.640 -0.302

0.700 -0.284

0.750 -0.072**

0.820 -0.257

0.870 -0.218

0.930 -0.112

O.960 -0.054

Lower Surface

0.020 0.006 0.020 0.151 0.020 0.255 0.020 0.569

0.110 -0.093 0.060 0.085 0.060 0.168 0.060 -0.032

0.230 -0.007 0.090 0.059 0.090 0.096 0.110 0.131

0.400 -0.054 0.120 0_001 0.120 -0.040 0.250 -0.109

0.490 -0.031 0.200 -0.013 0.200 0.042 0.400 -0.109

0.630 0.787** 0.260 -0.063 0.250 -0.080 0.490 -0.121

0.750 -0.007 0.400 -0.069 0.400 -0.084 0.580 -0.152

0.850 0.029 0.490 -0.092 0.490 -0.074 0.650 -0.075

0.900 0.122 0.580 -0.116 0.580 -0.133 0.750 0.125

0.960 0.103 0.640 0.020 0.650 -0.080 0.830 0.228

0.750 0.129 0.750 -0.038 0.900 0.264

0.870 0.208 0.890 0.251 0.960 0.213

0.930 0.168 0.930 0.199

0.960 0.125 0.960 0.203

CN = 0.196 0.322 0.322 0.389

573
Table 1-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-1-30-000, MINF = 0.500, Camber = 0/2, ALPT = 6.30, BETA = 0.34, QINF = 300.8,

RNPU = 3.6E+06, CNWP = 0.2135

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.513 0.000 0.580 0.000 0.346** 0.010 - 1.583

0.060 -0.342 0.020 -0.910 0.020 - 1.153 0.020 - 1.124

0.110 -0.317 0.040 -0.557 0.060 -0.405" * 0.060 -0.807

0.200 -0.253 0.060 -0.602 0.090 -0.577 0.110 -0.629

0.230 -0.266 0.090 -0.444 0.110 -0.533 0.140 -0.580

0.400 -0.228 0.130 -0.449 0.130 -5.721 * * 0.190 -5.721 * *

0.490 -0.194 0.150 -0.400 0.150 -0.487 0.250 -0.474

0.590 -0.207 0.200 -0.374 0.210 -0.481 0.400 -0.388

0.630 -0,218 0.250 -0.354 0.250 -0.419 0.490 -0.313

0.700 -0.229 0.260 -0.352 0.340 -0.379 0.580 -0.298

0.750 -0.236 0.280 -0.343 0.370 -0.381 0.650 -0.349

0.810 -0.201 0.290 -0.334 0.400 -0.337 0.700 -0.312

0.840 -0.219 0.310 -0.319 0.410 - 1.233" * 0.750 -0.325

0.900 -0.144 0.320 -0.350 0.430 -0.358 0.800 -0.289

0.960 -0.038 0.340 -0.320 0.440 -0.338 0.830 -0.276

0.350 -0.153** 0.460 -0.333 0.900 -0.189

0.370 -0.310 0.490 -0.321 0.960 -0.025

0.380 -0.339 0.500 -0.326

0.400 -0.286 0.520 -0.345

0.410 -0.312 0.540 -0.324

0.430 -0.274 0.550 -0.303

0.440 -0.284 0.580 -0.296

0.460 -0.266 0.600 -0.314

0.470 -0.290 0.610 -0.326

0.490 -0.305 0.650 -0.392

0.500 -0.290 0.700 -0.329

0.520 -0.263 0.750 -0.306

0.530 -0.289 0.820 -0.290

0.550 -0.300 0.890 -0.151

0.560 -0.321 0.900 -0.130

0.580 -0.255 0.960 -0.019

0.590 -0.282

0.600 -0.273

0.640 -0.305

0.700 -0.288

0.750 -0.063**

0.820 -0.258

0.870 -0.222

0.930 -0.101

0.960 -0.055

Lower Surface

0.020 0.049 0.020 0.188 0.020 0.287 0.020 0.581

0.110 -0.077 0.060 0.136 0.060 0.196 0.060 -0.029

0.230 0.003 0.090 0.079 0.090 0.108 0.110 0.153

0.400 -0.051 0.120 -0.014 0.120 -0.020 0.250 -0.110

0.490 -0.028 0.200 0.001 0.200 0.052 0.400 -0.099

0.630 0.789** 0.260 -0.053 0.250 -0.066 0.490 -0.111

0.750 0.011 0.400 -0.055 0.400 -0.082 0.580 -0.1 44

0.850 0.028 0.490 -0.081 0.490 -0.085 0.650 -0.086

0.900 0.107 0.580 -0.106 0.580 -0.123 0.750 0.127

0,960 0,101 0.640 0.013 0.650 -0.064 0.830 0.230

0.750 0.131 0.750 -0.049 0.900 0.271

0.870 0.192 0.890 0.260 0.960 0.215

0.930 0.156 0.930 0.187

0.960 0.119 0.960 0.197

CN = 0.210 0.340 0.338 0.404

574
Table I-2. Continued.

Flight 216, Wing sweep = 26 °. Time = 9-1-47-000, MINF = 0.496, Camber = 0/2, ALPT = 7.06, BETA = -0.41, QINF = 295.1,

RNPU = 3.6E+06, CNWP = 0.2285

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.639 0.000 0.429 0.000 0.277 ** 0.010 -2.050

0.060 -0.356 0.020 - I. l 13 0.020 - 1.353 0.020 - 1.228

0.110 -0.333 0.040 -0.669 0.060 -0.499** 0.060 -0.905

0.200 -0.282 0.060 -0.674 0.090 -0.618 0.110 -0.673

0.230 -0.302 0.090 -0.494 0.110 -0.587 0.140 -0.606

0.400 -0.224 0.130 -0.481 0.130 -5.801"* 0.190 -5.801"*

0.490 -0.209 0.150 -0.442 0.150 -0.520 0.250 -0.495

0.590 -0.238 0.200 -0.414 0.210 -0.516 0.400 -0.422

0.630 -0.242 0.250 -0.385 0.250 -0.447 0.490 -0.331

0.700 -0.239 0.260 -0.384 0.340 -0.414 0.580 -0.316

0.750 -0.236 0.280 -0.379 0.370 -0.416 0.650 -0.363

0.810 -0.217 0.290 -0.356 0.400 -0.334 0.700 -0.330

0.840 -0.217 0.310 -0.356 0.410 -1.226"* 0.750 -0.329

0.900 -0.165 0.320 -0.359 0.430 -0.377 0.800 -0.278

0.960 -0.065 0.340 -0.338 0.440 -0.353 0.830 -0.269

0.350 -0.159** 0.460 -0.343 0.900 -0.181

0.370 -0.343 0.490 -0.325 0.960 -0.023

0.380 -0.339 0.500 -0.330

0.400 -0.301 0.520 -0.352

0.410 -0.328 0.540 -0.328

0.430 -0.302 0.550 -0.321

0.440 -0.286 0.580 -0.314

0.460 -0.281 0.600 -0.330

0.470 -0.313 0.610 -0.315

0.490 -0.306 0.650 -0.454

0.500 -0.288 0.700 -0.355

0.520 -0.281 0.750 -0.313

0.530 -0.289 0.820 -0.302

0.550 -0.303 0.890 -0.152

0.560 -0.331 0.900 -0.130

0.580 -0.272 0.960 -0.002

0.590 -0.317

0.600 -0.286

0.640 -0.330

0.700 -0.313

0.750 -0.065**

0.820 -0.268

0.870 -0.228

0.930 -0.108

0.960 -0.049

Lower Surface

0.020 0.124 0.020 0.265 0.020 0.368 0.020 0.622

0.110 -0.049 0.060 0.190 0.060 0.249 0.060 -0.04 1

0.230 0.025 0.090 0.130 0.090 0.164 0. 110 0.200

0.400 -0.020 0.120 0.028 0.120 0.011 0.250 -0.056

0.490 -0.018 0.200 0.032 0.200 0.069 0.400 -0.069

0.630 0.845"* 0.260 -0.026 0.250 -0.039 0.490 -0.084

0.750 0.002 0.400 -0.035 0.400 -0.056 0.580 -0.124

0.850 0.031 0.490 -0.075 0.490 -0.063 0.650 -0.049

0.900 0.106 0.580 -0.086 0.580 -0.115 0.750 0.128

0.960 0.101 0.640 0.04 1 0.650 -0.063 0.830 0.237

0.750 0.145 0.750 -0.033 0.900 0.273

0.870 0.207 0.890 0.253 0.960 0.215

0.930 0.172 0.930 0.208

0.960 0.128 0.960 0.169

CN = 0.237 0.388 0.375 0.448

575
Table I-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-2-1-500. MINF = 0.500, Camber = 0/2, ALPT -- 8.07, BETA = 0.25, QINF -- 297.4,

RNPU = 3.6E+06, CNWP = 0.2661

vl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.927 0.000 0.050 0.000 -0.024 * * 0.010 -2.959

0.060 -0.525 0.020 - 1.531 0.020 - 1.858 0.020 -1.472

0.110 -0.424 0.040 -0.097 0.060 -0.575** 0.060 -1.058

0.200 -0.331 0.060 -0.828 0.090 -0.751 0.1 l0 -0.774

0.230 -0.380 0.090 -0.631 0.110 -0.702 0.140 -0.711

0.400 -0.275 0.130 -0.588 0.130 -5.715'* 0.190 -5.715"*

0.490 °0.243 0.150 -0.534 0.150 -0.579 0.250 -0.535

0.590 -0.251 0.200 -0.492 0.210 -0.598 0.400 -0.441

0.630 -0.251 0.250 -0.433 0.250 -0.518 0.490 -0.349

0.700 -0.262 0.260 -0.438 0.340 -0.472 0.580 -0.316

0.750 -0.255 0.280 -0.425 0.370 -0.448 0.650 -0.362

0.8 l0 -0.239 0.290 -0.407 0.400 -0.385 0.700 -0.325

0.840 -0.254 0.310 -0.392 0.410 - 1.176** 0.750 -0.314

0.900 -0.185 0.320 -0.407 0.430 -0.414 0.800 -0.263

0.960 -0.080 0.340 -0.392 0.440 -0.393 0.830 -0.260

0.350 -0.186 ** 0.460 -0.384 0.900 -0.145

0.370 -0.375 0.490 -0.369 0.960 -0.024

0.380 -0.384 0.500 -0.367

0.400 -0.333 0.520 -0.385

0.410 -0.356 0.540 -0.354

0.430 -0.322 0.550 -0.343

0.440 -0.322 0.580 -0.334

0.460 -0.328 0.600 -0.367

0.470 -0.345 0,610 -0.341

0.490 -0.337 0.650 -0.446

0.500 -0.336 0.700 -0.350

0.520 -0.312 0.750 -0.323

0.530 -0.331 0.820 -0.301

0.550 -0.339 0.890 -0.166

0.560 -0.341 0.900 -0,131

0.580 -0.312 0.960 -0.004

0.590 -0.338

0.600 -0.310

0.640 -0.348

0.700 -0.316

0.750 -0.059**

0.820 -0.279

0.870 -0.238

0.930 -0.116

0.960 -0.062

Lower Surface

0.020 0.257 0.020 0.424 0.020 0.511 0.020 0.711

0.110 0.003 0.060 0.282 0.060 0.346 0.060 -0.042

0.230 0.054 0.090 0.190 0.090 0.251 0.110 0.299

0.400 -0.025 0.120 0.100 0.120 0.110 0.250 -0.017

0.490 -0.005 0.200 0.082 0.200 0.128 0.400 -0.04 1

0.630 0.896** 0.260 0.020 0.250 0.008 0.490 -0.054

0.750 -0.003 0.400 -0.013 0.400 -0.032 0.580 -0.105

0.850 0.018 0.490 -0.043 0.490 -0.068 0.650 -0.049

0.900 0.107 0.580 -0.075 0.580 -0.101 0.750 0.135

0.960 0.087 0.640 0.043 0.650 -0.050 0.830 0.238

0.750 0.142 0.750 -0.034 0.900 0,275

0.870 0.195 0.890 0.264 0.960 0.209

0.930 0.173 0.930 0.204

0.960 0.125 0.960 0.176

CN = 0.293 0.448 0.44 1 0.501

576
Table i-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-3-38-000, MINF = 0.497, Camber = 0/2, ALPT = 3.98, BETA = 0.48, QINF = 293.0,

RNPU = 3.5E+06, CNWP = 0.1361

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.075 0.000 0.803 0.000 0.707"* 0.010 -0.804

0.060 -0.125 0.020 -0.270 0.020 -0.466 0.020 -0.592

0.1 l0 -0.162 0.040 -0.188 0.060 -0.144** 0.060 -0.500

0.200 -0.171 0.060 -0.301 0.090 -0.329 0.110 -0.419

0.230 -0.183 0.090 -0.240 0.110 -0.309 0.140 -0.408

0.400 -0.165 0.130 -0.261 0.130 -5.788 * * 0.190 -5.788 **

0.490 -0.160 0.150 -0.254 0.150 -0.310 0.250 -0.372

0.590 -0.190 0.200 -0.247 0.210 -0.337 0.400 -0.319

0.630 -0.190 0.250 -0.233 0.250 -0.309 0.490 -0.263

0.700 -0.210 0.260 -0.248 0.340 -0.302 0.580 -0.256

0.750 -0.210 0.280 -0.241 0.370 -0.301 0.650 -0.320

0.810 -0.173 0.290 -0.249 0.400 -0.254 0.700 -0.281

0.840 -0.204 0.310 -0.236 0.410 - 1.180** 0.750 -0.296

0.900 -0.133 0.320 -0.255 0.430 -0.289 0.800 -0.281

0.960 -0.027 0.340 -0.238 0.440 -0.277 0.830 -0.269

0.350 -0.138"* 0.460 -0.271 0.900 -0.208

0.370 -0.242 0.490 -0.258 0.960 -0.011

0.380 -0.254 0.500 -0.272

0.400 -0.218 0.520 -0.276

0.410 -0.237 0.540 -0.263

0.430 -0.212 0.550 -0.249

0.440 -0.212 0.580 -0.246

0.460 -0.214 0.600 -0.274

0.470 -0.245 0.610 -0.265

0.490 -0.239 0.650 -0.360

0.500 -0.239 0.700 -0.291

0.520 -0.220 0.750 -0.279

0.530 -0.234 0.820 -0.272

0.550 -0.256 0.890 -0.144

0.560 -0.253 0.900 -0.125

0.580 -0.214 0.960 -0.011

0.590 -0.262

0.600 -0.234

0.640 -0.269

0.700 -0.261

0.750 -0.070**

0.820 -0.240

0+870 -0.204

0.930 -0.103

0.960 -0.058

Lower Surface

0.020 -0.288 0.020 -0.222 0.020 -0.069 0.020 0.272

0.110 -0.201 0.060 -0.082 0.060 -0.027 0.060 -0.043

0.230 -0.076 0.090 -0.105 0.090 -0.060 0. 110 -0.043

0.400 -0.085 0.120 -0.144 0.120 -0.175 0.250 -0.207

0.490 -0.057 0.200 -0.099 0.200 -0.074 0.400 -0.175

0.630 0.946"* 0.260 -0.150 0.250 -0.182 0.490 -0.177

0.750 -0.006 0.400 -0.124 0.400 -0.158 0.580 -0.203

0.850 0.035 0.490 -0.136 0.490 -0.087 0.650 -0.111

0.900 0.130 0.580 -0.150 0.580 -0.173 0.750 0.107

0.960 0.120 0.640 -0.006 0.650 -0.079 0.830 0.205

0.750 0.113 0.750 -0.050 0.900 0.253

0.870 0.183 0.890 0.246 0.960 0.201

0.930 0.161 0.930 0.185

0.960 0.117 0.960 0.213

CN = 0.115 0.191 0.201 0.257

577
Table I-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-5-50-500, MINF = 0.502, Camber = 10/2, ALPT = 6.22, BETA = 0.45, QINF = 304.1,

RNPU = 3.6E+06, CNWP = 0.2446

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.362 0.000 0.261 0.000 0.692"* 0.010 -0.166

0.060 -0.137 0.020 0.237 0.020 0.081 0.020 -0.313

0.110 -0.418 0.040 -0.001 0.060 -0.258** 0.060 -0.801

0.200 -0.413 0.060 -0.371 0.090 -0.697 0.110 - 1.050

0.230 -0.375 0.090 -0.560 0.110 -0.841 0.140 -0.804

0.400 -0.237 0.130 -0.755 0.130 -5.675 * * 0.190 -5.675 * *

0.490 -0.208 0.150 -0.793 0.150 -0.711 0.250 -0.513

0.590 -0.211 0.200 -0.618 0.210 -0.615 0.400 -0,414

0.630 -0.229 0.250 -0.427 0.250 -0.489 0.490 -0.326

0.700 -0.244 0.260 -0.425 0.340 -0.42 l 0.580 -0.307

0.750 -0.233 0.280 -0.410 0.370 -0.418 0.650 -0.357

0.810 -0,216 0.290 -0.393 0.400 -0.358 0.700 -0.321

0.840 -0.230 0.310 -0.374 0,410 - 1.236** 0.750 -0.324

0.900 -0.160 0.320 -0.397 0.430 -0.386 0.800 -0.288

0.960 -0.040 0.340 -0.366 0.440 -0.358 0.830 -0.284

0.350 -0.175"* 0.460 -0.354 0.900 -0.198

0.370 -0.356 0.490 -0.335 0.960 -0.035

0.380 -0.361 0.500 -0.343

0.400 -0.318 0.520 -0.363

0.410 -0.332 0.540 -0.336

0.430 -0.307 0.550 -0.314

0.440 -0.288 0.580 -0.313

0.460 -0.301 0.600 -0.337

0.470 -0.321 0.610 -0.324

0.490 -0.318 0.650 -0.390

0.500 -0.316 0.700 -0.338

0.520 -0.293 0.750 -0.316

0.530 -0.299 0.820 -0.301

0.550 -0.317 0.890 -0.164

0.560 -0.324 0.900 -0.141

0.580 -0.275 0.960 -0.0 l 7

0.590 -0.316

0.600 -0.292

0.640 -0.321

0.700 -0.302

0.750 -0.064"*

0.820 -0.272

0.870 -0.233

0.930 -0.124

0.960 -0.064

Lower Surface

0.020 -0.446 0.020 -0.386 0.020 -0.271 0.020 -0.160

0.110 -0.085 0.060 -0.005 0.060 0.023 0.060 -0.031

0.230 -0.040 0.090 -0.005 0.090 0.045 0.110 0.030

0.400 -0.031 0.120 0.037 0.120 0.003 0.250 -0.065

0.490 -0.023 0.200 -0.049 0.200 -0.031 0.400 -0.093

0.630 0.844** 0.260 0.016 0.250 -0.028 0.490 -0.115

0.750 -0,006 0.400 -0.035 0.400 -0.073 0.580 -0.145

0.850 0.025 0.490 -0.071 0.490 -0.073 0.650 -0.074

0.900 0.112 0.580 -0.103 0.580 -0.124 0.750 0.124

0.960 0.098 0.640 0.024 0.650 -0.065 0.830 0.217

0.750 0.128 0.750 -0.037 0.900 0.260

0.870 0.187 0.890 0.255 0.960 0.204

0.930 0.173 0.930 0.189

0.960 0.119 0.960 0.224

CN = 0.224 0.356 0.372 0.416

578
Table 1-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-6-12-000, MINF = 0.500, Camber = 10/2, ALPT = 8.02, BETA = 0.95, QINF = 302,4,

RNPU = 3.6E+06, CNWP = 0.3026

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.130 0.000 0.700 0.000 0.796"* 0.010 -0.654

0.060 -0.313 0.020 -0.089 0.020 -0.303 0.020 -0,675

0. 110 -0.570 0,040 -0,200 0.060 -0.551 ** 0.060 - 1.126

0.200 -0.505 0.060 -0.669 0.090 -0.958 0.110 - 1.298

0.230 -0.440 0.090 -0.792 0.110 -1.111 0.140 -0.974

0.400 -0.272 0.130 -0.975 0.130 -5.723 * * 0.190 -5.723 * *

0.490 -0.228 0.150 -0.983 0.150 -0.879 0.250 -0.588

0.590 -0.247 0.200 -0,757 0.210 -0.751 0.400 -0.447

0,630 -0.246 0.250 -0.519 0.250 -0.581 0.490 -0.350

0.700 -0.257 0.260 -0.511 0.340 -0.487 0.580 -0.324

0.750 -0.239 0.280 -0.497 0.370 -0.456 0.650 -0.358

0.810 -0.206 0,290 -0.471 0.400 -0.408 0.700 -0.322

0.840 -0,250 0.310 -0,442 0.410 -1.259"* 0.750 -0.315

0.900 -0.172 0,320 -0.463 0.430 -0.422 0.800 -0.265

0.960 -0.064 0.340 -0,425 0.440 -0.410 0.830 -0.248

0,350 -0.197** 0.460 -0.394 0.900 -0.144

0.370 -0.409 0.490 -0.371 0.960 -0.024

0.380 -0.416 0.500 -0.381

0.400 -0.385 0.520 -0.388

0.410 -0.377 0.540 -0.368

0,430 -0.344 0.550 -0.342

0.440 -0.340 0.580 -0,338

0.460 -0.339 0,600 -0.357

0.470 -0.370 0.610 -0,342

0.490 -0.352 0,650 -0.436

0.500 -0,350 0.700 -0,359

0.520 -0.322 0.750 -0.325

0.530 -0,328 0.820 -0.301

0.550 -0.344 0.890 -0.154

0.560 -0.352 0.900 -0.131

0.580 -0,305 0.960 -0.003

0.590 -0.342

0.600 -0.317

0.640 -0.338

0.700 -0.318

0.750 -0,057**

0.820 -0.274

0.870 -0.238

0.930 -0.118

0.960 -0.060

Lower Surface

0.020 -0.209 0.020 -0.072 0.020 0.047 0.020 0.267

0.110 -0.009 0.060 0.147 0.060 0.204 0.060 -0.020

0,230 0.004 0.090 0.122 0.090 0.171 0.110 0,161

0.400 0.002 0,120 0.121 0.120 0.115 0.250 0.013

0.490 0.003 0.200 -0.016 0.200 0.006 0.400 -0.032

0,630 0.844** 0.260 0.091 0.250 0.059 0.490 -0.053

0.750 0.000 0,400 0.013 0.400 -0.014 0.580 -0.105

0.850 0.021 0.490 -0.023 0.490 -0.063 0.650 -0.04 1

0.900 0.110 0.580 -0.066 0.580 -0.078 0.750 0.154

0.960 0.089 0.640 0.054 0.650 -0.062 0.830 0.237

0.750 0.147 0.750 -0,026 0.900 0,272

0.870 0.199 0.890 0.267 0.960 0.207

0.930 0.174 0.930 0.208

0.960 0.124 0.960 0.204

CN = 0.298 0.470 0.478 0.522

579
Table I-2. Continued.

Flight 216, Wing sweep = 26 °. Time = 9-7-33-500, MINF = 0.505, Camber = 10/2, ALPT = 3.44, BETA = 0.66, QINF -- 303.3,

RNPU = 3.6E+06, CNWP = 0.1656

q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 0.587 0.000 -0.811 0.000 0.331 ** 0.010 0.312

0.060 0.089 0.020 0.635 0.020 0.5 | 8 0,020 0.1 44

0.110 -0.210 0.040 0.358 0.060 0.022"* 0.060 -0.365

0.200 -0.280 0.060 -0.031 0.090 -0.334 0.110 -0.681

0.230 -0.263 0.090 -0.234 0.110 -0.491 0.140 -0.573

0.400 -0.174 0.130 -0.437 0.130 -5.603 * * 0.190 -5.603 * *

0.490 -0.165 0.150 -0.507 0.150 -0.459 0.250 -0.372

0.590 -0.184 0.200 -0.392 0.210 -0.402 0.400 -0.314

0.630 -0.192 0.250 -0.273 0.250 -0.335 0.490 -0.258

0.700 -0.207 0.260 -0.279 0.340 -0.307 0,580 -0.253

0.750 -0.211 0.280 -0.269 0.370 -0.299 0.650 -0.314

0.810 -0.170 0.290 -0.269 0.400 -0.253 0.700 -0.277

0.840 -0.197 0.310 -0.251 0.410 -1.152"* 0.750 -0.306

0.900 -0.136 0.320 -0.275 0.430 -0.294 0.800 -0.292

0.960 -0.043 0.340 -0.255 0.440 -0.283 0.830 -0.263

0.350 -0.140"* 0.460 -0.269 0.900 -0.217

0.370 -0.255 0.490 -0.279 0.960 -0.047

0.380 -0.257 0.500 -0.266

0.400 -0.228 0.520 -0.277

0.410 -0.243 0.540 -0.294

0.430 -0.218 0.550 -0.278

0.440 -0.224 0.580 -0.240

0.460 -0.215 0.600 -0.274

0.470 -0.254 0.610 -0.268

0.490 -0.258 0.650 -0.325

0.500 -0.243 0.700 -0.288

0.520 -0.220 0.750 -0.273

0.530 -0.236 0.820 -0.277

0.550 -0.251 0.890 -0.144

0.560 -0.254 0.900 -0.141

0.580 -0.219 0.960 -0.010

0,590 -0.243

0.600 -0.231

0.640 -0.282

0.700 -0.259

0.750 -0.064**

0.820 -0.239

0.870 -0.208

0.930 -0.099

0.960 -0.052

Lower Surface

0.020 - 1.253 0.020 - 1.020 0.020 -0.822 0.020 -0.918

0.110 -0.219 0.060 -0.332 0.060 -0.231 0.060 -0.027

0.230 -0.077 0.090 -0.214 0.090 -0.158 0.110 -0.226

0.400 -0.042 0.120 -0.117 0.120 -0.162 0.250 -0.198

0.490 -0.04 1 0.200 -0.084 0.200 -0.060 0.400 -0.190

0.630 0.943"* 0.260 -0.094 0.250 -0.140 0.490 -0.193

0.750 -0.006 0.400 -0.113 0.400 -0.171 0.580 -0.211

0.850 0.022 0.490 -0.128 0.490 -0.087 0.650 -0.122

0.900 0.100 0.580 -0.137 0.580 -0.178 0.750 0.077

0.960 0.106 0.640 -0.005 0.650 -0.076 0.830 0.196

0.750 0.095 0.750 -0.061 0.900 0.241

0.870 0.164 0.890 0.238 0.960 0.197

0.930 0.149 0.930 0.179

0.960 0.109 0.960 0.181

CN =

0.124 0.168 0.199 0.228

580
Table I-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-10-16-500, MINF = 0.499, Camber -- 10110, ALPT = 4.02, BETA = 0.37, QINF = 299.6,

RNPU = 3.6E-)-06, CNWP = 0.3256

Yl= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.493 0.000 -0.185 0.000 0.594** O.OlO O.115

0.060 0.020 0.020 0.424 0.020 0.306 0.020 -0.035

0.110 -0.378 0.040 0.184 0.060 -0.200"* 0.060 -0.515

0.200 -0.400 0.060 -0.206 0.090 -0.536 0.110 -0.877

0.230 -0.353 0.090 -0.433 0.110 -0.691 0.140 -0.730

0.400 -0.277 0.130 -0.649 0.130 -5.742 * * 0.190 -5.742 * *

0.490 -0.268 0.150 -0.702 0.150 -0.630 0.250 -0.474

0.590 -0.366 0.200 -0.559 0.210 -0.564 0.400 -0.430

0.630 -0.404 0.250 -0.426 0.250 -0.478 0.490 -0.379

0.700 -0.518 0.260 -0.426 0.340 -0.455 0.580 -0.416

0.750 -0.687 0.280 -0.427 0.370 -0.449 0.650 -0.530

0.810 -0.617 0.290 -0.396 0.400 -0.398 0.700 -0.497

0.840 -0.649 0.310 -0.385 0.410 - 1.236"* 0.750 -0.646

0.900 -0.318 0.320 -0.409 0.430 -0.449 0.800 -0.685

0.960 -0.108 0.340 -0.407 0.440 -0.430 0.830 -0.697

0.350 -0.193"* 0.460 -0.424 0.900 -0.218

0.370 -0.392 0.490 -0.428 0.960 -0.086

0.380 -0.416 0.500 -0.447

0.400 -0.389 0.520 -0.471

0.410 -0.398 0.540 -0.459

0.430 -0.384 0.550 -0.446

0.440 -0.377 0.580 -0.411

0.460 -0.392 0.600 -0.490

0.470 -0.403 0.610 -0.499

0.490 -0.403 0.650 -0.639

0.500 -0.405 0.700 -0.595

0.520 -0.391 0.750 -0.621

0.530 -0.410 0.820 -0.730

0.550 -0.448 0.890 -0.224

0.560 -0.456 0.900 -0.185

0.580 -0.433 0.960 -0.059

0.590 -0.479

0.600 -0.466

0.640 -0.590

0.700 -0.638

0.750 -0.087**

0.820 -0.599

0.870 -0,427

0.930 -0.290

0.960 -0.209

Lower Surface

0.020 -0.598 0.020 -0.538 0.020 -0.462 0.020 -0.488

0.110 -0.070 0.060 -0.049 0.060 -0.022 0.060 0.001

0.230 -0.017 0.090 -0.028 0.090 -0.011 0.110 -0.065

0.400 0.020 0.120 0.033 0.120 -0.016 0.250 -0.087

0.490 0.098 0.200 -0.039 0.200 0.002 0.400 -0.056

0.630 0.925 ** 0.260 0.034 0.250 -0.004 0.490 -0.040

0.750 0.171 0.400 0.038 0.400 -0.012 0.580 -0.011

0.850 0.173 0.490 0.028 0.490 -0.078 0.650 0.107

0.900 0.279 0.580 0.068 0.580 0.023 0.750 0.334

0.960 0.169 0,640 0.242 0.650 -0.091 0.830 0.401

0.750 0.294 0.750 0.009 0.900 0.454

0.870 0.384 0.890 0.453 0.960 0.313

0.930 0.299 0.930 0.350

0.960 0.212 0.960 0.294

CN = 0.420 0.550 0.509 0.547

581
Table 1-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-10-54-000, MINF = 0.497, Camber = 10/1 I, ALPT = 4.06, BETA = -0.04, QINF = 297.6,

RNPU = 3.6E+06, CNWP = 0.3149

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.479 0.000 -0.181 0.000 0.553** 0.010 0,109

0.060 -0.046 0.020 0.427 0.020 0.296 0.020 -0.041

0.110 -0.344 0.040 0,169 0.060 -0.180"* 0.060 -0.560

0,200 -0.398 0.060 -0.217 0.090 -0.524 0.110 -0.844

0.230 -0.365 0.090 -0.427 0.110 -0.696 0.140 -0.713

0.400 -0.284 0.130 -0.642 0.130 -5.776 * * 0.190 -5.776* *

0.490 -0.272 0.150 -0.690 0.150 -0.621 0.250 -0.487

0.590 -0.360 0.200 -0.566 0.210 -0.564 0.400 -0.436

0.630 -0.402 0.250 -0.424 0.250 -0,477 0.490 -0.381

0.700 -0.53 l 0.260 -0.424 0,340 -0,454 0.580 -0.414

0.750 -0.695 0.280 -0.417 0.370 -0,437 0.650 -0.543

0.810 -0.623 0.290 -0.399 0.400 -0.396 0.700 -0.495

0.840 -0.670 0.310 -0.390 0.410 -1.240"* 0.750 -0.625

0.900 -0.313 0.320 -0.417 0.430 -0.434 0.800 -0.692

0.960 -0.111 0.340 -0.399 0.440 -0.442 0.830 -0.711

0.350 -0.176"* 0,460 -0.430 0.900 -0.229

0.370 -0.400 0.490 -0.427 0.960 -0.096

0.380 -0.410 0.500 -0.427

0.400 -0.376 0.520 -0.470

0.410 -0.393 0.540 -0.443

0,430 -0.370 0.550 -0.444

0.440 -0.375 0.580 -0,441

0.460 -0.390 0.600 -0.474

0.470 -0.422 0.610 -0.483

0.490 -0.415 0.650 -0.632

0,500 -0.412 0.700 -0.612

0.520 -0.418 0.750 -0.634

0.530 -0.419 0.820 -0.748

0.550 -0.437 0.890 -0.223

0.560 -0.463 0.900 -0.171

0.580 -0.425 0,960 -0.076

0,590 -0.487

0.600 -0.445

0.640 -0.597

0.700 -0.651

0.750 -0.079"*

0,820 -0.574

0.870 -0.443

0.930 -0.328

0.960 -0.238

Lower Surface

0.020 -0.588 0.020 -0.555 0.020 -0.459 0.020 -0.494

0.110 -0.083 0.060 -0.049 0.060 -0.031 0.060 0.019

0.230 -0.012 0.090 -0.038 0.090 -0.009 0.110 -0.075

0.400 0.024 0.120 0.038 0.120 -0.020 0.250 -0.075

0.490 0.089 0,200 -0.034 0.200 -0.008 0.400 -0.065

0.630 0.926"* 0.260 0.053 0.250 -0.014 0.490 -0.036

0.750 0.166 0.400 0.028 0,400 -0.008 0.580 -0.006

0.850 0.193 0.490 0.037 0.490 -0.074 0.650 0.126

0.900 0.286 0.580 0.055 0.580 0.028 0.750 0.326

0.960 0.171 0.640 0.244 0.650 -0.087 0.830 0.386

0.750 0,292 0.750 -0.001 0.900 0,442

0.870 0,391 0,890 0.447 0.960 0.299

0.930 0.302 0.930 0.357

0.960 0.196 0.960 0.298

CN = 0,425 0.554 0.508 0.551

582
Table I-2. Continued.

Flight 216, Wing sweep = 26 °, Time = 9-11-16-000, MINF = 0.507, Camber = 10/10, ALPT = 8.00, BETA = 0.05, QINF = 307.2,

RNPU = 3.6E+06, CNWP = 0.4295

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.016 0.000 0.787 0.000 0.779"* 0.010 -0.812

0.060 -0.454 0.020 -0.309 0.020 -0.522 0.020 -0.832

0.110 -0.696 0.040 -0.019 0.060 -0.796 ** 0.060 - 1.297

0.200 -0.637 0.060 -0.859 0.090 - 1.152 0.110 - 1.451

0.230 -0.557 0.090 -0.976 0.110 -1.298 0.140 - 1.111

0.400 -0.394 0.130 - 1.177 0.130 -5.565"* 0.190 -5.565"*

0.490 -0.376 0.150 - 1.169 0.150 - 1.022 0.250 -0.687

0.590 -0.453 0.200 -0.921 0.210 -0.895 0.400 -0.555

0.630 -0.490 0.250 -0.665 0.250 -0.714 0.490 -0.490

0.700 -0.619 0.260 -0.653 0.340 -0.629 0.580 -0.487

0.750 -0.779 0.280 -0.636 0.370 -0.615 0.650 -0.584

0.810 -0.720 0.290 -0.602 0.400 -0.547 0.700 -0.564

0.840 -0.792 0.310 -0.572 0.410 - 1.170"* 0.750 -0.637

0.900 -0.414 0.320 -0.594 0.430 -0.579 0.800 -0.598

0.960 -0.201 0.340 -0.575 0.440 -0.569 0.830 -0.613

0.350 -0.236** 0.460 -0.553 0.900 -0.226

0.370 -0.550 0.490 -0.522 0.960 -0.110

0.380 -0.568 0.500 -0.547

0.400 -0.515 0.520 -0.547

0.410 -0.529 0.540 -0.558

0.430 -0.502 0.550 -0.531

0.440 -0.498 0.580 -0.533

0.460 -0.509 0.600 -0.585

0.470 -0.536 0.610 -0.583

0.490 -0.522 0.650 -0.732

0.500 -0.528 0.700 -0.655

0.520 -0.495 0.750 -0.663

0.530 -0.513 0.820 -0.706

0.550 -0.539 0.890 -0.177

0.560 -0.562 0.900 -0.161

0.580 -0.511 0.960 -0.098

0.590 -0.553

0.600 -0.543

0.640 -0.666

0.700 -0.711

0.750 -0.070"*

0.820 -0.669

0.870 -0.459

0.930 -0.265

0.960 -0.196

Lower Surface

0.020 -0.083 0.020 0.091 0.020 0.1 64 0.020 0.369

0.110 0.048 0.060 0.234 0.060 0.257 0.060 0.023

0.230 0.053 0.090 0.199 0.090 0.234 0.110 0.235

0.400 0.047 0.120 0.190 0.120 0.199 0.250 0.082

0.490 0.088 0.200 0.048 0.200 0.069 0.400 0.039

0.630 0.932* * 0.260 0.167 0.250 0.139 0.490 0.062

0.750 0.140 0.400 0.100 0.400 0.091 0.580 0.055

0.850 0.148 0.490 0.100 0.490 -0.034 0.650 0.176

0.900 0.228 0.580 0.1 04 0.580 0.073 0.750 0.371

0.960 0.128 0.640 0.258 0.650 -0.074 0.830 0.416

0.750 0.322 0.750 0.017 0.900 0.477

0.870 0.387 0.890 0.447 0.960 0.321

0.930 0.295 0.930 0.356

0.960 0.203 0.960 0.277

CN= 0.5_ 0.8_ 0.741 0.8_

583
Table I-2. Continued.

Flight 216, Wing sweep = 26", Time = 9-11-52-500, MINF = 0.498, Camber = 10/10, ALPT = 3.13, BETA = 0.57, QINF = 298.6,

RNPU = 3.6E+06, CNWP = 0.2945

"q = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x,,/c CP

0.020 0.555 0.000 -0.589 0.000 0.430** 0.010 0.285

0.060 0.046 0.020 0.542 0.020 0.461 0,020 0.114

0.110 -0.264 0.040 0.302 0.060 -0.127 ** 0,060 -0.403

0.200 -0.348 0.060 -0.108 0.090 -0.413 0.110 -0.700

0.230 -0.310 0.090 -0.311 0. 110 -0.550 0.140 -0.605

0.400 -0.255 0.130 -0.524 0.130 -5.759* * 0.190 -5.759 * *

0,490 -0.251 0.150 -0.598 0.150 -0,528 0.250 -0.417

0.590 -0.334 0.200 -0.476 0.210 -0.480 0.400 -0.394

0.630 -0.380 0.250 -0.361 0.250 -0.425 0.490 -0.345

0.700 -0.502 0.260 -0.370 0.340 -0.409 0.580 -0.383

0.750 -0.656 0.280 -0.365 0.370 -0.407 0.650 -0.513

0.810 -0.588 0.290 -0.357 0.400 -0.352 0.700 -0.489

0.840 -0.641 0.310 -0.337 0.410 - 1.238"* 0.750 -0.624

0.900 -0.287 0.320 -0.379 0.430 -0.403 0.800 -0.699

0.960 -0.084 0.340 -0.352 0.440 -0.416 0.830 -0.711

0.350 -0.170"* 0.460 -0.392 0.900 -0.248

0.370 -0.353 0.490 -0.389 0.960 -0.078

0.380 -0.369 0.500 -0.409

0.400 -0.333 0.520 -0.437

0.410 -0.352 0.540 -0.417

0.430 -0.336 0.550 -0.408

0.440 -0.339 0.580 -0.407

0.460 -0.343 0.600 -0.453

0.470 -0.351 0.610 -0.471

0,490 -0.376 0.650 -0.598

0.500 -0.380 0.700 -0.571

0.520 -0,357 0.750 -0.597

0.530 -0.387 0.820 -0.719

0.550 -0.415 0.890 -0.204

0.560 -0.432 0.900 -0.178

0.580 -0.413 0,960 -0.082

0.590 -0.457

0.600 -0.431

0.640 -0.585

0.700 -0.622

0.750 -0.078**

0.820 -0.575

0.870 -0.426

0.930 -0.311

0.960 -0.236

Lower Surface

0.020 - 1.201 0.020 -0.742 0.020 -0.647 0.020 -0.779

0.110 -0.132 0.060 -0.140 0.060 -0.099 0.060 0.003

0.230 -0.048 0.090 -0.098 0.090 -0.065 0.110 -0.138

0.400 0.033 0.120 -0.008 0.120 -0.065 0.250 -0. I 18

0,490 0,068 0.200 -0.047 0.200 -0.017 0.400 -0.089

0.630 0.936** 0.260 0.015 0.250 -0.045 0.490 -0.045

0.750 0.152 0,400 0.011 0.400 -0,030 0.580 -0.022

0.850 0.172 0.490 0.027 0.490 -0.073 0.650 0.109

0.900 0.255 0.580 0.053 0.580 0.018 0.750 0.337

0.960 0.172 0.640 0.241 0.650 -0.082 0.830 0.391

0.750 0.283 0.750 0.001 0.900 0.450

0.870 0.373 0.890 0.439 0.960 0.314

0.930 0.299 0.930 0.354

0.960 0.212 0.960 0.271

CN = 0.367 0.490 0.448 0.488

584
Table I-2. Continued.

Flight 192, Wing sweep = 26 °, Time = 10-44-34-000, MINF = 0.506, Camber = 5/10, ALPT = 11.09, BETA = 0.05, QINF = 123.6,

RNPU = 1.5E+06, CNWP = 0.5703

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.320 0.000 -0.326 0.000 -2.499* '_ 0.010 -3.543

0.060 -0.895 0.020 -2.929** 0.020 -3.359 0.020 -2.244

0,110 -0.922 0.040 - 1.456 0.060 - 1,487 0.060 - 1.746

0.200 -0.650 0,060 - 1.526 0.090 - 1.374 0.110 - 1.344

0.230 -0.642 0.090 -1.323 0,110 -1.623 0.140 -1.031

0.400 -0.410 0.130 -1.329 0.130 -1.391 0.190 -5.044**

0.490 -0.417 0.150 - 1.305 0.150 - 1.156 0.250 -0.654

0.590 -0,501 0.200 -0.957 0.210 - 1.102 0.400 -0.425

0.630 -0,524 0.250 -0,837 0.250 -0,664 0.490 -0.493

0.700 -0.595 0.260 -0.585 0,340 -0.647 0.580 -0.484

0.750 -0,809 0.280 -0.680 0.370 -0.575 0,650 -0.465

0.810 -0.890 0.290 -0.713 0.400 -0.729 0.700 -0.477

0.840 -0.863 0.310 -0.619 0.410 -0.498 0.750 -0.507

0.900 -0.338 0.320 -0.587 0.430 -0.570 0.800 -0,577

0.960 -0.264 0.340 -0.583 0.440 -0.520 0.830 -0.375

0,350 -0.266"* 0.460 0.059** 0.900 -0.242

0.370 -0.556 0.490 -0.412 0,960 -0.194

0,380 -0.546 0,500 -0.537

0.400 -0.363 0,520 -0,450

0.410 -0.588 0.540 -0.494

0.430 -0.533 0,550 -0.477

0.440 -0.420 0.580 -0.513

0.460 -0.665 0.600 -0.478

0.470 -0.514 0.610 -0.284

0.490 -0,536 0.650 1.566**

0.500 -0.504 0,700 -0.573

0,520 -0.500 0.750 -0.763

0.530 -0.460 0,820 -0,475

0.550 -0.544 0.890 -0,113

0.560 -0.472 0.900 -0.125

0.580 -0.460 0,960 -0.113

0.590 -0.539

0,600 -0.586

0.640 1.957"*

0.700 -0.643

0.750 -0.660

0.820 1.553"*

0.870 -0304

0.930 -0.127

0.960 -0.083

Lower Surface

0.020 0.304 0.020 0.810 0,020 0.687 0.020 0.855

0.110 0.203 0.060 0.614 0.060 0.779 0.060 5.287"*

0.230 0.222 0.090 0.401 0.090 0.501 0. | 10 0.308

0.400 0.170 0.120 0,404 0.120 -0.463 0.250 0.274

0.490 0.125 0.200 0.235 0.200 0.010 0.400 0,279

0.630 8.619"* 0.260 0.202 0.250 0,367 0.490 0.116

0.750 0.192 0.400 1.494** 0,400 0.244 0.580 0.114

0,850 0.244 0.490 0.184 0.490 0.121 0.650 0.264

0.900 0.341 0.580 0.333 0.580 0,204 0,750 0.419

0.960 0.147 0.640 0.910* * 0.650 0.389 0.830 0.498

0.750 0,368 0.750 0.511 0.900 0.565

0.870 0.427 0.890 ******** 0.960 0.344

0,930 0.408 0.930 0.423

0.960 0.200 0.960 1.815"*

CN = 0.751 0.953 0.928 0.923

585
Table I-2. Continued.

Flight 192, Wing sweep = 26 °, Time = 10-51-35-500, MINF = 0.508, Camber = 0/10, ALPT = 12.22, BETA = 0.76, QINF = 134.1,

RNPU = 1.6E+06, CNWP = 0.3622

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 - 1.958 0,000 - 1.225 0.000 -2.680* * 0.010 -2.272

0.060 - 1.155 0.020 -3.115 ** 0.020 -2.734 0.020 -2.089

0.110 - 1.023 0.040 - 1.970 0.060 - 1.434 0.060 -2.054

0.200 -0.706 0.060 - 1.874 0.090 - 1.662 0.110 - 1.612

0.230 -0.612 0.090 - 1.512 0.110 - 1.679 0.140 - 1.130

0.400 -0.466 0.130 - 1.275 0.130 - 1.195 0.190 -5.027"*

0.490 -0.389 0.150 - 1.182 0.150 - 1.124 0.250 -0.746

0.590 -0.466 0.200 -0.928 0.210 - 1.036 0.400 -0.537

0.630 -0,478 0.250 -0.851 0.250 -0.649 0.490 -0,580

0.700 -0.502 0.260 -0.590 0.340 -0.619 0.580 -0.608

0.750 -0.570 0.280 -0.727 0.370 -0.515 0.650 -0.532

0.810 -0.706 0,290 -0.698 0.400 -0.611 0.700 -0.532

0.840 -0.682 0.310 -0.633 0.410 -0.462 0.750 -0.537

0,900 -0.315 0.320 -0.572 0.430 -0.512 0.800 -0.624

0.960 -0.312 0.340 -0.589 0.440 -0.452 0.830 -0.387

0.350 -0.358** 0.460 0.059** 0.900 -0.346

0.370 -0.517 0.490 -0.367 0.960 -0.292

0.380 -0.543 0.500 -0.473

0.400 -0.379 0.520 -0.358

0.410 -0.570 0.540 -0.414

0.430 -0.512 0.550 -0.433

0.440 -0.367 0,580 -0.415

0.460 -0.628 0.600 -0.347

0.470 -0.422 0.610 -0.157

0.490 -0.465 0.650 1.066"*

0.500 -0.437 0.700 -0.365

0.520 -0.481 0.750 -0.564

0.530 -0.382 0.820 -0.280

0.550 -0.442 0.890 -0.188

0.560 -0.302 0,900 -0.207

0.580 -0.371 0.960 -0.174

0.590 -0.413

0.600 -0.507

0.640 1.426"*

0.700 -0.392

0.750 -0.274

0.820 1,054"*

0.870 -0.164

0.930 -0.203

0.960 -0.130

Lower Surface

0.020 0.413 0.020 0.970 0.020 0,858 0.020 0.868

0.110 0.275 0.060 0.678 0.060 0.816 0.060 4.495**

0.230 0.252 0.090 0.488 0.090 0.584 0.110 0.400

0.400 0.169 0.120 0.452 0.120 -0.389 0,250 0.338

0.490 0.119 0.200 0.422 0.200 0.148 0.400 0.286

0.630 7.567** 0.260 0.198 0.250 0.384 0.490 0.120

0.750 0.207 0.400 0.999"* 0.400 0.227 0.580 0.152

0.850 0.256 0,490 0.183 0.490 0.124 0.650 0.240

0.900 0.323 0.580 0.319 0.580 0.233 0.750 0.420

0,960 0.143 0.640 0.860** 0.650 0.378 0.830 0.495

0.750 0.356 0.750 0.484 0.900 0.587

0.870 0.414 0.890 ******** 0.960 0.317

0.930 0.364 0.930 0.386

0.960 0.188 0.960 1.296"*

CN = 0.757 0.912 0.869 1.042

586
Table i-2. Continued.

Flight 192, Wing sweep = 26 °, Time = 11-13-15-500, MINF = 0.497, Camber = 10/16, ALPT = 10.03, BETA = -0.72, QINF = 118.0,

RNPU = 1.4E+06, CNWP = 0.5683

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.713 0.000 0.628 0.000 ******** 0.010 - 1.982

0.060 -0.739 0.020 -2.012"* 0,020 - 1,435 0.020 - 1.292

0.110 -0.805 0.040 - 1.062 0.060 -0.911 0,060 - 1.787

0.200 -0.763 0.060 - 1.530 0.090 - 1.479 0.110 - 1.671

0.230 -0.685 0,090 - 1,443 0. l 10 -2.012 0.140 - 1.273

0.400 -0,479 0.130 -1.612 0.130 -1.783 0.190 44***4**

0.490 -0.412 0.150 - 1.671 0.150 - 1.414 0.250 -0.625

0.590 -0.547 0.200 - 1.150 0.210 -1.252 0.400 -0.475

0.630 -0.600 0.250 -0.956 0.250 -0.670 0.490 -0.613

0.700 -0.710 0.260 -0.590 0.340 -0,693 0.580 -0,666

0.750 -0.967 0.280 -0.784 0.370 -0.554 0,650 -0.631

0.810 - 1.138 0.290 -0.759 0.400 -0.776 0.700 -0.647

0.840 - 1.031 0.310 -0.668 0.410 -0.553 0.750 -0.785

0.900 -0.397 0.320 -0.643 0.430 -0.648 0.800 -0.871

0.960 -0.542 0.340 -0.623 0.440 -0.584 0.830 -0.631

0.350 -0.446** 0.460 -0.030** 0.900 -0.277

0.370 -0.586 0.490 -0.501 0.960 -0.278

0.380 -0.632 0,500 -0.684

0.400 -0.364 0.520 -0.418

0.410 -0.669 0.540 -0.602

0.430 -0.631 0.550 -0.612

0.440 -0.443 0.580 -0.616

0.460 -0.861 0.600 -0.569

0.470 -0.518 0.610 -0.418

0.490 -0.614 0.650 -5.954 * *

0.500 -0.554 0.700 -0.758

0.520 -0.574 0.750 - 1.040

0.530 -0.521 0.820 -0.615

0.550 -0.650 0.890 -0.295

0.560 -0.543 0.900 -0.354

0.580 -0.565 0.960 -0.27 I

0.590 -0.635

0.600 -0.775

0.640 -5.544"*

0.700 -0.815

0.750 -0.703

0.820 -5.967**

0.870 -0.294

0.930 -0.247

0.960 -0.211

Lower Surface

0.020 0.061 0.020 0.579 0.020 0.588 0.020 0.653

0. 110 0.201 0.060 0.585 0,060 0.720 0.060 3.566**

0.230 0.087 0.090 0.393 0.090 0.475 0.110 0.259

0.400 0.195 0.120 0.450 0.120 -0.622 0.250 0.337

0.490 0.212 0.200 0.115 0.200 -0.166 0.400 0.299

0.630 3.628"* 0.260 0.182 0.250 0.430 0.490 0.129

0.750 0.249 0.400 -6.029** 0.400 0.259 0.580 -0.036

0.850 0,360 0.490 0.239 0.490 0.162 0.650 0,322

0,900 0.390 0.580 0.393 0.580 0.314 0.750 0.538

0.960 0.132 0.640 1.051 ** 0.650 0.487 0.830 0.559

0.750 0.480 0.750 0.581 0.900 0.733

0.870 0.506 0,890 ***4*4** 0.960 0.403

0.930 0.527 0.930 0.527

0.960 0.310 0.960 -5.692**

CN = 0.836 1.078 1.034 1.048

587
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-54-1-000, MINF = 0.519, Camber = 15/10, ALPT = 3.93, BETA = 0.83, QINF = 276.0,

RNPU = 3.2E+06, CNWP = 0.3442

I] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.624 0.000 -0.905 0,000 0.366** 0.010 0.482

0,060 0.075 0.020 0.519 0,020 0,652 0.020 0,297"*

0,110 -0.421 0.040 0.429 0.060 0.759** 0.060 -0.512**

0,200 -0.457 0.060 -0.154 0.090 -0.534 0.110 - 1.105

0.230 -0,386 0,090 -0.471 0.110 -0,904 0.140 -0.853

0.400 -0.265 0.130 -0.800 0.130 - 1.054 0.190 -5.311 **

0,490 -0,257 0.150 -0.949 0.150 -0.785 0.250 -0,489

0.590 -0,372 0.200 -0,666 0.210 -0,625 0.400 -0.427

0.630 -0.379 0,250 -0.486 0,250 -0.454 0.490 -0.409

0.700 -0.483 0.260 -0,430 0.340 -0.444 0.580 -0.411

0.750 -0.665 0,280 -0.456 0.370 -0,468 0,650 -0,529

0.810 -0.613 0.290 -0.432 0.400 -0,430 0.700 -0.503

0.840 -0,646 0.310 -0.419 0.410 -0.421 0.750 -0,641

0.900 -0.284 0.320 -0.413 0,430 -0,438 0.800 -0.718

0,960 -0.099 0.340 -0,395 0.440 -0,408 0.830 -0.710

0.350 -0.250** 0.460 -0.165 0.900 -0.205

0,370 -0.399 0.490 -0.390 0.960 -0.091 **

0,380 -0.430 0.500 -0,438

0.400 -0.369 0.520 -0.402

0.410 -0,415 0,540 -0.436

0.430 -0,386 0.550 -0.440

0,440 -0.366 0.580 -0.425

0,460 -0,408 0.600 -0,488

0.470 -0,407 0.610 -0.480

0,490 -0,414 0.650 0.028**

0.500 -0.426 0.700 -0.603

0.520 -0.413 0.750 -0.667

0.530 -0.404 0,820 -0.395

0,550 -0,434 0.890 -0.241

0,560 -0.446 0.900 -0.172

0.580 -0.424 0.960 -0.043

0.590 -0,493

0.600 -0,488

0.640 -0.574

0.700 -0.619

0,750 -0.002"*

0,820 -0,570

0,870 -0.394

0.930 -0.277

0.960 -0.204

Lower Surface

0.020 - 1.028 0.020 -0.711 0.020 -0.686 0.020 - 1,051

O. 110 -0,272 0.060 -0.430 0,060 -0.050 0.060 - 1.207

0.230 -0.04 1 0.090 -0.174 0.090 0.021 O. 110 0.057

0.400 O. 104 O. 120 0.042' * O. 120 -0,098 0.250 -0.04 1

0,490 0.117 0,200 -0.040 0.200 -0.076 0.400 -0.042

0.630 1.475"* 0,260 0,055 0.250 0.045 0,490 -0.018

0.750 0.158 0.400 0,043 0.400 0.015 0.580 -0,009

0.850 0.185 0.490 0.052 0.490 0,004 0.650 0.125

0,900 0.261 0.580 0,081 0.580 0.058 0,750 0.344

0.960 0.156 0.640 0,247 0.650 0.019 0.830 0.429

0.750 0.316 0,750 -0,035"* 0,900 0.489

0.870 0,399 0.890 0.451 0.960 0.329

0.930 0,307 0,930 0.366

0.960 0.208 0,960 0.477

CN = 0,398 0.535 0,524 0,544

588
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-54-22-000, MINF = 0.508, Camber = 15/10, ALPT = 4.00, BETA = 0.86, QINF = 273.4,

RNPU = 3.2E+06, CNWP = 0.3278

r1 = 0.93 0.76 0.59 0.40

Upper Surface

x,"c CP x/c CP x/c CP x/c CP

0.020 0.617 0.000 -0.957 0.000 0.429 * * 0.010 0.416

0.060 0.069 0.020 0.538 0.020 0.619 0.020 0.229"*

O. 110 -0.372 0,040 0,426 0.060 0,701 ** 0,060 -0,587"*

0.200 -0.455 0,060 -0.169 0,090 -0,564 O. 110 - 1.185

0.230 -0.412 0.090 -0,495 O. 110 -0.931 O.140 -0.889

0,400 -0.275 O.130 -0.820 O. 130 - 1.086 O,190 -5.547 * *

0.490 -0.271 0.150 -0.966 0.150 -0.785 0.250 -0.519

0.590 -0.373 0.200 -0.677 0.210 -0.649 0.400 -0.440

0.630 -0.389 0.250 -0.483 0.250 -0.474 0.490 -0.420

0.700 -0.490 0.260 -0.437 0.340 -0.447 0.580 -0.423

0.750 -0.681 0.280 -0.461 0.370 -0.460 0.650 -0.543

0.810 -0.612 0.290 -0.442 0.400 -0.426 0.700 -0.522

0.840 -0.647 0.310 -0.425 0.410 -0.431 0.750 -0.667

0.900 -0.291 0.320 -0.421 0.430 -0.457 0.800 -0.743

0.960 -0.094 0.340 -0.402 0.440 -0.426 0.830 -0.740

0.350 -0.271 ** 0.460 -0.194 0.900 -0.245

0.370 -0.403 0.490 -0.400 0.960 -0.087**

0.380 -0.436 0.500 -0.459

0.400 -0.397 0.520 -0.417

0.410 -0.424 0.540 -0.428

0A30 -0.413 0.550 -0.452

0.440 -0.373 0.580 -0.439

0.460 -0.421 0.600 -0.501

0.470 -0.423 0.610 -0_503

0.490 -0.414 0.650 -0.020"*

0.500 -0.424 0.700 -0.6 l 3

0.520 -0.448 0.750 -0.673

0.530 -0.417 0.820 -0.421

0.550 -0.457 0.890 -0.247

0.560 -0.451 0.900 -0.170

0.580 -0.432 0.960 -0.037

0.590 -0.498

0.600 -0.508

0.640 -0.588

0.700 -0.644

0.750 -0.047**

0.820 -0.627

0.870 -0.438

0.930 -0.255

0.960 -0.174

Lower Surface

0.020 - 1.048 0.020 -0.797 0.020 -0.603 0.020 -0.883

0.110 -0.293 0.060 -0.384 0.060 -0.041 0.060 - 1.218

0.230 -0.073 0.090 -0.160 0.090 0.034 0.110 0.038

0.400 0.126 0.120 0.070"* 0.120 -0.086 0.250 -0.038

0.490 O. 118 0.200 -0.069 0.200 -0.111 0.400 -0.067

0.630 1.312** 0.260 0.062 0.250 0.046 0.490 -0.046

0.750 0.166 0.400 0.045 0.400 -0.006 0.580 -0.036

0.850 0.189 0.490 0.051 0.490 -0.036 0.650 0.103

0.900 0.269 0.580 0.080 0.580 0.051 0.750 0.330

0.960 0. 159 0.640 0.247 0.650 -0.029 0.830 0.422

0.750 0.301 0.750 -0.022** 0.900 0.485

0.870 0.395 0.890 0.470 0.960 0.323

0.930 0.301 0.930 0.366

0.960 0.2 l 8 0.960 0.464

CN = 0.401 0.550 0.524 0.558

589
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-55-2-500, MINI== 0.407, Camber = 20/18, ALPT = 4.05, BETA = 1.12, QINF = 189.8,

RNPU = 2.7E+06, CNWP = 0.4625

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.678 0.000 - 1.528 0.000 0.405** 0.010 0.592

0.060 0.093 0.020 0.560 0.020 0.716 0.020 0.405"*

0.110 -0.460 0.040 0.533 0.060 1.221 ** 0.060 -0.628 **

0.200 -0.560 0.060 -0.215 0.090 -0.726 0.110 - 1.461

0.230 -0.519 0.090 -0.639 0.110 - 1.209 0.140 - 1.059

0.400 -0.320 0.130 - 1.076 0.130 - 1.340 0.190 -8.623 **

0.490 -0.327 0.150 - 1.240 0.150 -0.999 0.250 -0.585

0.590 -0.480 0.200 -0.837 0.210 -0.779 0.400 -0.526

0.630 -0.510 0.250 -0.623 0.250 -0.539 0.490 -0.485

0.700 -0.702 0.260 -0.533 0.340 -0.543 0.580 -0.501

0.750 -0.937 0.280 -0.547 0.370 -0.538 0.650 -0.705

0.810 -0.874 0.290 -0.506 0.400 -0.525 0.700 -0.682

0.840 -0.922 0.310 -0.512 0.410 -0.530 0.750 -0.942

0.900 -0.288 0.320 -0.504 0.430 -0.524 0.800 - 1.083

0.960 -0.340 0.340 -0.483 0.440 -0.490 0.830 -0.990

0.350 -0.307"* 0.460 -0.174 0.900 -0.385

0.370 -0.482 0.490 -0.502 0.960 -0.430**

0.380 -0.546 0.500 -0.564

0.400 -0.462 0.520 -0.522

0.410 -0.533 0.540 -0.532

0.430 -0.505 0.550 -0.537

0.440 -0.433 0.580 -0.551

0.460 -0.503 0.600 -0.612

0.470 -0.494 0.610 -0.607

0.490 -0.524 0.650 0.046**

0.500 -0.501 0.700 -0.773

0.520 -0.509 0.750 -0.877

0.530 -0.498 0.820 -0.381

0.550 -0.525 0.890 -0.367

0.560 -0.586 0.900 -0.312

0.580 -0.526 0.960 -0.307

0.590 -0.621

0.600 -0.626

0.640 -0.752

0.700 -0.853

0.750 0.008**

0.820 -0.674

0.870 -0.596

0.930 -0.321

0.960 -0.315

Lower Surface

0.020 - 1.070 0.020 -0.747 0.020 -0.524 0.020 -0.591

0.110 -0.169 0.060 -0.483 0.060 0.119 0.060 -1.552

0.230 -0.041 0.090 -0.049 0.090 0.228 0.110 0.204

0.400 0.198 0.120 0.246"* 0.120 0.033 0.250 0.081

0.490 0.205 0.200 -0.030 0.200 -0.073 0.400 0.071

0.630 1.299** 0.260 0.177 0.250 0.166 0.490 0.122

0.750 0.242 0.400 0.154 0.400 0.115 0.580 0.129

0.850 0.269 0.490 0.162 0.490 0.012 0.650 0.295

0.900 0.352 0.580 0.239 0.580 0.218 0.750 0.506

0.960 0.154 0.640 0.407 0.650 0.001 0.830 0.554

0.750 0.435 0.750 -0.220** 0.900 0.610

0.870 0.506 0.890 0.571 0.960 0.424

0.930 0.401 0.930 0.469

0.960 0.286 0.960 0.603

CN = 0.581 0.758 0.735 0.805

59O
Table i-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-55-27-000, MINF = 0.368, Camber = 20/17, ALPT = 5.12, BETA = 0.89, QINF = 161.9,

RNPU = 2.6E+06, CNWP = 0.4656

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.626 0.000 - 1.169 0.000 0.860"* 0,010 0.425

0.060 -0.022 0.020 0.384 0.020 0.585 0.020 O. 187"*

O. 1 lO -0.552 0.040 0.423 0.060 1.154** 0.060 -0.844**

0.200 -0.650 0.060 -0.416 0.090 -0.881 O. 110 - 1.675

0.230 -0,557 0.090 -0.846 O.l 10 - 1.451 O, 140 - 1.150

0.400 -0.379 0.130 -1.278 0.130 -1.544 0.190 ********

0.490 -0.360 0.150 -1.410 0.150 -1.100 0.250 -0.651

0.590 -0.523 0.200 -0.967 0.210 -0.887 0.400 -0.582

0.630 -0.550 0.250 -0.698 0.250 -0.636 0.490 -0.551

0.700 -0.736 0.260 -0.604 0.340 -0.626 0.580 -0.556

0.750 -0.993 0.280 -0.610 0.370 -0.633 0.650 -0.723

0.810 -0.909 0.290 -0.610 0.400 -0.552 0,700 -0,696

0.840 -0.987 0.310 -0.582 0.410 -0.570 0.750 -0.948

0.900 -0.346 0.320 -0.575 0.430 -0.615 0.800 - 1.080

0.960 -0.350 0.340 -0.545 0.440 -0.554 0.830 - 1.027

0.350 -0.347** 0.460 -0.144 0.900 -0.409

0.370 -0.542 0,490 -0.521 0.960 -0.451 **

0,380 -0,598 0.500 -0.583

0.400 -0.497 0.520 -0.540

0.410 -0.574 0.540 -0,577

0.430 -0.540 0.550 -0.601

0.440 -0.4% 0.580 -0.573

0,460 -0.551 0.600 -0.642

0.470 -0,548 0.610 -0.604

0.490 -0,554 0,650 0.045**

0.500 -0.554 0,700 -0,780

0.520 -0.571 0.750 -0.902

0,530 -0.541 0.820 -0.388

0.550 -0.582 0.890 -0.362

0,560 -0.610 0.900 -0.324

0.580 -0.572 0,960 -0.266

0.590 -0.679

0.600 -0.660

0.640 -0.756

0.700 -0.881

0,750 -0.014'*

0.820 -0.703

0.870 -0.547

0.930 -0.325

0.960 -0.338

Lower Surface

0.020 - 1.137 0.020 -0.587 0.020 -0.227 0.020 -0.565

0.110 -0.129 0.060 0.014 0,060 0.269 0.060 - 1.754

0.230 -0.031 0.090 0.206 0.090 0.276 0.110 0.266

0.400 0.201 0.120 0.393"* 0.120 0.053 0.250 0.115

0.490 0.230 0.200 -0.032 0.200 -0.091 0.400 0,093

0.630 1.119** 0.260 0.190 0.250 0.203 0.490 0.153

0.750 0.271 0.400 0.175 0.400 0.153 0.580 0.159

0.850 0.255 0.490 0.171 0,490 0.023 0.650 0.313

0.900 0.350 0.580 0.213 0.580 0.224 0.750 0.480

0.960 0.148 0.640 0.404 0.650 0.009 0.830 0.565

0.750 0.442 0.750 -0.043* * 0,900 0.635

0.870 0.516 0.890 0.571 0.960 0.409

0,930 0,418 0.930 0.463

0.960 0.263 0.960 0.604

CN = 0.649 0.874 0.801 0.870

591
Table i-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-55-44-500, MINF = 0,345, Camber = 20/17, ALPT = 6.02, BETA = 0.63, QINF = 145.7,

RNPU = 2.4E+06, CNWP = 0.5411

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.547 0.000 -0.845 0,000 1,054"* 0,010 0.299

0.060 -0,055 0,020 0.258 0.020 0,497 0,020 0.078**

0.110 -0,615 0.040 0.361 0,060 1,325"* 0.060 -0.996**

0.200 -0,698 0.060 -0.531 0.090 - 1.067 0.110 - 1,754

0,230 -0.592 0.090 -0.948 0.110 - 1.567 0.140 - 1.233

0.400 -0,371 0.130 -1.380 0,130 -1,668 0,190 ********

0.490 -0.312 0.150 - 1.490 0.150 - 1.125 0,250 -0,668

0,590 -0.514 0.200 -1.012 0.210 -0.921 0.400 -0,576

0.630 -0,553 0.250 -0.749 0.250 -0,678 0,490 -0,546

0.700 -0,728 0,260 -0,616 0.340 -0.638 0.580 -0.598

0.750 -0.988 0.280 -0.651 0,370 -0.644 0.650 -0.714

0.810 -0.924 0.290 -0.643 0.400 -0.526 0.700 -0,703

0.840 - 1.009 0.310 -0.615 0.410 -0,575 0.750 -0.936

0.900 -0.321 0,320 -0.613 0.430 -0.626 0,800 - 1.058

0.960 -0.376 0,340 -0.579 0.440 -0.546 0.830 - 1.039

0,350 -0,337"* 0,460 -0.127 0,900 -0,428

0.370 -0,573 0.490 -0.550 0.960 -0.341 **

0.380 -0.637 0.500 -0.630

0.400 -0.503 0,520 -0.504

0.410 -0,606 0.540 -0.587

0,430 -0.550 0,550 -0.619

0.440 -0.492 0.580 -0,573

0,460 -0.561 0.600 -0.636

0.470 -0.489 0.610 -0.616

0.490 -0.576 0.650 0.048**

0.500 -0.544 0,700 -0.780

0.520 -0.588 0.750 -0.928

0,530 -0.538 0.820 -0.333

0.550 -0.564 0.890 -0,334

0,560 -0.600 0,900 -0,300

0.580 -0.596 0.960 -0.239

0.590 -0.663

0.600 -0.674

0.640 -0,738

0.700 -0.869

0.750 0.004**

0.820 -0.654

0.870 -0.506

0.930 -0.296

0.960 -0.325

Lower Surface

0,020 -0.796 0.020 -0.078 0.020 -0.094 0,020 -0.353

0.110 0,074 0.060 0.306 0,060 0.326 0.060 - 1.937

0.230 0.009 0.090 0.256 0.090 0.305 0.110 0.302

0.400 0.258 0.120 0.403" * 0.120 0.068 0.250 0.168

0.490 0.252 0.200 -0.001 0,200 -0.102 0,400 0.153

0.630 1,021 ** 0.260 0.238 0,250 0.267 0,490 0.184

0.750 0.292 0.400 0.214 0.400 0.158 0.580 0.193

0,850 0,274 0.490 0.217 0.490 0.024 0,650 0.331

0,900 0,416 0.580 0.240 0.580 0.247 0,750 0.530

0.960 0,174 0.640 0.421 0.650 -0.006 0,830 0.557

0,750 0,466 0,750 -0.163"* 0.900 0.629

0.870 0.544 0,890 0.617 0.960 0.457

0.930 0.447 0.930 0.495

0.960 0.274 0.960 0,706

CN -- 0.710 0.933 0.841 0,907

592
Table !-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-56-4-500, MINT = 0.315, Camber = 20/18, ALPT = 7.26, BETA = 0.66, QINF = 124.2,

RNPU = 2.3E+06, CNWP = 0.6770

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.540 0,000 -0.429 0.000 1.488"* 0.010 O. 112

0.060 -0,153 0.020 0.250 0.020 0.428 0.020 -0.046"*

0.110 -0.798 0.040 0.254 0.060 1.441 ** 0.060 - 1.341 **

0.200 -0.806 0.060 -0.792 0.090 - 1.314 0.110 -2.173

0.230 -0.670 0.090 -1.216 0.110 -1.989 0.140 -1.445

0.400 -0.482 0.130 -1.702 0.130 -1.972 0.190 ********

0.490 -0.448 0.150 - 1.807 0.150 - 1.401 0.250 -0.770

0.590 -0.614 0.200 -1.166 0.210 -1.078 0.400 -0.611

0.630 -0.650 0.250 -0.868 0.250 -0.765 0.490 -0.570

0.700 -0.847 0.260 -0.743 0.340 -0.698 0.580 -0.511

0.750 - 1.123 0.280 -0.752 0.370 -0.719 0.650 -0.637

0.810 - 1.053 0.290 -0.741 0.400 -0.637 0.700 -0.621

0.840 - 1.150 0.310 -0.701 0.410 -0.676 0.750 -0.767

0.900 -0.433 0.320 -0.695 0.430 -0.684 0.800 -0.657

0.960 -0.478 0.340 -0.650 0.440 -0.611 0.830 -0.646

0.350 -0.416"* 0.460 -0.096 0.900 -0.326

0.370 -0.651 0.490 -0.595 0.960 -0.361 **

0.380 -0.712 0.500 -0.658

0.400 -0.610 0.520 -0.612

0.410 -0.690 0.540 -0.643

0.430 -0.637 0.550 -0.654

0.440 -0.568 0.580 -0.693

0.460 -0.650 0.600 -0.738

0.470 -0.672 0.610 -0.678

0.490 -0.643 0.650 0.070**

0.500 -0.645 0.700 -0.882

0.520 -0.676 0.750 - 1.031

0.530 -0.616 0.820 -0.522

0.550 -0.682 0.890 -0.441

0.560 -0.679 0.900 -0.397

0.580 -0.654 0.960 -0.267

0.590 -0.755

0.600 -0.766

0.640 -0.822

0.700 -0.961

0.750 0.019"*

0.820 -0.860

0.870 -0.375

0.930 -0.377

0.960 -0.403

Lower Surface

0.020 -0.608 0.020 0.091 0.020 0.054 0.020 -0.077

0.110 0.059 0.060 0.366 0.060 0.426 0.060 -2.187

0.230 -0.010 0.090 0.343 0.090 0.438 0.110 0.432

0.400 0.283 0.120 0.489** 0.120 0.112 0.250 0.241

0.490 0.320 0.200 -0.004 0.200 -0.074 0.400 0.195

0.630 0.896** 0.260 0.302 0.250 0.346 0.490 0.214

0.750 0.322 0.400 0.277 0.400 0.247 0.580 0.186

0.850 0.344 0.490 0.262 0.490 0.077 0.650 0.375

0.900 0.481 0.580 0.289 0.580 0.321 0.750 0.556

0.960 0.214 0.640 0.483 0.650 -0.092 0.830 0.626

0.750 0.537 0.750 -0.011 ** 0.900 0.694

0.870 0.619 0.890 0.669 0.960 0.452

0.930 0.504 0.930 0.561

0.960 0.337 0.960 0.847

CN = 0.849 1.102 0.991 0.944

593
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-56-37-500, MINF = 0.289, Camber = 20/17, ALPT = 7.93, BETA = 0.89, QINF = 107.3,

RNPU = 2.1E+06, CNWP = 0.7357

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.548 0.000 -0.048 0.000 1.910* * 0.010 -0.005

0.060 -0.191 0.020 0.181 0.020 0.285 0.020 -0.158"*

0.110 -0.847 0.040 0.163 0.060 1.701 ** 0.060 - 1.481 **

0.200 -0.833 0.060 -0.948 0.090 - 1.450 0.110 -2.228

0.230 -0.660 0.090 -1.322 0.110 -2.113 0.140 -1.536

0.400 -0.504 0.130 -1.793 0.130 -2.!05 0.190 ********

0.490 -0.466 0.150 - 1.887 0.150 - 1.446 0.250 -0.801

0.590 -0.645 0.200 - 1.227 0.210 - 1.132 0.400 -0.617

0.630 -0.665 0.250 -0.886 0.250 -0.791 0.490 -0.569

0.700 -0.842 0.260 -0.790 0.340 -0.751 0.580 -0.522

0.750 - 1.114 0.280 -0.797 0.370 -0.689 0.650 -0.626

0.810 - 1.046 0.290 -0.749 0.400 -0.642 0.700 -0.562

0.840 - 1.132 0.310 -0.728 0.410 -0.663 0.750 -0.692

0.900 -0.433 0.320 -0.731 0.430 -0.696 0.800 -0.631

0.960 -0.463 0.340 -0.663 0.440 -0.637 0.830 -0.660

0.350 -0.424** 0.460 -0.006 0.900 -0.278

0.370 -0.669 0.490 -0.593 0.960 -0.293**

0.380 -0.748 0.500 -0.671

0.400 -0.602 0.520 -0.601

0.410 -0.696 0.540 -0.656

0.430 -0.661 0.550 -0.676

0.440 -0.576 0.580 -0.692

0.460 -0.640 0.600 -0.741

0.470 -0.675 0.610 -0.660

0.490 -0.655 0.650 0.054"*

0.500 -0.643 0.700 -0.865

0.520 -0.662 0.750 - 1.016

0.530 -0.612 0.820 -0.463

0.550 -0.650 0.890 -0.419

0.560 -0.705 0.900 -0.366

0.580 -0.652 0.960 -0.238

0.590 -0.788

0.600 -0.778

0.640 -0.800

0.700 -0.956

0.750 0.034**

0.820 -0.836

0.870 -0.341

0.930 -0.362

0.960 -0.393

Lower Surface

0.020 -0.393 0.020 0.147 0.020 0.139 0.020 0.048

0.110 0.294 0.060 0.425 0.060 0.469 0.060 -2.560

0.230 0.011 0.090 0.393 0.090 0.480 0.1 t 0 0.455

0.400 0.308 0.120 0.526 ** 0.120 0.106 0.250 0.291

0.490 0.351 0.200 -0.031 0.200 -0.093 0.400 0.247

0.630 0.680** 0.260 0.332 0.250 0.372 0.490 0.287

0.750 0.353 0.400 0.311 0.400 0.231 0.580 0.252

0.850 0.389 0.490 0.283 0.490 0.081 0.650 0.394

0.900 0.531 0.580 0.314 0.580 0.343 0.750 0.537

0.960 0.237 0.640 0.487 0.650 -0.018 0.830 0.642

0.750 0.553 0.750 -0.001 ** 0.900 0.707

0.870 0.599 0.890 0.686 0.960 0.461

0.930 0.524 0.930 0.558

0.960 0.361 0.960 0.892

CN = 0.917 1.137 1.022 0.951

594
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-57-0-000, MINF = 0.279, Camber = 20/17, ALPT = 9.10, BETA = 0.95, QINF = 101.4,

RNPU = 2.1E+06, CNWP = 0.8558

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 0.421 0.000 0.406 0.000 1.962"* 0.010 -0,331

0.060 -0,358 0,020 -0,050 0.020 0.049 0,020 -0,431 **

0,110 -1.015 0.040 -0.028 0.060 1.645"* 0.060 -1.770**

0,200 -0.936 0.060 - 1,158 0.090 - 1.706 0.110 -2.434

0.230 -0.770 0.090 - 1.570 0.110 -2,334 0.140 - 1.643

0.400 -0.528 0.130 -2.050 0.130 -2,350 0.190 ********

0,490 -0.521 0,150 -2.086 0,150 - 1.622 0,250 -0.865

0.590 -0.689 0.200 - 1.366 0.210 - 1.270 0.400 -0.670

0.630 -0.722 0.250 -0,993 0.250 -0.876 0,490 -0.591

0,700 -0.886 0.260 -0.853 0.340 -0.771 0.580 -0.569

0.750 - 1.161 0.280 -0.887 0.370 -0.793 0.650 -0.679

0.810 - 1.103 0.290 -0,861 0.400 -0.828 0.700 -0.627

0.840 -1.237 0.310 -0.806 0,410 -0.719 0.750 -0.772

0.900 -0.453 0.320 -0.804 0.430 -0.754 0.800 -0.706

0.960 -0.486 0.340 -0.739 0.440 -0.691 0.830 -0.688

0.350 -0.466** 0.460 -0,024 0.900 -0.298

0.370 -0.736 0.490 -0.622 0.960 -0.255**

0.380 -0.822 0.500 -0.699

0,400 -0.655 0.520 -0.654

0.410 -0.764 0,540 -0.711

0.430 -0,716 0.550 -0,697

0.440 -0.645 0.580 -0.646

0.460 -0.730 0.600 -0.766

0.470 -0.712 0.610 -0,715

0.490 -0.710 0.650 0.081 **

0,500 -0,714 0.700 -0.878

0.520 -0.741 0.750 - 1.050

0,530 -0,664 0,820 -0,464

0.550 -0.705 0.890 -0,449

0.560 -0,726 0.900 -0.397

0.580 -0.687 0.960 -0.227

0.590 -0.825

0,600 -0.797

0.640 -0.825

0.700 -0.975

0.750 -0.003**

0.820 -0.824

0.870 -0.356

0.930 -0.389

0,960 -0.433

Lower Surface

0.020 -0.200 0.020 0.252 0.020 0.268 0,020 0,278

0.110 0.332 0.060 0.499 0.060 0.537 0.060 - 2.661

0.230 0.005 0.090 0.434 0.090 0.532 0.110 0.525

0.400 0.319 0.120 0.551 ** 0.120 0.170 0.250 0.310

0,490 0.332 0.200 -0.009 0,200 -0.115 0.400 0.266

0.630 0.479** 0.260 0.344 0.250 0.420 0.490 0.33 I

0.750 0.345 0.400 0.323 0.400 0.297 0.580 0.223

0.850 0.360 0.490 0.282 0.490 0.068 0,650 0,422

0.900 0.513 0,580 0.304 0.580 0,367 0.750 0.578

0.960 0.197 0.640 0.487 0.650 0,046 0.830 0.637

0.750 0.544 0.750 -0.018"* 0.900 0.7 04

0.870 0.630 0,890 0.687 0,960 0.470

0.930 0.505 0.930 0.563

0.960 0.322 0.960 0.950

CN = 0.980 1.223 1.121 1.029

595
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-58-22-500, MINF = 0.268, Camber = 20/17, ALPT = 9.90, BETA = 1.32, QINF = 97.7,

RNPU = 2.1E+06, CNWP = 0.9262

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.245 0.000 0.791 0.000 2.257** 0.010 -0.734

0.060 -0.575 0.020 -0.315 0.020 -0.289 0.020 -0.708 **

0.110 - 1.168 0.040 -0.316 0.060 1.495 ** 0.060 -2.066 * *

0.200 - 1.002 0.060 - 1.412 0.090 - 1.999 0,110 -2.619

0.230 -0.857 0.090 -1.813 0.I 10 -2.615 0.140 -1.732

0.400 -0.567 0.130 -2.301 0.130 -2.593 0.190 ********

0.490 -0.547 0.150 -2.287 0.150 - 1.733 0.250 -0.828

0.590 -0.699 0.200 - 1.494 0.2 t 0 - 1.376 0.400 -0.647

0.630 -0.745 0.250 - 1.042 0.250 -0.949 0.490 -0.586

0.700 -0.904 0.260 -0.900 0.340 -0.819 0.580 -0.563

0.750 - 1.178 0.280 -0.947 0.370 -0.819 0.650 -0.631

0.810 - 1.117 0.290 -0.893 0.400 -0.719 0.700 -0.576

0.840 - 1.233 0.310 -0.849 0.410 -0.766 0.750 -0.706

0.900 -0.466 0.320 -0.847 0.430 -0.755 0.800 -0.620

0.960 -0.477 0.340 -0.782 0.440 -0.690 0.830 -0.603

0.350 -0.473** 0.460 -0.014 0.900 -0.282

0.370 -0.759 0.490 -0.664 0.960 -0.188"*

0.380 -0.840 0.500 -0.727

0.400 -0.686 0.520 -0.651

0.410 -0.775 0.540 -0.690

0.430 -0.716 0.550 -0.695

0.440 -0.642 0.580 -0.643

0.460 -0.694 0.600 -0.809

0.470 -0.632 0.610 -0.673

0.490 -0.722 0.650 0.111 **

0.500 -0.714 0.700 -0.817

0.520 -0.742 0.750 -0.983

0.530 -0.662 0.820 -0.383

0.550 -0.621 0.890 -0.402

0.560 -0.745 0.900 -0.385

0.580 -0.686 0.960 -0.219

0.590 -0.829

0.600 -0.800

0.640 -0.798

0.700 -0.939

0.750 0.036**

0.820 -0.804

0.870 -0.298

0.930 -0.365

0.960 -0.388

Lower Surface

0.020 -0.119 0.020 0.439 0.020 0.449 0.020 0.492

O. 110 0.393 0.060 0.591 0.060 0.605 0.060 -2.689

0.230 0.056 0.090 0.522 0.090 0.623 O. 110 0.603

0.400 0.313 O. 120 0.621 ** O. 120 0.204 0.250 0.389

0.490 0.441 0.200 0.007 0.200 -0.071 0.400 0.326

0.630 -0.252' * 0.260 0.418 0.250 0.486 0.490 0.382

0.750 0.362 0.400 0.374 0.400 0.336 0.580 0.301

0.850 0.378 0.490 0.332 0.490 0.098 0.650 0.442

0.900 0.535 0.580 0.331 0.580 0.397 0.750 0.6 t 2

0.960 0.219 0.640 0.510 0.650 0.075 0.830 0.676

0.750 0.553 0.750 0.008** 0.900 0.740

0.870 0.639 0.890 0.718 0.960 0.506

0.930 0.518 0.930 0.577

0.960 0.339 0.960 0.952

CN = 1.074 1.299 1.185 1.072

596
Table I-2. Continued.

Flight 201, Wing sweep = 9", Time = 9-52-31-000, MINF = 0.592, Camber = 15/10, ALPT = 3.01, BETA = 0.89. QINF = 309,7,

RNPU = 3.2E+06, CNWP = 0.2814

'0 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.695 0.000 -0.958 0.000 O. 199* * 0.010 0.634

0.060 0.159 0.020 0.625 0.020 0.729 0.020 0.482**

0.110 -0.273 0.040 0,534 0.060 0,813"* 0,060 -0,279"*

0.200 -0.406 0.060 -0.016 0.090 -0.383 0.110 -0.945

0,230 -0.356 0.090 -0.347 0.110 -0.760 0.140 -0,758

0.400 -0.242 0.130 -0.693 0.130 -0,960 0.190 -4.076**

0.490 -0.238 0.150 -0.875 0.150 -0.698 0,250 -0.428

0.590 -0,337 0.200 -0.578 0.210 -0.556 0,400 -0,379

0,630 -0,366 0.250 -0,432 0.250 -0,396 0.490 -0.372

0.700 -0,469 0.260 -0.382 0,340 -0.394 0,580 -0.385

0,750 -0.670 0.280 -0.396 0.370 -0.401 0,650 -0.509

0.810 -0.607 0.290 -0.388 0,400 -0.361 0.700 -0,487

0.840 -0.638 0,310 -0,372 0.410 -0,367 0.750 -0.636

0.900 -0.235 0.320 -0.357 0.430 -0,403 0.800 -0,729

0.960 -0.046 0.340 -0.351 0.440 -0,372 0.830 -0.723

0.350 -0.223"* 0.460 -0.176 0.900 -0.198

0.370 -0.354 0,490 -0,368 0.960 -0,096**

0,380 -0,390 0,500 -0,407

0.400 -0.317 0.520 -0.390

0,410 -0.367 0.540 -0,400

0.430 -0.354 0.550 -0,402

0,440 -0.327 0,580 -0.411

0.460 -0.373 0,600 -0,445

0.470 -0.360 0.610 -0.451

0.490 -0.379 0,650 0,026**

0,500 -0.378 0.700 -0,596

0.520 -0.389 0.750 -0.640

0,530 -0.383 0.820 -0.390

0.550 -0.412 0.890 -0.198

0,560 -0.420 0.900 -0.118

0,580 -0,382 0,960 -0.054

0.590 -0.464

0.600 -0,462

0.640 -0.567

0.700 -0,624

0,750 -0.004**

0,820 -0.521

0.870 -0,410

0.930 -0.299

0,960 -0.202

Lower Surface

0.020 - 1.087 0.020 -0.805 0.020 -0,865 0.020 - 1,397

0.110 -0,432 0.060 -0.513 0.060 -0.470 0.060 - 1.166

0.230 -0.064 0.090 -0,441 0.090 -0,255 0.110 -0,040

0,400 0,087 0.120 -0.260"* 0.120 -0.280 0,250 -0,098

0.490 O. 126 0.200 -0.063 0.200 -0.099 0.400 -0.085

0.630 1.869** 0.260 -0.103 0.250 0.014 0.490 -0.058

0.750 0,139 0.400 0.018 0,400 -0,004 0,580 -0,036

0,850 0.184 0,490 0.045 0.490 0.012 0.650 0.127

0.900 0.237 0,580 0.088 0.580 0.061 0.750 0,345

0.960 0.153 0.640 0.214 0.650 0.012 0.830 0.425

0.750 0.266 0.750 -0,030* * 0,900 0.490

0.870 0,330 0,890 0,424 0,960 0.335

0.930 0.285 0.930 0.335

0.960 0.205 0,960 0,458

CN = 0.331 0.437 0.431 0.477

597
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-54-25-500, MINF = 0.496, Camber = 15/9, ALPT = 4.02, BETA = 1.21, QINF = 262.9,

RNPU = 3.2E+06, CNWP = 0.3380

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0,613 0.000 - 1.002 0.000 0.469** 0.010 0.360

0.060 0.070 0.020 0.494 0.020 0.588 0.020 0.149"*

0.110 -0.349 0.040 0.416 0.060 0.666** 0.060 -0.684"*

0.200 -0.476 0.060 -0.195 0.090 -0.612 0.110 - ] .234

0.230 -0.388 0.090 -0.512 0.110 -0.980 0.140 -0.936

0.400 -0.270 0.130 -0.840 0.130 -1.117 0.190 -5.803**

0.490 -0.262 0.150 -0.983 0.150 -0.828 0.250 -0.525

0.590 -0.354 0.200 -0.692 0.210 -0.666 0.400 -0.451

0.630 -0.371 0.250 -0.504 0.250 -0.478 0.490 -0.443

0.700 -0,481 0.260 -0.448 0.340 -0.466 0.580 -0.423

0.750 -0.665 0.280 -0.471 0.370 -0.471 0.650 -0.548

0.810 -0.613 0.290 -0.451 0.400 -0.436 0.700 -0.533

0.840 -0.645 0.310 -0.433 0.410 -0.440 0.750 -0.662

0.900 -0.290 0.320 -0.425 0,430 -0.460 0.800 -0.742

0.960 -0.099 0.340 -0.404 0.440 -0.421 0.830 -0.729

0.350 -0.289** 0.460 -0.184 0.900 -0.246

0.370 -0.404 0.490 -0.418 0.960 -0.092**

0.380 -0.440 0.500 -0.447

0.400 -0.377 0.520 -0.436

0.410 -0.424 0.540 -0.463

0.430 -0.420 0.550 -0,457

0.440 -0.365 0.580 -0.448

0.460 -0.412 0.600 -0.495

0.470 -0.420 0.610 -0.510

0.490 -0.418 0.650 -0.034"*

0.500 -0.405 0.700 -0.614

0.520 -0.439 0.750 -0.676

0.530 -0.415 0.820 -0.410

0.550 -0.435 0.890 -0.254

0.560 -0.449 0.900 -0.172

0.580 -0.428 0.960 -0.036

0.590 -0.499

0.600 -0.497

0.640 -0.582

0.700 -0.642

0.750 -0.037**

0.820 -0.607

0.870 -0.424

0.930 -0.262

0.960 -0.195

Lower Surface

0.020 - 1.160 0.020 -0.930 0.020 -0.540 0.020 -0.722

0.110 -0.208 0.060 -0.370 0.060 -0.014 0.060 - 1.247

0.230 -0.068 0.090 -0.04 1 0,090 0.050 0.110 0,061

0.400 0.113 0.120 0.139** 0.120 -0.081 0.250 -0.049

0.490 0.105 0.200 -0.065 0.200 -0.101 0.400 -0.087

0.630 1.350** 0.260 0.064 0.250 0.046 0.490 -0.053

0.750 0.159 0.400 0.046 0.400 -0.002 0.580 -0.050

0.850 0.191 0.490 0.056 0.490 -0.035 0.650 0.097

0.900 0.273 0.580 0.082 0.580 0.051 0.750 0.331

0.960 0.174 0.640 0.260 0.650 -0.031 0.830 0.418

0.750 0.321 0.750 -0.072"* 0.900 0.490

0.870 0.404 0.890 0.459 0.960 0.328

0.930 0.325 0.930 0.375

0.960 0.226 0.960 0.459

CN = 0.400 0.567 0.537 0.563

598
Table 1-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-54-29-500, MINF = 0.484, Camber = 15/10, ALPT = 5.03, BETA = 0.86, QINF = 251.8,

RNPU = 3.lE+06, CNWP = 0.3694

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.560 0.000 -0.624 0.000 0.696"* 0.010 0.175

0.060 -0.013 0.020 0.485 0.020 0.458 0.020 -0.003"*

0.110 -0.475 0.040 0.288 0.060 0.638** 0.060 -0.873**

0.200 -0.518 0.060 -0.353 0.090 -0.777 0.110 - 1.406

0.230 -0.478 0.090 -0.658 0.110 - 1.147 0.140 - 1.058

0.400 -0.303 0.130 -0.986 0.130 - 1.281 0.190 -6.094 **

0.490 -0.281 0.150 -1.108 0.150 -0.929 0.250 -0.575

0.590 -0.391 0.200 -0.782 0.210 -0.757 0.400 -0.498

0.630 -0.421 0.250 -0.557 0.250 -0.545 0.490 -0.470

0.700 -0.531 0.260 -0.510 0.340 -0.524 0.580 -0.469

0.750 -0.724 0.280 -0.528 0.370 -0.531 0.650 -0.574

0.810 -0.651 0.290 -0.514 0.400 -0.475 0.700 -0.558

0.840 -0.689 0.310 -0.479 0.410 -0.489 0.750 -0.676

0.900 -0.337 0.320 -0.487 0.430 -0.483 0.800 -0.710

0.960 -0.130 0.340 -0.464 0.440 -0.478 0.830 -0.730

0.350 -0.281 ** 0.460 -0.221 0.900 -0.242

0.370 -0.450 0.490 -0.448 0.960 -0.119"*

0.380 -0.482 0.500 -0.502

0.400 -0.417 0.520 -0.476

0.410 -0.479 0.540 -0.468

0.430 -0.465 0.550 -0.494

0.440 -0.410 0.580 -0.484

0.460 -0.443 0.600 -0.533

0.470 -0.463 0.610 -0.533

0.490 -0.450 0.650 -0.020"*

0.500 -0.447 0.700 -0.639

0.520 -0.455 0.750 -0.712

0.530 -0.460 0.820 -0.409

0.550 -0.471 0.890 -0.248

0.560 -0.493 0.900 -0.175

0.580 -0.472 0.960 -0.044

0.590 -0.522

0.600 -0.527

0.640 -0.621

0.700 -0.681

0.750 -0.045**

0.820 -0.635

0.870 -0.427

0.930 -0.280

0.960 -0.184

Lower Surface

0.020 - 1.093 0.020 -0.652 0.020 -0.345 0.020 -0.44 1

0.110 -0.052 0.060 -0.027 0.060 0.077 0.060 - 1.238

0.230 -0.059 0.090 0.046 0.090 0.128 0.110 0.086

0.400 0.115 0.120 0.194"* 0.120 -0.045 0.250 0.003

0.490 0.108 0.200 -0.044 0.200 -0.107 0.400 -0.050

0.630 1.375"* 0.260 0.107 0.250 0.098 0.490 -0.030

0.750 0.176 0.400 0.080 0.400 0.020 0.580 -0.042

0.850 0.184 0.490 0.078 0.490 -0.017 0.650 0.116

0.900 0.270 0.580 0.096 0.580 0.061 0.750 0.321

0.960 0.155 0.640 0.256 0.650 -0.034 0.830 0.427

0.750 0.314 0.750 -0.060"* 0.900 0.474

0.870 0.421 0.890 0.456 0.960 0.312

0.930 0.337 0.930 0.371

0.960 0.238 0.960 0.513

CN = 0.474 0.658 0.604 0.626

599
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-55-45-500, MINF = 0.344, Camber -- 20/17, ALPT = 6.03, BETA = 0.63, QINF = 144.5,

RNPU -- 2.4E+06, CNWP = 0.5245

-- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.549 0.000 -0.850 0.000 1.077"* 0.010 0.271

0.060 -0.071 0.020 0.324 0.020 0.469 0.020 0.092"*

O. 110 -0.636 0.040 0.319 0.060 1.192 * * 0.060 - 1.020 * *

0.200 -0.690 0.060 -0.550 0.090 - 1.062 0.110 - 1.784

0.230 -0.535 0.090 -0.971 0. I 10 - 1.614 0.140 - 1.258

0.400 -0.397 0.130 -1.393 0.130 -t.668 0.190 ********

0.490 -0.376 0.150 - 1.517 0.150 - 1.202 0.250 -0.717

0.590 -0.534 0.200 - 1.024 0.210 -0.944 0.400 -0.596

0.630 -0.565 0.250 -0.744 0.250 -0.670 0.490 -0.566

0.700 -0.750 0,260 -0.636 0.340 -0.629 0.580 -0.568

0.750 -0.995 0.280 -0.671 0.370 -0.648 0.650 -0.735

0.810 -0.932 0.290 -0.635 0.400 -0.591 0.700 -0.724

0.840 -0.986 0.310 -0.607 0.410 -0.595 0.750 -0.944

0.900 -0.344 0.320 -0.605 0.430 -0.617 0.800 - 1.068

0.960 -0.380 0.340 -0.570 0.440 -0.565 0.830 - 1.063

0.350 -0.366** 0.460 -0.115 0.900 -0.447

0.370 -0.565 0.490 -0.541 0.960 -0.325"*

0.380 -0.629 0.500 -0.602

0.400 -0.522 0.520 -0.523

0.410 -0.591 0.540 -0.578

0.430 -0.569 0,550 -0.611

0.440 -0.505 0.580 -0.593

0.460 -0.581 0.600 -0.657

0.470 -0.562 0.610 -0.636

0.490 -0.567 0.650 0.062**

0.500 -0.575 0.700 -0.801

0.520 -0.595 0.750 -0.914

0.530 -0.550 0.820 -0.351

0.550 -0.603 0.890 -0.343

0.560 -0.620 0.900 -0.306

0.580 -0.588 0.960 -0.256

0.590 -0.675

0.600 -0.677

0.640 -0.745

0.700 -0.877

0.750 -0.004"*

0.820 -0.659

0.870 -0.487

0.930 -0.322

0.960 -0.314

Lower Surface

0.020 -0.916 0.020 -0.101 0.020 -0.081 0.020 -0.316

0.110 0.046 0.060 0.293 0.060 0.287 0.060 - 1.968

0.230 -0.014 0.090 0.249 0.090 0.321 0.110 0.289

0.400 0.222 0.120 0.391 * * 0.120 0.054 0.250 0.154

0.490 0.239 0.200 -0.009 0.200 -0.076 0.400 0.131

0.630 0.999** 0.260 0.224 0.250 0.254 0.490 0.183

0.750 0.247 0.400 0.200 0.400 0.1 44 0.580 0.190

0.850 0.282 0.490 0.195 0.490 0.009 0.650 0.332

0.900 0.393 0.580 0.234 0.580 0.263 0.750 0.519

0,960 0.160 0.640 0.417 0.650 0.022 0.830 0.575

0.750 0.472 0.750 -0.180** 0.900 0.636

0.870 0.533 0.890 0.592 0.960 0.445

0.930 0.420 0.930 0.477

0.960 0.276 0.960 0.639

CN = 0.697 0.932 0.844 0.918

600
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-56-19-500, MINF = 0.289, Camber = 20/18, ALP'I" = 8.02, BETA = 0.74, QINF = 105.5,

RNPU = 2.1E+06, CNWP = 0.6455

_q = 0.93 0,76 0,59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.484 0.000 -0.019 0.000 1.915"* 0.010 -0.024

0.060 -0.249 0.020 0.195 0.020 0.239 0.020 -0.249**

0.110 -0.792 0,040 0.116 0.060 1.680"* 0.060 - 1.496 **

0.200 -0.858 0,060 -0.949 0.090 - 1.534 0.110 -2.296

0.230 -0.752 0.090 - 1.335 0.110 -2.153 0.140 - 1,501

0.400 -0,509 0,130 -1.814 0.130 -2.137 0.190 ********

0.490 -0.442 0.150 - 1.937 0.150 - 1.436 0.250 -0.844

0.590 -0.630 0.200 - 1.222 0.210 - 1,141 0.400 -0.656

0.630 -0.684 0.250 -0.930 0.250 -0,774 0.490 -0.580

0.700 -0.896 0.260 -0.754 0.340 -0.753 0.580 -0.500

0.750 - 1.122 0.280 -0.840 0.370 -0.752 0.650 -0.622

0.810 - 1.054 0.290 -0.790 0.400 -0.682 0,700 -0.541

0.840 - 1.162 0.310 -0.751 0.410 -0.664 0.750 -0.691

0.900 -0.476 0,320 -0.733 0.430 -0.694 0.800 -0.611

0.960 -0.460 0,340 -0,704 0.440 -0.647 0.830 -0.570

0.350 -0,460"* 0,460 -0.035 0.900 -0.401

0.370 -0.699 0.490 -0.592 0.960 -0.326**

0.380 -0.763 0.500 -0.645

0.400 -0.641 0.520 -0.641

0.410 -0,688 0.540 -0.657

0,430 -0.701 0.550 -0.699

0.440 -0.575 0.580 -0.633

0.460 -0,674 0.600 -0.748

0,470 -0.697 0.610 -0.699

0.490 -0.694 0,650 0.105 **

0.500 -0,637 0.700 -0.888

0.520 -0.702 0.750 - 1.023

0.530 -0.651 0.820 -0.475

0.550 -0.651 0.890 -0.416

0,560 -0.710 0.900 -0.385

0.580 -0.652 0.960 -0.340

0.590 -0,779

0.600 -0.793

0.640 -0,833

0.700 -0.991

0.750 0.066**

0.820 -0.818

0.870 -0.365

0.930 -0.418

0.960 -0.438

Lower Surface

0.020 -0. 869 0,020 0,151 0.020 0.113 0.020 0.056

0.110 0.232 0.060 0.372 0.060 0.485 0.060 -2.601

0.230 -0.017 0.090 0.372 0,090 0.473 0.110 0.435

0.400 0.306 0.120 0.517"* 0.120 0.127 0.250 0.258

0.490 0.329 0,200 -0.020 0.200 -0.123 0.400 0.263

0.630 0.917"* 0.260 0.309 0.250 0.371 0.490 0.253

0.750 0.330 0.400 0.288 0.400 0.246 0.580 0.228

0,850 0.356 0.490 0.299 0.490 0,093 0.650 0.362

0.900 0.536 0.580 0.291 0.580 0.321 0.750 0.557

0.960 0.212 0.640 0.478 0.650 -0.282 0.830 0.612

0.750 0.534 0.750 -0.019"* 0.900 0.721

0.870 0,633 0.890 0.669 0.960 0.463

0.930 0.474 0.930 0.550

0.960 0.318 0.960 0.868

CN = 0.909 1.146 0.999 0.961

601
Table I-2. Continued.

Flight 201, Wing sweep = 9 °, Time = 9-56-58-000, MINF = 0.280, Camber = 20/18, ALPT = 8.98, BETA = 1.35, QINF = I01.7,

RNPU = 2.1E+06, CNWP = 0.8802

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.412 0.000 0.396 0.000 2.013"* 0.010 -0.346

0.060 -0.342 0.020 -0.035 0.020 0.063 0.020 -0.415"*

0.110 -0.896 0.040 -0.024 0.060 1.678 ** 0.060 - 1.812"*

0.200 -0.900 0.060 - 1.140 0.090 - 1.686 0.110 -2.441

0.230 -0.780 0.090 - 1.550 0.110 -2.312 0.140 - 1.623

0.400 -0.534 0.130 -2.029 0.130 -2.328 0.190 * * * * * * * *

0.490 -0.494 0.150 -2.077 0.150 - 1.627 0.250 -0.848

0.590 -0.660 0.200 - 1.347 0.210 - 1.251 0.400 -0.653

0.630 -0.705 0.250 -0.975 0.250 -0.899 0.490 -0.602

0.700 -0.891 0.260 -0.836 0.340 -0.798 0.580 -0.553

0.750 - 1.177 0.280 -0.869 0.370 -0.799 0.650 -0.677

0.810 - 1.127 0.290 -0.818 0.400 -0.702 0.700 -0.626

0.840 - 1.218 0.310 -0.789 0.410 -0.747 0.750 -0.776

0.900 -0.474 0.320 -0.786 0.430 -0.777 0.800 -0.709

0.960 -0.491 0.340 -0.763 0.440 -0.674 0.830 -0.725

0.350 -0.450** 0.460 -0.025 0.900 -0.308

0.370 -0.719 0.490 -0.627 0.960 -0.216**

0.380 -0.805 0.500 -0.710

0.400 -0.638 0.520 -0.678

0.410 -0.746 0.540 -0.654

0.430 -0.665 0.550 -0.698

0.440 -0.610 0.580 -0.681

0.460 -0.713 0.600 -0.749

0.470 -0.714 0.610 -0.698

0.490 -0.693 0.650 0.096**

0.500 -0.713 0.700 -0.872

0.520 -0.678 0.750 - 1.042

0.530 -0.647 0.820 -0.457

0.550 -0.742 0.890 -0.445

0.560 -0.709 0.900 -0.381

0.580 -0.670 0.960 -0.233

0.590 -0.834

0.600 -0.780

0.640 -0.817

0.700 -0.957

0.750 0.044**

0.820 -0.817

0.870 -0.340

0.930 -0.362

0.960 -0.384

Lower Surface

0.020 -0.213 0.020 0.266 0.020 0.259 0.020 0.274

0.110 0.346 0.060 0.513 0.060 0.609 0.060 -2.638

0.230 0.032 0.090 0.447 0.090 0.546 0.110 0.479

0.400 0.345 0.120 0.564** 0.120 0.160 0.250 0.333

0.490 0.325 0.200 0.006 0.200 -0.090 0.400 0.280

0.630 0.503** 0.260 0.348 0.250 0.423 0.490 0.334

0.750 0.359 0.400 0.326 0.400 0.311 0.580 0.238

0.850 0.385 0.490 0.296 0.490 0.042 0.650 0.414

0.900 0.542 0.580 0.318 0.580 0.381 0.750 0.591

0.960 0.211 0.640 0.501 0.650 0.061 0.830 0.650

0.750 0.557 0.750 -0.003" * 0.900 0.717

0.870 0.684 0.890 0.711 0.960 0.501

0.930 0.530 0.930 0.546

0.960 0.336 0.960 0.963

CN = 0.983 1.222 1.131 1.034

602
Table I-2. Continued.

Flight 222, Wing sweep = 16 °, Time = 12-20-11-500, MINF = 0.306, Camber = 20/18, ALPT = 10.03, BETA = 1.03, QINF = 95.6,

RNPU = 1.8E+06, CNWP = 0.6852

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.3 l 4 0.000 0.605 0.000 1.679"* 0.010 -0.410

0.060 -0.497 0.020 0.008 0.020 -0.131 0.020 -0.516

0.110 -1.425 0.040 -0.466 0.060 ******** 0.060 -1.870

0.200 - 1.071 0.060 - 1.286 0.090 - 1.933 0.110 -2.424

0.230 -0.817 0.090 - 1.696 0.110 -2.506 0.140 - 1.633

0.400 -0.595 0.130 -2.213 0.130 -2.588 0.190 ********

0.490 -0.588 0.150 -2.208 0.150 - 1.646 0.250 -0.802

0.590 -0.728 0.200 - 1.489 0.210 - 1.420 0.400 -0.68 I

0.630 -0.751 0.250 - 1.052 0.250 -0.896 0.490 -0.567

0.700 -0.975 0.260 -0.942 0.340 -0.923 0.580 -0.564

0.750 - 1.205 0.280 -0.972 0,370 -0.899 0.650 -0.763

0.810 - 1.161 0.290 -0.944 0.400 -0.774 0.700 -0.707

0.840 -1.207 0.310 -0.884 0.410 ******** 0.750 -0.762

0.900 -0.539 0.320 -0.883 0.430 -0.858 0.800 -0.763

0.960 -0.574 0.340 -0.864 0.440 -0.791 0.830 -0.731

0.350 -0.553** 0.460 -0.813 0.900 -0.402

0.370 -0.736 0.490 -0.647 0.960 -0.278

0.380 -0.887 0.500 -0.829

0.400 -0.890 0.520 -0.805

0.410 -0.838 0.540 -0.813

0.430 -0.746 0.550 -0.682

0.440 -0.665 0.580 -0.634

0.460 -0.795 0.600 -0.833

0.470 -0.773 0.610 -0.733

0.490 -0.724 0.650 -2.573**

0.500 -0.748 0.700 -0.898

0.520 -0.747 0.750 - 1.102

0.530 -0.707 0.820 - 1.044

0.550 -0.807 0.890 -0.434

0.560 -0.809 0.900 -0.396

0,580 -0.766 0.960 -0.344

0.590 -0,933

0.600 -0.796

0.640 -0.839

0.700 -0.989

0.750 -0.140"*

0.820 -0.684

0.870 -0.379

0.930 -0.413

0.960 -0.449

Lower Surface

0.020 -0.051 0.020 0.275 0.020 0.446 0.020 0.357

0.110 0.336 0.060 0.507 0.060 0.573 0.060 -3.481 **

0.230 -0.052 0.090 0.411 0.090 -0.590"* 0.110 0.689

0.400 0.246 0.120 0.434 0.120 0.337 0.250 0.301

0.490 0.341 0.200 -0.091 0.200 -0.096 0.400 0.270

0.630 4.488** 0.260 0.386 0.250 0.410 0.490 0.293

0.750 0.259 0.400 0.284 0.400 0.182 0.580 0.222

0.850 0.372 0.490 0.253 0.490 -0.032 0.650 0.436

0.900 0.418 0.580 0.409 0.580 0.377 0.750 0.495

0.960 0.189 0.640 0.470 0.650 -0.211 0.830 0.670

0.750 0.570 0.750 0.085 0.900 0.670

0.870 0.625 0.890 0.580 0.960 0.44 1

0.930 0.478 0.930 0.504

0.960 0.283 0.960 ********

CN = 1.028 1.277 1.161 1.235

603
Table I-2. Continued.

Flight 222, Wing sweep = 16 °, Time = 12-20-15-000, MINF = 0.304, Camber = 20/18, ALPT = 9.97, BETA = 0.72, QINF = 94.6,

RNPU = 1.8E+06. CNWP = 0.6993

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.310 0.000 0.580 0.000 1.709"* 0.010 -0.479

0.060 -0.505 0.020 -0.084 0.020 -0.216 0.020 -0.553

0.110 -0.668 0,040 -0,491 0,060 ******** 0.060 -1.789

0.200 - 1.074 0.060 - 1.332 0.090 -2.002 0.110 -2.451

0.230 -0.682 0.090 -1.719 0.110 -2,536 0.140 -1.597

0.400 -0.610 0.130 -2.268 0.130 -2,610 0.190 ********

0.490 -0.603 0.150 -2.237 0.150 - 1.669 0.250 -0.842

0.590 -0.854 0.200 - 1.519 0.210 - t .423 0,400 -0.698

0.630 -0.791 0.250 - 1.095 0.250 -0.937 0.490 -0.605

0.700 - 1.017 0.260 -0.940 0.340 -0.965 0.580 -0.569

0.750 -1.225 0.280 -0.986 0.370 -0.841 0.650 -0.803

0.810 - 1.160 0.290 -0.959 0.400 -0.791 0.700 -0.746

0.840 - 1.252 0.310 -0,925 0.4t0 ******** 0.750 -0.790

0.900 -0.553 0.320 -0.910 0.430 -0.899 0.800 -0,804

0,960 -0.612 0.340 -0.905 0.440 -0.832 0.830 -0.713

0.350 -0.608"* 0.460 -0.836 0.900 -0.410

0.370 -0.753 0.490 -0.686 0.960 -0.288

0.380 -0.914 0.500 -0.870

0.400 -0.932 0.520 -0.898

0.410 -0.868 0.540 -0.854

0.430 -0.785 0.550 -0.721

0.440 -0.723 0.580 -0.672

0.460 -0.798 0.600 -0.874

0.470 -0.793 0.610 -0.772

0.490 -0,739 0.650 -2.588**

0,500 -0.753 0.700 -0.928

0.520 -0.787 0.750 - 1.134

0.530 -0.746 0.820 - 1.074

0.550 -0.847 0.890 -0.458

0.560 -0.889 0.900 -0.483

0,580 -0.785 0.960 -0.335

0.590 -0.905

0.600 -0,837

0.640 -0.859

0.700 -1.008

0.750 -0.174"*

0.820 -0.628

0.870 -0.392

0.930 -0.426

0.960 -0.427

Lower Surface

0.020 -0.084 0.020 0.234 0.020 0.419 0.020 0.328

0.110 0.307 0.060 0,480 0.060 0.547 0.060 -3.505**

0.230 -0.097 0.090 0.392 0.090 -0.583** 0.110 0.664

0.400 0.216 0.120 0,522 0.120 0.282 0.250 0.272

0.490 0.324 0.200 -0.123 0.200 -0.151 0.400 0.241

0.630 4.503** 0.260 0.359 0.250 0.359 0.490 0.252

0.750 0.230 0.400 0.267 0.400 0.241 0.580 0.224

0.850 0.332 0,490 0.212 0.490 -0.019 0.650 0.385

0.900 0.416 0,580 0,402 0.580 0.326 0,750 0.453

0.960 0.146 0.640 0.419 0.650 -0.245 0.830 0.645

0.750 0.544 0.750 0.054 0,900 0.626

0.870 0.570 0.890 0.554 0.960 0.413

0.930 0.439 0.930 0.477

0.960 0.254 0.960 ********

CN -.- 0.961 1.271 1.174 1.221

604
Table 1-2. Continued.

Flight 222, Wing sweep = 16 °, Time = 12-21-25-000, MINF = 0.295, Camber = 20/18, ALPT = 10.05, BETA = 1.21, QINF = 89.3,

RNPU = 1.7E+06, CNWP = 0.6392

"q = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 0.332 0.000 0.616 0.000 1.745"* 0.010 -0,408

0.060 -0_505 0,020 -0.059 0.020 -0.192 0.020 -0,556

0.110 -1.142 0.040 -0.442 0.060 ******** 0.060 -1.795

0.200 - 1.065 0.060 - 1.329 0.090 - 1.933 0.110 -2.401

0.230 -0.802 0.090 - 1.674 0.110 -2.473 0.140 - 1.572

0.400 -0.591 0.130 -2.197 0.130 -2.576 0.190 ********

0.490 -0.423 0.150 -2.190 0.150 - 1.681 0.250 -0.769

0.590 -0.771 0.200 - 1.484 0.210 - ! .383 0.400 -0,662

0.630 -0.769 0.250 - 1.023 0.250 -0.902 0.490 -0.579

0.700 -0.984 0,260 -0.920 0.340 -0.989 0.580 -0.537

0.750 - 1.202 0,280 -0.986 0.370 -0.861 0.650 -0.752

0.810 - l. 174 0.290 -0.927 0,400 -0.833 0.700 -0.726

0,840 -1.221 0.310 -0,896 0.410 ******** 0.750 -0.746

0.900 -0.573 0.320 -0.889 0.430 -0.871 0.800 -0.751

0.960 -0.547 0.340 -0.883 0.440 -0,782 0.830 -0.695

0.350 -0.578"* 0.460 -0.818 0.900 -0,374

0.370 -0.731 0.490 -0.621 0.960 -0.275

0.380 -0.891 0.500 -0.860

0.400 - 1.104 0.520 -0.865

0.410 -0.846 0,540 -0.876

0.430 -0.763 0.550 -0,692

0,440 -0.684 0.580 -0.623

0.460 -0.815 0.600 -0.814

0,470 -0.679 0.610 -0.743

0,490 -0.712 0.650 -2.805 * *

0.500 -0,767 0.700 -0.940

0.520 -0.777 0.750 - 1.157

0.530 -0.713 0.820 - 1.065

0.550 -0.867 0.890 -0.428

0.560 -0.828 0.900 -0.428

0.580 -0.757 0.960 -0.30 l

0.590 -0.913

0.600 -0.807

0.640 -0.835

0.700 - 1.001

0.750 -0.142"*

0.820 -0.610

0.87O -0,348

0.930 -0.397

0.960 -0.410

Lower Surface

0.020 0.008 0.020 0.255 0.020 0.421 0.020 0.378

0.110 0.286 0.060 0.513 0.060 0.565 0.060 -3.777 * *

0.230 -0.073 0.090 0.416 0.090 -0.666** 0.110 0.665

0.400 0.221 0.120 0.559 0.120 0.314 0.250 0.307

0.490 0.386 0.200 -0.089 0.200 -0.129 0.400 0.260

0.630 4.722** 0.260 0.385 0.250 0.398 0,490 0.297

0.750 0.261 0.400 0.240 0.400 0.205 0,580 0.233

0.850 0.355 0,490 0,241 0.490 -0.085 0.650 0.438

0.900 0.461 0.580 0.473 0.580 0.350 0.750 0.494

0.960 0.185 0.640 0.474 0.650 -0,230 0.830 0.638

0.750 0.503 0.750 0.074 0.900 0.672

0.870 0.541 0.890 0.593 0,960 0.38 I

0.930 0.434 0.930 0.510

0.960 0.274 0.960 ********

CN = 1.006 1.258 1.164 1,207

6O5
Table I-2. Concluded.

Flight 222, Wing sweep = 16 °, Time = 12-22-23-000, MINF = 0.285, Camber = 20/18, ALPT = 11.58, BETA = 0.83, QINF = 83.3,

RNPU = 1.7E+06, CNWP = 0.7351

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0,059 0.000 0.875 0.000 1.885"* 0.010 -0.877

0,060 -0,783 0.020 -0.512 0.020 -0.596 0.020 -0.785

0.110 -1,554 0.040 -0.880 0.060 ******** 0.060 -2.115

0,200 - 1.227 0.060 - 1.743 0.090 -2.300 0. l 10 -2.579

0.230 -0,848 0.090 -2.022 0.110 -2.804 0.140 - 1.725

0.400 -0.700 0,130 -2.537 0.130 -2,836 0.190 ********

0.490 -0.652 0.150 -2.476 0.150 - 1.964 0,250 -0.864

0.590 -0.866 0.200 - 1.671 0.210 - 1.540 0.400 -0.724

0,630 -0.850 0.250 - 1.182 0.250 -0,993 0.490 -0.592

0.700 - 1.067 0.260 - 1.050 0.340 -0,994 0.580 -0.540

0.750 - 1.314 0,280 -1.045 0,370 -0.962 0.650 -0,736

0.810 - 1,273 0.290 - 1.033 0.400 -0.693 0.700 -0.618

0.840 -1.321 0.310 -0.949 0.410 ******** 0.750 -0,629

0.900 -0.581 0.320 - 1.009 0,430 -0.920 0.800 -0,682

0.960 -0.651 0.340 -0,986 0.440 -0,840 0.830 -0.621

0.350 -0,640** 0,460 -0.877 0.900 -0.473

0.370 -0.822 0.490 -0,677 0.960 -0.275

0.380 -0.962 0,500 -0.844

0.400 - 1.065 0.520 -0.906

0.410 -0.924 0,540 -0.878

0.430 -0.807 0.550 -0.687

0.440 -0.751 0.580 -0,897

0.460 -0.849 0.600 -0.869

0.470 -0.837 0.610 -0.787

0.490 -0.789 0.650 -2.998 * *

0.500 -0.862 0.700 -0,955

0.520 -0.705 0.750 - 1.136

0.530 -0,778 0.820 -0.999

0,550 -0.838 0,890 -0.441

0.560 -0.854 0,900 -0.422

0,580 -0.827 0.960 -0.361

0,590 -0.971

0.600 -0,904

0.640 -0,875

0,700 - 1.020

0.750 -0.166**

0.820 -0,625

0,870 -0.386

0.930 -0.424

0.960 -0.400

Lower Surface

0.020 -0.174 0.020 0,373 0.020 0.581 0.020 0.504

0.110 0.343 0.060 0.525 0,060 0.662 0.060 -4.040**

0.230 -0.117 0.090 0.439 0.090 -0.702 ** 0.110 0,748

0.400 0.252 0.120 0,508 0.120 0.313 0.250 0.314

0.490 0.348 0,200 -0.121 0,200 -0.177 0.400 0.293

0.630 5.028** 0.260 0.388 0,250 0.452 0,490 0.293

0.750 0.213 0,400 0.270 0.400 0.217 0,580 0.211

0.850 0.301 0.490 0.220 0,490 -0,029 0.650 0.404

0.900 0.417 0.580 0.371 0.580 0.364 0.750 0.474

0.960 0.130 0.640 0.443 0.650 -0,234 0.830 0.666

0.750 0.523 0,750 0.041 0.900 0.640

0,870 0.575 0.890 0.596 0,960 0.399

0.930 0.440 0.930 0.506

0,960 0.229 0.960 ********

CN -- 1.119 1.356 1.249 1,269

606
APPENDIX J

Wing Pressure Coefficients for Dynamic Pressures

From 250 to 800 lb/ft 2 and Mach Numbers From 0.60 to 0.90.

Leading-edge wing sweep is 26 ° unless otherwise indicated at flight number. Table J-1 contains a summary of

the data listing in table J-2. The asterisks (*) in table J-2 indicate invalid values. Flight 228 and Flight 231 have less

data in two upper rows because the pressure transducers were used for boundary-layer data. Camber is _)LE/TE"Refer

to Nomenclature for definitions.

Table J- 1. Summary of data.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

228 12-45-12-500 0.610 0/2 7.10 0.11 312.0 3.2E+06 0.1939

228 12-45-16-500 0.602 0/2 8.10 0.14 304.7 3.1E+06 0.2266

228 12-45-22-000 0.608 0/2 10.21 -0.01 309.5 3.1E+06 0.2434

228 12-45-24-500 0.606 0/2 12.01 0.54 307.8 3.1E+06 0.2957

228 12-45-28-000 0.598 0/2 13.04 0.83 299.6 3.1E+06 0.3296

228 12-45-37-500 0.594 0/2 12.03 -0.44 296.6 3.1E+06 0.2431

228 12-45-59-000 0.602 0/2 13.00 0.60 299.3 3.1E+06 0.2755

228 12-46-32-500 0.595 0/2 13.06 -0.88 296.2 3.1E+06 0.3285

228 12-48-50-000 0.605 3/5 6.70 0.77 304.5 3.1E+06 0.3074

228 12-48-55-000 0.627 4/7 8.30 -0.76 326.1 3.2E+06 0.3554

228 12-48-57-500 0.638 6/9 10.11 -0.12 336.8 3.3E+06 0.4391

228 12-49-1-000 0.635 8/12 11.43 -0.41 330.8 3.2E+06 0.5211

228 12-49-10-500 0.611 9/14 12.02 0.48 301.9 3.0E+06 0.5898

228 12-49-12-500 0.606 10/17 13.08 -0.91 296.9 3.0E+06 0.7796

228 12-49-20-500 0.581 9/13 11.28 -0.59 272.0 2.9E+06 0.5458

228 12-49-41-500 0.595 8/12 11.16 -0.30 286.1 2.9E+06 0.5101

228 12-50-6-500 0.604 8/13 11.15 -0.44 292.2 3.0E+06 0.5446

228 12-50-15-000 0.612 8/12 11.12 -0.56 301.0 3.0E+06 0.4970

228 12-50-17-000 0.622 5/7 7.05 1.03 310.6 3.1E+06 0.3478

223 10-23-15-500 0.695 2/4 5.30 0.40 294.8 2.7E+06 0.2553

223 10-23-23-000 0.696 2/4 5.09 0.43 295.9 2.7E+06 0.2613

223 10-23-23-500 0.696 1/4 4.60 0.40 296.2 2.7E+06 0.2330

223 10-23-26-000 0.699 1/3 3.14 0.45 299.2 2.7E+06 0.1724

223 10-23-30-500 0.713 0/3 3.72 0.54 315.6 2.8E+06 0.1549

223 10-23-33-000 0.724 1/4 6.08 0.51 328.8 2.9E+06 0.2425

223 10-23-34-000 0.726 2/5 7.32 0.37 332.3 2.9E+06 0.3374

223 10-23-36-000 0.725 4/7 9.06 0.40 333.5 2.9E+06 0.4253

223 10-23-39-500 0.700 6/9 11.08 0.60 308.1 2.8E+06 0.4649

607
TableJ-I. Continued.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

223 10-23-41-500 0.674 7/10 I 1.66 0.57 282.0 2.6E+06 0.4807

220 9-36-44-000 0.803 1/4 5.09 -0.38 303.4 2.5E+06

220 9-37-0-000 0.803 3/6 8.12 -0.18 311.0 2.5E+06

220 9-37-4-500 0.793 5/8 11.01 - 1.54 311.8 2.6E+06

220 9-37-6-500 0.781 6/11 12.94 0.43 308.5 2.6E+06

220 9-37-10-500 0.778 5/8 9.12 -0.33 318.7 2.7E+06

220 9-37-14-000 0.788 3/6 7.20 0.57 333.9 2.8E+06

226 8-42-6-000 0.801 5/10 3.03 0.31 604.6 5.0E+06 0.2071

226 8-42-43-000 0.804 5/10 3.03 0.19 607.5 5.0E+06 0.2073

226 8-43-5-500 0.801 5/10 3.89 0.40 603.9 5.0E+06 0.2690

226 8-43-13-000 0.810 5/10 6.01 0.66 615.0 5.0E+06 0.3171

226 8-43-17-000 0.804 5/6 6.97 0.74 605.8 5.0E+06 0.3917

226 8-43-22-500 0.790 5/- 1 8.20 0.83 577.9 4.8E+06 0.4390

226 8-43-29-000 0.791 5/-1 8.04 0.66 573.9 4.8E+06 0.4273

220 9-43-0-000 0.801 1/4 5.00 0.02 297.8 2.4E+06

220 9-43-15-000 0.805 1/5 6.23 -0.44 303.0 2.5E+06

220 9-43-16-000 0.805 2/5 6.96 -0.27 304.6 2.5E+06

220 9-43-18-000 0.806 3/7 8.04 -0.50 307.9 2.5E+06

220 9-43-19-000 0.806 3/2 9.05 -0.30 309.7 2.5E+06

220 9-43-20-000 0.805 4/-1 10.12 -0.56 311.3 2.5E+06

220 9-43-21-000 0.804 5/-1 11.12 -0.59 312.7 2.6E+06

220 9-43-22-500 0.799 6/- 1 13.15 -0.56 313.5 2.6E+06

220 9-43-25-000 0.794 7/- 1 13.18 2.31 319.4 2.6E+06

220 9-43-28-000 0.810 3/6 6.18 -0.56 348.7 2.8E+06

221 13-15-18-000 0.859 5/10 3.98 0.22 303.4 2.4E+06 0.3052

221 13-15-22-500 0.864 5/10 5.10 0.14 307.9 2.4E+06 0.3560

221 13-15-29-500 0.864 5/10 6.05 0.19 309.6 2.4E+06 0.3875

221 13-15-34-000 0.861 5/10 7.05 0.31 308.5 2.4E+06 0.4677

221 13-15-37-500 0.858 5/10 8.16 0.02 307.9 2.4E+06 0.5349

221 13-15-38-000 0.857 5/9 8.41 0.08 307.7 2.4E+06 0.5392

221 13-15-38-500 0.857 5/7 8.88 0.43 307.8 2.4E+06 0.5397

221 13-15-39-000 0.856 5/4 9.27 -0.07 307.8 2.4E+06 0.4812

221 13-15-40-000 0.855 5/3 9.57 0.86 307.5 2.4E+06 0.4201

221 13-15-41-500 0.852 5/2 10.29 0.48 307.1 2.4E+06 0.3694

221 13-15-42-000 0.851 5/0 10.90 0.60 307.2 2.4E+06 0.3690

221 13-15-43-000 0.849 5/-1 11.80 0.28 306.8 2.4E+06 0.3500

221 13-15-44-000 0.846 5/-1 12.61 0.14 306.1 2.4E+06 0.2887

608
TableJ-1.Continued.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

211 9-51-57-500 0.704 5/11 2.15 0.25 605.3 5.5E+06 0.3064

211 9-52-4-000 0.703 5/11 4.19 0.17 604.2 5.5E+06 0.3873

211 9-52-10-500 0.710 5/11 6.26 0.14 611.4 5.5E+06 0.3234

211 9-52-15-000 0.705 5/10 7.10 0.11 601.1 5.4E+06 0.3654

211 9-52-19-500 0.695 5/10 8.26 0.11 582.0 5.3E+06 0.4441

211 9-55-37-500 0.697 5/- 1 2.04 0.17 583.0 5.3E+06 0.2090

211 9-55-47-500 0.708 5/-1 6.26 0.28 601.0 5.4E+06 0.3272

211 9-55-51-500 0.712 5/-1 7.06 0.43 606.7 5.4E+06 0.3830

211 9-55-56-500 0.704 5/-1 8.09 0.25 590.5 5.3E+06 0.4400

211 9-55-58-000 0.700 5/-1 8.46 0.25 583.6 5.3E+06 0.4425

211 10-36-20-000 0.802 0/2 4.05 0.66 605.6 5.0E+06 0.1504

225 8-48-5-000 0.801 0/2 4.00 0.45 602.7 4.9E+06 0.1639

225 8-48-22-000 0.800 0/2 5.99 0.34 602.6 5.0E+06 0.2813

223 8-59-41-500 0.797 0/2 4.07 1.09 591.4 4.9E+06 0.1505

223 8-59-54-500 0.803 0/2 5.10 0.77 601.9 4.9E+06 0.2200

223 9-0-1-000 0.808 0/2 6.03 0.86 610.7 5.0E+06 0.2402

223 9-0-7-000 0.806 0/2 7.06 0.86 606.9 5.0E+06 0.2613

223 9-0-16-500 0.801 0/2 8.05 0.80 602.8 4.9E+06 0.3377

223 9-0-22-500 0.807 0/2 8.09 0.74 623.8 5.1E+06 0.3411

223 9-0-30-000 0.800 0/2 9.03 0.69 618.6 5.1E+06 0.4026

223 9-0-35-500 0.795 0/2 10.00 0.74 613.8 5.1E+06 0.3760

211 10-31-44-000 0.796 10/2 4.13 0.63 595.1 4.9E+06 0.2126

211 10-32-11-500 0.800 10/2 5.00 0.28 597.9 4.9E+06 0.2623

211 10-32-18-500 0.791 10/2 6.07 0.37 579.8 4.8E+06 0.2747

211 10-32-35-500 0.809 10/2 7.98 0.74 606.2 4.9E+06 0.4022

211 10-32-37-000 0.812 10/2 8.05 0.54 611.8 5.0E+06 0.4026

223 10-7-25-000 0.691 5/15 3.01 0.66 310.4 2.8E+06 0.3089

223 8-54-32-000 0.812 10/2 4.28 0.57 613.4 5.0E+06 0.1835

223 8-54-38-500 0.804 10/2 5.18 0.72 601.2 4.9E+06 0.2224

223 8-54-44-000 0.801 10/2 6.08 0.63 595.8 4.9E+06 0.2493

223 8-55-1-000 0.804 10/2 9.02 0.66 610.5 5.0E+06 0.4424

223 8-55-3-500 0.793 10/2 9.06 0.69 594.7 4.9E+06 0.3973

223 8-50-5-500 0.801 5/10 2.99 0.83 601.7 4.9E+06 0.1594

223 8-50-31-000 0.802 5/10 5.00 0.69 609.5 5.0E+06 0.2512

223 8-50-40-000 0.810 5/10 6.02 0.69 619.2 5.0E+06 0.2762

223 8-50-45-000 0.804 5/10 7.08 0.57 608.2 5.0E+06 0.3166

223 8-50-49-500 0.789 5/10 8.00 0.57 584.2 4.8E+06 0.3653

609
TableJ-1.Continued.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

211 10-28-38-500 0.800 5/10 3.03 0.31 601.9 4.9E+06 0.2194

211 10-29-3-500 0.794 5/10 2.93 0.54 593.2 4.9E+06 0.2350

211 10-29-11-500 0.798 5/10 4.10 0.80 597.7 4.9E+06 0.2996

211 10-29-15-500 0.797 5/10 5.15 0.48 595.9 4.9E+06 0.3278

211 10-29-19-000 0.796 5/10 5.95 0.66 593.9 4.9E+06 0.3689

211 10-29-28-500 0.788 5/10 8.13 0.74 582.1 4.8E+06 0.4656

211 9-57-50-000 0.798 5/11 3.16 0.25 786.2 6.5E+06 0.1765

211 9-58-1-500 0.812 5/10 5.23 0.22 811.0 6.6E+06 0.3021

211 9-58-4-500 0.805 5/10 5.81 0.43 793.8 6.5E+06 0.2369

223 9-2-37-500 0.856 0/2 4.02 0.54 595.5 4.7E+06 0.1865

223 9-2-45-000 0.863 0/2 5.21 0.80 605.2 4.7E+06 0.2049

223 9-2-50-000 0.860 0/2 6.06 0.77 600.1 4.7E+06 0.2962

223 9-2-53-500 0.862 0/2 7.29 0.77 603.3 4.7E+06 0.4023

223 9-2-57-500 0.859 0/2 8.07 0.83 601.1 4.7E+06 0.4515

223 9-3-3-500 0.857 0/2 9.22 0.83 606.2 4.8E+06 0.4920

223 9-3-15-000 0.848 0/2 9.91 0.66 610.5 4.8E+06 0.4793

208 15-2-25-000 0.851 0/2 4.10 -0.10 598.2 4.7E+06 0.1806

208 15-2-29-500 0.853 0/2 5.07 0.31 600.8 4.7E+06 0.2395

208 15-2-39-000 0.857 0/2 6.99 0.25 608.5 4.8E+06 0.3620

208 15-2-48-500 0.854 0/2 8.06 0.25 610.5 4.8E+06 0.4296

208 15-2-57-000 0.849 0/2 9.11 0.17 619.4 4.9E+06 0.4840

208 14-57-18-000 0.854 10/2 4.00 0.40 600.1 4.7E+06 0.1731

208 14-57-43-000 0.851 10/2 4.02 0.45 596.3 4.7E+06 0.1775

208 14-57-56-000 0.851 10/2 4.05 0.45 596.3 4.7E+06 0.1789

208 14-58-10-000 0.854 10/2 5.18 0.34 599.8 4.7E+06 0.2939

208 14-58-14-500 0.853 10/2 6.02 0.19 598.6 4.7E+06 0.3008

208 14-58-21-500 0.856 10/2 7.15 0.22 603.1 4.7E+06 0.4154

208 14-58-29-500 0.849 10/2 8.06 0.11 597.3 4.7E+06 0.4509

208 14-58-32-000 0.847 10/2 7.97 0.34 596.2 4.7E+06 0.4603

208 14-58-46-000 0.841 10/2 9.15 0.72 580.5 4.6E+06 0.4966

208 14-58-50-500 0.840 10/2 10.26 0.48 582.8 4.6E+06 0.4567

224 9-10-37-500 0.847 10/2 4.09 0.57 587.1 4.6E+06 0.1963

224 9-11-20-000 0.849 10/2 8.01 0.34 587.7 4.6E+06 0.4529

224 9-11-33-500 0.859 10/2 7.99 0.25 612.7 4.8E+06 0.4575

208 14-52-18-000 0.862 5/10 3.07 0.08 611.4 4.8E+06 0.1502

208 14-53-36-000 0.857 5/10 3.00 0.17 598.7 4.7E+06 0.1234

208 14-54-9-500 0.852 5/10 8.03 0.40 604.5 4.8E+06 0.4939

610
TableJ-1.Concluded.

Flight Time MINF Camber ALPT BETA QINF RNPU CNWP

208 14-54-11-000 0.851 5/10 7.93 -0.24 606.5 4.8E+06 0.4625

224 9-7-47-000 0.849 5/10 3.03 0.43 588.2 4.6E+06 0.1959

224 9-8-12-500 0.858 5/11 4.08 0.28 600.7 4.7E+06 0.2656

224 9-8-18-500 0.858 5/11 5.12 0.22 598.5 4.7E+06 0.3537

224 9-8-26-500 0.855 5/10 6.97 0.22 594.5 4.7E+06 0.4279

224 9-8-31-000 0.848 5/10 8.00 0.02 583.5 4.6E+06 0.4797

211 11-53-1-500 0.900 0/2 3.52 0.63 601.5 4.6E+06 0.1955

211 11-53-16-000 0.897 0/3 3.99 -0.04 595.2 4.5E+06 0.2007

211 11-53-20-000 0.898 0/2 4.98 0.57 597.1 4.5E+06 0.2452

211 11-53-26-500 0.897 0/2 7.14 0.28 595.2 4.5E+06 0.3855

211 11-53-30-500 0.897 0/2 8.10 0.19 600.0 4.6E+06 0.4332

211 11-53-32-000 0.902 0/2 8.11 1.18 610.3 4.6E+06 0.4627

211 11-48-2-000 0.901 10/2 4.04 0.63 599.9 4.6E+06 0.2434

211 11-48-23-500 0.892 10/2 5.96 0.34 588.0 4.5E+06 0.3356

211 11-48-28-000 0.895 10/2 7.01 0.25 590.4 4.5E+06 0.3709

211 11-48-29-000 0.897 10/2 7.02 0.34 592.9 4.5E+06 0.3783

211 11-48-36-000 0.902 10/2 7.92 0.40 606.0 4.6E+06 0.4400

211 11-48-38-500 0.905 10/2 8.01 0.40 613.1 4.6E+06 0.4479

211 11-48-46-000 0.908 10/2 9.13 0.19 634.3 4.8E+06 0.4844

211 11-45-23-500 0.896 5/10 3.20 0.17 596.0 4.5E+06 0.1808

211 11-45-51-500 0.899 5/11 4.09 -0.10 596.2 4.5E+06 0.3033

211 11-45-57-000 0.900 5/10 6.03 0.02 594.8 4.5E+06 0.3696

211 11-46-1-000 0.891 5/10 7.16 0.05 580.3 4.4E+06 0.4117

211 11-46-14-500 0.894 5/10 7.99 0.22 628.8 4.8E+06 0.4275

211 11-46-17-000 0.898 5/10 8.05 0.05 650.2 4.9E+06 0.4384

231 13-33-23-000 0.631 7/-1 11.45 -0.27 387.6 3.8E+06 0.4439

211 11-38-33-000 0.850 0/2 5.51 0.08 253.3 2.0E+06 0.2692

211 11-39-16-000 0.850 0/2 5.60 0.11 252.9 2.0E+06 0.2661

611
Table J-2. Listing of data.

Flight 228, Wing sweep = 26 °, Time = 12-45-12-500, MINF = 0.610. Camber = 0/2, ALPT = 7.10, BETA = 0.11, QINF = 312.0.

RNPU = 3.2E+06. CNWP = 0.1939

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.569 0.000 0.481 0.000 4.765"* 0.010 -2.127

0.060 -0.410 0.020 - 1.149 0.020 - 1.794 0.020 - 1.783

0.110 -0.359 0.040 -1.508"* 0.060 -2.078** 0.060 -0.837

0.200 -0.240 0.060 -0.670 0.090 -0.610 0.110 -0.605

0.230 -0.241 0.090 -0.479 0.110 -0.582 0.140 -0.561

0.400 -0.198 0.130 -0.487 0.130 -0.518 0.190 -3.845"*

0.490 -0.213 0.150 -0.477 0.150 -0.505 0.250 -0.455

0.590 -0.246 0.200 -0.405 0.210 -0.493 0.400 -0.427

0.630 -0.242 0.250 1.773** 0.250 -0.444 0.490 -0.291

0.700 -0.224 0.260 -0.397 0.340 0.454** 0.580 -0.256

0.750 -0.225 0.280 1.748"* 0.370 - 1.377'* 0.650 -0.330

0.810 -0.199 0.290 -0.010"* 0.400 -0.360 0.700 -0.285

0.840 -0.209 0.310 1.275** 0.410 -0.180** 0.750 -0.305

0.900 -0.169 0.320 0.994** 0.430 -1.311 ** 0.800 -0.250

0.960 -0.021 0.340 1.160** 0.440 -0.929** 0.830 -0.233

0.350 -0.888** 0.460 -0.481 ** 0.900 -0.155

0.370 1.183** 0.490 -0.366 0.960 -0.016

0.380 -0.894** 0.500 0.977**

0.400 -0.359 0.520 - 1.500"*

0.410 1.188"* 0.540 0.565"*

0.430 0.760** 0.550 0.749**

0.440 -0.298 0.580 -0.237

0.460 0.751 ** 0.600 0.717"*

0.470 0.618"* 0.610 0.608**

0.490 -0.280 0.650 3.796"*

0.500 0.791"* 0.700 -0.361

0.520 0.435** 0.750 -0.315

0.530 -0.298 0.820 -0.272

0.550 0.123"* 0.890 -0.126

0.560 0.682** 0.900 -0.100

0.580 -0.283 0.960 -0.010

0.590 1.053"*

0.600 0.981 **

0.640 -0.311

0.700 -0.287

0.750 -0.059**

0.820 -0.262

0.870 -0.051

0.930 -0.100

0.960 -0.058

Lower Surface

0.020 0.137 0.020 0.257 0.020 0.398 0.020 0.638

0.110 -0.047 0.060 0.154 0.060 0.242 0.060 3.651 **

0.230 0.001 0.090 0.084 0.090 2.309** 0.110 0.198

0.400 -0.012 0.120 -0.686* * 0.120 0.064 0.250 -0.059

0.490 0.010 0.200 -0.008 0.200 0.061 0.400 -0.073

0.630 1.839"* 0.260 -0.015 0.250 -0.038 0.490 -0.095

0.750 -0.017 0.400 -0.049 0.400 -0.096 0.580 -0.153

0.850 0.010 0.490 -0.088 0.490 -0.026 0.650 -0.075

0.900 0.100 0.580 -0.090 0.580 -0.117 0.750 0.106

0.960 0.087 0.640 0.024 0.650 -0.060 0.830 0.253

0.750 0.158 0.750 -0.018 0.900 0.289

0.870 0.204 0.890 0.218 0.960 0.220

0.930 0.138 0.930 0.188

0.960 0.110 0.960 -1.684**

CN = 0.223 0.377 0.348 0.440

612
Table J-2. Continued.

Flight 228, Wing sweep = 26 _, Time = 12-45-16-500, MINF = 0.602, Camber = 0/2, ALPT = 8.10, BETA = 0.14, QINF = 304.7,

RNPU = 3. IE+06, CNWP = 0.2266

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.786 0.000 0.237 0.000 4.880** 0.010 -2.506

0.060 -0.520 0.020 -2.145 0.020 -2.361 0.020 -2.461

0.110 -0.424 0.040 -1.684"* 0.060 -2.126"* 0.060 -0.877

0.200 -0.297 0.060 -0.807 0.090 -0.701 0.110 -0.677

0.230 -0.279 0.090 -0.588 0.110 -0.634 0.140 -0.640

0.400 -0.239 0. 130 -0.569 0.130 -0.602 0.190 -3.936"*

0.490 -0.232 0.150 -0.530 0.150 -0.580 0.250 -0.493

0.590 -0.258 0.200 -0.484 0.210 -0.555 0.400 -0.429

0.630 -0.244 0.250 1.816"* 0.250 -0.476 0.490 -0.311

0.700 -0.250 0.260 -0.446 0.340 0.466** 0.580 -0.302

0.750 -0.255 0.280 1.799** 0.370 - 1.416"* 0.650 -0.322

0.810 -0.217 0.290 -0.010"* 0.400 -0.404 0.700 -0.295

0.840 -0.232 0.310 1.292"* 0.410 -0.184"* 0.750 -0.290

0.900 -0.184 0.320 1.018"* 0.430 - 1.356"* 0.800 -0.228

0.960 -0.049 0.340 1.174"* 0.440 -0.951 ** 0.830 -0.216

0.350 -0.909** 0.460 -0.501 ** 0.900 -0.131

0.370 1.209** 0.490 -0.389 0.960 -0.046

0.380 -0.914"* 0.500 0.987**

0.400 -0.313 0.520 - 1.535"*

0.410 1.206"* 0.540 0.586**

0.430 0.779** 0.550 0.753**

0.440 -0.319 0.580 -0.273

0.460 0.770** 0.600 0.735"*

0.470 0.640** 0.610 0.609**

0.490 -0.316 0.650 3.887**

0.500 0.810"* 0.700 -0.362

0.520 0.408** 0.750 -0.336

0.530 -0.300 0.820 -0.284

0.550 0.127"* 0.890 -0.127

0.560 0.680"* 0.900 -0.102

0.580 -0.296 0.960 -0.006

0.590 1.064**

0.600 1.005**

0.640 -0.335

0.700 -0.297

0.750 -0.052**

0.820 -0.281

0.870 -0.062

0.930 -0.112

0.960 -0.059

Lower Surface

0.020 0.232 0.020 0.381 0.020 0.516 0.020 0.680

0.110 0.005 0.060 0.244 0.060 0.313 0.060 3.739**

0.230 0.032 0.090 0.149 0.090 2.365 * * 0.110 0.204

0.400 -0.011 0.120 -0.637** 0.120 0.134 0.250 -0.015

0.490 -0.018 0.200 0.046 0.200 0.093 0.400 -0.038

0.630 1.883"* 0.260 0.014 0.250 -0.002 0.490 -0.066

0.750 -0.013 0.400 -0.030 0.400 -0.054 0.580 -0.140

0.850 0.011 0.490 -0.055 0.490 -0.040 0.650 -0.047

0.900 0.093 0.580 -0.083 0.580 -0.083 0.750 0.124

0.960 0.078 0.6443 0.040 0.650 -0.061 0.830 0.246

0.750 0.148 0.750 -0.032 0.900 0.276

0.870 0.210 0.890 0.231 0.960 0.215

0.930 0.138 0.930 0.172

0.960 0.102 0.960 - 1.723"*

CN = 0.264 0.459 0.402 0.497

613
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-45-22-000, MINF = 0.608, Camber = 0/2, ALPT = 10.21, BETA = -0.01, QINF = 309.5,

RNPU = 3.1E+06, CNWP = 0.2434

rl -- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.912 0.000 -0.195 0.000 4.808 * * 0.010 -2.753

0.060 -0.758 0.020 -2.645 0.020 -2.716 0.020 -2.748

0.110 -0.567 0.040 - 1.798"* 0.060 -2.089"* 0.060 - 1.534

0.200 -0.383 0.060 - 1.271 0.090 - 1.207 0.110 -0.838

0.230 -0.453 0.090 -0.712 0.110 - 1.013 0.140 -0.733

0.400 -0.297 0.130 -0.675 0.130 -0.826 0.190 -3.871 * *

0.490 -0.278 0.150 -0.647 0.150 -0.757 0.250 -0.522

0.590 -0.296 0.200 -0.590 0.210 -0.645 0.400 -0.459

0.630 -0.299 0.250 1.779** 0.250 -0.577 0.490 -0.343

0.700 -0.290 0.260 -0.514 0.340 0.455** 0.580 -0.330

0.750 -0.282 0.280 1.772"* 0.370 - 1.444** 0.650 -0.318

0.810 -0.259 0.290 -0.009** 0.400 -0.429 0.700 -0.303

0.840 -0.283 0.310 1.268"* 0.410 -0.177"* 0.750 -0.296

0.900 -0.217 0.320 0.999"* 0.430 -1.360"* 0.800 -0.240

0.960 -0.085 0.340 1.161"* 0.440 -0.958** 0.830 -0.203

0.350 -0.891 ** 0.460 -0.521 ** 0.900 -0.163

0.370 1.190** 0.490 -0.416 0.960 -0.125

0.380 -0.877** 0.500 0.980**

0.400 -0.375 " 0.520 -1.542"*

0.410 1.187** 0.540 0.575**

0.430 0.768"* 0.550 0.736**

0.440 -0.350 0.580 -0.285

0.460 0.764** 0.600 0.730**

0.470 0.629"* 0.610 0.605"*

0.490 -0.351 0.650 3.831 **

0.500 0.800** 0.700 -0.317

0.520 0.397** 0.750 -0.298

0.530 -0.336 0.820 -0.220

0.550 0.116** 0.890 -0.092

0.560 0.676** 0.900 -0.085

0.580 -0.312 0.960 -0.011

0.590 1.062**

0.600 0.993"*

0.640 -0.331

0.700 -0.285

0.750 -0.033**

0.820 -0.259

0.870 -0.040

0.930 -0.085

0.960 -0.054

Lower Surface

0.020 0.368 0.020 0.556 0.020 0.639 0.020 0.770

0.110 0.093 0.060 0.378 0.060 0.396 0.060 3.685**

0.230 0.086 0.090 0.261 0.090 2.332** 0.110 0.346

0.400 0.000 0.120 -0.536"* 0.120 0.249 0.250 0.079

0.490 0.015 0.200 0.141 0.200 0.188 0.400 0.023

0.630 1.865"* 0.260 0.094 0.250 0.087 0.490 -0.011

0.750 -0.010 0.400 0.018 0.400 -0.011 0.580 -0.091

0.850 0.007 0.490 -0.014 0.490 -0.014 0.650 -0.014

0.900 0.088 0.580 -0.053 0.580 -0.050 0.750 0.140

0.960 0.067 0.640 0.061 0.650 -0.042 0.830 0.248

0.750 0.164 0.750 -0.014 0.900 0.272

0.870 0.198 0.890 0.224 0.960 0.181

0.930 0.133 0.930 0.166

0.960 0.101 0.960 - 1.692"*

CN = 0.366 0.565 0.511 0.619

614
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-45-24-500, MINF = 0.606, Camber = 0/2, ALPT = 12.01, BETA = 0.54, QINF = 307.8,

RNPU = 3.1E+06, CNWP = 0.2957

_] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1,650 0.000 -0.438 0,000 4.836"* 0.010 -2. 156

0.060 - 1.310 0.020 -2.178 0,020 - 1.837 0,020 -2.112

0.110 -0.872 0,040 - 1.807 * * 0.060 -2.099 * * 0.060 - 1.632

0.200 -0.470 0.060 - 1.307 0,090 - 1.273 0.110 - 1.357

0,230 -0.436 0.090 -1.067 0.110 -1.182 0.140 -1.082

0.400 -0.348 0,130 -0.982 0.130 -1.077 0.190 -3.891"*

0.490 -0.332 0,150 -0,897 0.150 - 1.079 0.250 -0.728

0.590 -0.326 0,200 -0.819 0.210 -0.945 0,400 -0.555

0,630 -0,326 0,250 1.791 ** 0.250 -0,889 0.490 -0,426

0.700 -0.305 0.260 -0.648 0,340 0.459** 0.580 -0,361

0.750 -0.267 0,280 1.784** 0.370 -1.535** 0.650 -0,383

0.810 -0.25 l 0,290 -0.033"* 0,400 -0,545 0.700 -0,363

0.840 -0.276 0,310 1.274"* 0,410 -0.176"* 0.750 -0.353

0.900 -0.214 0.320 1.001"* 0.430 - 1.454"* 0.800 -0.280

0.960 -0.101 0.340 1.162"* 0.440 - 1.042"* 0.830 -0.256

0,350 -0.894** 0,460 -0.606** 0,900 -0.242

0.370 1.195** 0.490 -0.512 0.960 -0,207

0.380 -0.885** 0,500 0,978**

0.400 -0.471 0.520 - 1.631 **

0.410 1.192"* 0.540 0.580**

0.430 0,769** 0.550 0.741 **

0.440 -0.426 0.580 -0.319

0,460 0.759"* 0.600 0.735"*

0,470 0.628"* 0,610 0.609"*

0.490 -0.386 0,650 3.853**

0.500 0.811 ** 0,700 -0.335

0.520 0.408** 0.750 -0,313

0.530 -0.371 0.820 -0,236

0.550 0.119"* 0.890 -0.133

0.560 0.681"* 0.900 -0.151

0.580 -0,338 0.960 -0.075

0.590 1.047"*

0.600 0,986**

0.640 -0,266

0.700 -0.252

0,750 -0.039**

0.820 -0.197

0,870 -0,038

0.930 -0.134

0.960 -0.113

Lower Surface

0.020 0.465 0.020 0,635 0.020 0,727 0.020 0.794

0.110 0.153 0.060 0.451 0.060 0.523 0,060 3.707" *

0,230 0.110 0,090 0.329 0,090 2.346** 0.110 0.448

0.400 0,019 0.120 -0.470** 0.120 0.331 0.250 0,145

0,490 0.031 0.200 0.196 0.200 0.262 0,400 0.074

0.630 1.873"* 0,260 0.153 0.250 0.146 0,490 0.027

0.750 -0.019 0.400 0.053 0,400 0.019 0.580 -0.070

0.850 -0.010 0.490 0.002 0.490 -0.012 0,650 -0,005

0.900 0.061 0.580 -0.040 0,580 -0.031 0,750 0.147

0.960 0.040 0,640 0,059 0.650 -0.040 0.830 0.247

0.750 0.150 0.750 -0.012 0.900 0,264

0,870 0.182 0.890 0.206 0,960 0.154

0.930 0.093 0,930 0.140

0.960 0.050 0,960 -1.700"*

CN = 0.452 0.635 0.643 0,754

615
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-45-28-000, MINF = 0.598, Camber = 0/2, ALPT = 13.04, BETA = 0.83, QINF = 299.6,

RNPU = 3. IE+06, CNWP = 0.3296

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.855 0.000 -0.578 0.000 4.969** 0.010 -2.304

0.060 - 1.387 0.020 - 1.786 0.020 - 1.561 0.020 - 1.862

0.110 -0.823 0.040 -1.856"* 0.060 -2.156"* 0.060 - 1.484

0.200 -0.480 0.060 - 1.080 0.090 - 1.189 0,110 - 1.242

0.230 -0.452 0.090 -0.943 0.110 - 1.119 0.140 - 1.079

0.400 -0.328 0.130 -0.876 0.130 - 1.038 0.190 -3.996**

0.490 -0.341 0.150 -0.854 0.150 - 1.051 0.250 -0.874

0.590 -0.336 0.200 -0.775 0.210 -0.947 0.400 -0.716

0.630 -0.323 0.250 1.855** 0.250 -0.877 0.490 -0.53 l

0.700 -0.306 0.260 -0.712 0.340 0.471 ** 0.580 -0.450

0.750 -0.259 0.280 1.839"* 0.370 -1.632** 0.650 -0.465

0.810 -0,225 0.290 -0.106 * * 0.400 -0.612 0.700 -0.441

0.840 -0.253 0.310 1.317"* 0.410 -0.180"* 0.750 -0.399

0.900 -0.212 0.320 1.025** 0.430 - 1.554"* 0.800 -0.315

0.960 -0.128 0.340 1.202** 0.440 - 1.128** 0.830 -0.303

0.350 -0.918"* 0.460 -0.679** 0.900 -0.260

0.370 1.235"* 0.490 -0.617 0.960 -0,230

0.380 -0.908** 0.500 1.011 **

0.400 -0.491 0.520 - 1.745"*

0.410 1.222"* 0.540 0.596**

0.430 0.805** 0.550 0.764**

0.440 -0.471 0.580 -0.435

0.460 0.794** 0.600 0.744**

0.470 0.639** 0.610 0.627"*

0.490 -0.409 0.650 3.959**

0.500 0.826** 0.700 -0.414

0.520 0.411 ** 0.750 -0.395

0.530 -0.431 0.820 -0.308

0.550 0.137** 0.890 -0.194

0.560 0.702** 0.900 -0.210

0.580 -0.352 0.960 -0.154

0.590 1.082**

0.600 1.023"*

0.640 -0.285

0.700 -0.259

0.750 -0.029**

0.820 -0.202

0.870 -0.043

0.930 -0.153

0.960 -0.145

Lower Surface

0.020 0.535 0.020 0.674 0.020 0.778 0.020 0.791

0.110 0.193 0.060 0.497 0.060 0.559 0.060 3.809'*

0.230 0.125 0.090 0.374 0.090 2.411 ** 0,110 0.455

0.400 0.020 0.120 -0.446 ** 0.120 0.394 0.250 0.197

0.490 0.028 0.200 0.239 0.200 0.311 0.400 0.117

0.630 1.931 ** 0.260 0.190 0.250 0.187 0.490 0.043

0.750 -0.005 0.400 0.080 0.400 0.045 0.580 -0.037

0.850 0.001 0.490 0.025 0.490 -0.019 0.650 0.003

0.900 0.064 0.580 -0.026 0.580 -0.006 0.750 0.142

0.960 0.023 0.640 0.072 0.650 -0.048 0.830 0.243

0.750 0.139 0.750 0.006 0.900 0.256

0.870 0.175 0.890 0.197 0.960 0.141

0.930 0.067 0.930 0.125

0.960 0.022 0.960 - 1.746**

CN = 0,463 0.638 0.708 0.824

616
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-45-37-500, MINF = 0.594, Camber = 0/2, ALPT = 12.03, BETA = -0.44, QINF = 296.6,

RNPU = 3. IE+06, CNWP = 0.2431

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0,020 - 1.728 0.000 -0.496 0.000 5.004* * 0.010 -2.321

0.060 - 1.245 0.020 -2.222 0.020 - 1.930 0,020 -2.275

0.110 -0,823 0.040 -1.875"* 0_060 -2.193"* 0.060 -1.768

0.200 -0.449 0.060 - 1.247 0.090 - 1.201 0.110 - 1.289

0.230 -0.284 0.090 -1.002 0.110 -1.154 0.140 -1.033

0.400 -0.316 0.130 -0.940 0.130 -1.040 0.190 -4.052**

0.490 -0.322 0.150 -0.861 0.150 - 1.017 0.250 -0.670

0.590 -0.323 0.200 -0.763 0.210 -0,877 0.400 -0.541

0.630 -0.314 0.250 1.833"* 0.250 -0.762 0.490 -0.414

0.700 -0.283 0.260 -0.617 0.340 0.446** 0.580 -0.385

0.750 -0.250 0.280 1.834"* 0.370 -1.553"* 0.650 -0.361

0.810 -0,224 0,290 -0.122** 0.400 -0.580 0.700 -0.345

0.840 -0,248 0.310 1.300"* 0.410 -0.197"* 0,750 -0,344

0.900 -0.207 0.320 1.026"* 0.430 - 1.493"* 0.800 -0.304

0.960 -0.080 0.340 1.186** 0.440 - 1.067"* 0.830 -0.238

0.350 -0,942** 0.460 -0.614"* 0.900 -0.232

0.370 1.214"* 0.490 -0.478 0.960 -0.198

0.380 -0.909** 0.500 1.002"*

0.400 °0.445 0.520 -1.678"*

0.410 1.214"* 0.540 0.581 **

0.430 0.789** 0.550 0.759**

0.440 -0.383 0.580 -0.277

0.460 0.778** 0.600 0.753**

0.470 0.641 ** 0.610 0,634**

0.490 -0.376 0.650 3.985"*

0.500 0.809** 0.700 -0.314

0.520 0.384** 0.750 -0.294

0.530 -0.346 0.820 -0.215

0.550 0.114"* 0.890 -0.116

0.560 0.676** 0.900 -0.133

0.580 -0.324 0.960 -0.078

0.590 1.083"*

0.600 1.008"*

0.640 -0.286

0.700 -0.232

0.750 -0.037**

0.820 -0.208

0.870 -0.043

0,930 -0.147

0.960 -0.147

Lower Surface

0.020 0.461 0.020 0.635 0,020 0.722 0.020 0.786

0.1 I0 0.146 0.060 0.449 0.060 0.556 0.060 3.832**

0.230 0.107 0.090 0.321 0.090 2.421 ** 0.110 0.439

0.400 0.009 0.120 -0.466"* 0.120 0.337 0.250 0.138

0.490 0.025 0.200 0.193 0.200 0.252 0.400 0,084

0.630 1.921 * * 0.260 0.144 0.250 0.145 0,490 0,020

0.750 -0.005 0.400 0,058 0,400 0.010 0.580 -0,073

0.850 0.004 0.490 0.002 0.490 -0.013 0.650 -0.013

0.900 0.06 l 0.580 -0.04 1 0,580 -0.021 0.750 0.133

0.960 0.038 0.640 0.069 0.650 -0.027 0.830 0.254

0.750 0.148 0.750 -0.012 0.900 0.270

0.870 0.180 0.890 0.199 0.960 0.140

0.930 0.103 0.930 0.134

0,960 0.055 0.960 - 1.779**

CN = 0.418 0.618 0.608 0.742

617
Table J-2. Continued.

Hight 228, Wing sweep = 26 °, Time = 12-45-59-000, MINF = 0.602, Camber = 0/2, ALPT = 13.00, BETA = 0.60, QINF = 299.3,

RNPU = 3. IE+06, CNWP = 0.2755

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.796 0.000 -0.556 0.000 5.037"* 0.010 - 1.919

0.060 - 1.361 0.020 - 1.798 0.020 - 1.565 0.020 - 1.749

0.110 -0.938 0.040 -1.782"* 0.060 -2.097** 0.060 -1.433

0.200 -0.491 0.060 - 1.122 0.090 - 1.179 0.110 - 1.293

0.230 -0.444 0.090 -0.993 0.110 - 1.139 0.140 - 1.108

0.400 -0.349 0.130 -0.920 0.130 - 1.014 0.190 -3.939 **

0.490 -0.322 0.150 -0.857 0.150 - 1.037 0.250 -0.906

0.590 -0.315 0.200 -0.820 0.210 -0.921 0.400 -0.713

0.630 -0.315 0.250 1.872"* 0.250 -0.859 0.490 -0.480

0.700 -0.290 0.260 -0.695 0.340 0.507** 0.580 -0.471

0.750 -0.250 0.280 1.866** 0.370 - 1.613** 0.650 -0.435

0.810 -0.239 0.290 -0.142'* 0.400 -0.652 0.700 -0.420

0.840 -0.263 0.310 1.350** 0.410 -0.118"* 0.750 -0.380

0.900 -0.205 0.320 1.071"* 0.430 -1.536** 0.800 -0.325

0.960 -0.117 0.340 1.235"* 0.440 - 1.108 ** 0.830 -0.295

0.350 -0.857** 0.460 -0.657** 0.900 -0.270

0.370 1.263** 0.490 -0.575 0.960 -0.224

0.380 -0.915'* 0.500 1.039"*

0.400 -0.568 0.520 -1.706**

0.410 1.263"* 0.540 0.628**

0.430 0.830"* 0.550 0.819**

0.440 -0.488 0.580 -0.358

0.460 0.821 ** 0.600 0.791 **

0.470 0.677" * 0.610 0.666' *

0.490 -0.436 0.650 4.026**

0.500 0.867** 0.700 -0.351

0.520 0.440** 0.750 -0.324

0.530 -0.366 0.820 -0.247

0.550 0.163 ** 0.890 -0.176

0.560 0.731 ** 0.900 -0.167

0.580 -0.403 0.960 -0.121

0.590 1.109"*

0.600 1.053"*

0.640 -0.286

0.700 -0.251

0.750 -0.042"*

0.820 -0.231

0.870 -0.049

0.930 -0,207

0.960 -0.207

Lower Surface

0.020 0.504 0.020 0.630 0.020 0.761 0.020 0.791

0.110 0.180 0.060 0.484 0.060 0.556 0.060 3.875"*

0.230 0.126 0.090 0.353 0.090 2.476** 0,110 0.466

0.400 0.032 0.120 -0.457"* 0.120 0.376 0.250 0.181

0.490 0.022 0.200 0.222 0.200 0.291 0.400 0.103

0.630 1.972"* 0.260 0.177 0.250 0.185 0.490 0.047

0.750 -0.019 0.400 0.067 0.400 0.035 0.580 -0.047

0.850 -0.009 0.490 0.011 0.490 -0.008 0.650 0.007

0.900 0.055 0.580 -0.036 0.580 -0.016 0.750 0.146

0.960 0.021 0.640 0.058 0.650 -0.043 0.830 0.246

0.750 0.143 0.750 -0.007 0.900 0.264

0.870 0.165 0.890 0.191 0.960 0.155

0.930 0.075 0.930 0.119

0.960 0.023 0.960 -1.686"*

CN = 0.462 0.650 0.667 0.821

618
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-46-32-500, MINF = 0.595, Camber = 0/2, ALPT = 13.06, BETA = -0.88. QINF = 296.2,

RNPU = 3AE+06, CNWP = 0.3285

= 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 - 1.903 0.000 -0.624 0.000 5.038"* 0.010 -2.164

0.060 - 1.358 0.020 - 1.713 0.020 - 1.493 0.020 -1.781

0.110 -0.800 0.040 - 1.865"* 0.060 -2.169"* 0.060 - 1.440

0.200 -0.490 0.060 - 1.063 0.090 - I. 126 0.110 - 1.318

0.230 -0.441 0.090 -0.948 0.110 - 1.071 0.140 - 1.040

0.400 -0.342 0.130 -0.895 0.130 -0.993 0.190 -4.030"*

0.490 -0.303 0.150 -0.870 0.150 - 1.023 0.250 -0.943

0.590 -0.311 0.200 -0.806 0.210 -0.922 0.400 -0.663

0.630 -0.306 0.250 1.835"* 0.250 -0.904 0.490 -0.487

0.700 -0.289 0.260 -0.674 0.340 0.444** 0.580 -0.426

0.750 -0.245 0.280 1.817** 0.370 - 1.636** 0.650 -0.432

0.810 -0.227 0.290 -0.168"* 0.400 -0.718 0.700 -0.417

0.840 -0.213 0.310 1.301 ** 0.410 -0.170** 0.750 -0.413

0.900 -0.197 0.320 1.017"* 0.430 -1.558"* 0.800 -0.335

0.960 -0.103 0.340 1.172"* 0.440 - l. 122"* 0.830 -0.309

0.350 -0.916"* 0.460 -0.661"* 0.900 -0.253

0.370 1.213"* 0.490 -0.642 0.960 -0.194

0.380 -0.921 ** 0.500 0.987**

0.400 -0.533 0.520 - 1.748' *

0.410 1.207"* 0.540 0.573**

0.430 0.776** 0.550 0.744**

0.440 -0.535 0.580 -0.439

0.460 0.753** 0.600 0.740**

0.470 0.626** 0.610 0.619"*

0.490 -0.425 0.650 4.017"*

0.500 0.850** 0.700 -0.369

0.520 0.374** 0.750 -0.349

0.530 -0.445 0.820 -0.259

0.550 0.108"* 0.890 -0.179

0.560 0.677** 0.900 -0.188

0.580 -0.406 0.960 -0.129

0.590 1.042"*

0.600 0.982**

0.640 -0.261

0.700 -0.242

0.750 -0.050**

0.820 -0.241

0.870 -0.035

0.930 -0.194

0.960 -0.183

Lower Surface

0.020 0.506 0.020 0.680 0.020 0.753 0.020 0.772

0.110 0.178 0.060 0.485 0.060 0.556 0.060 3.865" *

0.230 0.127 0.090 0.364 0.090 2.451 ** 0.110 0.484

0.400 0.025 0.120 -0.454"* 0.120 0.379 0.250 0.183

0.490 0.030 0.200 0.232 0.200 0.292 0.400 0.105

0.630 1.914"* 0.260 0.186 0.250 0.194 0.490 0.049

0.750 -0.035 0.400 0.064 0.400 0.043 0.580 -0.040

0.850 -0.020 0.490 0.026 0.490 -0.008 0.650 0.008

0.900 0.040 0.580 -0.040 0.580 -0.008 0.750 O. 155

0.960 0.010 0.640 0.066 0.650 -0.036 0.830 0.237

0.750 0.144 0.750 0.000 0.900 0.263

0.870 0.165 0.890 0.190 0.960 0.152

0.930 0.072 0.930 0.128

0.960 0.024 0.960 - 1.754**

CN = 0.440 0.642 0.701 0.818

619
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-48-50-000, M1NF = 0.605, Camber = 3/5, ALPT = 6.70, BETA = 0.77, QINF = 300.5,

RNPU = 3. IE+06, CNWP = 0.3074

rl -- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.333 0.000 0.744 0.000 4.912"* 0.010 - 1.675

0.060 -0.371 0.020 -0.699 0.020 -0.913 0.020 -0.955

0.110 -0.508 0.040 - 1.331 ** 0.060 -2.098** 0.060 -0.909

0.200 -0.329 0.060 -0.640 0.090 -0.702 0.110 -0.802

0.230 -0.340 0.090 -0.576 0.110 -0.726 0.140 -0.716

0.400 -0.254 0.130 -0.636 0.130 -0.712 0.190 -3.909"*

0.490 -0.250 0.150 -0.654 0.150 -0.658 0.250 -0.505

0.590 -0.320 0.200 -0.550 0.210 -0.589 0.400 -0.455

0.630 -0.334 0.250 1.708** 0.250 -0.496 0.490 -0.356

0.700 -0.373 0.260 -0.457 0.340 0.355** 0.580 -0.324

0.750 -0.444 0.280 1.697"* 0.370 -1.410"* 0.650 -0.422

0.810 -0.392 0.290 0.011 ** 0.400 -0.432 0.700 -0.398

0.840 -0.408 0.310 1.181 ** 0.410 -0.154"* 0.750 -0.469

0.900 -0.266 0.320 0.909** 0.430 -1.341 ** 0.800 -0.417

0.960 -0.089 0.340 1.078"* 0.440 -0.932** 0.830 -0.428

0.350 -0.880"* 0.460 -0.488"* 0.900 -0.199

0.370 1.102"* 0.490 -0.441 0.960 -0.024

0.380 -0.907** 0.500 0.890**

0.400 -0.348 0.520 - 1.539**

0.410 1.107 * * 0.540 0.475 * *

0.430 0.673"* 0.550 0.626"*

0.440 -0.363 0.580 -0.347

0.460 0.660* * 0.600 0.623"*

0.470 0.517'* 0.610 0.507**

0.490 -0.369 0.650 3.919"*

0.500 0.701"* 0.700 -0.506

0.520 0.277** 0.750 -0.505

0.530 -0.376 0.820 -0.478

0.550 0.022** 0.890 -0.200

0.560 0.570** 0.900 -0.159

0.580 -0.371 0.960 -0.017

0.590 0.938**

0.600 0.909**

0.640 -0.471

0.700 -0.451

0.750 -0.037**

0.820 -0.482

0.870 -0.047

0.930 -0.166

0.960 -0.090

Lower Surface

0.020 -0.097 0.020 0.094 0.020 0.239 0.020 0.520

0.110 -0.037 0.060 0.129 0.060 0.226 0.060 3.771 **

0.230 0.024 0.090 0.076 0.090 2.396 ** 0.110 0.164

0.400 0.000 0.120 -0.715"* 0.120 0.054 0.250 -0.024

0.490 0.027 0.200 0.004 0.200 0.003 0.400 -0.037

0.630 1.829** 0.260 0.033 0.250 0.006 0.490 -0.051

0.750 0.066 0.400 0.004 0.400 -0.048 0.580 -0.081

0.850 0.098 0.490 -0.011 0.490 -0.024 0.650 0.034

0.900 0.176 0.580 -0.008 0.580 -0.010 0.750 0.214

0.960 0.120 0.640 0.144 0.650 -0.005 0.830 0.342

0.750 0.235 0.750 -0.002 0.900 0.383

0.870 0.303 0.890 0.324 0.960 0.291

0.930 0.218 0.930 0.260

0.960 0.161 0.960 - 1.694**

CN = 0.351 0.504 0.477 0.544

620
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-48-55-000, MINF = 0.627, Camber = 4/7, ALPT = 8.30, BETA = -0.76, QINF = 326.1,

RNPU = 3.2E+06, CNWP = 0.3554

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.597 0.000 0.605 0,000 4.602" * 0.010 - 1.900

0.060 -0.533 0.020 - 1.077 0.020 - 1,212 0.020 -1.840

0.110 -0.572 0.040 - 1.552"* 0.060 - 1.943"* 0.060 - 1.185

0.200 -0.428 0.060 -0.925 0.090 -0.981 0.110 - 1.026

0.230 -0.408 0.090 -0.826 0.110 - 1.004 0.140 -0.885

0.400 -0.311 0.130 -0.907 0.130 -0.973 0.190 -3.634 * *

0.490 -0.329 0.150 -0.887 0.150 -0.848 0.250 -0.584

0.590 -0.379 0.200 -0.724 0.210 -0.717 0.400 -0.499

0.630 -0.400 0.250 1.606"* 0.250 -0.601 0.490 -0.381

0.700 -0.454 0.260 -0.554 0.340 0.347** 0.580 -0.389

0.750 -0.564 0.280 1.602** 0.370 -1.331 ** 0.650 -0.431

0.810 -0.502 0.290 0.023** 0.400 -0.476 0.700 -0.409

0.840 -0.523 0.310 1.111"* 0.410 -0.128"* 0.750 -0.475

0.900 -0.337 0.320 0.857** 0.430 -1.279** 0.800 -0.393

0.960 -0.139 0.340 1.016"* 0.440 -0.879** 0.830 -0.379

0.350 -0.806** 0.460 -0.465"* 0.900 -0.169

0.370 1.041 ** 0.490 -0.480 0.960 -0.068

0.380 -0.831 ** 0.500 0.843**

0.400 -0.437 0.520 - 1.439**

0.410 1.041"* 0.540 0.460"*

0.430 0.636** 0.550 0.603**

0,440 -0.411 0.580 -0.407

0.460 0,623** 0.600 0,599**

0.470 0.506** 0,610 0,477**

0,490 -0,424 0.650 3,675"*

0.500 0.623"* 0.700 -0,565

0.520 0.281 ** 0,750 -0.562

0,530 -0,430 0,820 -0.513

0,550 0.025** 0,890 -0,169

0.560 0,545 ** 0,900 -0,129

0.580 -0,422 0.960 -0,007

0.590 0.884**

0.600 0.824**

0.640 -0.545

0.700 -0.520

0.750 -0.018"*

0.820 -0.549

0.870 -0.025

0.930 -0.177

0.960 -0.106

Lower Surface

0.020 0.058 0.020 0.277 0.020 0.367 0.020 0.573

0.110 0.028 0.060 0.240 0.060 0.313 0.060 3.537**

0.230 0.111 0.090 0.170 0.090 2.253"* 0.110 0.201

0.400 0.032 0.120 -0.545" * 0.120 0.143 0.250 0.049

0.490 0.054 0.200 0.106 0.200 0.131 0.400 0.021

0.630 1.716** 0.260 0.109 0.250 0.089 0.490 0.002

0.750 0.084 0.400 0.050 0.400 0.011 0.580 -0.037

0.850 0.110 0.490 0.040 0.490 0.000 0.650 0.081

0.900 0.188 0.580 0.039 0.580 0.033 0.750 0.255

0.960 0.110 0.640 0.191 0.650 -0.026 0.830 0.372

0.750 0.271 0.750 0.027 0.900 0.414

0.870 0.337 0.890 0.358 0.960 0.290

0.930 0.239 0.930 0.285

0.960 0.176 0.960 - 1.566**

CN = 0,463 0.660 0.601 0.669

621
Table J-2. Continued.

Flight 228. Wing sweep = 26 °, Time = 12-48-57-500, MINF = 0.638. Camber = 6/9. ALPT = 10. I 1. BETA = -0.12. QINF = 336.8.

RNPU = 3.3E+06, CNWP = 0.4391

rl -- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.781 0.000 0.510 0.000 4.470"* 0.010 - 1.802

0.060 -0.771 0.020 - 1.612 0.020 - 1.809 0.020 - 1.799

0.110 -0.814 0.040 - 1.589** 0.060 - 1.869'* 0.060 - 1.743

0.200 -0.568 0.060 - 1.327 0.090 - 1.599 0.110 - 1.253

0.230 -0.538 0.090 - 1.399 0.110 - 1.540 0.1 40 - 1.105

0.400 -0.384 0.130 - 1.142 0.130 - 1.609 0.190 -3.507 * *

0.490 -0.382 0.150 - 1.426 0.150 - 1.076 0.250 -0.615

0.590 -0.439 0.200 -0.936 0.2 I0 -0.797 0.400 -0.526

0.630 -0.496 0.250 1.576** 0.250 -0.680 0.490 -0.398

0.700 -0.579 0.260 -0.668 0.340 0.360"* 0.580 -0.413

0.750 -0.750 0.280 1.566"* 0.370 - 1.335"* 0.650 -0.433

0.810 -0.703 0.290 0.014* * 0.400 -0.542 0.700 -0.413

0.840 -0.745 0.310 1.097"* 0.410 -0.111 ** 0.750 -0.474

0.900 -0.406 0.320 0.848"* 0.430 -1.281 ** 0.800 -0.373

0.960 -0.185 0.340 1.004** 0.440 -0.905** 0.830 -0.337

0.350 -0.768"* 0.460 -0.503"* 0.900 -0.210

0.370 1.027** 0.490 -0.527 0.960 -0.158

0.380 -0.775** 0.500 0.838**

0.400 -0.483 0.520 - 1.446"*

0.410 1.029"* 0.540 0.459**

0.430 0.638** 0.550 0.600**

0.440 -0.475 0.580 -0.419

0.460 0.631 ** 0.600 0.584**

0.470 0.505"* 0.610 0.488"*

0.490 -0.479 0.650 3.572**

0.500 0.666"* 0.700 -0.590

0.520 0.275"* 0.750 -0.601

0.530 -0.486 0.820 -0.507

0.550 0.078** 0.890 -0.111

0.560 0.549"* 0.900 -0.101

0.580 -0.483 0.960 -0.037

0.590 0.878**

0.600 0.823**

0.640 -0.621

0.700 -0.596

0.750 0.001 **

0.820 -0.557

0.870 -0.006

0.930 -0.203

0.960 -0.146

Lower Surface

0.020 0.193 0.020 0.412 0.020 0.490 0.020 0.666

0.110 0.121 0.060 0.350 0.060 0.411 0.060 3.437" *

0.230 0.159 0.090 0.267 0.090 2.194** 0.110 0.340

0.400 0.069 0.120 -0.413'* 0.120 0.252 0.250 0.149

0.490 0.090 0.200 0.160 0.200 0.189 0.400 0.097

0.630 1.683"* 0.260 0.205 0.250 0.189 0.490 0.060

0.750 0.122 0.400 0.126 0.400 0.084 0.580 0.038

0.850 0.137 0.490 0.107 0.490 0.031 0.650 0.163

0.900 0.215 0.580 0.107 0.580 0.109 0.750 0.319

0.960 0.112 0.640 0.253 0.650 0.000 0.830 0.425

0.750 0.337 0.750 0.067 0.900 0.466

0.870 0.373 0.890 0.404 0.960 0.303

0.930 0.267 0.930 0.321

0.960 0.189 0.960 - 1.504**

CN = 0.624 0.853 0.762 0.807

622
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-49-1-000, MINF = 0.635, Camber = 8/12, ALPT = 11.43, BETA = -0.4l, QINF = 330.8,

RNPU = 3.2E+06, CNWP = 0.5211

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.872 0.000 0.381 0.000 4.580** 0.010 -1.856

0.060 - 1.024 0.020 - 1.728 0.020 - 1.891 0.020 - 1.910

0.110 -1.021 0.040 -1.589"* 0.060 -1.874"* 0.060 -1.872

0.200 -0.699 0.060 - 1.432 0.090 - 1.782 0.110 - 1.579

0.230 -0.648 0.090 -1.643 0.110 -1.733 0.140 -1.334

0.400 -0.476 0.130 - 1.433 0.130 -1.911 0.190 -3.541"*

0.490 -0.512 0.150 - 1.779 0.150 - 1.459 0.250 -0.725

0.590 -0.559 0.200 - 1.445 0.2 l0 - 1.283 0.400 -0.563

0.630 -0.607 0.250 1.621"* 0.250 -0.924 0.490 -0.423

0.700 -0.729 0.260 -0.707 0.340 0.376** 0.580 -0.442

0.750 -0.927 0.280 1.619 ** 0.370 - 1.435"* 0.650 -0.443

0.810 -0.888 0.290 -0.040** 0.400 -0.562 0.700 -0.423

0.840 -0.968 0.310 1.139"* 0.410 -0.084"* 0.750 -0.486

0.900 -0.390 0.320 0.884** 0.430 -1.369** 0.800 -0.433

0.960 -0.345 0.340 1.039"* 0.440 -0.989** 0.830 -0.343

0.350 -0.752** 0.460 -0.586** 0.900 -0.336

0.370 1.065"* 0.490 -0.541 0.960 -0.313

0.380 -0.785'* 0.500 0.878**

0.400 -0.525 0.520 - 1.547 * *

0.410 1.070"* 0.540 0.497"*

0.430 0.672" * 0.550 0.638"*

0.440 -0.533 0.580 -0.521

0.460 0.659** 0.600 0.624**

0.470 0.548** 0.610 0.520**

0.490 -0.539 0.650 3.666**

0.500 0.699** 0.700 -0.621

0.520 0.311 ** 0.750 -0.646

0.530 -0.529 0.820 -0.500

0.550 0.080** 0.890 -0.184

0.560 0.581 ** 0.900 -0.183

0.580 -0.542 0.960 -0.117

0.590 0.919"*

0.600 0.890**

0.640 -0.684

0.700 -0.673

0.750 0.014"*

0.820 -0.571

0.870 0.001

0.930 -0.210

0.960 -0.202

Lower Surface

0.020 0.269 0.020 0.475 0.020 0.558 0.020 0.694

0.110 0.188 0.060 0.424 0.060 0.483 0.060 3.529"*

0.230 0.168 0.090 0.336 0.090 2.263** 0.110 0.418

0.400 0.114 0.120 -0.378** 0.120 0.335 0.250 0.219

0.490 0.142 0.200 0.170 0.200 0.191 0.400 0.18 l

0.630 1.740"* 0.260 0.281 0.250 0.269 0.490 0.145

0.750 0.162 0.400 0.186 0.400 0.160 0.580 0.109

0.850 0.163 0.490 0.170 0.490 0.061 0.650 0.250

0.900 0.223 0.580 0.177 0.580 0.186 0.750 0.393

0.960 0.074 0.640 0.322 0.650 0.007 0.830 0.491

0.750 0.360 0.750 0.081 0.900 0.534

0.870 0.438 0.890 0.467 0.960 0.335

0.930 0.298 0.930 0.370

0.960 0.202 0.960 -1.502**

CN = 0.788 0.998 0.919 0.960

623
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-49-10-500, MINF = 0.61 I, Camber = 9/14, ALPT = 12.02, BETA = 0.48, QINF = 301.9,

RNPU = 3.0E+06, CNWP = 0.5898

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.966 0,000 0.356 0.000 5.073"* 0.0 l0 - 1.995

0.060 - I. 119 0,020 - 1.839 0,020 -2.028 0.020 -2.008

0.110 -1,107 0.040 -1.686"* 0.060 -1.998'* 0.060 -1.811

0.200 -0.766 0.060 - 1.558 0,090 - 1.965 0.110 - 1.538

0.230 -0.717 0.090 -I .802 0.110 -1.930 0.140 -1,270

0,400 -0,525 0.130 - 1.516 0.130 - 1.918 0.190 -3.825"*

0,490 -0.501 0.150 - 1.965 0.150 - 1.529 0,250 -0.712

0.590 -0.604 0.200 - 1.509 0.210 - 1.357 0.400 -0,577

0.630 -0.668 0.250 1.825"* 0.250 - 1.036 0.490 -0.433

0.700 -0.809 0,260 -0.783 0.340 0.448** 0.580 -0.431

0,750 - 1.004 0,280 1.837** 0.370 - 1.613 ** 0,650 -0,443

0.810 -0,961 0,290 -0.119"* 0,400 -0.582 0.700 -0,441

0.840 - 1.078 0.310 1.294** 0.410 -0.037** 0.750 -0.506

0.900 -0.453 0,320 1.029** 0.430 -1.547** 0.800 -0.449

0.960 -0.451 0.340 1.183"* 0.440 - 1.118 * * 0.830 -0.364

0.350 -0.769** 0.460 -0.683** 0.900 -0.347

0.370 1.212"* 0.490 -0.558 0.960 -0.323

0.380 -0.858** 0,500 0.996"*

0.400 -0.596 0.520 - 1.731 **

0.410 1.219"* 0.540 0.582**

0.430 0,780** 0.550 0.734**

0.440 -0,582 0.580 -0.472

0.460 0,767** 0,600 0.744**

0.470 0.645"* 0.610 0.614"*

0,490 -0.581 0.650 4.072**

0.500 0.816* * 0.700 -0.614

0.520 0.406** 0,750 -0.692

0.530 -0,589 0.820 -0.532

0,550 0.126"* 0.890 -0.248

0,560 0.677 * * 0,900 -0.245

0.580 -0.582 0.960 -0.176

0.590 1.063"*

0.600 0.997**

0.640 -0.739

0.700 -0.736

0.750 0.031"*

0.820 -0.588

0.870 0.009

0.930 -0,232

0.960 -0.231

Lower Surface

0.020 0.337 0,020 0.525 0,020 0.608 0.020 0.715

0.110 0.230 0.060 0,492 0.060 0.541 0,060 3.922"*

0,230 0.170 0.090 0.389 0.090 2.535** 0.110 0.476

0.400 0.149 0.120 -0.359 ** 0.120 0.392 0.250 0.278

0.490 0,182 0.200 0,169 0.200 0.180 0.400 0.211

0,630 1.963"* 0.260 0.327 0,250 0,328 0,490 0.186

0,750 0.198 0.400 0,253 0.400 0.188 0.580 0.157

0.850 0.210 0.490 0.233 0.490 0.080 0.650 0.323

0.900 0.261 0.580 0,248 0,580 0.245 0,750 0,462

0.960 0.070 0.640 0.369 0.650 0.009 0,830 0.550

0,750 0,423 0.750 0.101 0,900 0.603

0.870 0,478 0.890 0.510 0.960 0,383

0.930 0.349 0.930 0.411

0.960 0,226 0,960 - 1.591 **

CN = 0,880 1.108 0,998 1.010

624
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-49-12-500, MINF = 0.606, Camber = 10/17, ALPT = 13.08, BETA = -0.91, QINF = 296.9,

RNPU = 3.0E+06, CNWP = 0.7796

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.007 0.000 0.218 0.000 5.158"* 0.0 lO -2.029

0.060 - 1.258 0.020 - 1.909 0.020 -2.069 0.020 -2.026

0.1 I0 -1.176 0.040 -1.715"* 0.060 -2.033** 0.060 -1.920

0,200 -0.948 0.060 - 1.662 0.090 -2.093 O. 110 - 1.544

0.230 -0.800 0.090 - 1.929 0.110 - 1.899 0.140 - 1.328

0.400 -0.587 0.130 - 1.542 0.130 - 1.356 0.190 -3.890 **

0.490 -0.569 0.150 - 1.648 0.150 - 1.383 0.250 -0.640

0.590 -0.657 0.200 - 1.573 0.210 - 1.264 0.400 -0.539

0.630 -0.722 0.250 1.854** 0.250 - 1.200 0.490 -0.427

0.700 -0.871 0.260 -1.111 0.340 0.470** 0.580 -0.442

0.750 -0.863 0.280 1.853"* 0.370 - 1.752"* 0.650 -0.435

0.810 -0.891 0.290 -0.180"* 0.400 -0.838 0.700 -0.433

0.840 -0.982 0.310 1.318** 0.410 -0.039** 0.750 -0.501

0.900 -0.555 0.320 1.045"* 0.430 -1.680** 0.800 -0.471

0.960 -0.553 0.340 1.209** 0.440 -1.272** 0.830 -0.450

0.350 -0.783** 0.460 -0.818"* 0.900 -0.423

0.370 1.239"* 0.490 -0.667 0.960 -0.384

0.380 -0.873** 0.500 1.017"*

0.400 -0.555 0.520 - 1.880**

0.410 1.238"* 0.540 0.591"*

0.430 0.792** 0.550 0.758**

0.440 -0.619 0.580 -0.548

0.460 0.779** 0.600 0.753**

0.470 0.654"* 0.610 0.637"*

0.490 -0.599 0.650 4.139**

0.500 0.826** 0.700 -0.673

0.520 0.398** 0.750 -0.678

0.530 -0.603 0.820 -0.577

0.550 0.122"* 0.890 -0.354

0.560 0.688** 0.900 -0.378

0.580 -0.600 0.960 -0.311

0.590 1.074**

0.600 0.998**

0.640 -0.696

0.700 -0.683

0.750 0.013"*

0.820 -0.472

0.870 -0.002

0.930 -0.282

0.960 -0.258

Lower Surface

0.020 0.370 0.020 0.554 0.020 0.650 0.020 0.720

0.110 0.276 0.060 0.526 0.060 0.575 0.060 3.987"*

0.230 0.142 0.090 0.421 0.090 2.577"* 0.110 0.524

0.400 0.177 0.120 -0.285** 0.120 0.431 0.250 0.317

0.490 0.200 0.200 0.142 0.200 0.169 0.400 0.258

0.630 1.985** 0.260 0.382 0.250 0.371 0.490 0.249

0.750 0.232 0.400 0.281 0.400 0.230 0.580 0.220

0.850 0.221 0.490 0.271 0.490 0.091 0.650 0.385

0.900 0.282 0.580 0.284 0.580 0.300 0.750 0.512

0.960 0.079 0.640 0.413 0.650 0.001 0.830 0.604

0.750 0.456 0.750 0.088 0.900 0.653

0.870 0.522 0.890 0.547 0.960 0.442

0.930 0.369 0.930 0.447

0.960 0.255 0.960 - 1.619"*

CN = 0.951 1.161 1.103 1.066

625
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-49-20-500, MINF = 0.581, Camber = 9/13, ALPT = 11.28, BETA = -0.59, QINF = 272.0,

RNPU = 2.9E+06, CNWP -- 0.5458

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.807 0.000 0.454 0.000 5.640"* 0.010 -1.876

0.060 -0.934 0.020 - 1.317 0.020 - 1.571 0.020 - 1.276

O. 110 - 1.036 0.040 - 1.863 ** 0.060 -2.209** 0.060 - 1.952

0.200 -0.720 0.060 - 1.513 0.090 - 1.924 0.110 - 1.476

0.230 -0.615 0.090 -1.485 0.110 -1.877 0.140 -1.151

0.400 -0.465 0.130 - 1.742 0.130 - 1.865 0.190 -4.237 **

0.490 -0.471 0.150 -2.024 0.150 - 1.238 0.250 -0.705

0.590 -0.601 0.200 - I. 161 0.210 -0.982 0.400 -0.564

0.630 -0.625 0.250 2.046** 0.250 -0.792 0.490 -0.457

0.700 -0.764 0.260 -0.780 0.340 0.523** 0.580 -0.489

0.750 -0.975 0.280 2.026** 0.370 - 1.755"* 0.650 -0.515

0.810 -0.932 0.290 -0.217** 0.400 -0.595 0.700 -0.513

0.840 -1.018 0.310 1.450"* 0,410 -0.033"* 0.750 -0.597

0.900 -0.391 0.320 1.149"* 0.430 - 1.675"* 0.800 -0.567

0.960 -0.360 0.340 1.329** 0.440 - 1.213"* 0.830 -0.382

0.350 -0.845"* 0.460 -0.717"* 0.900 -0.299

0.370 1.366** 0.490 -0.593 0.960 -0.274

0.380 -0.949** 0.500 1.119"*

0.400 -0.563 0.520 -1.873"*

0.410 1.367"* 0.540 0.662**

0.430 0.884** 0.550 0.834**

0.440 -0.561 0.580 -0.489

0.460 0.857** 0.600 0.829**

0.470 0.721 ** 0.610 0.704**

0.490 -0.556 0.650 4.528**

0.500 0.913" * 0.700 -0.676

0.520 0.445** 0.750 -0.714

0.530 -0.564 0.820 -0.549

0.550 0.137"* 0.890 -0.189

0.560 0.772** 0.900 -0.209

0.580 -0.559 0.960 -0.14 l

0.590 1.176"*

0.600 1.110"*

0.640 -0.712

0.700 -0.703

0.750 0.015"*

0.820 -0.563

0.870 -0.001

0.930 -0.208

0.960 -0.207

LowerSurf_e

0.020 0.249 0.020 0.440 0.020 0.566 0.020 0.674

0.110 0.211 0.060 0.444 0.060 0.512 0.060 4.362**

0.230 0.136 0.090 0.351 0.090 2.822"* 0.110 0.476

0.400 0.170 0.120 -0.465"* 0.120 0.351 0.250 0.246

0.490 0.122 0.200 0.133 0.200 0.163 0.400 0.195

0.630 2.177** 0.260 0.308 0.250 0.301 0.490 0.174

0.750 0.179 0.400 0.213 0.400 0.169 0.580 0.145

0.850 0.189 0.490 0.198 0.490 0.073 0.650 0.286

0.900 0.253 0.580 0.202 0.580 0.225 0.750 0.426

0.960 0.084 0.640 0.349 0.650 0.010 0.830 0.522

0.750 0.392 0.750 0.089 0.900 0.567

0.870 0.462 0.890 0.487 0.960 0.372

0.930 0.316 0.930 0.392

0.960 0.212 0.960 - 1.758"*

CN = 0.795 1.025 0.932 0.980

626
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-49-41-500, MINF = 0.595, Camber = 8/12, ALPT = t 1.16, BETA = -0.30, QINF = 286.1,

RNPU = 2.9E+06, CNWP = 0.5101

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.895 0.000 0.413 0.000 5.351 ** 0.010 - 1.925

0.060 -0.948 0.020 - 1.422 0.020 - 1.905 0.020 - 1.977

0.110 -1.068 0.040 -l.902"* 0,060 -2.111"* 0.060 -1.943

0.200 -0.707 0.060 - 1.579 0,090 - 1.916 0.110 - 1.476

0.230 -0.672 0.090 -1.693 0.110 -l.905 0.140 -1.152

0.400 -0.492 0.130 - 1.653 0.130 -2.044 0.190 -4.038"*

0.490 -0.473 0.150 - 1.858 0.150 - 1.408 0.250 -0.754

0.590 -0.569 0.200 -1.170 0.210 -0.978 0,400 -0.583

0.630 -0.629 0.250 1.923** 0.250 -0.778 0,490 -0,470

0.700 -0.757 0.260 -0.787 0.340 0.478** 0.580 -0.487

0.750 -0.970 0.280 1.906** 0.370 -1.655** 0.650 -0.500

0.810 -0.934 0.290 -0.222" * 0.400 -0.592 0.700 -0.509

0,840 - 1.009 0.310 1.354"* 0.410 -0.042** 0.750 -0.574

0,900 -0.385 0.320 1.063"* 0.430 -1.603** 0.800 -0.535

0.960 -0.345 0.340 1.246** 0.440 - 1.138"* 0.830 -0.379

0.350 -0.814"* 0.460 -0.671 ** 0.900 -0.314

0.370 1.284** 0.490 -0.582 0.960 -0.297

0.380 -0.913"* 0.500 1.044"*

0.400 -0.554 0.520 - 1.776"*

0.410 1.268"* 0.540 0.612"*

0,430 0.820"* 0.550 0.770"*

0,440 -0.557 0.580 -0.494

0.460 0,785'* 0.600 0.765"*

0.470 0.670** 0,610 0.644**

0.490 -0.568 0.650 4.294**

0.500 0,850** 0.700 -0.677

0.520 0.403** 0.750 -0.697

0.530 -0.569 0.820 -0.532

0.550 0.101 ** 0.890 -0.186

0.560 0.712"* 0.900 -0.203

0.580 -0.555 0.960 -0.133

0.590 1.094**

0,600 1.024**

0,640 -0.718

0.700 -0.710

0.750 0.004**

0.820 -0,566

0.870 0.000

0.930 -0.216

0.960 -0.211

Lower Surface

0,020 0.259 0.020 0.452 0.020 0.560 0.020 0.677

0. l 10 0.187 0.060 0.427 0.060 0.483 0.060 4.136"*

0.230 0.135 0.090 0.335 0.090 2.672"* 0.110 0.421

0.400 0.127 0.120 -0.449"* 0.120 0.332 0.250 0.223

0.490 0.152 0.200 0.139 0,200 0.158 0.400 0.175

0.630 2,039** 0.260 0,290 0.250 0.276 0.490 0.155

0.750 0.159 0.400 0.192 0.400 0.150 0.580 0.117

0.850 0.180 0.490 0.173 0.490 0.059 0.650 0.262

0.900 0.236 0.580 0.196 0.580 0.196 0.750 0.405

0.960 0.089 0.640 0.340 0.650 -0.00 l 0.830 0.510

0.750 0.371 0.750 0.074 0.900 0.556

0.870 0.424 0.890 0.483 0.960 0.343

0.930 0.294 0.930 0,384

0,960 0.191 0.960 - 1.682"*

CN = 0.799 1,014 0.919 0,984

627
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-50-6-500, MINF = 0.604, Camber = 8/13, ALPT = 11.15, BETA = -0,44, QINF = 292.2,

RNPU = 3.0E+O6, CNWP = 0.5446

T1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.907 0,000 0.426 0.000 5.272"* 0.010 - 1.888

0.060 -0.968 0,020 - 1.447 0.020 - 1.921 0.020 - 1.907

0,110 - 1.063 0.040 - 1.829"* 0.060 -2.034"* 0,060 - 1.820

0.200 -0.715 0.060 -1.528 0.090 -1.933 0.110 -1.568

0.230 -0.659 0.090 - 1.702 0. t 10 - 1.874 0.140 - 1.164

0.400 -0.479 0.130 - 1.639 0.130 -2,025 0.190 -3.921 **

0.490 -0.468 0.150 - 1.926 0.150 - 1.516 0.250 -0.735

0,590 -0.571 0.200 - 1.195 0.210 - 1.092 0,400 -0.581

0.630 -0.626 0.250 1.884** 0.250 -0.744 0.490 -0,480

0.700 -0,757 0.260 -0.767 0,340 0.479** 0.580 -0.469

0.750 -0,959 0.280 1,884** 0.370 - 1.617"* 0.650 -0.503

0.810 -0.940 0.290 -0.163"* 0.400 -0.607 0.700 -0.502

0,840 -1.015 0,310 1,347"* 0.410 -0.008** 0.750 -0,559

0.900 -0.397 0.320 1.068** 0.430 - 1.551 ** 0.800 -0,527

0,960 -0.356 0.340 1.237'* 0.440 - 1.121 ** 0.830 -0.390

0,350 -0,764** 0.460 -0.659** 0.900 -0.308

0,370 1.272"* 0,490 -0,575 0.960 -0.272

0.380 -0.880** 0.500 1.049**

0.400 -0,539 0.520 -1.735**

0,410 1.270"* 0.540 0.602"*

0.430 0.812"* 0.550 0.778**

0.440 -0.552 0.580 -0.484

0.460 0.799** 0.600 0.767**

0,470 0.692** 0.610 0.649**

0,490 -0.551 0,650 4,237**

0.500 0.852** 0.700 -0.663

0.520 0.454** 0.750 -0.698

0,530 -0,575 0.820 -0.516

0.550 0.126 ** 0.890 -0.185

0.560 0,707"* 0.900 -0.192

0.580 -0.574 0,960 -0.130

0.590 1,089"*

0.600 1.026"*

0.640 -0.712

0,700 -0.699

0.750 0,022**

0.820 -0.567

0.870 0.007

0.930 -0.224

0.960 -0.226

Lower Surface

0.020 0.271 0.020 0,478 0.020 0.566 0.020 0.694

0.110 0,204 0.060 0.440 0,060 0.505 0.060 4,082**

0,230 0.150 0.090 0,349 0.090 2.649 ** 0.110 0.451

0.400 0.128 0.120 -0.414"* 0.120 0.343 0,250 0,237

0.490 0.159 0,200 0,154 0.200 0.152 0.400 0.175

0.630 2.030** 0.260 0.301 0,250 0.288 0.490 0.170

0.750 0.178 0.400 0.209 0.400 0.165 0.580 0.132

0.850 O. 183 0,490 0.195 0.490 0,076 0.650 0.282

0.900 0,252 0.580 0.203 0.580 0.217 0.750 0,424

0.960 0.078 0.640 0,344 0.650 0.014 0,830 0.520

0.750 0.389 0.750 0.091 0,900 0.566

0,870 0.447 0.890 0.491 0.960 0.369

0,930 0.321 0.930 0,387

0,960 0.212 0.960 - 1.614* *

CN = 0.808 1.027 0.936 0.991

628
Table J-2. Continued.

Flight 228, Wing sweep = 26 °, Time = 12-50-15-000. MINF = 0.612, Camber = 8/t2, ALPT = 11.12, BETA = -0.56. QINF = 301.0,

RNPU = 3.0E+06, CNWP = 0.4970

rl = 0.93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x,/c CP x/c CP

0.020 -0.799 0.000 0.503 0.000 5.112"* 0.010 - 1.703

0.060 -0.870 0.020 - 1.339 0.020 - 1.354 0.020 - 1.815

O. 110 -0.934 0.040 - 1.781 ** 0.060 - 1.980** 0.060 - 1.689

0.200 -0.662 0.060 - 1.427 0.090 - 1,736 O. 110 - 1.488

0.230 -0.590 0.090 -1.520 0.110 -1.755 0.140 -1.118

0.400 -0.433 0.130 -1.514 0.130 -1.860 0.190 -3.812"*

0.490 -0.420 0.150 - 1.726 0.150 - 1.301 0.250 -0.69 l

0.590 -0.518 0.200 - 1.098 0.210 -0.908 0.400 -0.542

0.630 -0.575 0.250 1.832** 0.250 -0.728 0.490 -0.425

0.700 -0.692 0.260 -0.730 0.340 0.459** 0.580 -0.456

0.750 -0.902 0.280 1.824"* 0.370 - 1.560"* 0,650 -0.484

0.810 -0.861 0.290 -0.138"* 0.400 -0.573 0.700 -0.482

0.840 -0.932 0.310 1.299"* 0.410 -0.013"* 0.750 -0.563

0.900 -0.349 0.320 1.026"* 0.430 -1.496"* 0,800 -0.497

0.960 -0.288 0.340 1.196"* 0.440 -1.073** 0.830 -0.366

0.350 -0.748** 0.460 -0.629** 0.900 -0,264

0.370 1.222** 0.490 -0,556 0.960 -0.254

0.380 -0.860"* 0.500 1.004"*

0.400 -0.529 0.520 -1.673**

0.410 1.224"* 0.540 0.586**

0.430 0.789** 0.550 0.743**

0.440 -0.526 0.580 -0.475

0.460 0.764** 0.600 0.739**

0.470 0.641 ** 0.610 0.624**

0.490 -0.524 0.650 4.107"*

0.500 0.811"* 0.700 -0.642

0.520 0.389** 0.750 -0.669

0.530 -0.532 0.820 -0.511

0.550 0.108"* 0.890 -0.157

0.560 0.687"* 0.900 -0.165

0.580 -0,530 0.960 -0.108

0.590 1.060**

0.600 0.995**

0.640 -0.684

0.700 -0.670

0.750 0.012"*

0.820 -0.548

0.870 -0,002

0.930 -0.193

0.960 -0.196

Lower Surface

0.020 0.227 0.020 0.438 0.020 0.513 0.020 0.662

0.110 0.173 0.060 0.407 0.060 0.458 0.060 3.957**

0.230 0.151 0.090 0,313 0,090 2.566"* 0.110 0.402

0.400 0.118 0.120 -0.436** 0.120 0.293 0.250 0.204

0.490 0.134 0.200 0.154 0.200 0.173 0.400 0.156

0.630 1.965"* 0.260 0.265 0.250 0.252 0.490 0.137

0,750 0.167 0.400 0.179 0.400 0.135 0.580 0.103

0.850 0.172 0,490 0.162 0.490 0.061 0.650 0.238

0.900 0.244 0,580 0.169 0.580 0.183 0.750 0.387

0.960 0,091 0.640 0.317 0.650 0.011 0.830 0.486

0.750 0.364 0,750 0.086 0900 0.526

0.870 0.428 0.890 0.464 0.960 0.341

0.930 0.302 0.930 0.367

0.960 0.193 0.960 -1.572"*

CN = 0.732 0.954 0.862 0.918

629
Table J-2. Continued.

Flight 228, Wing sweep = 26", Time = 12-50-17-000, MINF = 0.622, Camber = 5/7, ALPT = 7.05, BETA = 1.03, QINF = 310.6,

RNPU = 3. IE+06, CNWP = 0.3478

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.279 0.000 0.799 0.000 4.952"* 0.010 - 1.617

0.060 -0.429 0.020 -0.624 0.020 -0.816 0.020 -0.891

0.110 -0.529 0.040 - 1.332"* 0.060 - 1.921 * * 0.060 - 1.089

0.200 -0.407 0.060 -0.767 0.090 -0.875 0.110 - 1.007

0.230 -0.389 0.090 -0.744 0. t 10 -0.939 0.140 -0.832

0.400 -0.296 0.130 -0.850 0.130 -0.936 0.190 -3.696"*

0.490 -0.309 0.150 -0.866 0.150 -0.799 0.250 -0.551

0.590 -0.348 0.200 -0.694 0.210 -0.687 0.400 -0.489

0.630 -0.384 0.250 1.773** 0.250 -0.567 0.490 -0.388

0.700 -0.439 0.260 -0.535 0.340 0.431 ** 0.580 -0.393

0.750 -0.549 0.280 1.760"* 0.370 -1.380** 0.650 -0.467

0.810 -0.498 0.290 -0.090** 0.400 -0.434 0.700 -0.445

0.840 -0.533 0.310 1.254"* 0.410 -0.015"* 0.750 -0.533

0.900 -0.318 0.320 0.989** 0.430 - 1.334"* 0.800 -0.472

0.960 -0.131 0.340 1.147"* 0.440 -0.918"* 0.830 -0.483

0.350 -0.727"* 0.460 -0.480** 0.900 -0.153

0.370 1.180** 0.490 -0.458 0.960 -0.046

0.380 -0.860** 0.500 0.964**

0.400 -0.443 0.520 - 1.500"*

0.410 1.178"* 0.540 0.570**

0.430 0.752"* 0.550 0.710"*

0.440 -0.408 0.580 -0.383

0.460 0.743'* 0.600 0.711 **

0.470 0.607** 0.610 0.600**

0.490 -0.417 0.650 3.978"*

0.500 0.786** 0.700 -0.570

0.520 0.364** 0.750 -0.577

0.530 -0.419 0.820 -0.544

0.550 0.100'* 0.890 -0.187

0.560 0.656 ** 0.900 -0.146

0.580 -0.423 0.960 -0.002

0.590 0.995**

0.600 0.950**

0.640 -0.552

0.700 -0.527

0.750 -0.021 **

0.820 -0.567

0.870 -0.032

0,930 -0.184

0.960 -0.106

Lower Surface

0.020 -0.061 0.020 0.059 0.020 0.230 0.020 0.455

0.110 0.014 0.060 0.181 0.060 0.259 0.060 3.833**

0.230 0.082 0.090 0.122 0.090 2.485"* 0.110 0.195

0.400 0.028 0.120 -0.599** 0.120 0.086 0.250 0.023

0.490 0.051 0.200 0.082 0.200 0.100 0.400 0.010

0.630 1.891 ** 0.260 0.095 0.250 0.074 0.490 -0.011

0.750 0.097 0.400 0.043 0,400 0.006 0.580 -0.035

0.850 0.121 0.490 0.029 0.490 0.001 0.650 0.098

0.900 0.208 0.580 0.036 0.580 0.036 0.750 0.272

0.960 0.131 0.640 0.195 0.650 -0.026 0.830 0.393

0.750 0.279 0.750 0.023 0.900 0.44 1

0.870 0.367 0.890 0.385 0.960 0.316

0.930 0.249 0.930 0.294

0.960 0.183 0.960 - 1.525 **

CN = 0.439 0.628 0.570 0.641

630
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-23-15-500, MINF = 0.695, Camber = 2/4, ALPT = 5.30, BETA = 0.40, QINF = 294.8,

RNPU = 2.7E+06, CNWP = 0.2553

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.170 0.000 0.837 0.000 4.873** 0.010 - 1.275

0.060 -0.175 0.020 -0.522 0.020 -0.647 0.020 -0.644

0.110 -0.150 0.040 -0.411 0.060 -2.723"* 0.060 -0.717

0.200 -0.275 0.060 -0.500 0.090 -0.536 0.110 -0.641

0.230 -0.232 0.090 -0.440 0.110 -0.605 0.140 -0.642

0.400 -0.213 0.130 -0.461 0.130 -0.603 0.190 -2.959* *

0.490 -0.214 0.150 -0.506 0.150 -0.555 0.250 -0.448

0.590 -0.280 0.200 -0.418 0.210 -0.530 0.400 -0.375

0.630 -0.27 l 0.250 -0.397 0.250 -0.384 0.490 -0.332

0.700 -0.301 0.260 -0.358 0.340 -0.418 0.580 -0.314

0.750 -0.367 0.280 -0.381 0.370 -0.407 0.650 -0.438

0.810 -0.326 0.290 -0.372 0.400 -0.391 0.700 -0.412

0.840 -0.320 0.310 -0.362 0.410 -0.743** 0.750 -0.437

0.900 -0.189 0.320 -0.354 0.430 -0.405 0.800 -0.471 **

0.960 -0.053 0.340 -0.354 0.440 -0.376 0.830 -0.445

0.350 -0.216"* 0.460 -0.380 0.900 -0.226

0.370 -0.306 0.490 -0.306 0.960 -0.012

0.380 -0.352 0.500 -0.397

0.400 -0.271 0.520 -0.368

0.410 -0.355 0.540 -0.378

0.430 -0.317 0.550 -0.325

0.440 -0.276 0.580 -0.317

0.460 -0.335 0.600 -0.391

0.470 -0.334 0.610 -0.392

0.490 -0.316 0.650 3.479**

0.500 -0.352 0.700 -0.460

0.520 -0.317 0.750 -0.500

0.530 -0.317 0.820 -0.456"*

0.550 -0.367 0.890 -0.190

0.560 -0.355 0.900 -0.127

0.580 -0.327 0.960 0.013

0.590 -0.388

0.600 -0.367

0.640 -0.421

0.700 -0.437

0.750 -0.020"*

0.820 -0.398

0.870 -0.320

0.930 -0.149

0.960 -0.068

Lower Surface

0.020 -0.232 0.020 -0.068 0.020 0.076 0.020 0.399

0.110 -0.125 0.060 0.015 0.060 0.075 0.060 3.185"*

0.230 -0.071 0.090 -0.025 0.090 1.193" * 0.110 0.013

0.400 -0.019 0.120 -0.034 0.120 -0.173 0.250 -0.130

0.490 0.016 0.200 -0.056 0.200 -0.042 0.400 -0.109

0.630 1.966"* 0.260 -0.070 0.250 -0.072 0.490 -0.141

0.750 0.060 0.400 -0.058 0.400 -0.092 0.580 -0.161

0.850 0.136 0.490 -0.073 0.490 -0.014 0.650 -0.011

0.900 0.219 0.580 -0.047 0.580 -0.052 0.750 0.180

0.960 0.163 0.640 0.125 0.650 -0.036 0.830 0.351

0.750 0.240 0.750 -0.011 0.900 0.378

0.870 0.301 0.890 0.331 0.960 0.283

0.930 0.247 0.930 0.279

0.960 0.181 0.960 -0.832**

CN = 0.241 0.414 0.378 0.433

631
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-23-23-000, MINF = 0.696, Camber = 2/4, ALPT = 5.09, BETA = 0.43, QINF = 295.9,

RNPU = 2.7E+06, CNWP = 0.2613

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.146 0.000 0.846 0.000 4.853"* 0.010 - 1.186

0.060 -0.233 0.020 -0.483 0.020 -0.605 0.020 -0.658

0.110 -0.255 0.040 -0.385 0.060 -2.714"* 0.060 -0.715

0.200 -0.260 0.060 -0.484 0.090 -0.514 0.110 -0.620

0.230 -0.213 0.090 -0.422 0.110 -0.586 0.140 -0.605

0.400 -0.213 O. 130 -0.462 O. 130 -0.590 O. 190 -2.949**

0.490 -0.206 O. 150 -0.493 O. 150 -0.529 0.250 -0.419

0.590 -0.268 0.200 -0.400 0.2 lO -0.535 0.400 -0.375

0.630 -0.264 0.250 -0.375 0.250 -0.383 0.490 -0.322

0.700 -0.293 0.260 -0.351 0.340 -0.410 0.580 -0.315

0.750 -0.359 0.280 -0,381 0.370 -0.399 0.650 -0.427

0.810 -0.315 0.290 -0.363 0.400 -0.360 0.700 -0.412

0.840 -0.316 0.310 -0.352 0.410 -0.741 ** 0.750 -0.436

0.900 -0.177 0.320 -0.349 0.430 -0.389 0.800 -0.471 **

0.960 -0.047 0.340 -0.347 0.440 -0.355 0.830 -0.435

0.350 -0.2t6"* 0.460 -0.375 0.900 -0.236

0.370 -0.306 0.490 -0.306 0.960 -0.021

0.380 -0.362 0.500 -0.387

0.400 -0.271 0.520 -0.368

0.410 -0.348 0.540 -0.364

0.430 -0.317 0.550 -0.325

0.440 -0.289 0.580 -0.299

0.460 -0.320 0.600 -0.384

0.470 -0.334 0.610 -0,378

0.490 -0.316 0.650 3.464**

0.500 -0.330 0.700 -0.452

0.520 -0.341 0.750 -0.485

0.530 -0.313 0. 820 -0.462 **

0.550 -0.367 0.890 -0.186

0.560 -0.348 0.900 -0.128

0.580 -0.327 0.960 0.008

0.590 -0.410

0.600 -0.362

0.640 -0.414

0.700 -0.429

0.750 -0.021 **

0.820 -0.394

0,870 -0.316

0.930 -0.150

0.960 -0.065

Lower Surface

0.020 -0.271 0.020 -0.108 0.020 0.044 0.020 0.374

0.110 -0.139 0.060 0.002 0.060 0.166 0.060 3.171 **

0.230 -0.076 0.090 -0.035 0.090 1.187** 0.110 0.033

0.400 -0.024 0.120 -0.043 0.120 -0.183 0.250 -0.138

0.490 -0.008 0.200 -0.068 0.200 -0.030 0.400 -0.121

0.630 1.957** 0.260 -0.078 0.250 -0.080 0.490 -0.149

0.750 0.047 0.400 -0.063 0.400 -0.103 0.580 -0.157

0.850 0.134 0.490 -0.078 0.490 -0.016 0.650 -0.016

0.900 0.217 0.580 -0.052 0.580 -0.071 0.750 0.179

0.960 0.165 0.640 0.127 0.650 -0.037 0.830 0.348

0.750 0.237 0.750 -0.015 0.900 0.372

0.870 0.308 0.890 0.328 0.960 0.286

0.930 0.249 0.930 0.277

0.960 0.183 0.960 -0.830"*

CN= 0.234 0.403 0.370 0.424

632
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-23-23-500, MINF = 0.696, Camber = 1/4, ALPT = 4.60, BETA = 0.40, QINF = 296.2,

RNPU = 2.7E+06, CNWP = 0.2330

_1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.049 0.000 0.841 0.000 4.849"* 0.010 -0.974

0.060 -0.156 0.020 -0.348 0.020 -0.467 0.020 -0.604

0. 110 -0.243 0.040 -0.296 0.060 -2.712** 0.060 -0.630

0.200 -0.249 0.060 -0.389 0.090 -0.471 0. l l0 -0.560

0.230 -0.213 0.090 -0.352 0.110 -0.530 0.140 -0.550

0.400 -0.190 0.130 -0.406 0. t 30 -0.518 0.190 -2.947"*

0.490 -0.203 0.150 -0.439 0.150 -0.501 0.250 -0.39 l

0.590 -0.311 0.200 -0.360 0.210 -0.487 0.400 -0.368

0.630 -0.256 0.250 -0.364 0.250 -0.339 0.490 -0.312

0.700 -0.282 0.260 -0.316 0.340 -0.380 0.580 -0.25 l

0.750 -0.351 0.280 -0.345 0.370 -0.375 0.650 -0.43 I

0.810 -0.300 0.290 -0.332 0.400 -0.353 0.700 -0.391

0.840 -0.304 0.310 -0.329 0.410 -0.741 ** 0.750 -0.429

0.900 -0.172 0.320 -0.326 0.430 -0.373 0.800 -0.470"*

0.960 -0.033 0.340 -0.326 0.440 -0.344 0.830 -0.435

0.350 -0.205"* 0.460 -0.363 0.900 -0.236

0.370 -0.284 0.490 -0.268 0.960 -0.021

0.380 -0.338 0.500 -0.368

0.400 -0.259 0.520 -0.350

0.410 -0.328 0.540 -0.350

0.430 -0.299 0.550 -0.300

0.440 -0.264 0.580 -0.299

0.460 -0.325 0.600 -0.372

0.470 -0.327 0.610 -0.364

0.490 -0.299 0.650 3.462"*

0.500 -0.307 0.700 -0.466

0.520 -0.317 0.750 -0.480

0.530 -0.299 0.820 -0.457**

0.550 -0.348 0.890 -0.186

0.560 -0.342 0.900 -0.128

0.580 -0.313 0.960 0.008

0.590 -0.365

0.600 -0.322

0.640 -0.401

0.700 -0.432

0.750 -0.018"*

0.820 -0.386

0.870 -0.320

0.930 -0.146

0.960 -0.065

Lower Surface

0.020 -0.339 0.020 -0.214 0.020 -0.035 0.020 0.303

0.110 -0.165 0.060 -0.040 0.060 0.047 0.060 3.169 **

0.230 -0.091 0.090 -0.082 0.090 1.186"* 0.110 0.012

0.400 -0.028 0.120 -0.072 0.120 -0.232 0.250 -0.164

0.490 0.007 0.200 -0.094 0.200 -0.098 0.400 -0.136

0.630 1.955"* 0.260 -0.100 0.250 -0.102 0.490 -0.164

0.750 0.059 0.400 -0.078 0.400 -0.127 0.580 -0.167

0.850 0.142 0.490 -0.089 0.490 -0.016 0.650 -0.016

0.900 0.223 0.580 -0.075 0.580 -0.082 0.750 0.154

0.960 0.174 0.640 0. l 16 0.650 -0.037 0.830 0.348

0.750 0.237 0.750 -0.015 0.900 0.375

0.870 0.308 0.890 0.328 0.960 0.286

0.930 0.252 0.930 0.277

0.960 0.186 0.960 -0.829**

CN = 0.223 0.365 0.330 0.388

633
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-23-26-000, MINF = 0.699, Camber = 1/3, ALPT = 3.14, BETA = 0.45, Q1NF = 299.2,

RNPU = 2.7E+06, CNWP = 0.1724

1"1-- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.139 0.000 0.733 0.000 4.795" * 0.010 -0.529

0.060 0.000 0.020 -0.061 0.020 -0.100 0.020 -0.321

0.110 -0.108 0.040 -0.064 0.060 -2.689" * 0.060 -0.409

0.200 -0.139 0.060 -0.173 0.090 -0.242 0.110 -0.338

0.230 -0.068 0.090 -0.169 0.110 -0.311 0.140 -0.354

0.400 -0.133 0.130 -0.201 0.130 -0.310 0.190 -2.922**

0.490 -0.147 0.150 -0.268 0.150 -0.309 0.250 -0.28 l

0.590 -0.208 0.200 -0.202 0.210 -0.344 0.400 -0.270

0.630 -0.193 0.250 -0.238 0.250 -0.238 0.490 -0.258

0.700 -0.219 0.260 -0.208 0.340 -0.305 0.580 -0.243

0.750 -0.251 0,280 -0.234 0.370 -0.297 0.650 -0.336

0.810 -0.238 0.290 -0.225 0.400 -0.347 0.700 -0.334

0.840 -0.209 0.310 -0.240 0.410 -0.738** 0.750 -0.338

0.900 -0.102 0.320 -0.230 0.430 -0.299 0.800 -0.401 **

0.960 -0.017 0.340 -0.229 0.440 -0.278 0.830 -0.335

0.350 -0.203** 0.460 -0.276 0.900 -0.235

0.370 -0.209 0.490 -0.202 0.960 -0.018

0.380 -0.248 0.500 -0.304

0.400 -0.163 0.520 -0.276

0.410 -0.257 0.540 -0.298

0.430 -0.229 0.550 -0.228

0.440 -0.207 0.580 -0.228

0.460 -0.229 0.600 -0.289

0.470 -0.225 0.610 -0.292

0.490 -0.226 0.650 3.422**

0.500 -0.167 0.700 -0.353

0.520 -0.241 0.750 -0.392

0.530 -0.222 0.820 -0.340**

0.550 -0.259 0.890 -0.1 64

0.560 -0.277 0.900 -0.100

0.580 -0.235 0.960 0.010

0.590 -0.295

0.600 -0.265

0.640 -0.317

0.700 -0.308

0.750 -0.037**

0.820 -0.263

0.870 -0.245

0.930 -0.106

0.960 -0.033

Lower Surface

0.020 -0.567 0.020 -0.512 0.020 -0.305 0.020 0.046

0.110 -0.277 0.060 -0.217 0.060 -0.143 0.060 3.132 **

0.230 -0.186 0.090 -0.236 0.090 1.169 ** 0.110 -0.135

0.400 -0.074 0.120 -0.193 0.120 -0.357 0.250 -0.281

0.490 -0.050 0.200 -0.149 0.200 -0.225 0.400 -0.209

0.630 1.930"* 0.260 -0.213 0.250 -0.209 0.490 -0.242

0.750 0.045 0.400 -0.143 0.400 -0.186 0.580 -0.225

0.850 0.135 0.490 -0.161 0.490 -0.032 0.650 -0.080

0.900 0.221 0.580 -0.129 0.580 -0.141 0.750 0.124

0.960 0.183 0.640 0.042 0.650 -0.057 0.830 0.305

0.750 0.192 0.750 -0.035 0.900 0.315

0.870 0.272 0.890 0.283 0.960 0.258

0.930 0.222 0.930 0.247

0.960 0.168 0.960 -0.826"*

CN = 0.092 0.183 0.180 0.216

634
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-23-30-500, MINF = 0.713, Camber = 0/3, ALPT = 3.72, BETA = 0.54, QINF = 315.6,

RNPU = 2.8E+06, CNWP = 0.1549

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP .r./c CP x/c CP

0.020 0.060 0.000 0.806 0.000 4.508"* 0.010 -0.819

0.060 -0.010 0.020 -0.197 0.020 -0.287 0.020 -0.453

0.110 -0.243 0.040 -0.175 0.060 -2.587' * 0.060 -0.447

0.200 -0.177 0.060 -0.277 0.090 -0.313 0.110 -0.423

0.230 -0,162 0.090 -0,230 0.110 -0.391 0.140 -0.447

0.400 -0.157 0.130 -0.265 0.130 -0.388 0.190 -2.808 **

0,490 -0.159 0.150 -0.315 0.150 -0,399 0.250 -0.329

0.590 -0.229 0.200 -0,255 0.210 -0,393 0.400 -0.306

0.630 -0.211 0.250 -0.272 0.250 -0.277 0.490 -0.272

0.700 -0.222 0.260 -0.253 0.340 -0.328 0.580 -0.260

0.750 -0.263 0.280 -0.269 0.370 -0.329 0.650 -0.367

0.810 -0.235 0.290 -0.273 0.400 -0.275 0.700 -0.342

0.840 -0.229 0.310 -0.269 0.410 -0.738** 0,750 -0.358

0.900 -0.131 0.320 -0.266 0,430 -0.322 0,800 -0.390**

0.960 -0,008 0.340 -0.269 0.440 -0.294 0.830 -0.345

0.350 -0.217"* 0.460 -0.303 0.900 -0.227

0.370 -0.232 0.490 -0.230 0.960 -0.019

0.380 -0.284 0.500 -0.315

0.400 -0.196 0.520 -0.295

0.410 -0.273 0.540 -0.319

0.430 -0.235 0,550 -0.261

0.440 -0.203 0.580 -0,245

0.460 -0.261 0.600 -0.318

0.470 -0.266 0.610 -0.318

0.490 -0.254 0.650 3.206**

0,500 -0.257 0.700 -0.375

0.520 -0.253 0.750 -0.399

0.530 -0.261 0.820 -0.360"*

0.550 -0.290 0,890 -0.159

0.560 -0.294 0.900 -0.110

0.580 -0.277 0.960 0.017

0.590 -0.315

0.600 -0.298

0.640 -0.331

0.700 -0.333

0,750 -0.031 **

0.820 -0.273

0.87O -0,266

0.930 -0.110

0.960 -0.037

Lower Surface

0.020 -0.539 0.020 -0.372 0.020 -0. 180 0.020 0.167

0.110 -0.239 0.060 -0.159 0.060 -0.046 0.060 2.931 **

0,230 -0.176 0,090 -0.180 0,090 1.071"* 0.110 -0.042

0.400 -0.069 0.120 -0.165 0.120 -0.308 0.250 -0,244

0.490 -0.043 0,200 -0.109 0.200 -0.177 0.400 -0.194

0.630 1.793"* 0.260 -0.198 0.250 -0.194 0.490 -0.225

0.750 0.052 0.400 -0. 134 0.400 -0.186 0.580 -0.242

0.850 0.122 0.490 -0.145 0.490 -0.036 0.650 -0.086

0.900 0.202 0.580 -0.118 0.580 -0.147 0.750 0.126

0.960 0.176 0.640 0.062 0.650 -0.091 0.830 0.304

0.750 0.184 0.750 -0.026 0.900 0.331

0,870 0.283 0.890 0.293 0.960 0.25 I

0,930 0.222 0.930 0.231

0.960 0,170 0.960 -0,820"*

CN = 0,129 0.232 0,215 0.271

635
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-23-33-000, MINF = 0.724, Camber = 1/4, ALPT = 6.08, BETA = 0.51, QINF = 328.8,

RNPU = 29E+06, CNWP = 0.2425

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.363 0.000 0.830 0.000 4.296** 0,010 - 1.212

0.060 -0.322 0.020 -0.859 0.020 -0.813 0,020 - 1.287

O. I 10 -0.348 0.040 -0.580 0.060 -2.515 * * 0.060 - 1.142

0.200 -0.308 0,060 -0.654 0,090 -0.607 0.110 -0.617

0.230 -0.268 0.090 -0,545 0.1 I0 -0.701 0.140 -0.748

0.400 -0.232 0.130 -0.569 0.130 -0,712 0.190 -2.726**

0,490 -0.225 0.150 -0.580 0.150 -0,619 0.250 -0.472

0.590 -0.314 0.200 -0.482 0.210 -0.617 0.400 -0.406

0.630 -0.275 0.250 -0.448 0.250 -0.444 0,490 -0.342

0.700 -0.298 0.260 -0.396 0.340 -0.444 0.580 -0.333

0.750 -0.365 0.280 -0.415 0.370 -0.437 0.650 -0.455

0.810 -0.335 0.290 -0,412 0.400 -0.404 0.700 -0.420

0.840 -0.321 0.310 -0.391 0.410 -0.739** 0.750 -0.445

0.900 -0.184 0.320 -0.383 0.430 -0.418 0,800 -0.432"*

0.960 -0.061 0.340 -0.379 0.440 -0.387 0.830 -0.425

0.350 -0.197** 0.460 -0.398 0.900 -0.196

0.370 -0.338 0.490 -0,316 0.960 0.003

0.380 -0.393 0.500 -0.392

0.400 -0.296 0.520 -0.385

0.410 -0.373 0.540 -0.382

0.430 -0.341 0.550 -0.341

0.440 -0.303 0.580 -0.357

0.460 -0.361 0.600 -0.406

0.470 -0,358 0.610 -0.408

0.490 -0.331 0.650 3.046"*

0.500 -0.334 0.700 -0,479

0.520 -0.342 0.750 -0.489

0.530 -0.330 0.820 -0.467**

0.550 -0.372 0.890 -0.171

0.560 -0.381 0.900 -0.126

0.580 -0.355 0.960 0.031

0.590 -0.403

0.600 -0.386

0.640 -0.432

0.700 -0.435

0.750 -0.005"*

0.820 -0.392

0.870 -0.310

0.930 -0.134

0.960 -0.054

LowerSurf_e

0.020 -0.130 0.020 0.105 0.020 0.175 0.020 0.466

0.110 -0.106 0.060 0.092 0.060 0.187 0.060 2.782" *

0.230 -0.064 0.090 0.029 0.090 0.996** 0.110 0.083

0.400 -0.007 0.120 0.022 0.120 -0.110 0.250 -0.086

0.490 0.014 0.200 -0.020 0.200 -0.004 0.400 -0.088

0.630 1.689** 0.260 -0.043 0.250 -0.038 0.490 -0.140

0.750 0.061 0.400 -0.038 0.400 -0.076 0.580 -0.138

0.850 0.132 0.490 -0.055 0.490 -0.020 0.650 0.000

0.900 0.216 0.580 -0.039 0.580 -0.060 0.750 0,194

0.960 0.168 0.640 0.119 0.650 -0.053 0.830 0.363

0.750 0.248 0.750 -0.020 0.900 0.389

0.870 0.319 0.890 0.329 0.960 0.284

0.930 0.261 0.930 0.278

0.960 0.202 0.960 -0.819**

CN = 0.280 0.472 0.415 0.510

636
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-23-34-000, MINF = 0.726, Camber = 2/5, ALPT = 7.32, BETA = 0.37, QINF = 332.3,

RNPU = 2.9E+06, CNWP = 0.3374

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 -0.640 0.000 0.763 0.000 4.238** 0.010 -1.299

0.060 -0.482 0.020 - 1.229 0.020 - 1.257 0.020 - 1.391

0.110 -0.497 0.040 -0.947 0.060 -2.500** 0.060 - 1.327

0.200 -0.416 0.060 -0.898 0.090 - 1.141 0.110 - 1.247

0.230 -0.368 0.090 -0.720 0.110 - 1.188 0.140 - 1.096

0.400 -0.270 0.130 -0.802 0.130 -1.176 0.190 -2.710"*

0.490 -0.252 0.150 -0.881 0.150 -0.669 0.250 -0.503

0.590 -0.332 0.200 -0.635 0.210 -0.643 0.400 -0.432

0.630 -0.345 0.250 -0.532 0.250 -0.523 0.490 -0.380

0.700 -0.376 0.260 -0.496 0.340 -0.507 0.580 -0.343

0.750 -0.474 0.280 -0.504 0.370 -0.503 0.650 -0.468

0.810 -0.401 0.290 -0.488 0.400 -0.452 0.700 -0.457

0.840 -0.438 0.310 -0.462 0.410 -0.744"* 0.750 -0.485

0.900 -0.254 0.320 -0.457 0.430 -0.487 0.800 -0.455"*

0.960 -0.110 0.340 -0.447 0.440 -0.444 0.830 -0.445

0.350 -0.219** 0.460 -0.460 0.900 -0.161

0.370 -0.409 0.490 -0.400 0.960 -0.033

0.380 -0.454 0.500 -0.455

0.400 -0.378 0.520 -0.412

0.410 -0.428 0.540 -0.438

0.430 -0.385 0.550 -0.392

0.440 -0.353 0.580 -0.339

0.460 -0.394 0.600 -0.440

0.470 -0.422 0.610 -0.449

0.490 -0.385 0.650 3.001 **

0.500 -0.403 0.700 -0.506

0.520 -0.394 0.750 -0.553

0.530 -0.379 0.820 -0.518"*

0.550 -0.44 1 0.890 -0.179

0.560 -0.423 0.900 -0.120

0.580 -0.390 0.960 0.020

0.590 -0.453

0.600 -0.430

0.640 -0.505

0.700 -0.516

0.750 -0.004**

0.820 -0.475

0.870 -0.349

0.930 -0.152

0.960 -0.076

Lower Surface

0.020 0.007 0.020 0.276 0.020 0.314 0.020 0.571

0.110 -0.031 0.060 0.200 0.060 0.264 0.060 2.740**

0.230 0.015 0.090 0.127 0.090 0.973** 0.110 0.178

0.400 0.034 0.120 0.082 0. 120 0.006 0.250 -0.024

0.490 0.041 0.200 0.017 0.200 0.080 0.400 -0.030

0.630 1.659** 0.260 0.027 0.250 0.036 0.490 -0.084

0.750 0.074 0.400 0.000 0.400 -0.029 0.580 -0.095

0.850 0.155 0.490 -0.023 0.490 -0.012 0.650 0.035

0.900 0.214 0.580 -0.004 0.580 -0.019 0.750 0.228

0.960 0.165 0.640 0.186 0.650 -0.031 0.830 0.392

0.750 0.278 0.750 0.008 0.900 0.407

0.870 0.341 0.890 0.376 0.960 0.295

0.930 0.272 0.930 0.302

0.960 0.211 0.960 -0.823**

CN = 0.389 0.615 0.555 0.633

637
Table J-2. Continued,

Flight 223, Wing sweep = 26 °, Time = 10-23-36-000, MINF = 0,725, Camber = 4/7, ALPT = 9.06, BETA = 0.40, QINF = 333.5,

RNPU = 2.9E+06, CNWP = 0.4253

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.130 0.000 0.660 0.000 4.206** 0.010 - 1.497

0.060 -0,694 0.020 - 1.406 0,020 - 1.367 0.020 - 1.551

0.110 -0.649 0,040 - 1.070 0,060 -2,508"* 0.060 - 1.474

0.200 -0.528 0,060 - 1.165 0,090 - 1.367 0.110 - 1.563

0.230 -0,460 0.090 - 1.145 0.110 - 1.431 0.140 - 1.694

0.400 -0,361 0,130 -1.293 0.130 -1.478 0.190 -2,717"*

0,490 -0.337 0.150 - 1.387 0.150 - 1.483 0.250 -0.941

0,590 -0.422 0.200 - 1.371 0.210 - 1.506 0,400 -0.458

0.630 -0.431 0.250 -0.815 0.250 -0.902 0.490 -0.402

0.700 -0.510 0.260 -0,666 0.340 -0,509 0.580 -0,371

0.750 -0.680 0.280 -0,580 0.370 -0.465 0.650 -0,480

0.810 -0.622 0,290 -0.474 0.400 -0.435 0,700 -0.461

0.840 -0.653 0.310 -0.432 0.410 -0.758** 0.750 -0.473

0.900 -0.359 0.320 -0,421 0.430 -0,476 0,800 -0.455**

0,960 -0.176 0.340 -0.416 0,440 -0.469 0,830 -0.415

0,350 -0.167"* 0.460 -0.472 0,900 -0.181

0.370 -0.389 0.490 -0.410 0.960 -0.069

0,380 -0,463 0,500 -0,476

0.400 -0.393 0,520 -0.464

0.410 -0.456 0.540 -0,475

0,430 -0.429 0,550 -0.431

0.440 -0.395 0.580 -0.347

0.460 -0.445 0,600 -0,504

0,470 -0.438 0.610 -0,497

0.490 -0.432 0,650 2,974**

0.500 -0.454 0.700 -0.554

0,520 -0,447 0.750 -0.618

0,530 -0.435 0.820 -0.558**

0.550 -0.477 0.890 -0.146

0.560 -0.482 0,900 -0.103

0,580 -0.456 0.960 -0,018

0.590 -0.503

0.600 -0.502

0,640 -0,593

0.700 -0.619

0,750 0,003**

0,820 -0,485

0.870 -0.351

0.930 -0.258

0.960 -0.211

Lower Surface

0,020 0.134 0.020 0,439 0,020 0.419 0.020 0.616

0.110 0.064 0.060 0.313 0.060 0,382 0.060 2.714"*

0,230 0.140 0.090 0,228 0.090 0.953 ** 0.110 0,273

0,400 0,066 0.120 0.197 0.120 0.090 0.250 0.070

0.490 0,074 0,200 0.151 0,200 0.127 0.400 0.042

0,630 1.636** 0,260 0.121 0.250 0.134 0,490 0,003

0.750 0.104 0.400 0.080 0.400 0.051 0.580 -0.014

0.850 0.160 0,490 0.051 0.490 0.004 0.650 0.118

0.900 0.232 0.580 0.067 0.580 0,063 0,750 0.297

0.960 0.135 0.640 0.242 0.650 -0.011 0.830 0.424

0.750 0.311 0,750 0.037 0,900 0.461

0.870 0,384 0.890 0.413 0.960 0.317

0.930 0.291 0,930 0.344

0.960 0.203 0,960 -0,836**

CN = 0.555 0,829 0.748 0,837

638
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 10-23-39-500, MINF = 0.700, Camber = 6/9, ALPT = l 1.08, BETA = 0.60, QINF = 308.1,

RNPU = 2.8E+06, CNWP = 0.4649

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 - 1.341 0.000 0,509 0.000 4.573" * 0.010 - 1.639

0.060 -0.785 0.020 - 1.593 0.020 - 1.597 0.020 - 1.718

0.110 -1.096 0.040 -l.301 0.060 -2.693** 0.060 -1.717

0.200 -0.981 0.060 - 1.375 0.090 - 1.580 0.110 - 1.785

0.230 -0.531 0.090 -1.411 0.110 -1.698 0.140 -1.535

0.400 -0.446 0.130 -1.518 0.130 -1.406 0.190 -2.919"*

0.490 -0.358 0.150 - 1.676 0.150 - 1.134 0.250 - 1.142

0.590 -0.487 0.200 - 1.700 0.210 - 1.112 0.400 -0.420

0.630 -0.513 0.250 - 1.046 0.250 -0.980 0.490 -0.391

0.700 -0.597 0.260 -0.957 0.340 -0.896 0.580 -0.345

0.750 -0.805 0.280 -0.933 0.370 -0.841 0.650 -0.400

0.810 -0.756 0.290 -0.818 0.400 -0.780 0.700 -0.397

0.840 -0.786 0.310 -0.717 0.410 -0.799** 0.750 -0.378

0.900 -0.386 0.320 -0.680 0.430 -0.757 0.800 -0.417"*

0.960 -0.231 0.340 -0.595 0.440 -0.713 0.830 -0.326

0.350 -0.226** 0.460 -0.705 0.900 -0.306

0.370 -0.467 0.490 -0.599 0.960 -0.282

0.380 -0.524 0.500 -0.650

0.400 -0.362 0.520 -0.645

0.410 -0.494 0.540 -0.611

0.430 -0.460 0.550 -0.553

0.440 -0.42 l 0.580 -0.490

0.460 -0.472 0.600 -0.546

0.470 -0.466 0.610 -0.517

0.490 -0.458 0.650 3.240**

0.500 -0.459 0.700 -0.475

0.520 -0.462 0.750 -0.507

0.530 -0.446 0.820 -0.387**

0.550 -0.495 0.890 -0.231

0.560 -0.494 0.900 -0.234

0.580 -0.472 0.960 -0.159

0.590 -0.528

0.600 -0.499

0.640 -0.541

0.700 -0.588

0.750 0.010"*

0.820 -0.456

0.870 -0.327

0.930 -0.172

0.960 -0.154

Lower Surface

0.020 0.246 0.020 0.527 0.020 0.543 0.020 0.700

0.110 0.149 0.060 0.419 0.060 0.473 0.060 2.958**

0.230 0.180 0.090 0.325 0.090 1.053"* 0.110 0.396

0.400 0.108 0.120 0.305 0.120 0.181 0.250 0.170

0,490 0.112 0.200 0.192 0.200 0.168 0.400 0.127

0.630 1.792"* 0.260 0.212 0.250 0.234 0.490 0_075

0.750 0.122 0.400 0.141 0.400 0.139 0.580 0.065

0.850 0.176 0.490 0.109 0.490 0.040 0.650 0.170

0.900 0.244 0.580 0.120 0.580 0.124 0.750 0.357

0.960 0.115 0.640 0.287 0.650 0.027 0.830 0.465

0.750 0.329 0.750 0.058 0.900 0.482

0.870 0.4 |0 0.890 0.434 0.960 0.293

0.930 0.308 0.930 0.343

0.960 0.195 0.960 -0.884"*

CN = 0.713 0.964 0.860 0.933

639
Table J-2. Continued.

Hight 223, Wing sweep = 26 °, Time = 10-23-41-500, MINF = 0.674, Camber = 7/10, ALPT = I 1.66, BETA = 0.57, QINF = 282.0,

RNPU = 2.6E+06, CNWP = 0.4807

vl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.549 0.000 0.361 0.000 5.0454, 0.010 - 1.873

0.060 -0.893 0.020 - 1.876 0.020 - 1.837 0.020 - 1.893

O, 110 - 1.102 0.040 - 1.524 0.060 -2.896" * 0.060 - 1.891

0.200 -0.777 0.060 - 1.550 0.090 - 1.764 O. 110 - 1.945

0.230 -0.753 0.090 - 1.584 O. 110 - 1.889 O.140 - 1.503

0.400 -0.466 0.130 - 1.673 0.130 - 1.237 0.190 -3.1434.

0.490 -0.429 0.150 - 1.838 0.150 - 1.173 0.250 -0.580

0.590 -0.499 0.200 - 1.589 0.210 - 1.161 0.400 -0.496

0.630 -0.551 0.250 - 1.023 0.250 -0.982 0.490 -0.417

0.700 -0.647 0.260 -0.880 0.340 -0.866 0.580 -0.358

0.750 -0.858 0.280 -0.793 0.370 -0.783 0.650 -0.425

0.810 -0.818 0.290 -0.691 0.400 -0.718 0.700 -0.416

0.840 -0.867 0.310 -0.615 0.410 -0.826"* 0.750 -0.397

0.900 -0.381 0.320 -0.607 0.430 -0.715 0.800 -0.4554.

0.960 -0.275 0.340 -0.564 0.440 -0.663 0.830 -0.348

0.350 -0.206** 0.460 -0.645 0.900 -0.350

0,370 -0.494 0.490 -0.541 0.960 -0.315

0.380 -0.578 0.500 -0.605

0.400 -0.480 0.520 -0.594

0.410 -0.541 0.540 -0.582

0.430 -0.505 0.550 -0.528

0.440 -0.462 0.580 -0.476

0.460 -0.503 0.600 -0.547

0,470 -0.524 0.610 -0.508

0.490 -0.507 0.650 3.588"4

0.500 -0.500 0.700 -0.515

0.520 -0.495 0.750 -0.554

0.530 -0.480 0.820 -0.433'*

0.550 -0.489 0.890 -0.241

0.560 -0.529 0.900 -0.220

0.580 -0.495 0.960 -0.147

0.590 -0.559

0.600 -0.549

0.640 -0.574

0.700 -0.627

0.750 -0.008"*

0.820 -0.477

0.870 -0.337

0.930 -0.183

0.960 -0.171

Lower Surface

0.020 0.286 0.020 0.509 0.020 0.554 0.020 0.710

0.110 0.176 0.060 0.458 0.060 0.516 0.060 3.280**

0.230 0.174 0.090 0.352 0.090 1.19844 0.110 0.396

0.400 0.118 0.120 0.327 0.120 0.206 0.250 0.196

0.490 0. 123 0.200 0.183 0.200 0.151 0.400 0.162

0.630 2.0064* 0.260 0.240 0.250 0.264 0.490 0.095

0.750 0.127 0.400 0.163 0.400 0.142 0.580 0,093

0.850 0.169 0.490 0.125 0.490 0.037 0.650 0.195

0.900 0.243 0.580 0.136 0.580 0.152 0.750 0.370

0.960 0.097 0.640 0.295 0.650 0.077 0.830 0.462

0.750 0.341 0.750 0.052 0.900 0.480

0.870 0.404 0.890 0.432 0.960 0.280

0.930 0.302 0.930 0.352

0.960 0.198 0.960 -0.919* *

CN = 0.756 1.013 0.883 0.911

640
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-3644-000, MINF = 0.803, Camber = 1/4, ALPT = 5.09, BETA = -0.38, QINF = 303.4,

RNPU = 2.5E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP .r./c CP x/c CP x/c CP

0,020 -0.175 0.000 0.857 0.000 0.907** 0.010 -0,980

0.060 -0,227 0.020 -0.555 0.020 -0.552 0.020 -0.980

0.110 -0.28 l 0.040 -0.370 0.060 -2.828** 0.060 -0.811

0,200 -0.253 0.060 -0,496 0.090 -0.721 0.110 -0.866

0.230 -0.327 0.090 -0.472 0. l 10 -0.464 0.140 -0.916

0.400 -0.247 0.130 -0.525 0.130 -0.456 0.190 -2.217" *

0.490 -0.218 0.150 -0.486 0.150 -0.533 0.250 -0.446

0,590 -0.320 0.200 -0,461 0,210 -0.567 0.400 -0.368

0,630 -0,297 0.250 -0,402 0.250 -0.405 0.490 -0.361

0.700 -0,284 0.260 -0.359 0.340 -0.387 0.580 -0.368

0.750 -0.383 0.280 -0.381 0.370 -0.383 0.650 -0.416

0.810 -0.380 0,290 -0.364 0.400 -0.390 0.700 -0.401

0.840 -0.343 0.310 -0.375 0.410 -1.091 ** 0.750 -0.492

0.900 -0.157 0.320 -0.367 0.430 -0.374 0.800 -0.503

0.960 -0.048 0.340 -0.341 0.440 -0.346 0.830 -0,434

0.350 -0.257** 0.460 -0.369 0.900 -0.177

0.370 -0.308 0.490 -0.308 0.960 -0.014

0.380 -0.358 0.500 -0,368

0.400 -0.263 0.520 -0.335

0.410 -0.345 0.540 -0.338

0.430 -0.318 0.550 -0.351

0.440 -0.279 0.580 -0.370

0.460 -0.336 0.600 -0.348

0,470 -0.322 0.610 -0.365

0.490 -0.321 0.650 0.358

0.500 -0.331 0,700 -0.588

0.520 -0.342 0.750 -0.500

0.530 -0.325 0.820 -0.510

0.550 -0.376 0.890 -0.136

0.560 -0.337 0.900 -0.103

0.580 -0.335 0.960 0.027

0.590 -0.379

0.600 -0.387

0.640 -0.456

0.700 -0.417

0.750 -0.016**

0.820 -0.405

0.870 -0.278

0,930 -0.116

0.960 -0.047

Lower Surface

0,020 -0.378 0.020 -0.187 0.020 -0.043 0_020 0,286

0.110 -0.223 0.060 -0.029 0.060 0.023 0.060 1.078

0.230 -0.124 0.090 -0.095 0.090 1.367 0.110 -0.078

0.400 -0.063 0.120 -0.116 0.120 -0.297 0.250 -0.222

0.490 -0.032 0.200 -0.086 0.200 -0.165 0.400 -0.203

0.630 2.118"* 0.260 -0.175 0.250 -0.167 0.490 -0.250

0.750 0.063 0.400 -0.1 04 0.400 -0.139 0,580 -0.212

0.850 0.156 0,490 -0.108 0.490 -0.039 0.650 -0.076

0.900 0.235 0.580 -0.076 0.580 -0.126 0.750 0.155

0.960 0.181 0.640 0.115 0.650 -0.032 0,830 0.313

0.750 0.238 0.750 0.005 0.900 0.356

0,870 0.310 0.890 0.318 0.960 0.270

0.930 0,237 0,930 0.268

0.960 0.187 0.960 - 1.947"*

CN = 0.240 0.384 _ ¢ ::]:_ 0.490

641
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-37-0-000, MINF = 0.803, Camber = 3/6, ALPT = 8.12, BETA = -0.18, QINF = 311.0,

RNPU = 2.5E+06

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.760 0.000 0.806 0.000 0.972"* 0,010 - 1.145

0.060 -0.714 0.020 -0.988 0.020 -0.944 0.020 - 1.124

0.110 -0.638 0.040 -0.789 0.060 -2.982 ** 0,060 - 1.161

0.200 -0.833 0.060 -0.870 0.090 -0.998 0.110 - 1.228

0.230 -0.771 0.090 -0,896 0.110 -1.031 0.140 -1.325

0.400 -0.259 0.130 -0.946 0.130 - 1.025 0.190 -2.215"*

0,490 -0.229 0.150 - 1.547 0.150 - 1.121 0.250 - 1.314

0.590 -0.339 0.200 -2.229 0.210 -0.122 0.400 -0.783

0.630 -0.357 0.250 - 1.055 0.250 -0.313 0.490 -0.451

0.700 -0,354 0.260 - 1.056 0.340 - 1.121 0.580 -0.422

0.750 -0,806 0.280 - 1.055 0.370 - 1. I 13 0.650 -0.446

0.810 -0.773 0.290 - 1.055 0.400 - 1.131 0.700 -0.448

0.840 -0.781 0.310 -1.068 0.410 -1.966"* 0.750 -0.539

0.900 -0.283 0.320 - 1.068 0.430 - 1.085 0.800 -0.518

0.960 -0.157 0.340 0.624 0.440 -0,747 0.830 -0.408

0.350 -0.479** 0.460 -0.589 0.900 -0.140

0.370 - 1.022 0.490 -0,486 0.960 -0.059

0.380 - 1.078 0.500 -0.449

0.400 - 1.013 0.520 -0.375

0.410 - 1.036 0.540 -0.349

0.430 -0.735 0.550 -0.354

0.440 -0.833 0.580 -0.331

0.460 -0.421 0.600 -0.270

0.470 -0.348 0.610 -0.271

0.490 -0.324 0.650 0.590

0.500 -0.281 0.700 -0.402

0.520 -0.234 0.750 -0.491

0.530 -0.202 0.820 -0.567

0.550 -0.241 0.890 -0. t 16

0.560 -0.204 0.900 -0.087

0.580 -0.209 0.960 0.021

0.590 -0.254

0.600 2.138

0.640 -0.375

0.700 -0.406

0.750 0.028**

0.820 -0.439

0.870 -0.390

0,930 -0.272

0.960 -0,215

Lower Surface

0.020 0.007 0.020 0.272 0.020 0.246 0.020 0.535

0.110 -0.037 0.060 0.221 0.060 0.258 0.060 1.077

0.230 0.086 0.090 0.134 0.090 1.096 0. I 10 0.147

0.400 0.036 0.120 0.103 0.120 -0,076 0.250 -0.028

0.490 0.993 0.200 0.061 0.200 0.023 0.400 -0.050

0.630 1.885"* 0.260 0.026 0.250 0.042 0,490 -0.1 04

0.750 0.450 0.400 0.036 0.400 0.016 0.580 -0.063

0.850 0.162 0.490 0.019 0.490 -0.020 0.650 0.045

0.900 0.241 0.580 0.022 0.580 -0.006 0.750 0.263

0.960 0.149 0.640 0.228 0.650 0.002 0.830 0.418

0.750 0.281 0.750 0.059 0.900 0,452

0.870 0.358 0,890 0.406 0.960 0.322

0.930 0.274 0.930 0.330

0.960 0.215 0.960 -1.883"*

CN= 0.784 0.737 _¢_¢ 0.866

642
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-37-4-500, MINF = 0.793. Camber = 5/8, ALPT = 11.01, BETA = -1.54, QINF = 311.8,

RNPU = 2.6E+06

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.783 0,000 0.724 0.000 0.911"* 0.010 -1.135

0.060 -0.682 0,020 - 1.096 0.020 - 1.045 0.020 - 1.181

0.110 -0.801 0.040 -0.845 0.060 -3.165"* 0,060 -1.268

0.200 -1.111 0.060 -0.967 0.090 -1.094 0.110 -1.387

0.230 -1,053 0,090 -1.041 0.110 -1.208 0,140 -1.506

0.400 -0.815 0.130 -1.137 0.130 -1.248 0.190 -2.274**

0.490 -0.254 0.150 - 1.263 0.150 - 1.366 0.250 - 1.524

0,590 -0.322 0.200 -1.288 0.210 -1.318 0.400 -I .071

0.630 -0.384 0.250 - 1.286 0.250 - 1.357 0.490 -0.849

0.700 -0.401 0.260 - 1.277 0.340 - 1.329 0.580 -0.486

0.750 -0.981 0,280 - 1.277 0.370 - 1.354 0.650 -0.487

0.810 -0.935 0.290 - 1.277 0,400 - 1.391 0.700 -0.475

0.840 -0.978 0.310 - 1.300 0.410 -1.897"* 0.750 -0,485

0.900 -0.451 0.320 - 1.302 0.430 - 1.314 0.800 -0.429

0.960 -0.360 0.340 - 1.265 0.440 - 1.274 0.830 -0.368

0.350 -0.522"* 0.460 - 1.291 0.900 -0.188

0.370 - 1.277 0.490 -0.740 0.960 -0.092

0.380 - 1.329 0.500 - 1.301

0.400 - 1.260 0.520 - 1.268

0.410 - 1.200 0.540 -0.903

0.430 -1.190 0.550 -0.719

0.440 -0.769 0.580 -0.744

0.460 - 1.234 0.600 -0.650

0.470 -0.717 0.610 -0,625

0.490 -0.687 0.650 0.467

0,500 -0.722 0.700 -0,553

0.520 -0.661 0.750 -0,564

0.530 - 1.212 0.820 -0.369

0.550 -0.651 0.890 -0.389

0.560 -0.579 0.900 -0.263

0.580 -0.577 0.960 -0.173

0.590 -0.585

0.600 -0.550

0.640 -0.403

0.700 -0.369

0.750 0.049**

0.820 -0.279

0.870 -0,203

0.930 -0.201

0.960 -0.203

Lower Surface

0.020 0.130 0,020 0.462 0.020 0.326 0.020 0.624

0.110 0,056 0.060 0.332 0.060 0.390 0.060 1.011

0.230 0.176 0.090 0.236 0.090 1.200 0.110 0.260

0.400 0,072 0.120 0.215 0.120 0.020 0.250 0,119

0.490 0.051 0.200 0. 184 0,200 0.116 0.400 0.024

0.630 1.817"* 0.260 0.131 0,250 0.162 0.490 -0.032

0,750 0.077 0.400 0.115 0.400 0,099 0.580 0.030

0.850 0.161 0.490 0.080 0.490 1.237 0.650 0.109

0.900 0.228 0.580 0.097 0.580 0.089 0.750 0.306

0.960 0.074 0.640 0.274 0.650 0.031 0.830 0.460

0,750 0.314 0.750 0,094 0.900 0.498

0.870 0.375 0.890 0,426 0.960 0.328

0.930 0.285 0,930 0,343

0.960 0.187 0.960 - 1.924"*

CN = 0.746 0.958 _:_:;-+ 1.063

643
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-37-6-500, MINF = 0.781, Camber = 6/11, ALPT = 12.94, BETA = 0.43, Q1NF = 308.5.

RNPU = 2.6E+06

I1 = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 - 1.026 0.000 0.632 0.000 0,860"* 0.010 - 1.369

0.060 -0.984 0.020 - 1.296 0.020 - 1.205 0,020 - 1.428

0.110 -0.986 0.040 - 1.033 0,060 -3,420" * 0.060 - 1.472

0,200 -1.257 0.060 -1,159 0.090 -1,341 0.110 -1.626

0.230 - 1.248 0.090 - 1,264 0.110 - 1.404 0.140 - 1.722

0.400 -0,496 0.130 - 1.339 0.130 -0,972 0.190 -2.342 **

0.490 -0,317 0.150 - 1,463 0.150 -0,958 0.250 - t.358

0.590 -0.423 0,200 - 1.503 0.210 -0.912 0.400 - 1.083

0,630 -0,449 0.250 - 1.335 0,250 -0.893 0.490 -0,852

0.700 -0.475 0,260 - 1.231 0.340 -0.818 0.580 -0,600

0.750 -0,937 0.280 - 1.167 0,370 -0.798 0,650 -0.539

0.810 -0.914 0.290 - 1.074 0.400 -0.810 0.700 -0.498

0.840 -0.981 0.310 -1.039 0.410 - 1,961"* 0.750 -0.479

0.900 -0.448 0,320 - 1.005 0.430 -0.767 0,800 -0.492

0.960 -0.391 0.340 -0.953 0.440 -0.724 0.830 -0.462

0.350 -0,346* * 0.460 -0.729 0.9(_ -0.410

0.370 -0.810 0.490 -0.704 0.960 -0.373

0,380 -0.767 0.500 -0.740

0.400 -0.588 0.520 -0.707

0.410 -0.591 0.540 -0.711

0.430 -0.452 0.550 -0.736

0.440 -0,426 0.580 -0.709

0.460 -0,429 0,600 -0.666

0.470 -0.415 0.610 -0.641

0,490 -0.373 0.650 0.397

0,500 -0.403 0.700 -0.645

0,520 -0,375 0,750 -0.674

0.530 -0.379 0.820 -0.538

0,550 -0.405 0.890 -0,461

0.560 -0,379 0.900 -0.488

0,580 -0.349 0.960 -0.359

0.590 -0.43 ]

0,600 -0.436

0.640 -0.441

0.700 -0,437

0.750 0.046**

0,820 -0,356

0.870 -0.354

0.930 -0.372

0,960 -0.367

Lower Surface

0,020 0,220 0.020 0.651 0.020 0,554 0.020 0.743

0.110 0.168 0.060 0,463 0.060 0.5 ] 5 0.060 I. 107

0.230 0.214 0,090 0.363 0.090 1.184 0.110 0.380

0.400 0.130 0.120 0.338 0.120 0.196 0,250 0,230

0.490 0.131 0.200 0.210 0.200 0.163 0.400 0.166

0.630 1,793"* 0,260 0.223 0.250 0.281 0,490 0.097

0,750 0.171 0.400 0.200 0.400 0.167 0.580 0.113

0.850 0.214 0,490 0.158 0.490 0.059 0.650 0.232

0.900 0,297 0.580 0.154 0,580 0.157 0,750 0.393

0.960 0.117 0,640 0.346 0,650 0.024 0.830 0.506

0.750 0,372 0.750 0,098 0,900 0,539

0.870 0.447 0,890 0.473 0.960 0.340

0,930 0,326 0.930 0.361

0,960 0.213 0.960 - 1.988" *

CN= 0.854 0.983 _¢_ 1.230

644
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-37-10-500, MINF = 0.778, Camber = 5/8, ALPT = 9.12, BETA = -0.33, QINF = 318.7,

RNPU = 2.7E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 -0.504 0.000 0.816 0.000 1.083"* 0.010 - 1.047

0.060 -0.593 0.020 -0.820 0.020 -0.863 0.020 - 1.159

0.110 -0.814 0.040 -0.533 0.060 -3.072** 0.060 - 1.214

0.200 - 1.039 0.060 -0.856 0.090 - 1.070 0.110 - 1.350

0.230 -1.007 0.090 -1.014 0.110 -1.151 0.140 -1.524

0.400 -0.329 0.130 -1.098 0,130 -1.211 0.190 -2.361"*

0.490 -0.263 0.150 - 1.218 0.150 - 1.333 0.250 - 1.502

0.590 -0.363 0.200 - 1.256 0.210 - 1.292 0.400 -0.779

0.630 -0.413 0.250 - 1.269 0.250 - 1.329 0.490 -0.505

0.700 -0.422 0.260 - 1.255 0.340 - 1.327 0,580 -0.448

0.750 -0,977 0.280 - 1.253 0.370 -1.308 0.650 -0.456

0.810 -0.940 0.290 - 1.261 0.400 - 1.296 0.700 -0.469

0.840 -0.982 0.310 - 1.266 0.410 -1.992"* 0.750 -0.523

0.900 -0.376 0.320 - 1.269 0.430 -0.810 0.800 -0,430

0.960 -0,277 0.340 - 1.223 0.440 -0.726 0.830 -0.387

0.350 -0,507** 0.460 -0.691 0.900 -0.145

0.370 - 1.219 0.490 -0.629 0.960 -0.074

0.380 - 1.259 0.500 -0.621

0.400 - 1.169 0.520 -0.599

0.410 -1.219 0.540 -0.533

0.430 -0.775 0.550 -0.517

0.440 -0.633 0.580 -0.489

0.460 -0.584 0.600 -0.408

0.470 -0.498 0.610 -0.393

0,490 -0.462 0.650 0.581

0.500 -0.422 0.700 -0.456

0.520 -0.396 0.750 -0.546

0.530 -0,342 0.820 -0.460

0.550 -0.327 0.890 -0.111

0.560 -0.267 0.900 -0.095

0.580 -0.262 0.960 -0.021

0.590 -0.270

0.600 -0.295

0.640 -0.407

0.700 -0.459

0.750 0.040**

0.820 -0.459

0.870 -0.382

0.930 -0,257

0.960 -0.218

Lower Surface

0.020 0.044 0.020 0.407 0.020 0.320 0.020 0.564

0.110 0.031 0.060 0.295 0.060 0.338 0.060 1.102

0,230 0.167 0.090 0.197 0.090 1.051 0.110 0.209

0.400 0.083 0.120 0.185 0.120 0.027 0.250 0.062

0.490 0,073 0.200 0.151 0.200 0.110 0.400 0,033

0.630 1.849** 0.260 0.103 0.250 0.130 0.490 -0.022

0.750 0.139 0,400 0.098 0.400 0.071 0,580 0.008

0.850 0.192 0.490 0,084 0.490 0.025 0.650 0.137

0.900 0.286 0.580 0,094 0.580 0.072 0.750 0.342

0.960 0.127 0.640 0.274 0.650 0.018 0.830 0.462

0.750 0.337 0.750 0,080 0.900 0.498

0.870 0399 0.890 0.433 0.960 0.356

0.930 0.315 0.930 0.359

0.960 0.226 0.960 - 1.865" *

CN= 0.686 0.896 $¢$_ 0.985

645
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-37-14-000, MINF = 0.788, Camber = 3/6, ALPT = 7.20, BETA = 0.57, QINF = 333.9,

RNPU = 2.8E+06

rl = 0.93 0.7O 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.428 0.000 0.863 0.000 1.044"* 0.010 -0.972

0.060 -0.512 0.020 -0.779 0.020 -0.627 0.020 - 1.083

0.110 -0.576 0.040 -0.526 0.060 -2.986"* 0.060 - 1.080

0.200 -0.843 0.060 -0.767 0.090 -0.928 0.110 - 1.142

0.230 -0.597 0.090 -0.854 0.110 -0.989 0.140 - 1.249

0.400 -0.290 0.130 -0.911 0.130 -0.998 0.190 -2.300"*

0.490 -0.265 0.150 -0.991 0.150 - 1.094 0.250 - 1.236

0.590 -0.345 0.200 -0.968 0.210 - 1.042 0.400 -0.403

0.630 -0.355 0.250 - 1.012 0.250 - 1.090 0.490 -0.380

0.700 -0.362 0.260 - 1.002 0.340 -0.719 0.580 -0.396

0.750 -0.766 0.280 -0.995 0.370 -0.436 0.650 -0.464

0.810 -0.693 0.290 -0.979 0.400 -0.356 0.700 -0.453

0.840 -0.640 0.310 -0.972 0.410 -1.949"* 0.750 -0.553

0.900 -0.264 0.320 -0.971 0.430 -0.335 0.800 -0.544

0.960 -0.133 0.340 -0.455 0.440 -0.301 0.830 -0.485

0.350 -0.202"* 0.460 -0.319 0.900 -0.129

0.370 -0.268 0.490 -0.316 0.960 -0.032

0.380 -0.289 0.500 -0.345

0.400 -0.197 0.520 -0.333

0.410 -0.270 0.540 -0.336

0.430 -0.257 0.550 -0.353

0.440 -0.236 0.580 -0.399

0.460 -0.294 0.600 -0.360

0.470 -0.290 0.610 -0.397

0.490 -0.303 0.650 0.350

0.500 -0.328 0.700 -0.597

0.520 -0.335 0.750 -0.545

0.530 -0.331 0.820 -0.657

0.550 -0.384 0.890 -0.145

0.560 -0.352 0.900 -0.114

0.580 -0.356 0.960 0.006

0.590 -0.416

0.600 -0.417

0.640 -0.522

0.700 -0.469

0.750 0.011 **

0.820 -0.441

0.870 -0.434

0.930 -0.289

0.960 -0.218

Lower Surface

0.020 -0.076 0.020 0.198 0.020 0.174 0.020 0.452

0.110 -0.064 0.060 0.154 0.060 0.206 0.060 1.018

0.230 0.055 0.090 0.081 0.090 0.956 0.110 0.089

0.400 0.035 0.120 0.084 0.120 -0.096 0.250 -0.046

0.490 0.023 0.200 0.035 0.200 0.009 0.400 -0.061

0.630 1.718 ** 0.260 -0.007 0.250 0.005 0.490 -0.115

0.750 0.100 0.400 0.012 0.400 -0.014 0.580 -0.084

0.850 0.177 0.490 -0.008 0.490 -0.004 0.650 0.043

0.900 0.260 0.580 0.015 0.580 -0.017 0.750 0.258

0.960 0.170 0.640 0.207 0.650 -0.010 0.830 0.400

0.750 0.278 0.750 0.030 0.900 0.447

0.870 0.338 0.890 0.386 0.960 0.314

0.930 0.276 0.930 0.322

0.960 0.198 0.960 - 1.795 **

CN= 0.491 0.657 ¢_¢ 0.772

646
Table J-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 8-42-64)00, MINF = 0.801, Camber = 5/10, ALPT = 3.03, BETA = 0.31, Q1NF = 604.6,

RNPU = 5.0E+06, CNWP = 0.2071

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.466 0.000 0,357 0.000 2.800" * 0.010 0.153

0.060 0.124 0.020 0.407 0.020 0.384 0.020 0.027

0.110 -0.143 0.040 0.238 0.060 -3,685"* 0.060 -0.260

0,200 -0.208 0.060 0.016 0.090 -0.200 0.110 -0.473

0.230 -0.229 0.090 -0.115 0.110 -0.337 0.140 -0.673

0.400 -0.169 0.130 -0.279 0.130 -0.506 0.190 -2.225 * *

0.490 -0.185 0.150 -0.409 0.150 -0.424 0.250 -0.312

0.590 -0.267 0.200 -0.321 0.210 -0.386 0.400 -0.294

0.630 -0,290 0,250 -0.265 0.250 -0.283 0,490 -0.274

0.700 -0.350 0,260 -0.263 0.340 -0.299 0.580 -0.296

0.750 - 1,005 0,280 -0.270 0.370 -0.304 0.650 -0.404

0.810 -0.913 0.290 -0.270 0.400 -0.295 0.700 -0.384

0.840 -0.964 0.310 -0.274 0.410 -2.719"* 0.750 -0.428

0.900 -0.175 0.320 -0.271 0.430 -0.311 0.800 -0.929

0.960 -0.134 0.340 -0.261 0.440 -0.294 0.830 -0.642

0.350 -0.224** 0.460 -0.306 0.900 °0.393

0.370 -0.249 0.490 -0.241 0.960 -0.383

0.380 -0.271 0.500 -0.311

0.400 -0.232 0.520 -0.295

0.410 -0.270 0.540 -0.296

0.430 -0.253 0.550 -0.280

0.440 -0.244 0.580 -0.274

0.460 -0.264 0.600 -0.325

0.470 -0.274 0.610 -0.356

0.490 -0.274 0.650 2.121 **

0.500 -0,285 0.700 -0.521

0.520 -0.283 0.750 -0.390

0.530 -0.284 0,820 - 1.038

0.550 -0.316 0,890 -0.306

0,560 -0.304 0.900 -0.365

0.580 -0.293 0,960 -0.277

0.590 -0.330

0.600 -0.337

0.640 -0.474

0.700 -0.382

0.750 -0.059**

0.820 -0,550

0.870 -0.312

0.930 -0.268

0.960 -0.268

Lower Surface

0.020 -0.981 0.020 -0.927 0.020 - 1.376 0.020 -0.389

0.110 -0,427 0.060 -0.695 0.060 -0.445 0.060 1.977"*

0.230 -0.145 0.090 -0.497 0.090 0.543"* 0.110 -0.248

0.400 -0.008 0.120 -0.271 0.120 -0.312 0.250 -0.283

0.490 0.039 0.200 -0.150 0.200 -0.162 0,400 -0.228

0.630 0.920"* 0.260 -0.119 0.250 -0.207 0.490 -0.207

0,750 0.173 0.400 -0.069 0.400 -0.142 0.580 -0.152

0.850 0.211 0.490 -0.033 0.490 -0.049 0.650 0.065

0.900 0.287 0.580 0.035 0.580 -0.024 0.750 0.286

0.960 0.177 0.640 0.226 0.650 -0.063 0.830 0.416

0.750 0.293 0.750 -0.020 0.900 0.468

0.870 0.356 0,890 0.398 0.960 0.330

0.930 0.257 0.930 0.324

0.960 0.161 0.960 -2.762"*

CN = 0.292 0.290 0.301 0.360

647
Table J-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 8-42-43-000, MINF = 0.804, Camber = 5/10, ALP3" = 3.03, BETA = 0.19, QINF = 607.5,

RNPU = 5.0E+06, CNWP = 0.2073

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.471 0.000 0.346 0.000 2.790"* 0.010 0.169

0.060 0.147 0.020 0.420 0.020 0.394 0.020 0.054

0.110 -0.129 0.040 0.246 0.060 -3.664** 0.060 -0.252

0.200 -0.204 0.060 0.020 0.090 -0.180 0.110 -0.445

0.230 -0.222 0.090 -0.105 0.1 t 0 -0.326 0.140 -0.630

0.400 -0.168 0.130 -0.272 0.130 -0.513 0.190 -2.211 **

0.490 -0.184 0.150 -0.403 0.150 -0.413 0.250 -0.314

0.590 -0.270 0.200 -0.315 0.210 -0.379 0.400 -0.293

0.630 -0.288 0.250 -0.267 0.250 -0.279 0.490 -0.272

0.700 -0.352 0.260 -0.259 0.340 -0.294 0.580 -0.294

0.750 -0.962 0.280 -0.273 0.370 -0.307 0.650 -0.406

0.810 -0.905 0.290 -0.264 0.400 -0.290 0.700 -0.381

0.840 -0.963 0.310 -0.270 0.410 -2.703** 0.750 -0.426

0.900 -0.189 0.320 -0.269 0.430 -0.306 0.800 -0.921

0.960 -0.159 0.340 -0.260 0.440 -0.292 0.830 -0.656

0.350 -0.227** 0.460 -0.304 0.900 -0.395

0.370 -0.250 0.490 -0.266 0.960 -0.397

0.380 -0.274 0.500 -0.308

0.400 -0.208 0.520 -0.289

0.410 -0.268 0.540 -0.299

0.430 -0.256 0.550 -0.276

0.440 -0.247 0.580 -0.268

0.460 -0.266 0.600 -0.321

0.470 -0.270 0.610 -0.351

0.490 -0.271 0.650 2,114"*

0.500 -0.282 0.700 -0.562

0.520 -0.281 0.750 -0.387

0.530 -0.280 0.820 - 1.059

0.550 -0.318 0.890 -0.316

0.560 -0.304 0.900 -0.362

0.580 -0.302 0.960 -0.289

0.590 -0.326

0.600 -0.337

0.640 -0.479

0.700 -0.381

0.750 -0.070'*

0.820 -0.557

0.870 -0.316

0.930 -0.270

0.960 -0.278

Lower Surface

0.020 -0.980 0.020 -0.920 0.020 - 1.396 0.020 -0.425

0.110 -0.448 0.060 -0,734 0,060 -0.497 0.060 1.971 * *

0.230 -0.157 0.090 -0.522 0.090 0.544** 0.110 -0.301

0.400 -0.015 0.120 -0.299 0.120 -0.323 0,250 -0.292

0.490 0.035 0.200 -0.163 0.200 -0.168 0.400 -0.238

0.630 0.919"* 0.260 -0.129 0.250 -0.217 0.490 -0.210

0.750 0.157 0.400 -0.074 0.400 -0.153 0.580 -0.158

0.850 0.206 0.490 -0.035 0.490 -0.060 0.650 0.061

0.900 0.283 0.580 0.031 0.580 -0.030 0.750 0.278

0.960 0.174 0.640 0.221 0.650 -0.073 0.830 0.415

0.750 0.284 0.750 -0.027 0.900 0.465

0.870 0.341 0.890 0.394 0.960 0.327

0.930 0.252 0.930 0.317

0.960 0.158 0.960 -2.746 * *

CN = 0.278 0,279 0.292 0,344

648
Table J-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 8-43-5-500, MINF = 0.801, Camber = 5/10, ALPT -- 3.89, BETA = 0.40, QINF = 603.9,

RNPU = 5.0E+06, CNWP = 0.2690

lq = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.398 0.000 0.466 0.000 2.803"* 0.010 0.015

0.060 0.056 0.020 0.293 0.020 0.273 0,020 -0.085

0.110 -0.193 0.040 0.152 0.060 -3.689"* 0.060 -0.398

0.200 -0.251 0.060 -0.069 0.090 -0.299 0.110 -0,554

0.230 -0.268 0.090 -0.215 0.110 -0.447 0,140 -0,888

0.400 -0,195 0.130 -0.385 0.130 -0.646 0.190 -2.228 * *

0.490 -0.205 0,150 -0.529 0.150 -0.722 0.250 -0.354

0.590 -0.281 0.200 -0.418 0.210 -0.430 0.400 -0.335

0.630 -0.302 0.250 -0.327 0.250 -0,345 0,490 -0.310

0.700 -0.358 0.260 -0.324 0.340 -0.344 0.580 -0.326

0.750 -0.961 0.280 -0.329 0.370 -0,352 0.650 -0.427

0.810 -0.900 0.290 -0.324 0.400 -0.336 0.700 -0.408

0.840 -0.958 0.310 -0.322 0.410 -2.722** 0.750 -0.439

0.900 -0.195 0.320 -0.324 0.430 -0.349 0,800 -0.930

0.960 -0.142 0,340 -0.308 0.440 -0.334 0.830 -0,636

0.350 -0.222** 0.460 -0.340 0.900 -0.394

0.370 -0.290 0.490 -0.297 0.960 -0.385

0.380 -0.312 0.500 -0.346

0.400 -0.263 0.520 -0.322

0.410 -0.304 0.540 -0,323

0.430 -0.286 0.550 -0,304

0.440 -0.276 0.580 -0.302

0.460 -0.298 0,600 -0.342

0.470 -0.299 0.610 -0.376

0.490 -0.297 0.650 2.123**

0,500 -0.305 0.700 -0.604

0.520 -0.307 0.750 -0.411

0,530 -0.306 0.820 - 1.048

0.550 -0.336 0.890 -0.299

0.560 -0.329 0.900 -0.363

0.580 -0,313 0.960 -0.279

0.590 -0.350

0.600 -0.355

0.640 -0.602

0.700 -0.381

0,750 -0.039**

0.820 -0.536

0,870 -0.286

0.930 -0.259

0.960 -0,256

Lower Surface

0.020 -0,979 0.020 -0.928 0.020 - 1.197 0.020 -0.283

0.110 -0.236 0.060 -0.427 0.060 -0.188 0.060 1.979"*

0.230 -0.093 0.090 -0.268 0,090 0.544** 0.110 -0.156

0.400 0.007 0.120 -0.148 0.120 -0.238 0.250 -0.227

0,490 0,035 0.200 -0.098 0.200 -0.101 0.400 -0.193

0.630 0.921 ** 0,260 -0.098 0.250 -0.164 0.490 -0.178

0.750 0.165 0.400 -0.060 0.400 -0.121 0.580 -0.133

0.850 0.218 0.490 -0.030 0.490 -0.035 0.650 0.083

0.900 0.296 0.580 0.032 0.580 -0.021 0.750 0.298

0.960 0.168 0.640 0.232 0.650 -0,049 0.830 0.432

0.750 0.301 0.750 -0.017 0.900 0.479

0.870 0.368 0.890 0.422 0.960 0,334

0.930 0.272 0.930 0.344

0.960 0.172 0.960 -2.766"*

CN = 0.345 0.367 0.391 0.441

649
Table J-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 8--43-13-000, MINF = 0.810, Camber = 5/10, ALPT = 6.01, BETA = 0.66, QINF = 615.0,

RNPU = 5.0E+06, CNWP = 0.3171

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.201 0.000 0.713 0.000 2.761 ** 0.010 -0.367

0.060 -0.135 0.020 0.063 0.020 -0.047 0.020 -0.358

0.110 -0.371 0.040 -0.063 0.060 -3.614** 0.060 -0.732

0.200 -0.781 0.060 -0.316 0.090 -0.479 0.110 -0.872

0.230 -0.202 0.090 -0.401 0.110 -0.611 0.140 -1.073

0.400 -0.242 0.130 -0.598 0.130 -0.786 0.190 -2.179**

0.490 -0.236 0.150 -0.786 0.150 -0.882 0.250 -0.754

0.590 -0.313 0.200 -0.821 0.210 -0.891 0.400 -0.402

0.630 -0.339 0.250 -0.863 0.250 -0.905 0.490 -0.357

0.700 -0.362 0.260 -0.865 0.340 -0.392 0.580 -0.381

0.750 -0.911 0.280 -0.855 0.370 -0.319 0.650 -0.473

0.810 -0.784 0.290 -0.847 0.400 -0.307 0.700 -0.441

0.840 -0.832 0.310 -0.469 0.410 -2.665** 0.750 -0.486

0.900 -0.268 0.320 -0.389 0.430 -0.327 0.800 -0.905

0.960 -0.265 0.340 -0.264 0.440 -0.317 0.830 -0.653

0.350 -0.141 ** 0.460 -0.332 0.900 -0.421

0.370 -0.237 0.490 -0.306 0.960 -0.390

0.380 -0.269 0.500 -0.352

0.400 -0.243 0.520 -0.334

0.410 -0.281 0.540 -0.342

0.430 -0.277 0.550 -0.318

0.440 -0.276 0.580 -0.315

0.460 -0.301 0.600 -0.361

0.470 -0.316 0.610 -0.386

0.490 -0.313 0.650 2.093"*

0.500 -0.321 0.700 -0.626

0.520 -0.327 0.750 -0.508

0.530 -0.326 0.820 -0.908

0.550 -0.359 0.890 -0.321

0.560 -0.349 0.900 -0.383

0.580 -0.334 0.960 -0.295

0.590 -0.371

0.600 -0.367

0.640 -0.666

0.700 -0.495

0.750 -0.018"*

0.820 -0.575

0.870 -0.306

0.930 -0.297

0.960 -0.293

LowerSufface

0.020 -0.500 0.020 -0.399 0.020 -0.207 0.020 0.210

0.110 -0.148 0.060 -0.042 0.060 0.031 0.060 1.952 * *

0.230 -0.002 0.090 -0.063 0.090 0.543" * 0.110 0.015

0.400 0.020 0.120 -0.021 0.120 -0.084 0.250 -0.112

0.490 0.043 0.200 -0.001 0.200 -0.003 0.400 -0.110

0.630 0.913 ** 0.260 -0.020 0.250 -0.057 0.490 -0.116

0.750 0.176 0.400 -0.010 0.400 -0.055 0.580 -0.081

0.850 0.224 0.490 0.001 0.490 -0.015 0.650 0.119

0.900 0.302 0.580 0.053 0.580 0.013 0.750 0.336

0.960 0.142 0.640 0.269 0.650 -0.022 0.830 0.465

0.750 0.339 0.750 0.003 0.900 0.506

0.870 0.426 0.890 0.461 0.960 0.349

0.930 0.311 0.930 0.368

0.960 0.197 0.960 -2.707 **

CN= 0.432 0.562 0.544 0.638

650
Table J-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 8-43-17-000, MINF = 0.804, Camber = 5/6, ALPT = 6.97, BETA = 0.74, QINF = 605.8,

RNPU = 5.0E+06, CNWP = 0.3917

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.033 0.000 0.823 0.000 2.808** 0.010 -0.748

0.060 -0.263 0.020 -0.171 0.020 -0.242 0.020 -0.634

0.110 -0.461 0.040 -0.237 0.060 -3.665 * * 0.060 -0.849

0.200 -0.876 0.060 -0.464 0.090 -0.713 0.110 - 1.033

0.230 -0.754 0.090 -0.522 0.1 l0 -0.764 0.140 -1.213

0.400 -0.217 0.130 -0.699 0.130 -0.908 0.190 -2.208"*

0.490 -0.231 0.150 -0.868 0.150 -0.977 0.250 - 1.157

0.590 -0.315 0.200 -0.910 0.210 -0.978 0.400 -0.438

0.630 -0.334 0.250 -0.958 0.250 -0.916 0.490 -0.382

0.700 -0.362 0.260 -0.975 0.340 - 1.021 0.580 -0.384

0.750 -0.760 0.280 -0.975 0.370 - 1.020 0.650 -0.484

0.810 -0.672 0.290 -0.978 0.400 -0.908 0.700 -0.460

0.840 -0.690 0.310 -0.804 0.410 -2.701 ** 0.750 -0.518

0.900 -0.234 0.320 -0.956 0.430 -0.425 0.800 -0.914

0.960 -0.086 0.340 -0.858 0.440 -0.350 0.830 -0.825

0.350 -0.447** 0.460 -0.319 0.900 -0.419

0.370 -0.913 0.490 -0.225 0.960 -0.301

0.380 -0.965 0.500 -0.297

0.400 -0.440 0.520 -0.286

0.410 -0.339 0.540 -0.288

0.430 -0.252 0.550 -0.282

0.440 -0.217 0.580 -0.293

0.460 -0.211 0.600 -0.331

0.470 -0.203 0.610 -0.357

0.490 -0.213 0.650 2.129 **

0.500 -0.230 0.700 -0.590

0.520 -0.230 0.750 -0.449

0.530 -0.250 0.820 -0.932

0.550 -0.297 0.890 -0.258

0.560 -0.297 0.900 -0.307

0.580 -0.294 0.960 -0.246

0.590 -0.323

0.600 -0.339

0.640 -0.550

0.700 -0.405

0.750 -0.034**

0.820 -0.499

0.870 -0.258

0.930 -0.248

0.960 -0.272

Lower Surface

0.020 -0.285 0.020 -0.163 0.020 -0.019 0.020 0.320

0.110 -0.099 0.060 0.061 0.060 0.131 0.060 1.986"*

0.230 0.057 0.090 0.029 0.090 0.555** 0.110 0.094

0.400 0.009 0.120 0.036 0.120 0.000 0.250 -0.043

0.490 0.034 0.200 0.057 0.200 0.056 0.400 -0.054

0.630 0.931 ** 0.260 0.026 0.250 0.000 0.490 -0.073

0.750 0.092 0.400 0.009 0.400 -0.008 0.580 -0.044

0.850 0.148 0.490 0.010 0.490 -0.015 0.650 0.152

0.900 0.234 0.580 0.031 0.580 0.038 0.750 0.364

0.960 0.160 0.640 0.243 0.650 -0.032 0.830 0.479

0.750 0.248 0.750 0.014 0.900 0.526

0.870 0.287 0.890 0.469 0.960 0.373

0.930 0.175 0.930 0.373

0.960 0.074 0.960 -2.744**

CN = 0.456 0.599 0.666 0.782

651
Table J-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 8-43-22-500, MINF = 0.790, Camber = 5/-1, ALPT = 8.20, BETA = 0.83, QINF = 577.9,

RNPU = 4.8E+06, CNWP = 0.4390

rl -- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.254 0.000 0.855 0.000 2.967"* 0.010 -0.909

0.060 -0.523 0.020 -0.527 0.020 -0.610 0.020 - 1.015

0.110 -0.688 0.040 -0.451 0.060 -3.818 ** 0.060 - 1.037

0.200 -0.965 0.060 -0.735 0.090 -0.936 0.110 - 1.188

0.230 -0.889 0.090 -0.827 0.110 -0.993 0.140 -1.356

0.400 -0.226 0.130 -0.840 0.130 -1.113 0.190 -2.291"*

0.490 -0.225 0.150 - 1.045 0.150 - 1.147 0.250 - 1.34 I

0.590 -0.276 0.200 - 1.070 0.210 - 1.156 0.400 -0.675

0.630 -0.255 0,250 - 1.113 0.250 -0.937 0.490 -0.452

0.700 -0.192 0.260 - 1.125 0.340 - 1,206 0.580 -0.419

0.750 -0.177 0.280 - 1.118 0.370 - 1.199 0.650 -0.505

0.810 -0.160 0.290 - 1.125 0.400 - 1.188 0.700 -0.509

0.840 -0.156 0.310 -0.819 0.410 -2.808 * * 0.750 -0.590

0.900 -0.167 0.320 - 1.126 0.430 - 1.107 0.800 -0.601

0.960 -0.074 0.340 -0.876 0.440 -0.698 0.830 -0.589

0.350 -0.475"* 0.460 -0.588 0.900 -0.198

0.370 -0.933 0.490 -0.462 0.960 -0.152

0.380 - 1.145 0.500 -0.441

0.400 - 1.066 0.520 -0.389

0.410 -0.829 0.540 -0.342

0.430 -0.631 0.550 -0.310

0.440 -0.502 0.580 -0.291

0.460 -0.411 0.600 -0.318

0.470 -0.344 0.610 -0.326

0.490 -0.291 0.650 2.256**

0.500 -0.261 0.700 -0.463

0.520 -0.236 0.750 -0.460

0.530 -0.219 0.820 -0.803

0.550 -0.247 0.890 -0.175

0.560 -0.240 0.900 -0.143

0.580 -0.257 0.960 -0.098

0.590 -0.276

0.600 -0.291

0.640 -0.421

0.700 -0.423

0.750 -0.111"*

0.820 -0,616

0.870 -0.419

0.930 -0.319

0.960 -0.252

Lower Surface

0.020 -0.084 0.020 0.107 0.020 0.203 0.020 0.516

0.110 -0.022 0.060 0.194 0.060 0.264 0.060 2.106"*

0.230 0.114 0.090 0.144 0.090 0.606** 0.110 0.178

0.400 -0.012 0.120 0.153 0.120 0.101 0.250 0.031

0.490 -0.039 0.200 0.114 0.200 0.111 0.400 0.009

0.630 1.000** 0.260 0.085 0.250 0.081 0.490 -0.004

0.750 -0.055 0.400 0.040 0.400 0.039 0.580 0.0 t 4

0.850 -0.018 0.490 0.026 0.490 -0.045 0.650 0.178

0.900 0.033 0.580 0.022 0.580 0.068 0.750 0.396

0.960 0.064 0.640 0.194 0.650 -0.087 0.830 0.504

0.750 0.112 0.750 0.046 0.900 0.543

0.870 0.126 0.890 0.470 0.960 0.380

0.930 0.064 0.930 0.381

0.960 0.003 0.960 -2.853 * *

CN = 0.353 0.700 0.764 0.892

652
Table J-2. Continued.

Flight 226, Wing sweep = 26 °, Time = 8-43-29-000, MINF = 0.791, Camber = 5/-1, ALPT = 8.04, BETA = 0.66, QINF = 573.9,

RNPU = 4.8E+06, CNWP = 0.4273

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.232 0.000 0.86 l 0.000 3.010"* 0.010 -0.912

0.060 -0.510 0.020 -0.489 0.020 -0.543 0.020 - 1.001

0.110 -0.652 0.040 -0.439 0.060 -3.822** 0.060 - 1.000

0.200 -0.955 0.060 -0.716 0.090 -0.907 0.110 - 1.183

0.230 -0.884 0.090 -0.817 0.110 -0.969 0.140 - 1.347

0.400 -0.227 0.130 -0.824 0.130 - 1.097 0.190 -2.285 * *

0.490 -0.236 0.150 - 1.040 0.150 - 1.132 0.250 - 1.350

0.590 -0.275 0.200 - 1.056 0.210 - 1.150 0.400 -0.641

0.630 -0.255 0.250 - 1.094 0.250 -0.921 0.490 -0.438

0.700 -0.199 0.260 -1.113 0.340 -1.183 0.580 -0.424

0.750 -0.173 0.280 - 1.125 0.370 - 1.182 0.650 -0.508

0.810 -0.165 0.290 - 1.118 0.400 - 1.180 0.700 -0.509

0.840 -0.165 0.310 -0.802 0.410 -2.805** 0.750 -0.587

0.900 -0.166 0.320 - 1.116 0.430 -0.918 0.800 -0.622

0.960 -0.078 0.340 -0.860 0.440 -0.635 0.830 -0.662

0.350 -0.470** 0.460 -0.548 0.900 -0.22 l

0.370 -0.917 0.490 -0.434 0.960 -0.153

0.380 -1.139 0.500 -0.413

0.400 - 1.063 0.520 -0.357

0.410 -0.835 0.540 -0.323

0.430 -0.547 0.550 -0.293

0.440 -0.448 0.580 -0.284

0.460 -0.375 0.600 -0.308

0.470 -0.314 0.610 -0.329

0.490 -0.262 0.650 2.294**

0.500 -0.254 0.700 -0.472

0.520 -0.222 0.750 -0.465

0.530 -0.214 0.820 -0.805

0.550 -0.257 0.890 -0.194

0.560 -0.252 0.900 -0.183

0.580 -0.253 0.960 -0.145

0.590 -0.293

0.600 -0.293

0.640 -0.426

0.700 -0.428

0.750 -0.130**

0.820 -0.579

0.870 -0.412

0.930 -0.298

0.960 -0.236

Lower Surface

0.020 -0.102 0.020 0.069 0.020 0.188 0.020 0.495

0.110 -0.037 0.060 0.178 0.060 0.245 0.060 2.142"*

0.230 0.112 0.090 0.133 0.090 0.632** 0.110 0.171

0.400 -0.009 0.120 0.124 0.120 0.076 0.250 0.018

0.490 -0.043 0.200 0.108 0.200 0.114 0.400 -0.003

0.630 1.029** 0.260 0.074 0.250 0.078 0.490 -0.007

0.750 -0.069 0.400 0.046 0.400 0.031 0.580 0.006

0.850 -0.033 0.490 0.021 0.490 -0.049 0.650 0.187

0.900 0.040 0.580 0.025 0.580 0.076 0.750 0.391

0.960 0.058 0.640 0.211 0.650 -0.103 0.830 0.507

0.750 0.102 0.750 0.035 0.900 0.546

0.870 0.136 0.890 0.488 0.960 0.385

0.930 0.068 0.930 0.395

0.960 -0.001 0.960 -2.851 **

CN = 0.344 0.685 0.751 0.889

653
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-43-0-000, MINF = 0.801, Camber = 1/4, ALPT = 5.00, BETA = 0.02, QINF = 297.8,

RNPU = 2.4E+06

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.215 0.000 0.863 0.000 0.870"* 0.010 -0.996

0.060 -0.224 0.020 -0.615 0.020 -0.567 0.020 °0.989

0.110 -0.310 0.040 -0.392 0.060 -2.885"* 0.060 -0.837

0.200 -0.254 0.060 -0.534 0.090 -0.773 0.110 -0.898

0.230 -0.345 0.090 -0.510 0.110 -0.694 0.140 -0.927

0.400 -0.263 0.130 -0.544 0.130 -0.465 0.190 -2.226 * *

0.490 -0.234 0.150 -0.552 0.150 -0.547 0.250 -0.452

0.590 -0.307 0.200 -0.465 0.210 -0.556 0.400 -0.386

0.630 -0.288 0.250 -0.419 0.250 -0.446 0.490 -0.384

0.700 -0.275 0.260 -0.355 0.340 -0.384 0.580 -0.355

0.750 -0.363 0.280 -0.400 0.370 -0.402 0.650 -0.425

0.810 -0.370 0.290 -0.376 0.400 -0.387 0.700 -0.420

0.840 -0.331 0.310 -0.391 0.410 ol.831"* 0.750 -0.506

0.900 -0.167 0.320 -0.371 0.430 -0.378 0.800 -0.495

0,960 -0.053 0.340 -0.359 0.440 -0.364 0.830 -0.435

0.350 -0.263** 0.460 -0.367 0.900 -0.177

0.370 -0.322 0.490 -0.310 0.960 -0.01 l

0.380 -0.372 0.500 -0.372

0.400 -0.268 0.520 -0.338

0.410 -0.349 0.540 -0.341

0.430 -0.324 0.550 -0.354

0.440 -0.272 0.580 -0.371

0.460 -0.339 0.600 -0.354

0.470 -0.333 0.610 -0.384

0.490 -0.320 0.650 0.383

0.500 -0.376 0.700 -0.614

0.520 -0.368 0.750 -0.521

0.530 -0.321 0.820 -0.489

0.550 -0.386 0.890 -0.142

0.560 -0.334 0.900 -0.111

0.580 -0.353 0.960 0.019

0.590 -0.389

0.600 -0.406

0.640 -0.460

0.700 -0.410

0.750 -0.009**

0.820 -0.394

0.870 -0.284

0.930 -0.126

0.960 -0.060

Lower Surface

0.020 -0.359 0.020 -0.157 0.020 -0.024 0.020 0.287

0.110 -0.204 0.060 -0.042 0.060 0.038 0.060 1.086

0.230 -0.120 0.090 -0.097 0.090 1.233 0.110 -0.070

0.400 -0.030 0.120 -0.137 0.120 -0.332 0.250 -0.209

0.490 -0.044 0.200 -0.070 0.200 -0.165 0.400 -0.204

0.630 1.923"* 0.260 -0.186 0.250 -0.152 0.490 -0.244

0.750 0.053 0.400 -0.099 0.400 -0.138 0.580 -0.227

0.850 0.147 0.490 -0.110 0.490 -0.051 0.650 -0.082

0.900 0.240 0.580 -0.074 0.580 -0.125 0.750 0.147

0.960 0,168 0.640 0.113 0.650 -0.051 0,830 0.308

0.750 0.221 0.750 -0.029 0.900 0.351

0.870 0.262 0.890 0.305 0.960 0.257

0.930 0.229 0.930 0.254

0.960 0.171 0.960 - 1.957 **

CN = 0.244 0.386 ¢ _.:__ 0.499

654
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-43-15-000, MINF = 0.805, Camber = 1/5, ALPT = 6.23, BETA = -0.44, QINF = 303.0,

RNPU = 2.5E+06

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.477 0.000 0.842 0.000 0.928"* 0.010 -0.927

0.060 -0.465 0.020 -0,674 0.020 -0.784 0.020 - 1.066

0.110 -0.439 0.040 -0.637 0.060 -2.973"* 0.060 - 1.026

0.200 -0.316 0.060 -0.759 0.090 -0,879 0.110 -1.019

0.230 -0.387 0.090 -0.767 0.110 -0.917 0.140 - 1.098

0.400 -0.278 0.130 -0.803 0.130 -0.841 0.190 -2,207"*

0.490 -0,249 0,150 -0.830 0.150 -0.920 0.250 -0.850

0.590 -0.300 0.200 -0.757 0.210 -0.876 0.400 -0.369

0.630 -0.337 0,250 -0.729 0.250 -0.888 0.490 -0.367

0.700 -0.316 0.260 -0.434 0.340 -0.322 0.580 -0.386

0.750 -0.428 0.280 -0.317 0.370 -0.339 0.650 -0.433

0.810 -0.424 0.290 -0,299 0.400 -0.355 0.700 -0.429

0.840 -0.404 0.310 -0.321 0.410 - 1.819** 0.750 -0.523

0.900 -0.201 0.320 -0.324 0,430 -0.361 0.800 -0.581

0.960 -0,084 0.340 -0.308 0.440 -0.333 0.830 -0.511

0.350 -0.207** 0.460 -0.362 0.900 -0.146

0.370 -0.306 0.490 -0.303 0.960 -0.001

0.380 -0.359 0.500 -0.374

0.400 -0.282 0.520 -0.339

0.410 -0.358 0.540 -0.367

0.430 -0.328 0.550 -0.350

0.440 -0.257 0.580 -0.357

0.460 -0.373 0.600 -0,347

0.470 -0.335 0.610 -0,372

0.490 -0.340 0,650 0.343

0.500 -0.350 0.700 -0.633

0,520 -0.368 0.750 -0.626

0.530 -0.341 0.820 -0.621

0.550 -0.391 0.890 -0.126

0.560 -0.361 0.900 -0.095

0.580 -0,370 0.960 0.023

0.590 -0.406

0.600 -0.408

0.640 -0.605

0.700 -0.429

0.750 0.001"*

0,820 -0.429

0.870 -0.294

0.930 -0.165

0.960 -0.103

Lower Surface

0.020 -0.174 0.020 0.044 0.020 0.124 0.020 0.426

0.110 -0.132 0.060 0,077 0.060 0.140 0.060 1.100

0.230 -0.070 0.090 0.013 0.090 1.193 0.110 0.001

0.400 -0.005 0.120 -0.023 0.120 -0.229 0.250 -0.131

0.490 -0.004 0.200 -0.026 0.200 -0,092 0.400 -0.132

0.630 1.871 ** 0.260 -0.101 0.250 -0.075 0.490 -0.186

0.750 0.058 0.400 -0.046 0.400 -0.077 0.580 -0.174

0.850 0.147 0.490 -0.064 0.490 -0.033 0,650 -0.041

0.900 0.240 0.580 -0.050 0.580 -0.077 0.750 0.197

0.960 0.174 0.640 0.15 ! 0.650 -0,033 0.830 0.338

0.750 0.248 0,750 -0.018 0.900 0.394

0.870 0.305 0.890 0.324 0,960 0.290

0.930 0.257 0.930 0.293

0.960 0.197 0.960 - 1.937"*

CN = 0.327 0.513 **$* 0.632

655
Table J-2. Continued.

Flight 220, Wing sweep = 26", Time = 9-43-16-000, MINF = 0.805, Camber = 2/5, ALPT = 6.96, BETA = -0.27, QINF = 304.6,

RNPU = 2.5E+06

T1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.585 0.000 0.836 0.000 0.923** 0.010 -1.073

0.060 -0.502 0.020 -0.752 0.020 -0.851 0.020 - 1.059

O. 110 -0.623 0.040 -0.702 0.060 -3.019"* 0.060 - 1.075

0.200 -0.702 0.060 -0.809 0.090 -0.909 O. 110 - 1.083

0.230 -0.487 0.090 -0.815 0.110 -0.975 0.140 -1.173

0.400 -0.285 O. 130 -0.889 O. 130 -0.911 O. 190 -2.202 **

0.490 -0.251 O. 150 -0.914 O. 150 - 1.007 0.250 - 1.130

0.590 -0.333 0.200 -0.884 0.210 -0.960 0.400 -0.394

0.630 -0.347 0.250 -0.936 0.250 -0.997 0.490 -0.367

0.700 -0.341 0.260 -0.913 0.340 -0.965 0.580 -0.382

0.750 -0.721 0.280 -0.931 0.370 -0.477 0.650 -0.448

0.810 -0.655 0.290 -0.908 0.400 -0.375 0.700 -0.420

0.840 -0.592 0.310 -0.910 0.410 - 1.817 * * 0.750 -0.527

0.900 -0.235 0.320 -0.895 0.430 -0.308 0.800 -0.577

0.960 -0.126 0.340 -0.547 0.440 -0.253 0.830 -0.525

0.350 -0.241 ** 0.460 -0.279 0.900 -0.135

0.370 -0.247 0.490 -0.227 0.960 -0.022

0.380 -0.283 0.500 -0.319

0.400 -0.166 0.520 -0.311

0.410 -0.248 0.540 -0.303

0.430 -0.228 0.550 -0.317

0.440 -0.194 0.580 -0.340

0.460 -0.279 0.600 -0.341

0.470 -0.262 0.610 -0.357

0.490 -0.280 0.650 0.390

0.500 -0.315 0.700 -0.619

0.520 -0.335 0.750 -0.565

0.530 -0.322 0.820 -0.812

0.550 -0.372 0.890 -0.131

0.560 -0.333 0.900 -0.098

0.580 -0.340 0.960 0.026

0.590 -0.388

0.600 -0.404

0.640 -0.567

0.700 -0.431

0.750 0.008**

0.820 -0.398

O. 870 -0.401

0.930 -0.255

0.960 -0.196

Lower Surface

0.020 -0.147 0,020 O. 108 0.020 O. 161 0.020 0.462

O. 110 -0.098 0.060 O. 139 0.060 O. 199 0.060 1.101

0.230 -0.026 0.090 0.051 0.090 1.179 O. 110 0.043

0.400 0.020 O. 120 0.005 O. 120 -0.198 0.250 -0.099

0.490 -0.004 0.200 -0.030 0.200 -0.024 0.400 -0.092

0.630 1.853"* 0.260 -0.058 0.250 -0.031 0.490 -0.156

0.750 0.087 0.400 -0.031 0.400 -0.050 0.580 -0.141

0.850 O. 172 0.490 -0.035 0.490 -0.040 0.650 -0.011

0.900 0.249 0.580 -0.006 0.580 -0.048 0.750 0.207

0.960 O. 168 0.640 O.183 0.650 -0.026 0.830 0.374

0.750 0.266 0.750 -0.011 0.900 0.417

0.870 0.329 0.890 0.365 0.960 0.286

0.930 0.252 0.930 0.317

0.960 0.195 0.960 -1.915"*

CN = 0.438 0.603 $$$$ 0.712

656
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-43-18-000, MINF = 0.806. Camber = 3/7, ALPT = 8.04, BETA = -0.50. QINF = 307.9,

RNPU = 2.5E+06

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.701 0.000 0.815 0.000 0.923"* 0,010 - 1.059

0,060 -0.633 0,020 -0.909 0.020 -0.903 0,020 - 1,105

0.110 -0,708 0.040 -0.737 0.060 -3.001 ** 0.060 - 1.115

0.200 -0.825 0.060 -0.822 0.090 -0.981 0.110 - 1.2 l0

0.230 -0.832 0.090 -0.875 0.110 - 1.028 0.140 - 1.325

0.400 -0.279 0.130 -0,956 0.130 - 1.030 0.190 -2.198" *

0,490 -0,235 0.150 - 1.041 0.150 - 1.143 0.250 - 1.303

0.590 -0,342 0.200 - 1,007 0.210 - 1.081 0.400 -0.829

0.630 -0.357 0.250 - 1.071 0.250 - 1,138 0.490 -0.518

0.700 -0.365 0,260 - 1,052 0.340 - 1.107 0.580 -0.435

0.750 -0.851 0.280 - 1.067 0.370 - 1.089 0.650 -0.459

0.810 -0.792 0.290 - 1.053 0.400 - 1.196 0.700 -0.442

0.840 -0.822 0.310 - 1.075 0.410 - 1.817"* 0.750 -0.548

0.900 -0.294 0.320 - 1.065 0.430 - 1.1 O0 0.800 -0.513

0.960 -0.169 0.340 - 1.036 0.440 - 1.085 0.830 -0.416

0.350 -0.493 ** 0.460 -0.971 0.900 -0. 139

0.370 - 1.029 0.490 -0.546 0.960 -0,087

0.380 - 1.085 0.500 -0,544

0.400 -0.988 0.520 -0.481

0.410 - 1.043 0.540 -0.423

0,430 - 1.005 0.550 -0.400

0.440 -0,989 0.580 -0.386

0,460 -0.718 0.600 -0.302

0,470 -0.484 0.610 -0.291

0.490 -0.391 0.650 0.587

0,500 -0,355 0.700 -0.414

0.520 -0.330 0.750 -0.514

0,530 -0.250 0.820 -0.628

0.550 -0.297 0,890 -0.131

0.560 -0.216 0.900 -0.103

0.580 -0.229 0.960 0.015

0.590 -0,288

0,600 -0.285

0.640 -0.370

0,700 -0.420

0.750 0.025**

0,820 -0.461

0.870 -0,444

0.930 -0.311

0.960 -0.246

Lower Surface

0,020 -0.069 0.020 0.237 0,020 0.229 0.020 0.537

0.110 -0.061 0.060 0.191 0,060 0,244 0.060 1.099

0.230 0.073 0,090 0.106 0.090 t. 147 0.110 0.125

0.400 0.026 0.120 0,086 0.120 -0.099 0,250 -0.015

0,490 0,020 0.200 0.051 0,200 0.019 0.400 -0.036

0.630 1.815 ** 0.260 0.002 0.250 0.028 0.490 -0.108

0.750 O. 110 0.400 0.019 0.400 -0.001 0.580 -0.082

0.850 0.168 0.490 0.001 0.490 -0.009 0.650 0.042

0.900 0.257 0.580 0.026 0,580 -0.002 0.750 0,267

0.960 0.153 0.640 0.231 0.650 -0.037 0.830 0.396

0.750 0.281 0.750 0.016 0,900 0,439

0.870 0.344 0,890 0.392 0.960 0.304

0.930 0.273 0.930 0.330

0.960 0.199 0.960 - 1.925"*

CN = 0,555 0.770 ¢_¢_ 0.875

657
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-43-19-000, MINF = 0.806, Camber = 3/2, ALPT = 9.05, BETA = -0.30, QINF = 309.7,

RNPU = 2.5E+06

"q = 0,93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.851 0.000 0.779 0.000 0.933"* 0.010 - 1.098

0.060 -0.787 0.020 - 1.068 0.020 -0.974 0.020 - 1.117

0.110 -0.811 0.040 -0.819 0.060 -3.051"* 0.060 -1.215

0.200 -0.935 0.060 -0.921 0.090 - 1.061 0.110 - 1.316

0.230 -0.866 0.090 -0.961 0.110 - 1.107 0.140 - 1.405

0.400 -0.844 0.130 - 1.031 0.130 - 1.089 0.190 -2.199* *

0.490 -0.261 0.150 - 1.129 0. t 50 - 1.226 0.250 - 1,405

0.590 -0.276 0.200 - 1.115 0.210 - 1.158 0.400 -0.963

0.630 -0.324 0.250 - 1.142 0.250 - 1.199 0.490 -0.791

0.700 -0.277 0.260 - 1.122 0.340 - 1.202 0.580 -0.578

0.750 -0.390 0.280 - 1.130 0.370 - 1.196 0.650 -0.456

0.810 -0.397 0.290 - t. 130 0.400 - 1.216 0.700 -0.448

0.840 -0.385 0.310 -1.149 0.410 -1.819"* 0.750 -0.501

0.900 -0.289 0.320 - 1.147 0.430 - 1.194 0.800 -0.468

0.960 -0.174 0.340 - 1.113 0.440 - 1.162 0.830 -0.345

0.350 -0.515 ** 0.460 - 1.180 0.900 -0.163

0.370 - 1.118 0.490 -1.133 0.960 -0.079

0.380 -1.169 0.500 -1.191

0.400 -1.115 0.520 -1.147

0.410 - 1.130 0,540 -0.878

0.430 - 1.084 0,550 -0.738

0.440 - 1.052 0.580 -0.673

0.460 - 1.136 0.600 -0.564

0.470 - 1.099 0.6 |0 -0.502

0.490 - 1.125 0.650 0.571

0.500 -1.145 0.700 -0.417

0.520 - 1.124 0.750 -0.459

0.530 -0.724 0.820 -0.405

0.550 -0.588 0.890 -0.111

0.560 -0.477 0.900 -0.076

0.580 -0.445 0.960 0.017

0.590 -0.442

0.600 -0.391

0.640 -0.261

0.700 -0.314

0.750 0.001 **

0.820 -0.421

0.870 -0.362

0.930 -0.143

0.960 -0.051

Lower Surface

0.020 0.025 0.020 0.339 0.020 0.334 0.020 0.590

0.110 -0.007 0.060 0.264 0.060 0.322 0.060 1.108

0.230 0.113 0.090 0.160 0.090 1.127 0.110 0.185

0.400 0.020 0.120 0.144 0.120 -0.039 0.250 0.028

0.490 -0.008 0.200 0.123 0.200 0.053 0.400 0.005

0.630 1.791 ** 0.260 0.045 0.250 0.090 0.490 -0.063

0.750 0.014 0.400 0.045 0.400 0.034 0.580 -0.036

0.850 0,068 0.490 0.020 0.490 -0.007 0.650 0.090

0.900 0.141 0.580 0.034 0.580 0.034 0.750 0.289

0.960 0.089 0.640 0.201 0.650 -0.014 0.830 0.434

0.750 0.199 0.750 0.028 0.900 0.470

0.870 0.237 0.890 0.419 0.960 0.332

0.930 0.154 0.930 0.351

0.960 0.104 0.960 - 1.894"*

CN= 0.554 0.837 _*** 0.986

658
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-43-20-000, MINF = 0.805, Camber = 4/-1, ALPT = 10.12, BETA = -0.56, QINF = 31 t.3,

RNPU = 2.5E+06

"11= 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 -0.900 0.000 0.724 0.000 0.853"* 0.010 - 1.214

0.060 -0.861 0.020 - 1.095 0.020 - 1.038 0.020 - 1.257

0.110 -0.841 0.040 -0.851 0.060 -3.208"* 0.060 - 1.270

0,200 -1.041 0.060 -1.006 0.090 -1.131 0.110 -1.400

0.230 -0.983 0.090 -1.048 0.110 - 1.180 0.140 - 1.516

0.400 -0.985 0.130 -1.129 0.130 -1.198 0.190 -2.202**

0.490 -0.268 0.150 - 1.218 0.150 - 1.318 0.250 - 1.475

0.590 -0.235 0.200 - 1.245 0.210 - 1.251 0.400 - 1.065

0.630 -0.260 0,250 - 1.255 0.250 -1.305 0.490 -0.888

0.700 -0.150 0.260 - 1.235 0.340 - 1.319 0.580 -0.671

0.750 -0.205 0.280 - 1.240 0.370 - 1.318 0.650 -0.410

0.810 -0.189 0,290 - !.226 0.400 - 1.325 0,700 -0.401

0.840 -0.183 0.310 -l.242 0.410 -1.825"* 0.750 -0.412

0.900 -0.211 0.320 - 1.241 0.430 - 1,290 0.800 -0.399

0.960 -0.140 0.340 - 1.200 0.440 - 1.251 0.830 -0.335

0.350 -0.523"* 0.460 - 1.018 0.900 -0.172

0.370 - 1.226 0.490 -0.750 0.960 -0.086

0.380 - 1.292 0.500 -0.741

0.400 - 1.167 0.520 -0.702

0,410 -1.136 0.540 -0.680

0.430 -0.938 0.550 -0.678

0.440 -0.908 0,580 -0.643

0.460 -0.767 0.600 -0.597

0.470 -0.684 0.610 -0.573

0.490 -0.688 0.650 0.464

0.500 -0.676 0,700 -0.582

0.520 -0.677 0,750 -0.568

0.530 -0.636 0.820 -0,386

0.550 -0,678 0.890 -0.296

0.560 -0.583 0.900 -0.306

0.580 -0.599 0,960 -0,222

0.590 -0.583

0.600 -0.551

0.640 -0.386

0.700 -0.348

0.750 -0.055**

0.820 -0,267

0.870 -0.287

0,930 -0,229

0.960 -0.207

Lower Surface

0.020 0.038 0,020 0.393 0.020 0.370 0.020 0.604

0.110 0,018 0.060 0.308 0.060 0.344 0.060 1.101

0,230 0.134 0.090 0.209 0,090 1.106 0.110 0.207

0.400 -0,006 0.120 0.191 0. 120 0,009 0.250 0.067

0.490 -0.062 0,200 0.153 0.200 0.070 0.400 0.028

0.630 1.767"* 0.260 0.079 0.250 0.134 0,490 -0.035

0.750 -0.098 0.400 0.062 0.400 0.061 0.580 0.001

0.850 -0.040 0,490 0.019 0.490 -0.043 0.650 0.120

0.900 0.021 0,580 0.000 0,580 0.033 0.750 0.300

0.960 0,029 0,640 0.163 0.650 -0.067 0.830 0.429

0.750 0.093 0.750 0.013 0.900 0.484

0,870 0.083 0,890 0.388 0.960 0.330

0.930 0.046 0.930 0.305

0.960 -0.014 0.960 - 1.980**

CN = 0.504 0.820 "-_:__ 1.050

659
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-43-21-000, MINF = 0.804, Camber = 5/- 1, ALPT = 11.12, BETA = -0.59, QINF = 312.7,

RNPU = 2.6E+06

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.961 0.000 0.697 0.000 0.888"* 0.010 - 1.291

0.060 -0.926 0.020 - 1.188 0.020 - 1.083 0.020 - 1.329

0.110 -0.983 0.040 -0.918 0.060 -3.234 ** 0.060 - 1.347

0.200 -1.087 0.060 -1.064 0.090 -1.183 0.110 -1.438

0.230 -0.967 0.090 - 1.128 0.110 - 1.262 0.140 - 1.565

0.400 -0.565 0.130 -1.196 0.130 -1.274 0.190 -2.209**

0.490 -0.202 0.150 - 1.296 0.150 - 1.306 0.250 - 1.168

0.590 -0.266 0.200 - 1.309 0.210 -0.945 0.400 -0.943

0.630 -0.269 0.250 - 1.310 0.250 -0.852 0.490 -0.769

0.700 -0.162 0.260 - 1.282 0.340 -0.760 0.580 -0.626

0.750 -0.199 0.280 - 1.289 0.370 -0.759 0.650 -0.537

0.810 -0.238 0.290 - 1.275 0.400 -0.740 0.700 -0.516

0.840 -0.199 0.310 - 1.303 0.410 -1.833"* 0.750 -0.520

0.900 -0.205 0.320 -1.301 0.430 -0.725 0.800 -0.433

0.960 -0.141 0.340 - 1.190 0.440 -0.670 0.830 -0.406

0.350 -0.442"* 0.460 -0.678 0.900 -0.294

0.370 -0.959 0.490 -0.626 0.960 -0.221

0.380 -0.912 0.500 -0.658

0.400 -0.750 0.520 -0.606

0.410 -0.742 0.540 -0.625

0.430 -0.633 0.550 -0.651

0.440 -0.563 0.580 -0.653

0.460 -0.558 0.600 -0.585

0.470 -0.457 0.610 -0.545

0.490 -0.453 0.650 0.469

0.500 -0.384 0.700 -0.585

0.520 -0.402 0.750 -0.564

0.530 -0.302 0.820 -0.425

0.550 -0.332 0.890 -0.352

0.560 -0.285 0.900 -0.389

0.580 -0.284 0.960 -0.273

0.590 -0.318

0.600 -0.320

0.640 -0.385

0.700 -0.384

0.750 -0.060**

0.820 -0.211

0.870 -0.120

0.930 -0.212

0.960 -0.198

Lower Surface

0.020 0.089 0.020 0.480 0.020 0.447 0.020 0.660

0.110 0.060 0.060 0.355 0.060 0.411 0.060 1.094

0.230 0.160 0.090 0.256 0.090 1.085 0.110 0,277

0.400 0.013 0.120 0.223 0.120 0.057 0.250 0.122

0.490 -0.032 0.200 0.167 0.200 0.101 0.400 0.068

0.630 1.742 * * 0.260 0.111 0.250 0.163 0.490 -0.001

0.750 -0.085 0.400 0.074 0.400 0.077 0.580 -0.001

0.850 -0.024 0.490 0.024 0.490 -0.045 0.650 0.118

0.900 0.036 0.580 0.016 0.580 0.052 0.750 0.311

0.960 0.04 1 0.640 0.175 0.650 -0.064 0.830 0.435

0.750 0.087 0.750 0.025 0.900 0.468

0.870 0.095 0.890 0.384 0.960 0.281

0.930 0.058 0.930 0.295

0.960 -0.002 0.960 - 1.987"*

CN = 0.485 0.766 :_:_:_:_ 1.048

660
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-43-22-500, MINF = 0.799, Camber = 6/-1, ALPT = 13.15, BETA = -0.56, QINF = 313.5,

RNPU = 2.6E+06

r I = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -1.137 0,000 0.564 0,000 0,754** 0.010 -1.411

0.060 - 1.116 0,020 - 1.442 0,020 - 1.274 0.020 - 1.449

0.110 -1.282 0.040 - 1.153 0.060 -3.318** 0.060 -1.467

0.200 - 1.040 0.060 - 1.257 0,090 - 1.104 0.110 - 1.569

0.230 -0.897 0.090 - 1.261 0.110 -0.947 0.140 - 1.122

0.400 -0.345 0,130 -1.175 0.130 -0.822 0.190 -2.235**

0.490 -0.261 0.150 -0.983 0.150 -0,864 0.250 - 1.081

0.590 -0.305 0.200 -0.897 0.210 -0.796 0.400 -0,958

0.630 -0,268 0.250 -0.752 0,250 -0.750 0.490 -0.870

0.700 -0.180 0,260 -0.656 0,340 -0.704 0,580 -0,788

0,750 -0.225 0.280 -0.660 0,370 -0.701 0.650 -0.675

0.810 -0.262 0.290 -0.654 0,400 -0.700 0,700 -0.671

0.840 -0.238 0.310 -0.646 0.410 - 1.889"* 0.750 -0.623

0.900 -0.201 0,320 -0.657 0.430 -0,698 0,800 -0,522

0.960 -0.199 0.340 -0.559 0.440 -0,642 0.830 -0.530

0,350 -0.247** 0.460 -0,659 0,900 -0.474

0.370 -0.572 0,490 -0.592 0.960 -0.433

0.380 -0.611 0.500 -0.660

0,400 -0,545 0.520 -0.64 l

0.4 ! 0 -0.562 0.540 -0,602

0,430 -0.591 0.550 -0,630

0.440 -0,503 0.580 -0,655

0.460 -0.594 0.600 -0.587

0,470 -0.510 0.610 -0.549

0,490 -0.497 0.650 0.4 l 2

0,500 -0.502 0.700 -0,573

0.520 -0.494 0,750 -0,665

0,530 -0.441 0.820 -0.520

0.550 -0.500 0,890 -0.470

0,560 -0.395 0.900 -0.442

0,580 -0,446 0.960 -0.364

0.590 -0,414

0.600 -0.412

0.640 -0,299

0.700 -0.289

0.750 -0.061"*

0.820 -0.167

0,870 -0.207

0.930 -0.187

0,960 -0.212

Lower Surface

0,020 0.227 0,020 0.626 0.020 0.577 0.020 0,769

0.110 0.138 0,060 0,476 0.060 0.539 0,060 1.073

0.230 0.188 0,090 0,358 0.090 1.050 0.1 l0 0,374

0.400 0.055 0.120 0, 317 0.120 0.159 0.250 0.219

0.490 -0,008 0.200 0.191 0.200 0.129 0.400 0.133

0,630 1.706** 0.260 0,203 0.250 0.268 0.490 0.059

0.750 -0.1 04 0,400 0.153 0.400 0.149 0.580 0.057

0,850 -0.065 0.490 0,082 0.490 -0,028 0,650 0.178

0,900 -0.012 0.580 0.067 0,580 0.107 0.750 0.337

0,960 -0,018 0,640 0.199 0.650 -0,075 0.830 0,462

0.750 0.071 0,750 0.024 0.900 0.497

0.870 0.130 0.890 0.407 0.960 0.287

0,930 0.040 0.930 0.297

0,960 -0.037 0,960 -2.014"*

CN = 0.504 0,704 _ ¢ .-+-?- 1.149

661
Table J-2. Continued.

Flight 220, Wing sweep = 26 °, Time = 9-43-25-000, MINF = 0.794, Camber = 7/-1, ALPT = 13.18, BETA = 2.31, QINF = 319.4,

RNPU = 2.6E+06

"q= 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 -0.933 0.000 0.733 0.000 0.982" * 0.010 - 1.216

0.060 -0.873 0.020 - 1.155 0.020 - 1.105 0.020 - 1.313

0.110 -0.976 0.040 -0.894 0.060 -3.224** 0.060 - 1.409

0.200 - 1.284 0.060 - 1.063 0.090 - 1.268 0.110 - 1.566

0.230 -1.286 0.090 -1.202 0.110 -1.310 0.140 -1.391

0.400 -0.665 0.130 - 1.308 0.130 -0.895 0.190 -2.265" *

0.490 -0.503 0.150 - 1.443 0.150 -0.987 0.250 - 1.236

0.590 -0.411 0.200 - 1.492 0.210 -0.804 0.400 - 1.026

0.630 -0.356 0.250 - 1.299 0.250 -0.759 0.490 -0.895

0.700 -0.257 0.260 - 1.342 0.340 -0.750 0.580 -0.762

0.750 -0.271 0.280 - 1.164 0.370 -0.720 0.650 -0.670

0.810 -0.279 0.290 - 1.091 0.400 -0.731 0.700 -0.648

0.840 -0.264 0.310 -1.091 0.410 - 1.925"* 0.750 -0.617

0.900 -0.247 0.320 - 1.037 0.430 -0.701 0.800 -0.659

0.960 -0.224 0.340 - 1.055 0.440 -0.657 0.830 -0.543

0.350 -0,450"* 0.460 -0.661 0.900 -0.466

0.370 -0.910 0.490 -0.626 0.960 -0.429

0.380 -0.936 0.500 -0.627

0.400 -0.788 0.520 -0.602

0.410 -0.846 0.540 -0.604

0.430 -0.666 0.550 -0.618

0.440 -0.686 0.580 -0.615

0.460 -0.639 0.600 -0.565

0.470 -0.543 0.610 -0.551

0.490 -0.480 0.650 0.413

0.500 -0.363 0.700 -0.492

0.520 -0.458 0.750 -0.610

0.530 -0.251 0.820 -0.502

0.550 -0.283 0.890 -0.449

0.560 -0.219 0.900 -0.413

0.580 -0.226 0.960 -0.388

0.590 -0.245

0.600 -0.259

0.640 -0.276

0.700 -0.313

0.750 -0.055**

0.820 -0.145

0.870 -0.319

0.930 -0.294

0.960 -0.289

Lower Surface

0.020 0.268 0.020 0.692 0.020 0.592 0.020 0.761

0.110 0.197 0.060 0.514 0.060 0.578 0.060 1.065

0.230 0.179 0.090 0.412 0.090 0.959 0.110 0.383

0.400 0.105 0.120 0.378 0.120 0.216 0.250 0.264

0.490 0.032 0.200 0.182 0.200 0.126 0.400 0.205

0.630 1.603"* 0.260 0.272 0.250 0.337 0.490 0.136

0.750 -0.101 0.400 0.222 0.400 0.214 0.580 0.157

0.850 -0.070 0.490 0.147 0.490 -0.002 0.650 0.305

0.900 -0.021 0.580 0.150 0.580 0.195 0.750 0.491

0.960 -0.034 0.640 0.303 0.650 -0.068 0.830 0.596

0.750 0.155 0.750 0.032 0.900 0.64 1

0.870 0.178 0.890 0.534 0.960 0.396

0.930 0. t 13 0.930 0.422

0.960 0.010 0.960 -1.880**

CN= 0.633 0.880 _¢¢ 1.273

662
Table J-2. Continued.

Flight 220, Wing sweep = 26", Time = 9-43-28-000, MINF = 0,810, Camber = 3/6, ALPT = 6.18, BETA = -0.56, QINF = 348.7,

RNPU = 2.8E+06

r I = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.174 0.000 0,877 0.000 1.015"* 0.010 -0.928

0,060 -0.326 0.020 -0.515 0,020 -0,482 0.020 -0.874

0.110 -0.449 0.040 -0.373 0.060 -2.649"* 0.060 -0.883

0.200 -0.750 0.060 -0.652 0.090 -0.778 0.110 -0.973

0.230 -0,680 0.090 -0.667 0.110 -0.821 0.140 -1.117

0.400 -0.246 0.130 -0.710 0.130 -0.824 0.190 -2.175 **

0.490 -0.229 0,150 -0,794 0.150 -0.922 0.250 - 1.058

0.590 -0.308 0.200 -0.783 0.210 -0.883 0.400 -0.377

0.630 -0.334 0,250 -0.884 0.250 -0.911 0.490 -0.374

0.700 -0.312 0.260 -0,852 0.340 -0,906 0.580 -0,377

0.750 -0.731 0.280 -0.860 0,370 -0.469 0.650 -0.429

0.810 -0.686 0,290 -0.853 0.400 -0.338 0.700 -0.426

0.840 -0.661 0.310 -0.849 0.410 -1.864"* 0.750 -0.526

0.900 -0.201 0.320 -0.850 0.430 -0.305 0.800 -0.692

0,960 -0.095 0.340 -0.814 0,440 -0.280 0.830 -0.891

0.350 -0.291 ** 0,460 -0,288 0.900 -0.121

0.370 -0.30l 0.490 -0.254 0.960 -0.049

0.380 -0,270 0.500 -0.3 ] 2

0,400 -0.158 0.520 -0.287

0.410 -0.226 0.540 -0.296

0,430 -0.204 0.550 -0.304

0.440 -0.178 0.580 -0.332

0.460 -0.249 0.600 -0.324

0.470 -0.236 0.610 -0.343

0.490 -0.246 0.650 0.305

0.500 -0,283 0.700 -0.595

0.520 -0.291 0.750 -0,596

0.530 -0.284 0.820 -0.802

0.550 -0.333 0.890 -0.123

0.560 -0.313 0,900 -0.097

0,580 -0,316 0,960 -0.007

0,590 -0.361

0.600 -0.371

0.640 -0.576

0.700 -0.487

0.750 0.007**

0.820 -0.400

0.870 -0,429

0.930 -0.255

0.960 -0.184

Lower Surface

0.020 -0.213 0.020 0.105 0.020 0,036 0.020 0.345

0.110 -0.121 0.060 0.059 0.060 0.166 0.060 0.977

0.230 0.029 0.090 0.015 0.090 0.779 0.110 0.018

0.400 0.020 0.120 0.008 0.120 -0.196 0.250 -0.103

0.490 0.018 0.200 -0.011 0.200 -0.023 0.400 -0.106

0.630 1.369** 0.260 -0.047 0.250 -0.037 0.490 -0.165

0.750 0.115 0.400 -0.012 0.400 -0.045 0.580 -0.129

0.850 0.192 0.490 -0.025 0.490 -0.001 0.650 0.028

0.900 0.286 0.580 0.001 0.580 -0,032 0.750 0.258

0.960 0.198 0,640 0.205 0,650 -0.013 0,830 0.408

0.750 0.290 0,750 0.022 0,900 0.452

0.870 0.350 0.890 0.391 0.960 0.316

0.930 0.295 0,930 0.330

0.960 0.215 0.960 - 1.655"*

CN = 0.448 0.579 _::[::[:+-, 0.703

663
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-18-000, MINF = 0.859, Camber = 5/10, ALPT = 3.98, BETA = 0.22, QINF = 303.4,

RNPU = 2.4E+06, CNWP = 0.3052

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.347 0.000 0.583 0.000 3.469** 0.010 -0.032

0.060 -0.023 0.020 0.212 0.020 0.246 0.020 0.006

0.110 -0.274 0.040 0.124 0.060 -3.910 ** 0.060 -0.379

0.200 -0.694 0.060 -0.111 0.090 -0.245 0.110 -0.518

0.230 -0.546 0.090 -0.247 0.110 -0.428 0.140 -0.810

0.400 -0.154 0.130 -0.422 0.130 -0.569 0.190 - 1.935" *

0.490 -0.185 0.150 -0.608 0.150 -0.723 0.250 -0.593

0.590 -0.275 0.200 -0.645 0.210 -0.677 0.400 -0.329

0.630 -0.286 0.250 -0.700 0.250 -0.688 0.490 -0.286

0.700 -0.378 0.260 -0.671 0.340 -0.674 0.580 -0.308

0.750 -0.649 0.280 -0.664 0.370 -0.349 0.650 -0.377

0.810 -0.624 0.290 -0.651 0.400 -0.291 0.700 -0.352

0.840 -0.589 0.310 -0.654 0.410 2.528"* 0.750 -0.474

0.900 -0.270 0.320 -0.673 0.430 -0.296 0.800 -1.015

0.960 -0.289 0.340 -0.615 0.440 -0.256 0.830 -0.608

0.350 -0.317"* 0.460 -0.280 0.900 -0.399

0.370 -0.297 0.490 -0.208 0.960 -0.396

0.380 -0.248 0.500 -0.304

0.400 -0.136 0.520 -0.266

0.410 -0.203 0.540 -0.252

0.430 -0.185 0.550 -0.229

0.440 -0.187 0.580 -0.213

0.460 -0.200 0.600 -0.259

0.470 -0.208 0.610 -0.293

0.490 -0.217 0.650 2.115"*

0.500 -0.237 0.700 -0.526

0.520 -0.293 0.750 -0.551

0.530 -0.247 0.820 -0.859

0.550 -0.313 0.890 -0.375

0.560 -0.263 0.900 -0.451

0.580 -0.285 0.960 -0.365

0.590 -0.303

0.600 -0.315

0.640 -0.493

0.700 -0.482

0.750 -0.005"*

0.820 -0.539

0.870 -0.332

0.930 -0.298

0.960 -0.297

Lower Surface

0.020 - 1.353 0.020 - 1.186 0.020 -0.994 0.020 -0.193

0.110 -0.146 0.060 -0.378 0.060 -0.114 0.060 1.110 r*

0.230 -0.050 0.090 -0.192 0.090 1.998" * 0.110 -0.109

0.400 0.015 0.120 -0.112 0.120 -0.304 0.250 -0.229

0.490 0.052 0,200 -0.057 0.200 -0.073 0.400 -0.206

0.630 2.835'* 0.260 -0.088 0.250 -0.141 0.490 -0.210

0.750 0.154 0.400 -0.04 1 0.400 -0.101 0.580 -0.129

0.850 0.239 0.490 -0.014 0.490 -0.021 0.650 0.119

0.900 0.301 0.580 0.053 0.580 0.022 0.750 0.296

0.960 0.129 0.640 0.264 0.650 -0.042 0.830 0.461

0.750 0.347 0.750 -0.021 0.900 0.502

0.870 0.410 0.890 0.415 0.960 0.352

0.930 0.287 0.930 0.338

0.960 0.183 0.960 -2.073**

CN = 0.380 0.452 0.433 0.462

664
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-22-500, MINF = 0.864, Camber = 5/10, ALPT = 5.10, BETA = 0.14. QINF = 307.9,

RNPU = 2.4E+06, CNWP = 0.3560

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x,/c CP x/c CP

0,020 0.271 0.000 0.667 0.000 3.41 l ** 0.010 -0. l 0 l

0.060 -0.053 0.020 0.109 0.020 0.118 0.020 -0.109

0.110 -0.301 0.040 0.028 0.060 -3.862 * * 0.060 -0.504

0.200 -0,729 0.060 -0.208 0.090 -0.331 0.110 -0,662

0.230 -0.604 0.090 -0.296 0.110 -0.483 0. 140 -0.861

0.400 -0,358 0.130 -0.482 0.130 -0.612 0.190 -1.915"*

0.490 -0.140 0.150 -0.654 0.150 -0.763 0.250 -0.798

0.590 -0.238 0.200 -0.699 0.210 -0,739 0.400 -0.632

0.630 -0.268 0.250 -0.755 0.250 -0.771 0.490 -0.382

0.700 -0.274 0.260 -0.755 0.340 -0.804 0.580 -0.373

0.750 -0.898 0.280 -0.733 0.370 -0.766 0.650 -0.444

0.810 -0.853 0.290 -0.724 0,400 -0,770 0.700 -0.415

0.840 -0.870 0.310 -0.749 0,410 2,483"* 0.750 -0.532

0.900 -0.309 0.320 -0.749 0,430 -0,783 0.800 -0.736

0.960 -0.314 0.340 -0.703 0.440 -0.763 0.830 -0.471

0.350 -0.373** 0.460 -0.764 0.900 -0.352

0.370 -0.721 0.490 -0.529 0.960 -0.375

0.380 -0.753 0.500 -0.444

0,400 -0.655 0.520 -0.402

0.410 -0.720 0.540 -0.363

0.430 -0.683 0.550 -0.309

0.440 -0.702 0.580 -0.287

0,460 -0.726 0_600 -0.322

0.470 -0.661 0.610 -0.337

0.490 -0.715 0,650 2.076"*

0.500 -0,730 0,700 -0.523

0.520 -0.780 0,750 -0.530

0.530 -0.684 0.820 -0.753

0,550 -0.476 0.890 -0.315

0.560 -0.268 0.900 -0.366

0.580 -0.17l 0.960 -0,313

0.590 -0.199

0.600 -0.180

0.640 -0.278

0.700 -0.315

0.750 -0.009"*

0.820 -0.517

0.870 -0.442

0.930 -0.288

0.960 -0.279

Lower Surface

0,020 - 1.128 0.020 -0.935 0,020 -0.716 0.020 0.052

0.110 -0.165 0.060 -0.129 0,060 0.007 0.060 1.100"*

0.230 -0.028 0.090 -0.130 0.090 1.960"* 0.110 -0.067

0.400 -0.034 0.120 -0.083 0.120 -0.233 0.250 -0.167

0.490 0.051 0.200 -0.015 0,200 -0.047 0.400 -0.162

0.630 2.786'* 0.260 -0.060 0.250 -0.098 0.490 -0.164

0.750 0.170 0.400 -0,026 0.400 -0.079 0.580 -0.111

0.850 0.231 0.490 -0.011 0.490 -0.007 0,650 0. l 16

0.900 0.302 0.580 0.055 0.580 0.021 0.750 0.302

0.960 0.135 0,640 0.281 0.650 -0.028 0.830 0.467

0.750 0.341 0.750 -0.029 0.900 0.507

0.870 0.405 0.890 0.436 0.960 0.348

0.930 0.318 0.930 0.354

0.960 0.194 0.960 -2.051 **

CN = 0.447 0.568 0.543 0.576

665
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-29-500, MINF = 0.864, Camber = 5/10, ALPT = 6.05, BETA = 0,19, QINF = 309.6,

RNPU = 2.4E+06, CNWP = 0,3875

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.192 0,000 0.735 0.000 1.027"* 0.010 -0.306

0.060 -0.124 0.020 0.041 0.020 0,023 0.020 -0.288

0. l 10 -0.415 0.040 -0.043 0.060 -2.657 ** 0.060 -0.656

0,200 -0.753 0.060 -0,260 0.090 -0.453 0.110 -0.813

0.230 -0.697 0.090 -0.357 0.110 -0.509 0.140 - 1.002

0,400 -0.596 0.130 -0.536 0.130 -0.648 0.190 -1.912"*

0.490 -0.471 0.150 -0.695 0,150 -0.801 0.250 -0.978

0.590 -0,349 0.200 -0.738 0.210 -0.773 0.400 -0.716

0.630 -0.300 0.250 -0.808 0.250 -0.837 0.490 -0.510

0.700 -0.353 0.260 -0.804 0.340 -0.851 0.580 -0.455

0.750 -0.882 0.280 -0.796 0.370 -0.845 0.650 -0.465

0.810 -0.856 0.290 -0.787 0.400 -0.873 0.700 -0,466

0.840 -0.873 0.310 -0.800 0.410 2.462** 0.750 -0.571

0.900 -0.346 0.320 -0.803 0.430 -0.859 0.800 -0.591

0.960 -0.360 0.340 -0.772 0,440 -0.832 0.830 -0.452

0.350 -0.379** 0.460 -0.852 0.900 -0.358

0.370 -0.778 0.490 -0.833 0.960 -0.358

0.380 -0.822 0.500 -0.881

0.400 -0.740 0.520 -0.850

0.410 -0.794 0.540 -0.841

0.430 -0.740 0.550 -0.814

0.440 -0.753 0.580 -0.651

0.460 -0.785 0.600 -0,523

0.470 -0.770 0.610 -0.472

0.490 -0.785 0.650 0.425"*

0.500 -0.804 0.700 -0.616

0.520 -0.792 0.750 -0.616

0.530 -0.780 0.820 -0.426

0.550 -0.818 0.890 -0.291

0.560 -0.763 0.900 -0.341

0.580 -0.783 0.960 -0.267

0.590 -0.823

0.600 -0.810

0.640 -0.838

0.700 -0.824

0.750 -0.003**

0.820 -0.362

0.870 -0.231

0.930 -0.233

0.960 -0.239

Lower Surface

0.020 -0.598 0.020 -0.310 0.020 -0.222 0.020 0.156

0.110 -0.164 0.060 -0.034 0.060 0.052 0.060 1.080"*

0.230 -0.003 0.090 -0.066 0.090 1.942'* 0.110 -0.020

0.400 0.013 0.120 -0.040 0.120 -0.188 0.250 -0.137

0.490 0.036 0.200 -0.004 0.200 -0.027 0.400 -0.147

0.630 2.763"* 0.260 -0.046 0.250 -0.076 0.490 -0.171

0.750 0.175 0.400 -0.005 0.400 -0.043 0.580 -0.089

0.850 0.240 0.490 0.017 0.490 -0.008 0.650 0.108

0.900 0.304 0.580 0.069 0.580 0.013 0.750 0.316

0.960 0.125 0.640 0.283 0.650 -0.021 0.830 0.455

0.750 0,338 0.750 -0.022 0,900 0.500

0.870 0.414 0.890 0.451 0.960 0.333

0.930 0.340 0.930 0.366

0.960 0.217 0.960 -1.907"*

CN -- 0.563 0.709 0.635 0.669

666
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-34-000, MINF = 0.861, Camber = 5/10, ALPT = 7.05, BETA = 0.3l, QINF = 308.5,

RNPU = 2.4E+06, CNWP = 0.4677

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.085 0.000 0.803 0.000 1.026"* 0,010 -0.716

0,060 -0.198 0.020 -0.171 0.020 -0.115 0.020 -0.473

0.110 -0.397 0.040 -0.155 0.060 -2.711 ** 0.060 -0.732

0.200 -0,799 0.060 -0.373 0.090 -0.564 0.110 -0.922

0.230 -0.782 0.090 -0.440 0.110 -0.634 0.140 - 1.102

0.400 -0,700 0.130 -0.599 0.130 -0.734 0.190 - 1.925" *

0.490 -0.564 0.150 -0.752 0.150 -0.875 0.250 - 1.070

0.590 -0.536 0.200 -0.787 0.210 -0.849 0.400 -0.771

0,630 -0.390 0.250 -0.852 0.250 -0.906 0.490 -0.668

0.700 -0.390 0.260 -0.864 0.340 -0.919 0.580 -0.550

0.750 -0.771 0.280 -0.867 0.370 -0.908 0.650 -0.552

0.810 -0.781 0.290 -0.850 0.400 -0,933 0.700 -0.550

0.840 -0.832 0.310 -0.863 0.410 2,465** 0.750 -0.650

0.900 -0.430 0.320 -0.871 0.430 -0.927 0.800 -0.558

0.960 -0.429 0.340 -0.840 0.440 -0.906 0.830 -0.419

0.350 -0.383** 0.460 -0.925 0.900 -0.351

0.370 -0.840 0.490 -0.872 0.960 -0.351

0.380 -0.888 0.500 -0.950

0.400 -0.809 0.520 -0.943

0.410 -0.860 0.540 -0.929

0.430 -0.822 0.550 -0.964

0.440 -0.830 0.580 -0.952

0.460 -0.860 0.600 -0.879

0.470 -0.827 0.610 -0.843

0.490 -0,860 0.650 0.247**

0.500 -0.862 0.700 -0.738

0.520 -0.870 0,750 -0.740

0.530 -0.853 0.820 -0.342

0.550 -0.893 0.890 -0.280

0,560 -0.842 0.900 -0.313

0.580 -0.856 0.960 -0.250

0.590 -0.908

0,600 -0,919

0,640 -0.909

0.700 -0.453

0.750 0,009"*

0.820 -0.264

0.870 -0.259

0.930 -0.272

0.960 -0.275

Lower Surface

0,020 -0.421 0.020 -0.183 0.020 -0.078 0.020 0.239

0.110 -0.124 0.060 0.047 0.060 0.118 0.060 1.092"*

0.230 0.035 0.090 0.005 0.090 1.943"* 0.110 0.047

0.400 0.021 0.120 0.010 0.120 -0.114 0.250 -0.085

0.490 0.044 0.200 0,039 0.200 0.007 0,400 -0.1 04

0.630 2.767"* 0,260 -0.010 0.250 -0,019 0,490 -0.134

0.750 0.162 0.400 0.014 0.400 -0.016 0.580 -0.067

0.850 0,245 0.490 0.015 0.490 0,001 0.650 0.124

0.900 0.298 0.580 0.070 0.580 0.028 0.750 0.340

0.960 0.130 0.640 0.281 0.650 -0.006 0.830 0.473

0.750 0.340 0.750 0.001 0.900 0.510

0.870 0.410 0.890 0.457 0,960 0.336

0.930 0.314 0.930 0.368

0.960 0.209 0.960 - 1.906 **

CN = 0.627 0.734 0.742 0.773

667
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-37-500, MINF -- 0.858, Camber = 5/10, ALPT = 8.16, BETA = 0.02, QINF = 307.9,

RNPU = 2.4E+06, CNWP = 0.5349

lq = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.083 0.000 0.854 0.000 0.916 ** 0.010 -0.781

0.060 -0.336 0.020 -0.283 0.020 -0.300 0.020 -0.74 l

0.110 -0.414 0.040 -0.262 0.060 -2.896** 0.060 -0.832

0.200 -0.814 0.060 -0.522 0.090 -0.694 0.110 - 1.016

0.230 -0.801 0.090 -0.607 0.110 -0.750 0.140 - 1.121

0.400 -0.778 0.130 -0.709 0.130 -0.821 0.190 - 1.940* *

0.490 -0.640 0.150 -0.827 0.150 -0.966 0.250 - 1.179

0.590 -0.624 0.200 -0.854 0.210 -0.928 0.400 -0.843

0.630 -0.478 0.250 -0.937 0.250 -0.985 0.490 -0.725

0.700 -0.502 0.260 -0.921 0.340 - 1.006 0.580 -0.635

0.750 -0.747 0.280 -0.927 0.370 -0.976 0.650 -0.634

0.810 -0.751 0.290 -0.918 0.400 - 1.003 0.700 -0.629

0.840 -0.722 0.310 -0.937 0.410 2.459** 0.750 -0.725

0.900 -0.498 0.320 -0.945 0.430 - 1.013 0.800 -0.548

0.960 -0.474 0.340 -0.903 0.440 -0.981 0.830 -0.411

0.350 -0.396** 0.460 -0.990 0.900 -0.355

0.370 -0.906 0.490 -0.959 0.960 -0.358

0.380 -0.952 0.500 -I .012

0.400 -0.882 0.520 -0.993

0.410 -0.926 0.540 -0.992

0.430 -0.907 0.550 -l.019

0.440 -0.905 0.580 - 1.035

0.460 -0.937 0.600 -0.957

0.470 -0.906 0.610 -0.960

0.490 -0.928 0.650 -0.016'*

0.500 -0.941 0.700 - 1.029

0.520 -0.929 0.750 -0.658

0.530 -0.916 0.820 -0.357

0.550 -0.956 0.890 -0.313

0.560 -0.898 0.900 -0.368

0.580 -0.924 0.960 -0.308

0.590 -0.974

0.600 -0.97 ]

0.640 -0.374

0.700 -0.339

0.750 0.034**

0.820 -0,276

0.870 -0.285

0.930 -0.283

0.960 -0.279

Lower Surface

0.020 -0.255 0.020 0.025 0.020 0.091 0.020 0.378

0.110 -0.067 0.060 0.149 0.060 0.194 0.060 1.112"*

0.230 0.086 0.090 0.085 0.090 1.936 ** 0.110 0.1 04

0.400 0.043 0.120 0.085 0.120 -0.034 0.250 -0.009

0.490 0.040 0.200 0.089 0.200 0.044 0.400 -0.044

0.630 2.761 ** 0.260 0.039 0,250 0.042 0.490 -0.080

0.750 0.158 0.400 0.051 0.400 0.007 0.580 -0.044

0.850 0.223 0.490 0.030 0.490 0.004 0.650 0.149

0.900 0.301 0.580 0.092 0.580 0.039 0.750 0.344

0.960 0.124 0.640 0.296 0.650 -0.003 0.830 0.483

0.750 0.350 0.750 -0.010 0.900 0.526

0.870 0.420 0.890 0.462 0.960 0.335

0.930 0.315 0.930 0.379

0.960 0.213 0.960 - 1.900"*

CN = 0.688 0.783 0.845 0.876

668
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-38-000, MINF = 0.857, Camber = 5/9, ALPT = 8.41, BETA = 0.08, QINF = 307.7,

RNPU = 2.4E+06, CNWP = 0.5392

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.109 0.000 0.861 0.000 0.969"* 0.010 -0.783

0.060 -0.357 0.020 -0.340 0.020 -0.348 0.020 -0.804

0.110 -0.540 0.040 -0.285 0.060 -2.809** 0.060 -0.860

0.200 -0.834 0.060 -0.539 0.090 -0.737 0.110 - 1.023

0.230 -0.786 0.090 -0.643 0.110 -0.778 0.140 - 1.175

0.400 -0.795 0.130 -0.731 0.130 -0.858 0.190 - 1.943" *

0.490 -0.664 0.150 -0.861 0.150 -0.985 0.250 -1.196

0.590 -0.630 0.200 -0.884 0.210 -0.935 0.400 -0.852

0.630 -0.525 0.250 -0.949 0.250 - 1.008 0.490 -0.746

0.700 -0.548 0.260 -0.943 0.340 - 1.023 0.580 -0.647

0.750 -0.681 0.280 -0.938 0.370 -0.987 0.650 -0.656

0.810 -0.687 0.290 -0.938 0.400 - 1.027 0.700 -0.637

0.840 -0.689 0.310 -0.961 0.410 2.458** 0.750 -0.735

0.900 -0.449 0.320 -0.969 0.430 - 1.030 0.800 -0.550

0.960 -0.394 0.340 -0.926 0.440 - 1.004 0.830 -0.449

0.350 -0.383"* 0.460 - 1.014 0.900 -0.340

0.370 -0.926 0.490 -0.983 0.960 -0.356

0.380 -0.972 0.500 - 1.037

0.400 -0.892 0.520 - 1.0 ! 2

0.410 -0.944 0.540 - 1.022

0.430 -0.927 0.550 - 1.046

0,440 -0,922 0.580 - 1.092

0,460 -0,962 0.600 -0.983

0.470 -0.914 0.610 -0.988

0.490 -0.953 0.650 0.153"*

0.500 -0.965 0.700 -0.699

0.520 -0.947 0.750 -0.596

0.530 -0.939 0.820 -0.408

0.550 -0.985 0.890 -0.359

0.560 -0.919 0.900 -0.412

0.580 -0.946 0.960 -0.337

0.590 -0.994

0.600 -0.959

0.640 -0.364

0.700 -0.349

0.750 0.022**

0.820 -0.270

0.870 -0.298

0.930 -0.289

0.960 -0.277

Lower Surface

0.020 -0.220 0.020 0.061 0.020 0.119 0.020 0.410

0. 110 -0.057 0.060 0.162 0.060 0.224 0.060 1.111 **

0.230 0.095 0.090 0.100 0.090 1.935" * 0.110 0.108

0.400 0.055 0.120 0.090 0.120 -0.011 0.250 0.001

0.490 0.031 0.200 0.094 0.200 0.062 0.400 -0.039

0.630 2.761 ** 0.260 0.048 0.250 0.032 0.490 -0.075

0.750 0.133 0.400 0.052 0.400 0.005 0.580 -0.027

0.850 0.194 0.490 0.042 0.490 0.009 0.650 0.155

0.900 0.270 0.580 0.086 0.580 0.058 0.750 0.352

0.960 0.114 0.640 0.283 0.650 0.003 0.830 0.482

0.750 0.324 0.750 -0.012 0.900 0.527

0.870 0.391 0.890 0.463 0.960 0.347

0.930 0.292 0.930 0.370

0.960 0.179 0.960 - 1.895"*

CN = 0.684 0.792 0.848 0.898

669
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-38-500, MINF = 0.857, Camber = 5/7, ALPT = 8.88, BETA = 0.43, QINF = 307.8,

RNPU = 2.4E+06, CNWP = 0.5397

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0,020 -0.197 0.000 0,850 0,000 0.979"* 0.010 -0,745

0,060 -0.415 0.020 -0.454 0.020 -0,421 0.020 -0.847

0. l 10 -0.599 0.040 -0.338 0,060 -2.849"* 0.060 -0,924

0.200 -0.874 0.060 -0.572 0,099 -0.780 0.110 - 1,045

0.230 -0.807 0,090 -0.688 0.110 -0,834 0.140 - 1.213

0.400 -0.820 0.130 -0.785 0.130 -0,896 0.190 - 1.946 **

0.490 -0.706 0.150 -0.899 0.150 -0.996 0.250 - 1.226

0.590 -0,693 0.200 -0.925 0.210 -0.974 0.400 -0.882

0.630 -0.577 0.250 -0,977 0.250 - 1.039 0.490 -0,767

0.700 -0.213 0.260 -0.972 0.340 - t .041 0.580 -0.711

0.750 -0.601 0.280 -0.975 0.370 -1.028 0.650 -0.679

0.810 -0.616 0.290 -0.975 0.400 - 1.052 0.700 -0.670

0.840 -0.634 0.310 -0.992 0.410 2.454** 0.750 -0.752

0.900 -0.425 0.320 - 1.002 0.430 - 1.048 0.800 -0.553

0.960 -0.300 0.340 -0.962 0.440 - 1.026 0.830 -0.434

0.350 -0.391 * * 0.460 - 1.044 0.900 -0.330

0.370 -0.961 0.490 - 1.015 0.960 -0.331

0.380 -1.011 0,500 -1.058

0.400 -0.905 0.520 - 1.047

0,410 -0.978 0.540 - 1.037

0.430 -0.952 0.550 - 1.072

0,440 -0.957 0.580 - 1. I 12

0,460 - 1.000 0.600 - 1,021

0.470 -0.968 0,610 -0.991

0,490 -0.987 0.650 0.469**

0.500 - 1.000 0.700 -0.534

0.520 - 1.002 0.750 -0,563

0.530 -0.983 0.820 -0.444

0.550 - 1.006 0,890 -0,397

0.560 -0.723 0.900 -0.430

0.580 -0.604 0.960 -0.344

0.590 -0.491

0.600 -0.463

0.640 -0.341

0.700 -0.352

0,750 0.011 **

0.820 -0.299

0,870 -0.333

0.930 -0.299

0.960 -0.313

Lower Surface

0.020 -0.147 0.020 0.126 0.020 0.177 0.020 0.487

0.110 -0.047 0.060 0.210 0.060 0.253 0.060 1.107"*

0.230 0.103 0.090 0.125 0.090 1,931"* 0.110 0.149

0.400 0.016 0.120 0.115 0.120 0.007 0.250 0.018

0.490 -0.023 0,200 0.105 0,200 0.072 0,400 -0.021

0.630 2.757"* 0,260 0,055 0,250 0.072 0.490 -0,064

0.750 0.070 0.400 0,053 0,400 0,036 0.580 -0,025

0.850 0.139 0.490 0.032 0.490 -0.001 0,650 0.155

0.900 0.219 0.580 0.064 0.580 0,055 0.750 0,348

0.960 0.102 0.640 0.258 0.650 -0.007 0.830 0.487

0.750 0.257 0.750 -0.015 0.900 0.530

0,870 0.298 0.890 0.464 0.960 0,344

0,930 0.193 0.930 0,364

0.960 0,076 0.960 - 1.941 **

CN = 0.643 0.772 0.866 0.933

670
Table J-2. Continued.

Hight 221, Wing sweep = 26 °, Time = 13-15-39-000, MINF = 0.856, Camber = 5/4, ALPT = 9.27, BETA = -0.07, QINF = 307.8,

RNPU = 2.4E+06, CNWP = 0.4812

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.246 0.000 0.864 0.000 0.963 ** 0.010 -0.707

0.060 -0.444 0.020 -0.511 0.020 -0.408 0.020 -0.870

0.110 -0.634 0.040 -0.354 0.060 -2.820"* 0.060 -0.967

0.200 -0.889 0.060 -0.604 0.090 -0.802 0.110 - 1.075

0.230 -0.862 0.090 -0.732 0.110 -0.87 l 0.140 - 1.232

0.400 -0.859 0.130 -0.825 0.130 -0.921 0.190 - 1.947 **

0.490 -0.743 0.150 -0.932 0.150 - 1.055 0.250 - 1.242

0.590 -0.497 0.200 -0.960 0.210 -0.998 0.400 -0.904

0.630 -0.231 0.250 - 1.004 0.250 - 1.058 0.490 -0.796

0.700 -0.204 0.260 - 1.000 0.340 - 1.072 0.580 -0.713

0.750 -0.440 0.280 - 1.010 0.370 - 1.037 0.650 -0.700

0,810 -0.458 0.290 -0.993 0.400 - 1.075 0.700 -0.692

0.840 -0.469 0.310 - 1.028 0.410 2.452"* 0.750 -0.732

0.900 -0.405 0.320 - 1.034 0.430 - 1.079 0.800 -0.54 I

0.960 -0,205 0.340 -0.990 0.440 - 1.048 0.830 -0.409

0.350 -0.393"* 0.460 - 1.073 0.900 -0.349

0.370 -0.991 0.490 - 1.047 0.960 -0.337

0,380 - 1.039 0.500 - 1.088

0.400 -0.960 0.520 - 1.065

0.410 - 1.008 0.540 - 1.066

0.430 -0.988 0.550 - 1.086

0.440 -0.986 0.580 -0.789

0.460 - 1.025 0.600 -0.607

0.470 -0.976 0.610 -0.534

0.490 -0.973 0.650 0.499"*

0.500 -0.832 0.700 -0.525

0.520 -0.770 0.750 -0.569

0.530 -0.555 0.820 -0.467

0.550 -0.512 0.890 -0.406

0.560 -0.447 0.900 -0.437

0.580 -0.457 0.960 -0.346

0.590 -0.454

0.600 -0.446

0.640 -0.369

0.700 -0.364

0.750 -0.019"*

0.820 -0,312

0.870 -0.356

0.930 -0.309

0.960 -0.343

Lower Surface

0.020 -0.101 0.020 0.182 0.020 0.236 0.020 0.516

0.110 -0.023 0.060 0.226 0.060 0.289 0.060 1.105**

0.230 0.116 0.090 0.152 0.090 1.929'* 0.110 0.176

0.400 0.003 0,120 0.138 0.120 0.026 0.250 0.038

0.490 -0.025 0.200 0.117 0.200 0.083 0.400 -0.001

0.630 2.754** 0.260 0.071 0.250 0.092 0.490 -0.051

0.750 -0.003 0.400 0.051 0.400 0.043 0.580 -0.007

0.850 0.058 0.490 0.026 0.490 -0,017 0.650 0.164

0.900 0.141 0.580 0.043 0.580 0.057 0.750 0.341

0.960 0.076 0.640 0.233 0.650 -0.030 0.830 0.493

0.750 0.174 0.750 -0.017 0.900 0.530

0.870 0.197 0.890 0.455 0.960 0.348

0.930 0.106 0.930 0.358

0.960 0.002 0.960 - 1.934**

CN = 0.580 0.743 0.846 0.959

671
Table J-2. Continued.

Hight 221, Wing sweep = 26 °, Time = 13-15-40-000, MINF = 0.855, Camber = 5/3, ALPT = 9.57, BETA = 0.86, QINF = 307.5,

RNPU = 2.4E+06, CNWP = 0.4201

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0321 0.003 0.858 0.000 0.95 l ** 0.010 -0.856

0.060 -0.493 0.020 -0.532 0.020 -0.522 0.020 -0.932

O. 110 -0.675 0.040 -0.392 0.060 -2.912 ** 0.060 - 1.029

0.200 -0.922 0.060 -0.656 0.090 -0.844 O.110 - 1.145

0.230 -0.893 0,090 -0.770 0.110 -0.895 0.140 - 1.288

0.400 -0.880 0.130 -0.863 0.130 -0,965 0.190 - 1.955"*

0.490 -0.786 0.150 -0.977 0.150 - 1.085 0.250 - 1.291

0.590 -0.353 0.200 -0.995 0.210 - 1.042 0.400 -0.959

0.630 -0.233 0.250 - 1.035 0.250 - 1.105 0.490 -0.836

0.700 -0.210 0.260 -1.048 0.340 -1.108 0.580 -0.775

0.750 -0.412 0.280 - 1.034 0.370 - 1.112 0.650 -0.751

0.810 -0.416 0.290 - 1.034 0.400 - 1.118 0.700 -0.733

0.840 -0.403 0.310 - 1.072 0.410 2.448** 0.750 -0.718

0.900 -0.389 0.320 - 1.063 0.430 - 1.101 0.800 -0.527

0.960 -0.205 0.340 -1.035 0.440 - 1.090 0.830 -0.395

0.350 -0.400"* 0.460 - 1.110 0.900 -0.361

0.370 - 1.04 1 0.490 - 1.068 0.960 -0.362

0.380 - 1.073 0.500 -0.916

0.400 - 1.003 0.520 -0.726

0.410 - 1.031 0.540 -0.636

0.430 - 1.009 0,550 -0.630

0.440 -0.945 0.580 -0,606

0.460 -0.757 0.600 -0.55 l

0.470 -0.593 0.610 -0.529

0.490 -0.564 0.650 0.475"*

0.500 -0.529 0.700 -0.518

0.520 -0.526 0.750 -0.568

0.530 -0.500 0.820 -0.467

0.550 -0.489 0.890 -0.423

0.560 -0.468 0.900 -0.438

0.580 -0.471 0.960 -0.356

0.590 -0.510

0.600 -0.491

0.640 -0.415

0.700 -0.417

0.750 -0.053"*

0.820 -0.370

0.870 -0.391

0.930 -0.362

0.960 -0.360

Lower Surface

0.020 -0.088 0.020 0.209 0.020 0.230 0.020 0.502

0.110 -0.016 0.060 0.232 0.060 0.309 0.060 1.086**

0.230 0.117 0.090 0.154 0.090 1.925"* 0.110 0.160

0.400 0.001 0.120 0.164 0.120 0.045 0.250 0.048

0.490 -0.060 0.200 0.108 0.200 0.090 0.400 0.000

0.630 2.751 ** 0.260 0.065 0.250 0.085 0.490 -0.043

0.750 -0.072 0.400 0.045 0.400 0.033 0.580 -0.004

0.850 0.008 0.490 0.005 0.490 -0.048 0.650 0.1 44

0.900 0.103 0,580 0.019 0,580 0.054 0.750 0.359

0.960 0.052 0.640 0.206 0.650 -0.043 0.830 0.481

0.750 0.130 0.750 -0.023 0.900 0.519

0.870 0.168 0.890 0.441 0.960 0.342

0.930 0.079 0.930 0.352

0.960 -0.032 0.960 -1.958**

CN = 0.553 0.735 0.831 0.996

672
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-41-500, MINF = 0,852, Camber = 5/2, ALPT = 10.29, BETA = 0.48, QINF = 307.1,

RNPU = 2.4E+06, CNWP = 0.3694

I1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.503 0.000 0.824 0.000 0.992"* 0,010 -0.907

0.060 -0,574 0.020 -0,643 0.020 -0.752 0.020 -0,954

0. 110 -0.682 0.040 -0.621 0.060 -2.965** 0,060 - 1.086

0.200 -0.941 0.060 -0.697 0.090 -0.876 0.110 - 1.184

0.230 -0.937 0.090 -0.806 0.110 -0.952 0.140 - 1.320

0.400 -0.858 0.130 -0,920 0.130 - 1.004 0.190 - 1.967"*

0.490 -0.653 0,150 -1.014 0.150 -1.115 0,250 -1.350

0.590 -0.285 0.200 - 1.04 1 0.210 - 1.069 0,400 - 1.001

0.630 -0.255 0.250 - 1.081 0,250 - 1.150 0.490 -0.799

0,700 -0.227 0.260 - 1.083 0.340 - 1.149 0.580 -0.685

0.750 -0,335 0.280 - 1,082 0.370 - 1.147 0.650 -0.614

0.810 -0.320 0.290 - 1.073 0.400 - 1.057 0.700 -0,593

0.840 -0.319 0.310 - 1.106 0.410 2.442** 0,750 -0.615

0.900 -0,326 0.320 - 1.107 0.430 -0.818 0.800 -0.531

0.960 -0.213 0.340 - 1.066 0.440 -0,729 0.830 -0.535

0.350 -0.395** 0.460 -0.697 0.900 -0,483

0,370 -0.912 0.490 -0.571 0.960 -0,406

0.380 -0.842 0.500 -0.668

0,400 -0.653 0.520 -0.625

0.410 -0.659 0.540 -0.617

0.430 -0,573 0,550 -0.623

0.440 -0.580 0.580 -0.672

0.460 -0.552 0,600 -0.568

0.470 -0.517 0.610 -0.549

0.490 -0.526 0.650 0.467**

0.500 -0.515 0.700 -0,520

0.520 -0.538 0,750 -0.560

0.530 -0.502 0.820 -0.444

0,550 -0.523 0.890 -0.420

0.560 -0.473 0.900 -0.398

0.580 -0.485 0.960 -0.323

0.590 -0.508

0.600 -0.486

0.640 -0.403

0.700 -0,409

0.750 -0.065**

0.820 -0.387

0,870 -0.393

0.930 -0.390

0.960 -0.377

Lower Surface

0,020 0.034 0.020 0.311 0,020 0.327 0,020 0,609

0.110 0.009 0.060 0,303 0.060 0.353 0,060 1.092**

0.230 0.133 0.090 0,208 0.090 1.918"* 0.110 0.220

0.400 -0.001 0.120 0.184 0.120 0.092 0.250 0.085

0.490 -0.069 0.200 0.145 0.200 0.115 0.400 0.030

0.630 2,746"* 0.260 0.106 0.250 0.134 0.490 -0,016

0.750 -0.075 0.400 0.058 0.400 0.047 0,580 0.016

0.850 -0.028 0.490 0.036 0.490 -0.046 0.650 0.164

0.900 0,045 0.580 0.039 0.580 0.067 0.750 0.365

0,960 0.019 0.640 0.218 0,650 -0.066 0.830 0,493

0.750 0.126 0.750 -0.033 0.900 0.519

0,870 0.143 0.890 0.455 0,960 0.342

0,930 0.066 0.930 0.351

0,960 -0.023 0.960 - 1.967 **

CN = 0.526 0,741 0.817 1.028

673
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-42-000, MINF = 0.851, Camber = 5/0, ALPT = 10.90, BETA = 0.60, QINF = 307.2,

RNPU -- 2.4E+06, CNWP = 0.3690

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.694 0.000 0.808 0.000 0.913 ** 0.010 -0.978

0.060 -0.697 0.020 -0.832 0.020 -0.849 0.020 - 1.059

0.110 -0.742 0.040 -0.692 0.060 -3.044 ** 0.060 - 1.137

0.200 -0.969 0.060 -0.807 0.090 -0.961 0.110 - 1.245

0.230 -0.977 0.090 -0.890 0.110 -1.017 0.140 -1.361

0.400 -0.953 0.130 -0.965 0.130 - 1.066 0.190 - 1.971 **

0.490 -0.414 0.150 - 1.070 0.150 - 1.185 0.250 - 1.145

0.590 -0.319 0.200 - 1.094 0.210 - 1.127 0.400 -0.856

0.630 -0.292 0.250 -0.911 0.250 - 1.181 0.490 -0.785

0.700 -0.250 0.260 -0.968 0.340 - 1.079 0.580 -0.709

0.750 -0.313 0.280 -0.847 0.370 -0.914 0.650 -0.647

0.810 -0.317 0.290 -0.771 0.400 -0.736 0.700 -0.627

0.840 -0.308 0.310 -0.808 0.410 2.438"* 0.750 -0.597

0.900 -0.315 0.320 -0.790 0.430 -0.705 0.800 -0.540

0.960 -0.210 0.340 -0.731 0.440 -0.673 0.830 -0.566

0.350 -0.259** 0.460 -0.674 0.900 -0.522

0.370 -0.620 0.490 -0.656 0.960 -0.481

0.380 -0.658 0.500 -0.663

0.400 -0.592 0.520 -0.628

0.410 -0.609 0.540 -0.621

0.430 -0.588 0.550 -0.626

0.440 -0.581 0.580 -0.625

0.460 -0.579 0.600 -0.571

0.470 -0.546 0.610 -0.540

0.490 -0.569 0.650 0.483**

0.500 -0.530 0.700 -0.521

0.520 -0.587 0.750 -0.539

0.530 -0.544 0.820 -0.460

0.550 -0.598 0.890 -0.440

0.560 -0.531 0.900 -0.438

0.580 -0.541 0.960 -0.348

0.590 -0.560

0.600 -0.533

0.640 -0.455

0.700 -0.466

0.750 -0.094**

0.820 -0.402

0.870 -0.397

0.930 -0.386

0.960 -0.374

Lower Surface

0.020 0.079 0.020 0.372 0.020 0.398 0.020 0.642

0.110 0.031 0.060 0.332 0.060 0.388 0.060 1.088"*

0.230 0.155 0.090 0.235 0.090 1.913"* 0.110 0.270

0.400 0.002 0.120 0.209 0.120 0.113 0.250 0.107

0.490 -0.022 0.200 0.155 0.200 0.118 0.400 0.047

0.630 2.741 * * 0.260 0.123 0.250 0.151 0.490 0.002

0.750 -0.124 0.400 0.079 0.400 0.077 0.580 0.017

0.850 -0.073 0.490 0.040 0.490 -0.064 0.650 0.174

0.900 0.001 0.580 0.035 0.580 0.063 0.750 0.370

0.960 -0.002 0.640 0.214 0.650 -0.084 0.830 0.493

0.750 0.097 0.750 -0.037 0.900 0.530

0.870 0.112 0.890 0.451 0.960 0.332

0.930 0.048 0.930 0.354

0.960 -0.049 0.960 - 1.982**

CN = 0.540 0.733 0.820 1.018

674
Table J-2. Continued.

Flight 221, Wing sweep = 26", Time = 13-15-43-000, MINF = 0.849, Camber = 5/-1, ALPT = 11.80, BETA = 0.28, QINF = 306.8,

RNPU = 2.4E+06, CNWP = 0.3500

"q = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.791 0.000 0.745 0.000 0.851 ** 0.010 -1.087

0.060 -0.803 0.020 -0,939 0.020 -0.931 0.020 - 1.137

0.110 -0.839 0.040 -0.765 0.060 -3.028"* 0.060 - 1.195

0.200 - 1.003 0.060 -0.879 0.090 - 1.064 0.110 - 1.299

0.230 - 1.024 0.090 -0.979 0.110 - 1.083 0.140 - 1.427

0.400 -0.795 0.130 -1.050 0.130 -1.131 0,190 -1.983**

0.490 -0.645 0.150 -1.148 0.150 -1.231 0.250 -1.051

0.590 -0,363 0.200 - 1.157 0.210 - 1.105 0.400 -0.866

0.630 -0.265 0.250 - 1.069 0.250 -0.861 0.490 -0.780

0.700 -0.215 0.260 - 1.076 0.340 -0.751 0.580 -0.736

0.750 -0.250 0.280 -0.954 0.370 -0.734 0.650 -0.667

0.810 -0.270 0.290 -0.877 0.400 -0.746 0.700 -0.658

0.840 -0.238 0.310 -1.016 0,410 2.432** 0.750 -0.657

0.900 -0.249 0.320 -1.024 0,430 -0.701 0.800 -0.598

0.960 -0.206 0.340 -0.873 0.440 -0,663 0.830 -0.588

0.350 -0.342** 0,460 -0.670 0.900 -0.517

0.370 -0.841 0.490 -0.644 0.960 -0.445

0.380 -0.873 0.500 -0.686

0.400 -0.727 0.520 -0.657

0.410 -0.766 0.540 -0.670

0.430 -0.787 0.550 -0.694

0.440 -0.696 0.580 -0.655

0.460 -0.729 0.600 -0.614

0.470 -0,662 0.610 -0.614

0.490 -0.657 0.650 0.395"*

0.500 -0.659 0.700 -0.627

0.520 -0,674 0.750 -0,646

0.530 -0.619 0.820 -0.509

0.550 -0.638 0.890 -0.466

0.560 -0.551 0,900 -0.459

0.580 -0,589 0.960 -0,385

0.590 -0.573

0.600 -0.558

0,640 -0.405

0.700 -0.412

0,750 -0.078**

0.820 -0.250

0.870 -0.367

0.930 -0.255

0.960 -0.265

Lower Surface

0.020 0.164 0.020 0,446 0.020 0.458 0.020 0.671

0.110 0.062 0.060 0.367 0.060 0.432 0.060 1.095 **

0.230 0.157 0.090 0.278 0.090 1.907"* 0.110 0.276

0.400 0.014 0.120 0.221 0.120 0.152 0.250 0.145

0.490 -0.046 0,200 0.182 0.200 0.129 0.400 0.077

0.630 2.735 ** 0,260 0.156 0.250 0.178 0.490 0,007

0.750 -0.149 0,400 0.107 0.400 0.102 0.580 0.042

0.850 -0.076 0.490 0.056 0.490 -0.067 0.650 0.187

0.900 -0,029 0.580 0,037 0.580 0.082 0.750 0.376

0.960 -0.009 0.640 0.213 0.650 -0.086 0.830 0.495

0.750 0.082 0.750 -0.046 0.900 0.536

0.870 0.109 0.890 0.450 0,960 0.338

0.930 0.043 0.930 0.352

0.960 -0.051 0.960 - 1.964" *

CN = 0.539 0.778 0.825 1.044

675
Table J-2. Continued.

Flight 221, Wing sweep = 26 °, Time = 13-15-44-000, MINF = 0.846, Camber = 5/-1, ALPT = 12.61, BETA = 0.14, QINF = 306.1,

RNPU = 2.4E+06, CNWP = 0.2887

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.920 0.000 0.644 0.000 0.795** 0.010 -1.211

0,060 -0.980 0.020 - 1.117 0.020 - 1.051 0,020 - 1.230

0.1 l 0 - 1.008 0,040 -0.953 0.060 -3.135 ** 0.060 - 1.329

0.200 -1.114 0.060 -1.011 0.090 -1.163 0.110 -1.321

0.230 -1.112 0.090 -1.092 0.110 -1.165 0.140 -1.003

0.400 -0.556 0.130 - 1.164 0.130 -0.877 0.190 - 1.996 **

0.490 -0.441 0.150 - 1.232 0.150 -0.839 0.250 -0.965

0.590 -0.366 0.200 - 1.247 0.210 -0.772 0.400 -0.843

0.630 -0.286 0.250 - 1.031 0.250 -0.737 0.490 -0.810

0.700 -0.229 0.260 -0.935 0.340 -0.689 0.580 -0.757

0.750 -0.265 0.280 -0.940 0.370 -0.668 0.650 -0.679

0,810 -0.273 0.290 -0.914 0.400 -0.714 0.700 -0,695

0.840 -0.244 0.310 -0.893 0.410 2.428** 0,750 -0.660

0.900 -0.227 0.320 -0.927 0.430 -0.667 0.800 -0,614

0.960 -0.215 0.340 -0.758 0.440 -0.639 0.830 -0.572

0.350 -0.264** 0.460 -0.648 0.900 -0.528

0.370 -0.676 0.490 -0.603 0.960 -0.479

0,380 -0.660 0.500 -0,646

0.400 -0.545 0,520 -0.635

0.410 -0.562 0.540 -0,628

0.430 -0.560 0.550 -0.645

0.440 -0.500 0.580 -0.648

0.460 -0.550 0.600 -0.601

0.470 -0.527 0.610 -0.572

0.490 -0.466 0.650 0.403"*

0.500 -0.482 0,700 -0.584

0,520 -0,472 0.750 -0.595

0,530 -0.435 0.820 -0.523

0.550 -0.453 0.890 -0,457

0.560 -0.386 0.900 -0.490

0.580 -0.397 0.960 -0.381

0.590 -0.422

0.600 -0.414

0,640 -0.396

0.700 -0.408

0,750 -0.098**

0.820 -0.256

0.870 -0.360

0.930 -0.30 I

0.960 -0.282

Lower Surface

0.020 0.236 0.020 0.520 0.020 0.533 0.020 0,733

0.110 0.085 0.060 0.421 0.060 0.463 0.060 1.102 **

0,230 0.181 0.090 0,306 0.090 1.902" * 0.110 0.346

0.400 0.016 0.120 0.255 0.120 0.189 0.250 0.174

0,490 -0.056 0.200 0.188 0.200 0.154 0.400 0.111

0.630 2.732** 0.260 0.168 0.250 0.212 0.490 0.035

0.750 -0.148 0.400 0.109 0.400 0.127 0.580 0.043

0.850 -0.1 04 0.490 0.054 0.490 -0.054 0.650 0.185

0.900 -0.045 0,580 0.042 0.580 0.095 0.750 0.367

0.960 -0.042 0.640 0.200 0,650 -0.095 0.830 0.487

0.750 0.065 0.750 -0.055 0.900 0.521

0.870 0.105 0.890 0,427 0.960 0.332

0.930 0.037 0.930 0.322

0.960 -0.053 0.960 - 1.985" *

CN = 0.530 0.755 0.776 1.037

676
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 9-51-57-500, MINF = 0.704, Camber = 5/11, ALPT = 2.15, BETA = 0.25, QINF = 605.3,

RNPU = 5.5E+06, CNWP = 0.3064

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.506 0.000 0.106 0.000 0.441 * * 0.010 0.185

0.060 0.154 0.020 0.503 0.020 0.431 0.020 0.070

0.110 -0.075 0.040 0.315 0.060 0.708** 0,060 -0.237

0.200 -0.184 0,060 0.051 0.090 -0.165 0.110 -0.42 l

0.230 -0.205 0.090 -0.081 0.110 -0.280 O. 140 -0.438

0.400 -0.182 0.130 -0,218 0.130 -2,886** 0.190 -2.886**

0.490 -0.207 0.150 -0.311 0.150 -0,328 0.250 -0.300

0.590 -0.285 0.200 -0.255 0.210 -0.328 0.400 -0.295

0.630 -0.327 0.250 -0.234 0.250 -0.264 0.490 -0.281

0.700 -0.441 0.260 -0.224 0.340 -0.287 0.580 -0.320

0.750 -0.661 0.280 -0.241 0.370 -0.304 0.650 -0.442

0.810 -0.620 0,290 -0.241 0.400 -0.279 0.700 -0,428

0.840 -0,645 0.310 -0.240 0.410 -0.642** 0,750 -0.537

0.900 -0.191 0.320 -0.241 0,430 -0.306 0.800 -0.690

0,960 -0.027 0.340 -0.242 0.440 -0,303 0.830 -0.679

0.350 -0.190** 0,460 -0.317 0.900 -0.185

0.370 -0.245 0.490 -0.284 0.960 -0.106

0.380 -0.263 0.500 -0.331

0.400 -0.231 0.520 -0.325

0.410 -0.265 0.540 -0.338

0.430 -0.252 0.550 -0.328

0.440 -0.246 0.580 -0.340

0.460 -0.269 0,600 -0.378

0.470 -0.287 0.610 -0.410

0.490 -0.286 0,650 -0.558

0.500 -0.291 0.700 -0,508

0.520 -0.294 0.750 -0.499

0.530 -0.304 0.820 -0.718

0.550 -0.330 0.890 -0.198

0.560 -0,344 0.900 -0.190

0.580 -0.320 0,960 -0.136

0.590 -0,364

0.600 -0.364

0.640 -0.530

0.700 -0.514

0,750 -0.056**

0.820 -0,562

0.870 -0.542

0.930 -0,362

0.960 -0.272

Lower Surface

0.020 - 1.262 0.020 -0.907 0.020 - 1.286 0.020 -0.609

0.110 -0.299 0.060 -0.585 0.060 -0.375 0,060 - 1.522

0,230 -0.129 0,090 -0.389 0.090 -0.289 0.110 -0.323

0.400 -0.014 0.120 -0,223 0.120 -0.311 0.250 -0.255

0.490 0.043 0,200 -0.131 0.200 -0.133 0.400 -0.19 l

0.630 0,386"* 0.260 -0,128 0.250 -0.191 0.490 -0.169

0.750 0.172 0,400 -0.059 0.400 -0.122 0.580 -0.108

0.850 0.197 0.490 -0.014 0.490 -0.062 0.650 0.066

0.900 0.268 0.580 0.044 0.580 -0.019 0.750 0.300

0.960 0.195 0.640 0.234 0.650 -0.062 0.830 0.398

0.750 0.289 0.750 -0.026 0.900 0.458

0.870 0.344 0.890 0.436 0.960 0.332

0.930 0.292 0.930 0.353

0,960 0.207 0.960 0.320

CN = 0.260 0.324 0.287 0.232

677
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 9-52-4-000, MINF = 0.703, Camber = 5/11, ALPT = 4.19, BETA = 0.17, QINF = 604.2,

RNPU = 5.5E+06, CNWP -- 0.3873

rl = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.348 0.000 0,466 0.000 0,562** 0,010 -0,220

0.060 0.003 0,020 0.210 0.020 0.1 04 0.020 -0,297

0.110 -0.218 0.040 0.080 0.060 0.474 ** 0,060 -0.585

0,200 -0.286 0,060 -0,179 0,090 -0.413 0.110 -0,717

0,230 -0.306 0.090 -0.305 0.110 -0.541 0.140 -0.654

0.400 -0.238 0.130 -0.445 0.130 -2.889"* 0.190 -2.889**

0,490 -0.241 0.150 -0,520 0.150 -0.542 0.250 -0.437

0,590 -0.331 0,200 -0,428 0.210 -0.511 0.400 -0,380

0.630 -0.367 0,250 -0,369 0.250 -0,403 0.490 -0,354

0,700 -0.476 0.260 -0.354 0,340 -0.391 0.580 -0,383

0.750 -0,669 0.280 -0.361 0.370 -0,397 0.650 -0.497

0.810 -0.630 0.290 -0.351 0,400 -0.359 0.700 -0.479

0.840 -0.665 0.310 -0,336 0.410 -0.641 ** 0.750 -0.572

0.900 -0.219 0.320 -0,342 0,430 -0,402 0,800 -0.670

0.960 -0.071 0.340 -0.343 0,440 -0.389 0.830 -0,673

0.350 -0.186** 0.460 -0.391 0.900 -0,173

0,370 -0.336 0.490 -0.362 0,960 -0.138

0.380 -0.353 0.500 -0.404

0.400 -0.313 0,520 -0,393

0.410 -0,345 0,540 -0,397

0.430 -0.328 0.550 -0,392

0.440 -0,320 0,580 -0.402

0.460 -0.342 0.600 -0.440

0.470 -0.361 0.610 -0.468

0.490 -0.354 0,650 -0.615

0.500 -0.357 0,700 -0.557

0.520 -0,355 0.750 -0.528

0.530 -0.360 0.820 -0.746

0,550 -0.391 0.890 -0.224

0,560 -0,393 0.900 -0.203

0.580 -0.377 0,960 -0.171

0.590 -0.421

0.600 -0.422

0.640 -0.574

0,700 -0.542

0,750 -0.027**

0.820 -0,608

0,870 -0,583

0.930 -0.430

0.960 -0,337

Lower Surface

0.020 -0.687 0,020 -0.571 0.020 -0.453 0.020 -0.125

0.110 -0.185 0.060 -0.158 0,060 -0.096 0.060 -1.522

0.230 -0.034 0,090 -0,15 l 0.090 -0.098 0.110 -0.090

0.400 0.011 0.120 -0,089 0.120 -0.160 0,250 -0.161

0.490 0.041 0.200 -0.032 0.200 -0.037 0.400 -0.125

0.630 0.390* * 0.260 -0,055 0.250 -0.100 0.490 -0.116

0,750 0.190 0.400 -0.024 0.400 -0.060 0.580 -0.077

0.850 0.227 0.490 0.004 0.490 -0,036 0.650 0.097

0,900 0.311 0.580 0.053 0.580 0.007 0.750 0,333

0.960 0.203 0.640 0.268 0,650 -0,035 0.830 0.423

0.750 0,324 0,750 -0.010 0,900 0.478

0.870 0.402 0.890 0.464 0.960 0.329

0.930 0.332 0,930 0.374

0.960 0,225 0.960 0.321

CN = 0.359 0.495 0,443 0.391

678
Table J-2. Continued.

Flight 211, Wing sweep = 26", Time = 9-52-10-500, MINF = 0.710, Camber = 5/11, ALPT = 6.26, BETA = 0.14, QINF = 611.4,

RNPU = 5.5E+06. CNWP = 0.3234

r 1 = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 0,090 0.000 0.783 0.000 0.592"* 0.010 -0.762

0.060 -0.213 0.020 -0.163 0.020 -0.335 0.020 -0.657

0.110 -0.388 0,040 -0.228 0.060 0.159"* 0.060 - 1.040

0.200 -0.399 0,060 -0.499 0.090 -0.726 0.110 -0.917

0.230 -0.405 0,090 -0.591 0.110 -0.854 0.140 - 1.313

0.400 -0.293 0.130 -0.760 0.130 -2.836"* 0.190 -2.836**

0,490 -0.278 0.150 -0.792 0.150 -0,702 0.250 -0.545

0.590 -0.360 0.200 -0,623 0.210 -0.683 0.400 -0.461

0,630 -0.392 0.250 -0.504 0.250 -0.538 0.490 -0.423

0.700 -0.486 0.260 -0.473 0.340 -0,492 0.580 -0.436

0,750 -0.764 0.280 -0.481 0,370 -0.485 0.650 -0.551

0.810 -0.641 0.290 -0.464 0,400 -0.455 0.700 -0.535

0.840 -0.677 0.310 -0.437 0.410 -0.614"* 0.750 -0.595

0.900 -0.263 0.320 -0.441 0.430 -0.477 0.800 -0,641

0.960 -0.121 0.340 -0.438 0.440 -0.462 0.830 -0,673

0,350 -0.185** 0.460 -0.459 0.900 -0.187

0.370 -0.417 0.490 -0.431 0.960 -0.160

0.380 -0.436 0.500 -0,463

0.400 -0.381 0.520 -0.451

0.410 -0.415 0.540 -0.452

0.430 -0,396 0.550 -0.440

0.440 -0.385 0.580 -0.454

0.460 -0.406 0,600 -0.487

0.470 -0.417 0.610 -0.509

0.490 -0.415 0.650 -0.652

0.500 -0.416 0.700 -0.595

0.520 -0.407 0.750 -0.542

0.530 -0.409 0,820 -0.748

0.550 -0.439 0.890 -0.202

0.560 -0.442 0.900 -0.199

0.580 -0.416 0.960 -0.162

0,590 -0.457

0.600 -0.458

0.640 -0.602

0.700 -0.554

0.750 -0.022**

0.820 :0.652

0.870 -0.562

0.930 -0.279

0.960 -0.249

Lower Surface

0.020 -0.325 0.020 -0.200 0.020 -0.054 0.020 0.329

0.110 -0.102 0.060 0.031 0.060 0.111 0.060 0.019

0.230 0.043 0.090 0.006 0.090 0.066 0.110 0,060

0,400 0.032 0.120 0.025 0.120 -0.014 0.250 -0.056

0.490 0.049 0.200 0.038 0.200 0.043 0.400 -0.058

0.630 0.410* * 0.260 0.018 0.250 -0.007 0.490 -0.059

0.750 0.183 0.400 0.020 0.400 -0.001 0.580 -0.027

0.850 0.211 0.490 0.033 0.490 -0.023 0.650 0.130

0.900 0.311 0.580 0.070 0.580 0.031 0.750 0.358

0.960 0.184 0,640 0.282 0,650 -0.033 0.830 0.442

0.750 0.325 0.750 0.016 0.900 0,495

0.870 0.412 0.890 0,474 0.960 0.339

0.930 0.328 0.930 0.380

0.960 0.217 0.960 0.301

CN = 0.450 0.625 0.576 0.679

679
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 9-52-15-000, MINF = 0.705, Camber = 5/10, ALPT = 7.10, BETA = 0.11, QINF = 601.1,

RNPU = 5.4E+06, CNWP = 0.3654

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x,/c CP

0.020 -0.094 0.000 0.834 0.000 0.548"* 0.010 - 1.228

0.060 -0.339 0.020 -0.384 0.020 -0.571 0.020 -0.956

0. I 10 -0.483 0.040 -0.398 0.060 0.034 ** 0,060 - 1.206

0.200 -0.461 0.060 -0.668 0.090 -0.771 0.110 - 1.084

0.230 -0.468 0.090 -0.734 0.110 -0.947 0.140 - 1.304

0.400 -0.319 0.130 -0.808 0.130 -2.875"* 0.190 -2.875"*

0.490 -0.297 0.150 -0.998 0.150 - 1.162 0.250 -0.588

0.590 -0.386 0.200 -0.670 0.210 -0.716 0.400 -0,495

0.630 -0.415 0.250 -0.558 0.250 -0.578 0.490 -0.456

0.700 -0.507 0.260 -0.533 0.340 -0.536 0.580 -0.465

0.750 -0.772 0.280 -0.533 0.370 -0.523 0.650 -0.579

0.810 -0.654 0.290 -0.511 0.400 -0.494 0.700 -0.574

0.840 -0,698 0.310 -0.488 0.410 -0.616"* 0,750 -0.636

0.900 -0.288 0.320 -0.486 0.430 -0.510 0.800 -0.639

0.960 -0.1 40 0.340 -0.484 0.440 -0.494 0.830 -0.616

0.350 -0.182** 0.460 -0.498 0.900 -0.220

0.370 -0.453 0.490 -0.456 0.960 -0.175

0.380 -0.481 0.500 -0.490

0.400 -0.424 0.520 -0.492

0.410 -0.455 0.540 -0.492

0.430 -0.435 0.550 -0,469

0.440 -0.408 0.580 -0.472

0.460 -0.440 0.600 -0.517

0.470 -0.441 0.610 -0.543

0,490 -0.444 0,650 -0.705

0.500 -0.436 0.700 -0.612

0.520 -0.436 0.750 -0,567

0.530 -0,428 0.820 -0.715

0.550 -0.465 0.890 -0.208

0.560 -0.479 0.900 -0.199

0.580 -0.447 0.960 -0.156

0.590 -0.492

0.600 -0.476

0.640 -0.620

0.700 -0.573

0.750 -0.022**

0.820 -0.590

0.870 -0.578

0.930 -0.370

0.960 -0.299

Lower Surface

0.020 -0.195 0.020 -0.013 0.020 0.095 0.020 0.445

0.110 -0.055 0.060 0.124 0.060 0.194 0.060 0.029

0.230 0.085 0.090 0.086 0.090 0.132 0.110 0.150

0.400 0.044 0.120 0.078 0.120 0.056 0.250 -0.008

0.490 0.057 0.200 0.083 0.200 0.079 0.400 -0.028

0.630 0.425** 0.260 0.056 0.250 0.034 0.490 -0.027

0.750 0.174 0.400 0.042 0.400 0.027 0.580 0.001

0.850 0.205 0.490 0.050 0.490 -0.021 0.650 0.152

0.900 0.291 0.580 0.078 0.580 0.047 0.750 0.371

0.960 0.162 0.640 0.284 0.650 -0.038 0.830 0.456

0.750 0.325 0.750 0.026 0.900 0.509

0.870 0.405 0.890 0.480 0.960 0.350

0.930 0.310 0.930 0.381

0.960 0.207 0.960 0.313

CN = 0.499 0.692 0.647 0.751

680
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 9-52-19-500, MINF = 0.695, Camber = 5/10. ALPT = 8.26, BETA = 0.11, QINF = 582.0.

RNPU = 5.3E+06, CNWP = 0.4441

q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 -0.410 0.000 0.775 0.000 0.451 ** 0.010 - 1.290

0.060 -0.557 0.020 -0.837 0.020 - 1.011 0.020 - 1.485

0.110 -0.595 0.040 -0,682 0.060 -0.126"* 0.060 - 1.471

0.200 -0.533 0,060 - 1.007 0.090 - 1.306 0.110 - 1.546

0.230 -0.522 0.090 - 1.089 0.110 - 1.328 0.140 - 1.465

0.400 -0.361 0.130 -0.823 0.130 -2.959* * 0.190 -2,959* *

0.490 -0.343 0.150 - 1.020 0.150 - 1.406 0.250 -0.618

0.590 -0.417 0.200 - 1.119 0.210 -0.865 0.400 -0.514

0.630 -0.455 0.250 -0.617 0.250 -0.605 0.490 -0.470

0.700 -0.544 0.260 -0,588 0.340 -0.567 0.580 -0.491

0.750 -0.790 0.280 -0.593 0.370 -0.570 0.650 -0.580

0.810 -0.716 0.290 -0.563 0.400 -0,530 0.700 -0.578

0.840 -0.759 0.310 -0,532 0.410 -0.625** 0.750 -0.624

0.900 -0.328 0.320 -0,539 0.430 -0.548 0.800 -0.553

0.960 -0.187 0.340 -0.520 0,440 -0,527 0.830 -0.523

0.350 -0.188** 0,460 -0,523 0.900 -0.218

0.370 -0.503 0.490 -0.487 0.960 -0.129

0.380 -0.525 0.500 -0.530

0.400 -0.458 0.520 -0.515

0.410 -0.490 0.540 -0.525

0.430 -0.473 0.550 -0.498

0.440 -0.454 0.580 -0.496

0.460 -0.473 0.600 -0.541

0.470 -0.488 0.610 -0.556

0.490 -0.472 0.650 -0.741

0.500 -0.468 0.700 -0.634

0.520 -0.461 0.750 -0.599

0,530 -0.466 0.820 -0.668

0.550 -0.494 0.890 -0.190

0.560 -0.501 0,900 -0.165

0.580 -0.475 0.960 -0.130

0.590 -0.520

0.600 -0.507

0.640 -0.654

0.700 -0.620

0.750 -0.012"*

0.820 -0.651

0.870 -0.578

0.930 -0.287

0.960 -0.228

Lower Surface

0.020 0.050 0.020 0.205 0.020 0.284 0,020 0.573

0.110 0.012 0.060 0.238 0.060 0.300 0.060 0.041

0.230 0.137 0.090 0.181 0.090 0.238 0.110 0.229

0.400 0,056 0.120 0,159 0,120 0.140 0.250 0.046

0.490 0.064 0.200 0.138 0.200 0.134 0.400 0.027

0.630 0.457"* 0.260 0.106 0.250 0.099 0.490 0.014

0.750 0. 155 0.400 0.076 0.400 0,070 0.580 0.033

0.850 0. 190 0.490 0.083 0.490 0,004 0.650 0.168

0.900 0.270 0.580 0.103 0.580 0.085 0.750 0.387

0.960 0.147 0.640 0.291 0.650 -0.031 0.830 0,465

0.750 0.335 0.750 0.037 0.900 0.516

0.870 0.406 0.890 0.477 0.960 0.344

0.930 0.314 0.930 0.377

0.960 0.208 0.960 0.299

CN = 0.571 0.807 0.766 0.837

681
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 9-55-37-500, MINF = 0,697, Camber = 5/-1, ALPT = 2.04, BETA = 0.17, QINF = 583.0,

RNPU = 5.3E+06, CNWP = 0.2090

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0,488 0,000 0.140 0.000 0.480** 0.010 0.182

0.060 0.127 0,020 0,445 0.020 0.411 0,020 0.057

0.110 -0.094 0.040 0.279 0,060 0.676** 0.060 -0.235

0.200 -0.190 0.060 0.022 0,090 -0.181 0.110 -0,427

0.230 -0.205 0.090 -0.106 0.110 -0.299 0.140 -0.438

0.400 -0.150 0.130 -0,246 0.130 -2.939 ** 0.190 -2.939 * *

0,490 -0.135 0.150 -0.330 0.150 -0.345 0.250 -0.310

0.590 -0.165 0.200 -0,276 0.210 -0.338 0.400 -0.299

0,630 -0.153 0.250 -0.242 0,250 -0.288 0,490 -0.286

0.700 -0.125 0,260 -0.235 0.340 -0,297 0.580 -0.327

0.750 -0.102 0.280 -0,247 0.370 -0.311 0.650 -0,453

0.810 -0.087 0.290 -0.247 0.400 -0.278 0.700 -0.439

0.840 -0.093 0,310 -0.238 0.410 -0.609** 0.750 -0.559

0.900 -0.087 0.320 -0.245 0.430 -0.313 0.800 -0.687

0.960 -0,010 0.340 -0,247 0,440 -0.308 0.830 -0.662

0.350 -0.189"* 0,460 -0.313 0.900 -0.177

0,370 -0.250 0,490 -0,299 0.960 -0.112

0.380 -0,264 0,500 -0,328

0,400 -0,233 0.520 -0.332

0.410 -0.256 0.540 -0,336

0.430 -0.243 0.550 -0,328

0,440 -0.241 0.580 -0.339

0.460 -0.261 0.600 -0.373

0.470 -0,274 0.610 -0,397

0.490 -0.278 0,650 -0,546

0.500 -0.282 0.700 -0.512

0.520 -0.268 0.750 -0.506

0.530 -0.280 0.820 -0.670

0,550 -0.310 0.890 -0.178

0.560 -0.316 0,900 -0.161

0.580 -0,294 0.960 -0.119

0,590 -0.331

0,600 -0,339

0.640 -0.471

0,700 -0.479

0.750 -0.154"*

0.820 -0.471

0.870 -0,427

0.930 -0,297

0.960 -0,241

Lower Surface

0,020 - 1.262 0,020 -0.934 0.020 - 1.206 0,020 -0.722

0.110 -0.300 0.060 -0.545 0.060 -0.309 0.060 -0.038

0.230 -0.132 0.090 -0.350 0.090 -0.276 0.110 -0.317

0,400 -0.087 0.120 -0.231 0.120 -0,276 0.250 -0.257

0.490 -0,088 0.200 -0.130 0.200 -0.130 0.400 -0.194

0.630 0,529"* 0.260 -0.144 0.250 -0.191 0.490 -0.160

0,750 -0.025 0.400 -0.101 0.400 -0.135 0.580 -0.112

0.850 0.007 0.490 -0,072 0.490 -0.131 0.650 0,073

0.900 0.081 0,580 -0.034 0.580 -0.035 0.750 0.305

0,960 0.100 0.640 0.131 0.650 -0.138 0,830 0.394

0.750 0.071 0.750 -0.019 0,900 0.455

0.870 0.069 0.890 0.431 0,960 0.325

0.930 0.068 0.930 0.355

0.960 0,038 0.960 0.298

CN = 0.030 0.213 0,280 0,334

682
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 9-55-47-500, MINF = 0.708, Camber = 5/-1, ALPT = 6.26, BETA = 0.28, QINF = 601.0,

RNPU = 5.4E+06, CNWP = 0.3272

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.023 0.000 0.816 0,000 0.613"* 0.010 - 1.053

0.060 -0.288 0.020 -0.292 0.020 -0.428 0.020 -0.698

0.110 -0.444 0.040 -0.199 0.060 0. l 31 ** 0.060 - 1.093

0.200 -0.422 0,060 -0.603 0.090 -0.778 0.110 -0.905

0.230 -0.416 0.090 -0.664 0.110 -0.895 0.140 -1.319

0.400 -0.271 0.130 -0.820 0.130 -2.853 * * 0.190 -2.853 **

0.490 -0.234 0.150 -0,817 0.150 -0.931 0.250 -0.557

0,590 -0.24 l 0.200 -0.668 0.210 -0.686 0.400 -0.476

0.630 -0.227 0.250 -0,525 0.250 -0,558 0.490 -0.433

0.700 -0.183 0.260 -0.498 0.340 -0.511 0.580 -0.451

0.750 -0.154 0.280 -0.497 0,370 -0.504 0.650 -0.552

0.810 -0.130 0.290 -0.479 0,400 -0.462 0.700 -0.543

0.840 -0.140 0.310 -0.452 0.410 -0.593 ** 0.750 -0.619

0.900 -0.128 0.320 -0.458 0.430 -0.489 0.800 -0.624

0.960 -0.041 0.340 -0.448 0.440 -0.473 0.830 -0.624

0.350 -0.183"* 0.460 -0.470 0.900 -0.185

0.370 -0.431 0.490 -0.442 0.960 -0.163

0.380 -0.445 0.500 -0.469

0.400 -0.397 0.520 -0.462

0.410 -0.415 0.540 -0.463

0.430 -0.387 0.550 -0.445

0.440 -0.379 0.580 -0.449

0.460 -0.405 0.600 -0,492

0,470 -0.411 0.610 -0.501

0.490 -0.404 0.650 -0.660

0.500 -0.399 0.700 -0.587

0,520 -0.383 0.750 -0.557

0.530 -0.386 0.820 -0.669

0.550 -0,422 0.890 -0.190

0.560 -0.428 0.900 -0.177

0.580 -0.399 0.960 -0.152

0.590 -0.435

0.600 -0.434

0,640 -0.554

0.700 -0.539

0,750 -0.167"*

0,820 -0.595

0.870 -0.517

0.930 -0,363

0,960 -0.284

Lower Surface

0,020 -0.217 0.020 -0.091 0.020 0.012 0.020 0.361

0.110 -0.090 0,060 0.069 0.060 0.136 0.060 -0.039

0.230 0.044 0.090 0.042 0.090 0.093 0.110 0.105

0.400 -0.033 0.120 0,037 0.120 0.034 0.250 -0.047

0.490 -0.057 0.200 0.046 0.200 0.050 0,400 -0,047

0.630 0.514** 0.260 0.019 0.250 0.007 0.490 -0,045

0.750 -0.048 0.400 -0.004 0,400 -0.005 0.580 -0.02 I

0.850 -0.024 0.490 -0.008 0.490 -0.095 0.650 0.140

0.900 0.05 l 0.580 -0.001 0.580 0,028 0.750 0.366

0.960 0.083 0.640 O. 180 0.650 -0. 139 0.830 0.442

0.750 0.087 0.750 0.021 0.900 0.495

0.870 0.100 0.890 0.474 0.960 0.338

0.930 0.053 0.930 0.373

0.960 -0.002 0.960 0.301

CN = 0.220 0,539 0,583 0.692

683
Table J-2, Continued.

Flight 211, Wing sweep = 26 °, Time = 9-55-51-500, MINF = 0.712, Camber = 5/-1, ALPT = 7.06, BETA = 0.43, QINF = 606.7,

RNPU = 5.4E+06, CNWP -- 0.3830

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0,020 -0.192 0.000 0.839 0.000 0.559** 0.010 - 1.206

0.060 -0.414 0.020 -0.488 0.020 -0.625 0.020 - 1.204

0.110 -0.540 0.040 -0.477 0.060 -0.048"* 0.060 - 1.182

0.200 -0.473 0.060 -0.758 0.090 - 1.051 0.110 - 1.350

0.230 -0.468 0.090 -0.766 0.110 - 1.058 0.140 - 1.257

0.400 -0.294 0.130 -0.805 0.130 -2.819"* 0.190 -2.819"*

0.490 -0.255 0.150 - 1.007 0,150 - 1.172 0.250 -0.587

0.590 -0.264 0.200 -0.979 0.210 -0.792 0.400 -0.498

0.630 -0.244 0.250 -0.557 0.250 -0.591 0.490 -0.449

0.700 -0.197 0.260 -0.532 0.340 -0.536 0.580 -0.481

0.750 -0,166 0.280 -0.532 0.370 -0.538 0.650 -0.576

0.810 -0.146 0.290 -0.515 0.400 -0.494 0,700 -0.559

0.840 -0.157 0.310 -0.485 0.410 -0.580"* 0.750 -0,638

0.900 -0.142 0.320 -0,490 0.430 -0.517 0.800 -0.621

0.960 -0.061 0.340 -0.477 0.440 -0.502 0.830 -0.610

0.350 -0.182" * 0.460 -0.494 0.900 -0.220

0,370 -0.459 0.490 -0.464 0.960 -0.162

0.380 -0.474 0.500 -0,490

0.400 -0.418 0.520 -0.484

0.410 -0.439 0.540 -0.478

0.430 -0.417 0.550 -0.463

0.440 -0.404 0.580 -0.463

0.460 -0.429 0.600 -0.510

0,470 -0.435 0.610 -0.529

0.490 -0,424 0.650 -0,678

0.500 -0.423 0.700 -0.600

0.520 -0.410 0.750 -0.559

0.530 -0.411 0.820 -0.660

0.550 -0.438 0.890 -0.209

0.560 -0.441 0.900 -0.186

0.580 -0.411 0.960 -0.146

0.590 -0.450

0.600 -0.437

0.640 -0.564

0.700 -0.541

0.750 -0.169"*

0.820 -0.595

0.870 -0.514

0.930 -0.343

0.960 -0.264

Lower Surface

0.020 -0.113 0.020 0.043 0.020 0.127 0,020 0.455

0.110 -0.055 0.060 0.139 0.060 0.204 0.060 -0.03 I

0.230 0.077 0.090 0.102 0.090 0.149 0.110 0.159

0.400 -0.015 0.120 0.087 0.120 0.083 0.250 -0.005

0.490 -0.049 0.200 0.075 0,200 0.081 0.400 -0,018

0.630 0.517"* 0.260 0,048 0,250 0.042 0.490 -0,022

0.750 -0.055 0.400 0.019 0.400 0.018 0.580 -0.001

0,850 -0.035 0.490 0.009 0.490 -0.087 0.650 0.150

0.900 0.041 0.580 0.016 0.580 0.042 0.750 0.375

0.960 0.064 0.640 0.184 0.650 -0.141 0.830 0.461

0.750 0.083 0.750 0.028 0.900 0.506

0.870 0.097 0.890 0.475 0.960 0.349

0.930 0.047 0,930 0.373

0.960 -0.009 0.960 0.282

CN = 0.264 0.605 0.657 0.760

684
Table .1-2. Continued.

Flight 211. Wing sweep = 26 °, Time = 9-55-56-500, MINF = 0.704, Camber = 5/-1. ALPT = 8.09, BETA = 0.25, QINF = 590.5,

RNPU = 5.3E+06. CNWP = 0.4400

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.452 0.000 0.776 0.000 0.508"* 0.010 - 1.215

0.060 -0.564 0.020 -0.867 0.020 -0.971 0.020 - 1.431

0.110 -0.647 0.040 -0.672 0.060 -0.137"* 0.060 - 1.421

0.200 -0.532 0.060 -1.012 0.090 -1.290 0.110 -1.514

0.230 -0.509 0.090 - 1.076 0.110 - 1.303 0.140 - 1.700

0.400 -0.325 0.130 -0.815 0.130 -2.884* * 0.190 -2.884 * *

0.490 -0.271 0.150 - 1.022 0.150 - 1.386 0.250 -0.613

0.590 -0.279 0.200 -1.151 0.210 -1.162 0.400 -0.510

0.630 -0.266 0.250 -0.579 0.250 -0.577 0.490 -0.469

0.700 -0.218 0.260 -0.552 0.340 -0.547 0.580 -0.475

0.750 -0.186 0.280 -0.563 0.370 -0.546 0.650 -0.580

0.810 -0.157 0.290 -0.541 0.400 -0.510 0.700 -0.573

0.840 -0.172 0.310 -0.512 0.410 -0.584** 0.750 -0.640

0.900 -0.165 0.320 -0.521 0.430 -0.528 0.800 -0.551

0.960 -0.087 0.340 -0.506 0.440 -0.517 0.830 -0.516

0,350 -0.177** 0.460 -0.510 0.900 -0.202

0.370 -0.487 0.490 -0.473 0.960 -0.138

0.380 -0.498 0.500 -0.506

0.400 -0.444 0.520 -0.504

0.410 -0.470 0.540 -0.500

0.430 -0.439 0.550 -0.489

0.440 -0.424 0.580 -0.490

0.460 -0.448 0.600 -0.523

0.470 -0.458 0.610 -0.538

0.490 -0.443 0.650 -0.703

0.500 -0.447 0.700 -0.606

0.520 -0.426 0.750 -0.576

0.530 -0.425 0.820 -0.627

0.550 -0.454 0.890 -0.159

0.560 -0.459 0.900 -0.147

0.580 -0.427 0.960 -0.113

0.590 -0.473

0.600 -0.455

0.640 -0.575

0.700 -0.568

0.750 -0.162 **

0.820 -0.617

0.870 -0.529

0.930 -0.354

0.960 -0.267

Lower Surface

0.020 0.036 0.020 0.218 0.020 0.285 0.020 0.567

0.110 0.006 0.060 0.231 0.060 0.299 0.060 -0.020

0.230 0.131 0.090 0.188 0.090 0.237 0.110 0.245

0.400 -0.009 0.120 0.142 0.120 0.161 0.250 0.042

0.490 -0.031 0.200 0.127 0.200 0.129 0.400 0.027

0.630 0.550"* 0.260 0.105 0.250 0.099 0.490 0.023

0.750 -0.053 0.400 0.054 0.400 0.057 0.580 0.036

0.850 -0.040 0.490 0.040 0.490 -0.065 0.650 0.170

0.900 0.035 0.580 0.032 0.580 0.074 0.750 0.394

0.960 0.053 0.640 0.195 0.650 -0.132 0.830 0.464

0.750 0.096 0.750 0.041 0.900 0.511

0.870 0.096 0.890 0.489 0.960 0.353

0.930 0.049 0.930 0.380

0.960 -0.010 0.960 0.301

CN = 0.323 0.690 0.747 0.849

685
Table J-2. Continued.

Hight 211, Wing sweep = 26 °, Time = 9-55-58-000, MINF = 0.700, Camber = 5/-1, ALPT = 8.46, BETA = 0.25, QINF = 583.6,

RNPU = 5.3E+06, CNWP = 0.4425

I1 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.556 0.000 0.728 0.000 0.44.2"* 0.010 - 1.410

0.060 -0.666 0.020 -0.998 0.020 - 1.252 0.020 - 1.530

0.110 -0.682 0.040 -0.750 0.060 -0.150* * 0.060 - 1.505

0.200 -0.548 0.060 - 1.083 0.090 - 1.3 l9 0.110 - 1.579

0.230 -0.547 0.090 - 1.086 0.110 - 1.380 0.140 - 1.744

0.400 -0.330 0.130 -0.821 0.130 -2.915"* 0.190 -2.915"*

0.490 -0.291 0.150 - 1.031 0.150 - 1.458 0.250 -0.646

0.590 -0.300 0.200 -1.183 0.210 -1.172 0.400 -0.513

0.630 -0.274 0.250 -0.570 0.250 -0.614 0.490 -0.474

0.700 -0.222 0.260 -0.555 0.340 -0.557 0.580 -0.501

0.750 -0.197 0.280 -0.557 0.370 -0.560 0.650 -0.571

0.810 -0.170 0.290 -0.547 0.400 -0.513 0.700 -0.566

0.840 -0.186 0.310 -0.511 0.410 -0.588 ** 0.750 -0.614

0.900 -0.184 0.320 -0.528 0.430 -0.546 0.800 -0.533

0.960 -0.097 0.340 -0.519 0.440 -0.532 0.830 -0.502

0.350 -0.174** 0.460 -0.523 0.900 -0.213

0.370 -0.497 0.490 -0.486 0.960 -0.145

0.380 -0.519 0.500 -0.528

0.400 -0.458 0.520 -0.514

0.410 -0.481 0.540 -0.503

0.430 -0.454 0.550 -0.495

0.440 -0.438 0.580 -0.486

0.460 -0.467 0.600 -0.532

0.470 -0.470 0.610 -0.548

0.490 -0.462 0.650 -0.704

0.500 -0.455 0.700 -0.614

0.520 -0.443 0.750 -0.596

0.530 -0.439 0.820 -0.628

0.550 -0.465 0.890 -0.167

0.560 -0.478 0.900 -0.148

0.580 -0.436 0.960 -0.108

0.590 -0.473

0.600 -0.467

0.640 -0.593

0.700 -0.581

0.750 -0.159"*

0.820 -0.617

0.870 -0.539

0.930 -0.361

0.960 -0.275

Lower Surface

0.020 0.086 0.020 0.264 0.020 0.339 0.020 0.592

0.110 0.019 0.060 0.260 0.060 0.327 0.060 -0.017

0.230 0.131 0.090 0.211 0.090 0.259 0.110 0.259

0.400 0.004 0.120 0.174 0.120 0.184 0.250 0.058

0.490 -0.032 0.200 0.132 0.200 0.141 0.400 0.041

0.630 0.550** 0.260 0.117 0.250 0.106 0.490 0.034

0.750 -0.059 0.400 0.054 0.400 0.062 0.580 0.032

0.850 -0.052 0.490 0.04 1 0.490 -0.060 0.650 0.173

0.900 0.022 0.580 0.038 0.580 0.078 0.750 0.390

0.960 0.039 0.640 0.202 0.650 -0.131 0.830 0.461

0.750 0.081 0.750 0.044 0.900 0.508

0.870 0.088 0.890 0.478 0.960 0.352

0.930 0.040 0.930 0.383

0.960 -0.018 0.960 0.290

CN = 0.344 0.709 0.763 0.872

686
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 10-36-20-000, MINF = 0.802, Camber = 0/2, ALPT = 4.05, BETA = 0.66, QINF = 605.6,

RNPU = 5.0E+06, CNWP = 0.1504

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.021 0.000 0.846 0.000 0.706** 0.010 -0.865

0.060 -0.114 0.020 -0.189 0,020 -0.376 0.020 -0.926

0.110 -0.179 0.040 -0.184 0.060 0.276** 0.060 -0.739

0.200 -0.197 0.060 -0.304 0.090 -0.361 0.110 -0.360

0.230 -0.251 0.090 -0.254 0.110 -0.355 0.140 -0.527

0.400 -0.179 0.130 -0.293 0.130 -2.221 ** 0.190 -2.221 **

0.490 -0.173 0.150 -0.306 0.150 -0.375 0.250 -0.388

0.590 -0.212 0.200 -0.278 0.210 -0.427 0.400 -0.338

0.630 -0.227 0.250 -0.285 0.250 -0.354 0.490 -0.300

0.700 -0.222 0.260 -0.294 0.340 -0.335 0.580 -0.294

0.750 -0.230 0.280 -0.293 0.370 -0.337 0.650 -0.377

0.810 -0.202 0.290 -0.293 0.400 -0.294 0.700 -0.346

0.840 -0.212 0.310 -0.279 0.410 - 1.023"* 0.750 -0.369

0.900 -0.108 0.320 -0.293 0.430 -0.324 0.800 -0.326

0.960 0.006 0.340 -0.288 0.440 -0.313 0.830 -0.299

0.350 -0.225" * 0.460 -0.307 0.900 -0.197

0.370 -0.274 0.490 -0.284 0.960 -0.015

0.380 -0.280 0.500 -0.301

0.400 -0.25 ! 0.520 -0.307

0.410 -0.270 0.540 -0.293

0.430 -0.256 0.550 -0.282

0.440 -0.252 0.580 -0.261

0.460 -0.261 0.600 -0.308

0.470 -0.274 0.610 -0.329

0.490 -0.269 0.650 -0.367

0.500 -0.258 0.700 -0.362

0.520 -0.261 0.750 -0.305

0.530 -0.257 0.820 -0.313

0.550 -0.27 l 0.890 -0.126

0.560 -0.284 0.900 -0.092

0.580 -0.250 0.960 0.028

0.590 -0.284

0.600 -0.278

0.640 -0.351

0.700 -0.298

0.750 -0.066"*

0.820 -0.265

0.870 -0.230

0.930 -0.083

0.960 -0.018

Lower Surface

0.020 -0.603 0.020 -0.395 0.020 -0.170 0.020 0.309

0,110 -0.315 0,060 -0.157 0.060 -0.073 0.060 0.043

0.230 -0.192 0.090 -0.212 0.090 -0.119 0.110 -0.089

0.400 -0.119 0.120 -0.245 0.120 -0.193 0.250 -0.310

0.490 -0.089 0.200 -0.186 0.200 -0.279 0.400 -0.285

0.630 0.912"* 0.260 -0.265 0.250 -0.289 0.490 -0.291

0.750 0.028 0.400 -0.199 0.400 -0.256 0.580 -0.322

0.850 0.076 0,490 -0.194 0.490 -0.092 0.650 -0.152

0.900 0.179 0.580 -0.180 0.580 -0.257 0.750 0.118

0.960 0.171 0.640 0.006 0.650 -0.066 0.830 0.248

0.750 0.156 0.750 -0.052 0.900 0.301

0.870 0.236 0.890 0.295 0.960 0.257

0.930 0.212 0.930 0.241

0.960 0.174 0.960 0.221

CN = 0.104 0.187 0.191 0.267

687
Table J-2. Continued.

Flight 225, Wing sweep = 26 °. Time = 8-48-5-000, MINF = 0.801, Camber = 0/2, ALPT = 4.00, BETA = 0.45, QINF = 602.7,

RNPU = 4.9E+06, CNWP -- 0.1639

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.019 0.000 0.843 0.000 2.827** 0.010 -0.837

0.060 -0.093 0.020 -0.258 0.020 -0.365 0.020 -0.899

0. 110 -0.167 0.040 -0.216 0.060 -0.888** 0.060 -0.693

0.200 -0.166 0.060 -0.308 0.090 -0.336 0.110 -0.325

0.230 -0.209 0.090 -0.239 0.110 -0.355 0.140 -0.514

0.400 -0.163 0.130 -0.274 0.130 -0.37 t 0.190 -2.227"*

0.490 -0.161 0.150 -0.302 0.150 -0.371 0.250 -0.347

0.590 -0.223 0.200 -0.265 0.210 -0.420 0.400 -0.311

0.630 -0.210 0.250 -0.295 0.250 -0.308 0.490 -0.273

0.700 -0.206 0.260 -0.267 0.340 -0.316 0.580 -0.262

0.750 -0.228 0.280 -0.283 0.370 -0.333 0.650 -0.373

0.810 -0.209 0.290 -0.283 0.400 -0.316 0.700 -0.340

0.840 -0.201 0.310 -0.280 0.410 0.081"* 0.750 -0.363

0.900 -0.101 0.320 -0.280 0.430 -0.320 0.800 -0.344

0.960 0.015 0.340 -0.264 0.440 -0.298 0.830 -0.303

0.350 -0.252** 0.460 -0.301 0.900 -0.203

0.370 -0.249 0.490 -0.254 0.960 -0.008

0.380 -0.272 0.500 -0.307

0.400 -0.271 0.520 -0.279

0.410 -0.274 0.540 -0.287

0.430 -0.251 0.550 -0.254

0.440 -0.223 0.580 -0.256

0.460 -0.257 0.600 -0.294

0.470 -0.249 0.610 -0.313

0.490 -0.252 0.650 2.145"*

0.500 -0.256 0.700 -0.375

0.520 -0.269 0.750 -0.348

0.530 -0.250 0.820 -0.321

0.550 -0.291 0.890 -0.137

0.560 -0.260 0.900 -0.082

0.580 -0.250 0.960 0.022

0.590 -0.286

0.600 -0.293

0.640 -0.350

0.700 -0.294

0.750 -0.058**

0.820 -0.258

0.870 -0.215

0.930 -0.086

0.960 -0.019

Lower Surface

0.020 -0.633 0.020 -0.403 0.020 -0.165 0.020 0.232

0.110 -0.309 0.060 -0.186 0.060 -0.063 0.060 2.001 **

0.230 -0.177 0.090 -0.211 0.090 0.543** 0.110 -0.145

0.400 -0.122 0.120 -0.249 0.120 -0.277 0.250 -0.297

0.490 -0.085 0.200 -0.185 0.200 -0.295 0.400 -0.270

0.630 0.921 ** 0.260 -0.259 0.250 -0.285 0.490 -0.297

0.750 0.044 0.400 -0.189 0.400 -0.243 0.580 -0.311

0.850 0.112 0.490 -0.188 0.490 -0.073 0.650 -0.137

0.900 0.196 0.580 -0.170 0.580 -0.229 0.750 0.114

0.960 0.175 0.640 0.023 0.650 -0.062 0.830 0.276

0.750 0.175 0.750 -0.040 0.900 0.315

0.870 0.258 0.890 0.283 0.960 0.270

0.930 0.205 0.930 0.244

0.960 0.165 0.960 0.037 * *

CN= 0.1_ 0.1_ 0.182 0.244

688
Table J-2. Continued.

Flight 225, Wing sweep = 26 °, Time = 8-48-22-000, MINF = 0.800, Camber = 0/2, ALPT = 5.99, BETA = 0.34, QINF = 602.6,

RNPU = 5.0E+06, CNWP = 0.2813

'q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.324 0.000 0.823 0.000 1.718"* 0.010 - 1.027

0.060 -0.354 0.020 -0.860 0.020 -0.950 0.020 - 1.119

0.110 -0.319 0.040 -0.803 0.060 -2.004** 0.060 - 1.056

0.200 -0.261 0.060 -0.870 0.090 -0.965 0.110 -0.987

0.230 -0.309 0.090 -0.800 0.110 -0.969 0.140 - | .001

0.400 -0.229 0.130 -0.834 0.130 -0.911 0.190 -2.234*"

0.490 -0.210 0.150 -0.329 0.150 -0.838 0.250 -0.363

0.590 -0.255 0.200 -0.306 0.210 -0.846 0.400 -0.352

0.630 -0.243 0.250 -0.388 0.250 -0.300 0.490 -0.323

0.700 -0.228 0.260 -0.374 0.340 -0.371 0.580 -0.318

0.750 -0.250 0.280 -0.389 0.370 -0.387 0.650 -0.400

0.810 -0.231 0.290 -0.378 0.400 -0.366 0.700 -0.380

0.840 -0.222 0.310 -0.368 0.410 -1.029"* 0.750 -0.380

0.900 -0.131 0.320 -0.360 0.430 -0.372 0.800 -0.336

0.960 -0.020 0.340 -0.348 0.440 -0.357 0.830 -0.314

0.350 -0.230** 0.460 -0.360 0.900 -0. 184

0.370 -0.324 0.490 -0.302 0.960 -0.001

0.380 -0.349 0.500 -0.355

0.400 -0.286 0.520 -0.328

0.410 -0.333 0.540 -0.333

0.430 -0.309 0.550 -0.302

0.440 -0.268 0.580 -0.306

0.460 -0.315 0.600 -0.341

0.470 -0.312 0.610 -0.359

0.490 -0.304 0.650 2.140"*

0.500 -0.301 0.700 -0.430

0.520 -0.311 0.750 -0.376

0.530 -0.299 0.820 -0.332

0.550 -0.328 0.890 -0.134

0.560 -0.321 0.900 -0.086

0.580 -0.299 0.960 0.025

0.590 -0.331

0.600 -0.329

0.640 -0.388

0.700 -0.328

0.750 -0.051"*

0.820 -0.285

0.870 -0.229

0.930 -0.098

0.960 -0.031

Lower Surface

0.020 -0.119 0.020 0.056 0.020 0.169 0.020 0.466

0.110 -0.170 0.060 0.041 0.060 0.135 0.060 1.996 * *

0.230 -0.050 0.090 -0.021 0.090 0.537"* 0.110 0.017

0.400 -0.067 0.120 -0.074 0.120 -0.120 0.250 -0.172

0.490 -0.061 0.200 -0.083 0.200 -0.134 0.400 -0.176

0.630 0.915"* 0.260 -0.152 0.250 -0.153 0.490 -0.223

0.750 0.017 0.400 -0. l 31 0.400 -0.161 0.580 -0.255

0.850 0.083 0.490 -0.147 0.490 -0.057 0.650 -0.106

0.900 0.168 0.580 -0.143 0.580 -0.184 0.750 0.134

0.960 0.150 0.640 0.037 0.650 -0.057 0.830 0.292

0.750 0.183 0.750 -0.039 0.900 0.325

0.870 0.259 0.890 0.292 0.960 0.269

0.930 0.210 0.930 0.245

0.960 0.168 0.960 0.031 **

CN = 0.205 0.362 0.374 0.417

689
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 8-59-41-500, MINF = 0.797, Camber = 0/2, ALPT = 4.07, BETA = 1.09, QINF = 591.4,

RNPU = 4.9E+06, CNWP = 0.1505

"q = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 0.003 0.000 0.850 0.000 1.778"* 0.010 -0.868

0.060 -0.120 0.020 -0.197 0.020 -0.413 0,020 -0.909

0.110 -0.251 0.040 -0.241 0.060 -2.001 ** 0.060 -0.696

0.200 -0.179 0,060 -0,307 0,090 -0.330 0.110 -0.332

0.230 -0.195 0.090 -0,244 0.110 -0.348 0.140 -0.498

0.400 -0.171 0.130 -0.276 0.130 -0.385 0.190 -2.249**

0.490 -0.171 0.150 -0.296 0.150 -0.353 0.250 -0.372

0.590 -0.217 0.200 -0,273 0.210 -0.417 0.400 -0.325

0.630 -0.210 0.250 -0.288 0.250 -0.333 0.490 -0.284

0.700 -0.219 0.260 -0.283 0,340 -0.331 0.580 -0.262

0.750 -0.223 0.280 -0.290 0.370 -0.333 0.650 -0.373

0.810 -0.199 0.290 -0.290 0.400 -0,304 0.700 -0.347

0.840 -0.201 0.310 -0.281 0.410 -2.754** 0.750 -0.356

0,900 -0.103 0.320 -0.288 0.430 -0.320 0.800 -0.316"*

0.960 0.014 0.340 -0.277 0.440 -0.308 0.830 -0.308

0.350 -0.236** 0.460 -0.307 0.900 -0.203

0.370 -0.263 0.490 -0.275 0.960 -0.011

0.380 -0.281 0.500 -0.302

0.400 -0.238 0.520 -0.294

0.410 -0.266 0.540 -0.293

0,430 -0.247 0.550 -0.260

0.440 -0.236 0.580 -0.226

0.460 -0.254 0.600 -0.307

0.470 -0.264 0.610 -0.320

0,490 -0.258 0.650 1.083**

0,500 -0.256 0.700 -0.364

0.520 -0,251 0,750 -0.316

0.530 -0,252 0.820 -0.309**

0.550 -0.276 0.890 -0.127

0.560 -0.279 0.900 -0.084

0.580 -0.253 0.960 0.022

0.590 -0.289

0.600 -0.278

0.640 -0.343

0.700 -0.293

0.750 -0.065**

0.820 -0.256

0,870 -0.233

0.930 -0,085

0.960 -0.022

Lower Surface

0.020 -0.569 0.020 -0.348 0.020 -0.138 0.020 0.332

0.110 -0.306 0.060 -0.174 0.060 -0.051 0.060 0.936**

0.230 -0.168 0.090 -0.192 0.090 0.589"* 0.110 -0.128

0.400 -0.107 0.120 -0.240 0.120 -0.185 0.250 -0.297

0.490 -0.093 0.200 -0.181 0.200 -0.268 0.400 -0.269

0.630 0.938** 0.260 -0.245 0.250 -0.284 0.490 -0.286

0.750 0.025 0.400 -0.193 0.400 -0.243 0.580 -0.313

0.850 0.094 0,490 -0.190 0.490 -0.082 0.650 -0.140

0.900 0.183 0.580 -0.180 0.580 -0.238 0.750 0.108

0.960 0.174 0.640 0.005 0.650 -0,067 0.830 0.266

0,750 0.165 0.750 -0.045 0.900 0.303

0.870 0.244 0.890 0.281 0.960 0.260

0.930 0.208 0.930 0.233

0.960 0.167 0.960 - 1.058"*

CN = 0.105 0.188 0.178 0.250

690
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 8-59-54-500, MINF = 0.803, Camber = 0/2, ALPT = 5.10, BETA = 0.77, QINF = 601.9,

RNPU = 4.9E+06, CNWP = 0.2200

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.191 0.000 0.861 0.000 1.741 ** 0.010 -0.821

0.060 -0.243 0.020 -0.560 0.020 -0.536 0.020 - 1.027

0.110 -0.245 0.040 -0.463 0.060 -1.972** 0.060 -0.940

0.200 -0.225 0.060 -0.493 0.090 -0.819 0.110 -0.857

0.230 -0.264 0.090 -0.383 0. l 10 -0.431 0.140 -0.852

0.400 -0.197 0.130 -0.381 0.130 -0.341 0.190 -2.216"*

0.490 -0.191 0.150 -0.377 0.150 -0.366 0.250 -0.350

0.590 -0.248 0.200 -0.349 0.210 -0.481 0.400 -0.353

0.630 -0.228 0.250 -0.351 0.250 -0.387 0.490 -0.310

0.700 -0.233 0.260 -0.342 0.340 -0.376 0.580 -0.303

0.750 -0.235 0.280 -0.344 0.370 -0.376 0.650 -0.396

0.810 -0.212 0.290 -0.340 0.400 -0.338 0.700 -0.373

0.840 -0.215 0.310 -0.327 0.410 -2.712"* 0.750 -0.370

0.900 -0.113 0.320 -0.337 0.430 -0.358 0.800 -0.316"*

0.960 0.008 0.340 -0.322 0.440 -0.343 0.830 -0.303

0.350 -0.223** 0.460 -0.337 0.900 -0.189

0.370 -0.298 0.490 -0.303 0.960 -0.009

0.380 -0.323 0.500 -0.335

0.400 -0.271 0.520 -0.329

0.410 -0.306 0.540 -0.320

0.430 -0.283 0.550 -0.285

0.440 -0.266 0.580 -0.281

0.460 -0.288 0.600 -0.337

0.470 -0.291 0.610 -0.353

0.490 -0.291 0.650 1.058"*

0.500 -0.289 0.700 -0.386

0.520 -0.288 0.750 -0.333

0.530 -0.277 0.820 -0.319"*

0.550 -0.306 0.890 -0.127

0.560 -0.303 0.900 -0.088

0.580 -0.284 0.960 0.019

0.590 -0.314

0.600 -0.306

0.640 -0.377

0.700 -0.321

0.750 -0.059**

0.820 -0.280

0.870 -0.242

0.930 -0.086

0.960 -0.022

Lower Surface

0.020 -0.291 0.020 -0.117 0.020 0.036 0.020 0.440

0.110 -0.244 0.060 -0.057 0.060 0.042 0.060 0.914"*

0.230 -0.077 0.090 -0.092 0.090 0.572** 0.110 -0.054

0.400 -0.087 0.120 -0. | 57 0.120 -0.104 0.250 -0.232

0.490 -0.077 0.200 -0.145 0.200 -0.188 0.400 -0.220

0.630 0.9 |5"* 0.260 -0.193 0.250 -0.217 0.490 -0.250

0.750 0.026 0.400 -0.169 0.400 -0.203 0.580 -0.286

0.850 0.090 0.490 -0.172 0.490 -0.073 0.650 -0.121

0.900 0.178 0.580 -0.170 0.580 -0.2 l I 0.750 0.126

0.960 0.168 0.640 0.025 0.650 -0.063 0.830 0.283

0.750 0.169 0.750 -0.040 0.900 0.312

0.870 0.250 0.890 0.288 0.960 0.271

0.930 0.215 0.930 0.244

0.960 0.173 0.960 -1.046"*

CN = 0.160 0.272 0.284 0.356

691
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-0-1-000, MINF = 0.808, Camber = 0/2, ALPT = 6.03, BETA = 0.86. QINF = 610.7,

RNPU = 5.0E+06, CNWP = 0.2402

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.699 0.000 0.823 0,000 1,713"* 0.010 -1.068

0.060 -0.302 0.020 -0.84.4 0.020 -0.922 0.020 - 1.080

0.110 -0.307 0.040 -0.791 0.060 - 1.947" * 0.060 - 1.046

0.200 -0,268 0.060 -0.847 0.090 -0.956 0.110 -0.949

0.230 -0.327 0.090 -0.789 0.110 -0.938 0.140 -0.956

0,400 -0.226 0.130 -0.827 0.130 -0.903 0.190 -2.187"*

0.490 -0,214 0.150 -0.788 0.150 -0.810 0.250 -0.570

0.590 -0.257 0.200 -0.328 0.210 -0.836 0.400 -0.334

0.630 -0.247 0.250 -0.325 0.250 -0.324 0.490 -0.314

0.700 -0.244 0.260 -0.333 0.340 -0.330 0,580 -0.312

0.750 -0.247 0.280 -0.347 0.370 -0.355 0,650 -0.404

0.810 -0.216 0.290 -0.344 0.400 -0.333 0.700 -0.379

0.840 -0.226 0.310 -0.342 0.410 -2.676'* 0.750 -0.375

0.900 -0.132 0.320 -0.351 0.430 -0.363 0.800 -0.311 **

0.960 -0.013 0,340 -0.344 0.440 -0.351 0.830 -0.298

0.350 -0,212** 0.460 -0.349 0.900 -0.170

0.370 -0.320 0.490 -0.346 0.960 0.003

0.380 -0.341 0.500 -0,345

0.400 -0.297 0.520 -0.336

0.410 -0.325 0.540 -0.332

0.430 -0.298 0.550 -0.302

0.440 -0.287 0.580 -0.290

0.460 -0.309 0.600 -0.352

0.470 -0.318 0.610 -0.358

0.490 -0.306 0.650 1.040"*

0,500 -0.306 . 0.700 -0.401

0,520 -0.303 0.750 -0.342

0.530 -0,297 0.820 -0.322**

0.550 -0.327 0.890 -0.127

0.560 -0.326 0.900 -0.085

0.580 -0.296 0.960 0.021

0.590 -0.337

0.600 -0.331

0,640 -0.387

0.700 -0.325

0.750 -0.061 **

0.820 -0.283

0.870 -0.244

0.930 -0,088

0.960 -0,027

Lower Surface

0,020 -0.097 0.020 0.046 0.020 0.170 0.020 0.465

0.110 -0.181 0.060 0.040 0.060 0.110 0.060 0.898**

0.230 -0,055 0.090 -0.016 0.090 0.561"* 0.t 10 0.023

0.400 -0.081 0.120 -0.084 0.120 -0.051 0.250 -0.183

0.490 -0.075 0.200 -0.096 0.200 -0.126 0.400 -0.184

0.630 0.899** 0.260 -0. t 51 0.250 -0.170 0.490 -0.220

0.750 0.015 0.400 -0.145 0.400 -0.179 0.580 -0,270

0.850 0.072 0.490 -0.155 0.490 -0.071 0.650 -0.112

0,900 0.160 0.580 -0.158 0.580 -0.203 0.750 0.133

0.960 0.150 0.640 0.023 0.650 -0.064 0.830 0.285

0.750 0.170 0.750 -0.044 0,900 0.320

0.870 0.243 0.890 0.293 0.960 0.264

0.930 0.209 0.930 0.241

0.960 0.165 0.960 - 1.034 * *

CN = 0.196 0.364 0.352 0.426

692
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-0-7-000, MINF = 0.806, Camber = 0/2, ALPT = 7.06, BETA = 0.86, QINF = 606.9,

RNPU = 5.0E+06, CNWP = 0.2613

"q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.934 0.000 0.765 0.000 1.726" * 0.010 - 1.103

0.060 -0.856 0.020 -0.989 0.020 - 1.056 0.020 - 1.218

0.110 -0.796 0.040 -0.882 0.060 - 1.956** 0.060 - 1.177

0.200 -0.247 0.060 -0.980 0.090 - 1.087 0.110 - 1.062

0.230 -0.317 0.090 -0.978 0.110 - 1.059 0.140 - 1.058

0.400 -0.240 0.130 -0.873 0.130 - 1.056 0.190 -2.198"*

0.490 -0.222 0.150 -0.979 0.150 -0.955 0.250 - 1.082

0.590 -0.264 0.200 -0.889 0.210 -0.972 0.400 -0.323

0.630 -0.256 0.250 -0.900 0.250 -0.95 l 0.490 -0.283

0.700 -0.248 0.260 -0.908 0.340 -0.374 0.580 -0.284

0.750 -0.263 0.280 -0.455 0.370 -0.282 0.650 -0.366

0.810 -0.232 0.290 -0.283 0.400 -0.234 0.700 -0.341

0.840 -0.233 0.310 -0.227 0.410 -2.690* * 0.750 -0.339

0.900 -0.150 0.320 -0.219 0.430 -0.252 0.800 -0.276**

0.960 -0.033 0.340 -0.202 0.440 -0.247 0.830 -0.265

0.350 -0.130** 0.460 -0.256 0.900 -0.124

0.370 -0.202 0.490 -0.238 0.960 0.011

0.380 -0.232 0.500 -0.284

0.400 -0.208 0.520 -0.286

0.410 -0.244 0.540 -0.278

0.430 -0.233 0.550 -0.258

0.440 -0.233 0.580 -0.256

0.460 -0.262 0.600 -0.309

0.470 -0.269 0.610 -0.317

0.490 -0.271 0.650 1.049**

0.500 -0.274 0.700 -0.363

0.520 -0.276 0.750 -0.324

0.530 -0.272 0.820 -0.306"*

0.550 -0.301 0.890 -0.123

0.560 -0.304 0.900 -0.079

0.580 -0.278 0.960 0.016

0.590 -0.334

0.600 -0.306

0.640 -0.370

0.700 -0.325

0.750 -0.049**

0.820 -0.277

0.870 -0.239

0.930 -0.088

0.960 -0.028

Lower Surface

0.020 0.035 0.020 0.186 0.020 0.273 0.020 0.611

0.110 -0.127 0.060 0.132 0.060 0.211 0.060 0.906**

0.230 -0.021 0.090 0.065 0.090 0.567** 0.110 0.103

0.400 -0.061 0.120 -0.010 0.120 0.018 0.250 -0.119

0.490 -0.055 0.200 -0.035 0.200 -0.029 0.400 -0.137

0.630 0.907"* 0.260 -0.092 0.250 -0.111 0.490 -0.179

0.750 0.013 0.400 -0.1 04 0.400 -0.132 0.580 -0.233

0.850 0.063 0.490 -0.134 0.490 -0.062 0.650 -0.092

0.900 0.148 0.580 -0.136 0.580 -0.181 0.750 0.148

0.960 0.138 0.640 0.039 0.650 -0.058 0.830 0.289

0.750 0.189 0.750 -0.040 0.900 0.325

0.870 0.254 0.890 0.299 0.960 0.264

0.930 0.211 0.930 0.249

0.960 0.167 0.960 - 1.038" *

CN = 0.285 0.454 0.435 0.536

693
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-0-16-500, MINF = 0.801, Camber = 0/2, ALPT = 8.05, BETA = 0.80, QINF = 602.8,

RNPU = 4.9E+06, CNWP = 0.3377

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x.,'c CP x/c CP x/c CP

0.020 - 1.081 0.000 0,674 0,000 1.723 ** 0.010 - 1.257

0.060 - 1.064 0,020 - 1.133 0,020 - 1.185 0.020 - 1.338

0.110 - 1.005 0.040 -0,972 0.060 - 1.985** 0.060 - 1.286

0.200 -0.367 0.060 -1.112 0.090 -1,210 0.110 -1.212

0.230 -0,271 0.090 -1.119 0.110 -1.174 0.140 -1,221

0.400 -0.236 0.130 -0.894 0.130 - 1.174 0.190 -2.228"*

0,490 -0.227 0.150 - 1.076 0.150 - 1.074 0.250 - 1.214

0,590 -0.268 0.200 - 1.026 0.210 - 1.099 0.400 -0.467

0,630 -0,269 0,250 - 1.038 0,250 -0,973 0.490 -0.285

0.700 -0,265 0,260 - 1.047 0,340 - 1.157 0.580 -0.260

0.750 -0.275 0,280 - 1.069 0,370 -0,645 0.650 -0.315

0.810 -0.246 0.290 - 1.074 0.400 -0,472 0.700 -0,302

0.840 -0.258 0.310 -0.845 0.410 -2,724** 0.750 -0,281

0,900 -0,189 0.320 -1.035 0.430 -0.390 0.800 -0,230**

0,960 -0,060 0.340 -0.519 0.440 -0.333 0.830 -0.206

0.350 -0,229"* 0.460 -0.289 0,900 -0.100

0.370 -0.316 0,490 -0.215 0.960 -0.010

0.380 -0.289 0,500 -0.224

0.400 -0.202 0,520 -0.217

0,410 -0.192 0.540 -0.212

0.430 -0.164 0,550 -0.191

0.440 -0.177 0.580 -0.192

0,460 -0,166 0.600 -0,238

0.470 -0.184 0.610 -0,246

0.490 -0.185 0.650 1.041 **

0.500 -0.217 0.700 -0.298

0,520 -0.199 0.750 -0,274

0.530 -0.209 0,820 -0,259**

0.550 -0,241 0.890 -0.103

0.560 -0,246 0.900 -0.069

0,580 -0.223 0.960 0,023

0,590 -0.272

0.600 -0.261

0,640 -0.323

0.700 -0,294

0.750 -0.037**

0,820 -0.264

0,870 -0.231

0.930 -0.086

0,960 -0.035

Lower Surface

0.020 O. 112 0.020 0.315 0.020 0.381 0.020 0.685

0.110 -0.071 0.060 0,209 0.060 0.266 0.060 0,897"*

0,230 -0,012 0.090 0,131 0.090 0.556** 0.110 0,157

0.400 -0,048 0.120 0.047 0.120 0,082 0.250 -0,064

0.490 -0.053 0.200 0.016 0,200 0.059 0.400 -0.094

0.630 0,898 ** 0.260 -0,044 0.250 -0,048 0,490 -0.141

0.750 0.005 0.400 -0.079 0.400 -0,092 0,580 -0,201

0.850 0,054 0.490 -0.105 0.490 -0.038 0.650 -0.072

0,900 0,131 0.580 -0.118 0.580 -0,151 0.750 0,153

0.960 0.124 0.640 0.047 0.650 -0.038 0.830 0.299

0.750 0,179 0.750 -0.016 0,900 0.326

0.870 0.251 0.890 0.298 0.960 0.256

0.930 0.204 0,930 0.245

0.960 0.161 0.960 - 1.060"*

CN = 0.33t 0,541 0,541 0,613

694
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-0-22-500, MINF = 0.807, Camber = 0/2, ALPT = 8.09, BETA = 0.74, QINF = 623.8,

RNPU = 5. IE+06, CNWP = 0.3411

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 - 1.078 0.000 0.676 0.000 1.625 ** 0.010 - 1.243

0.060 - 1.053 0.020 - 1.130 0.020 - 1.170 0.020 - 1.321

0.110 -1.014 0.040 -0.979 0.060 -1.957"* 0.060 -1.282

0.200 -0.775 0.060 -1.110 0.090 -1.193 0.110 -1.212

0.230 -0.625 0.090 -1.116 0.110 -l. 170 0.140 -1.229

0.400 -0.219 0.130 -0.903 0.130 -1.172 0.190 -2.192"*

0.490 -0.220 0.150 - 1.079 0.150 - 1.072 0.250 - 1.214

0.590 -0.259 0.200 - 1.022 0.210 - 1.098 0.400 -0.754

0.630 -0.262 0.250 - 1.041 0.250 -0.979 0.490 -0.315

0.700 -0.258 0.260 - 1.045 0.340 - I. 160 0.580 -0.262

0.750 -0.270 0.280 - 1.065 0.370 - 1.157 0.650 -0.298

0.810 -0.243 0.290 - 1.082 0.400 -0.724 0.700 -0.287

0.840 -0.260 0.310 -0.856 0.410 -2.671 ** 0.750 -0.265

0.900 -0.183 0.320 - 1.059 0.430 -0.509 0.800 -0.217"*

0.960 -0.062 0.340 -0.895 0.440 -0.459 0.830 -0.189

0.350 -0.495"* 0.460 -0.416 0.900 -0.090

0.370 -0.592 0.490 -0.326 0.960 -0.008

0.380 -0.473 0.500 -0.300

0.400 -0.357 0.520 -0.273

0.410 -0.320 0.540 -0.236

0.430 -0.251 0.550 -0.189

0.440 -0.206 0.580 -0.168

0.460 -0.182 0.600 -0.200

0.470 -0.154 0.610 -0.204

0.490 -0.148 0.650 0.966"*

0.500 -0.150 0.700 -0.249

0.520 -0.149 0.750 -0.245

0.530 -0.156 0.820 -0.236**

0.550 -0.187 0.890 -0.090

0.560 -0.200 0.900 -0.060

0.580 -0.189 0.960 0.030

0.590 -0.227

0.600 -0.225

0.640 -0.285

0.700 -0.267

0.750 -0.033**

0.820 -0.257

0.870 -0.220

0.930 -0.076

0.960 -0.024

Lower Surface

0.020 0.185 0.020 0.335 0.020 0.393 0.020 0.697

0.110 -0.067 0.060 0.215 0.060 0.265 0.060 0.862**

0.230 -0.024 0.090 0.142 0.090 0.498" * 0. t l0 0.163

0.400 -0.049 0.120 0.059 0.120 0.089 0.250 -0.058

0.490 -0.046 0.200 0.024 0.200 0.056 0.400 -0.087

0.630 0.829** 0.260 -0.040 0.250 -0.041 0.490 -0.142

0.750 0.009 0.400 -0.072 0.400 -0.085 0.580 -0.209

0.850 0.052 0.490 -0.102 0.490 -0.042 0.650 -0.07 l

0.900 0.136 0.580 -0.114 0.580 -0.144 0.750 0.154

0.960 0.123 0.640 0.047 0.650 -0.035 0.830 0.302

0.750 0.183 0.750 -0.016 0.900 0.331

0.870 0.244 0.890 0.302 0.960 0.257

0.930 0.205 0.930 0.250

0.960 0.163 0.960 - 1.029"*

CN = 0.380 0.556 0.566 0.649

695
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-0-30-000, MINF = 0.800, Camber = 0/2, ALPT = 9.03, BETA = 0,69, QINF = 618.6,

RNPU = 5.1E+06, CNWP = 0.4026

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -1.217 0.000 0.590 0.000 1.615'* 0.010 -1.358

0.060 - 1.174 0.020 - 1.244 0.020 - 1.310 0.020 - 1,426

0.I 10 -1.132 0.040 -1.011 0.060 -1.998"* 0.060 -1.407

0.200 -0.878 0.060 - 1.245 0.090 - 1.294 0.110 - 1.333

0.230 -0.785 0.090 - 1.150 0.110 - 1.282 0.140 - 1.352

0.400 -0.215 0.130 -0.935 0.130 - 1.291 0.190 -2.235" *

0.490 -0.222 0.150 -1.112 0.150 -1.175 0.250 -1.314

0.590 -0.274 0,200 - 1.112 0.210 - 1.162 0.400 -0.769

0.630 -0.276 0.250 - 1.152 0.250 - 1.011 0.490 -0.380

0.700 -0.274 0.260 - 1.154 0.340 - 1.262 0.580 -0.265

0.750 -0.282 0.280 -1.112 0.370 - 1.249 0.650 -0.281

0.810 -0.255 0.290 - 1.119 0.400 -0.699 0.700 -0.270

0.840 -0.272 0.310 -0.887 0.410 -2.718** 0.750 -0.237

0,900 -0.210 0.320 - 1.122 0.430 -0.602 0.800 -0.185 **

0.960 -0.088 0.340 -0.927 0.440 -0.575 0.830 -0.166

0.350 -0.525"* 0.460 -0.555 0.900 -0.084

0.370 -0.739 0.490 -0.494 0.960 -0.011

0.380 -0.598 0.500 -0.488

0.400 -0.500 0.520 -0.462

0.410 -0.483 0.540 -0.425

0.430 -0.431 0.550 -0.363

0.440 -0,408 0.580 -0,280

0,460 -0.349 0.600 -0.300

0.470 -0.317 0.610 -0.259

0.490 -0.258 0.650 0.951 **

0.500 -0.246 0.700 -0.216

0.520 -0.194 0,750 -0.210

0.530 -0.174 0.820 -0.184"*

0.550 -0.184 0.890 -0.069

0,560 -0.178 0.900 -0.047

0.580 -0.159 0,960 0.028

0.590 -0.192

0.600 -0.190

0.640 -0.235

0.700 -0.241

0,750 -0.012"*

0.820 -0.229

0.870 -0.206

0.930 -0.079

0,960 -0.024

Lower Surface

0.020 0.232 0.020 0.411 0.020 0.459 0.020 0.749

0.110 -0.025 0.060 0,276 0.060 0.330 0.060 0.845**

0.230 -0.015 0.090 0.199 0.090 0.478" * 0.110 0.221

0.400 -0.036 0.120 0.I 10 0.120 0.137 0.250 -0.015

0.490 -0.040 0.200 0.063 0.200 0.093 0.400 -0.053

0.630 0.915 ** 0.260 0.003 0.250 0.004 0.490 -0.107

0.750 0.009 0.400 -0.048 0.400 -0.050 0.580 -0.165

0.850 0.044 0.490 -0.076 0.490 -0.018 0.650 -0,055

0.900 0.125 0.580 -0,094 0.580 -0.121 0.750 0.164

0,960 0.116 0.640 0.064 0.650 -0.018 0.830 0.302

0.750 0.188 0.750 0.021 0.900 0.328

0.870 0.248 0.890 0.297 0.960 0.255

0.930 0.207 0.930 0.240

0,960 0.155 0.960 - 1.062"*

CN = 0.438 0.616 0.644 0.713

696
Table J-2. Continued.

Flight 223, Wing sweep = 26", Time = 9-0-35-500, MINF = 0.795, Camber = 0/2, ALPT = 10.00, BETA = 0.74, QINF = 613.8o

RNPU = 5.1E+06, CNWP = 0.3760

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -1.327 0.000 0.488 0.000 1.619"* 0.010 -1.487

0.060 -1.300 0.020 - 1.370 0.020 - 1.417 0.020 -I .520

0.110 - 1.230 0.040 - 1.027 0.060 -2.022"* 0.060 - 1.500

0.200 -0.988 0.060 - 1.349 0.090 - 1.306 0.110 - 1.419

0.230 -0.887 0.090 -1.167 0.110 -1.360 0.140 -1.447

0.400 -0.226 0.130 -0.950 0.130 - 1.391 0.190 -2.261 * *

0.490 -0.249 0.150 - 1.129 0.150 - 1.254 0.250 - 1.414

0.590 -0.292 0.200 -1.126 0.210 -1.180 0.400 -0.763

0.630 -0.293 0.250 - 1.235 0.250 - 1.028 0.490 -0.435

0.700 -0.286 0.260 -1.147 0.340 -0.804 0.580 -0.280

0.750 -0.291 0.280 -0.922 0.370 -0.7 l 3 0.650 -0.25 l

0.810 -0.266 0.290 -0.756 0.400 -0.663 0.700 -0.225

0.840 -0.287 0.310 -0.700 0.4 l0 -2.747"* 0.750 -0.182

0.900 -0.224 0.320 -0.708 0.430 -0.660 0.800 -0.170"*

0.960 -0.104 0.340 -0.697 0.440 -0.641 0.830 -0.150

0.350 -0.329** 0.460 -0.629 0.900 -0.099

0.370 -0.648 0.490 -0.593 0.960 -0.054

0.380 -0.677 0.500 -0.590

0.400 -0.615 0.520 -0.578

0.410 -0.607 0.540 -0.555

0.430 -0.574 0.550 -0.515

0.440 -0.556 0.580 -0.497

0.460 -0.543 0.600 -0.477

0.470 -0.518 0.610 -0.439

0.490 -0.472 0.650 0.950**

0.500 -0.475 0.700 -0.331

0.520 -0.429 0.750 -0.299

0.530 -0.422 0.820 -0.195**

0.550 -0.393 0.890 -0.086

0.560 -0.375 0.900 -0.079

0.580 -0.340 0.960 -0.018

0.590 -0.36 l

0.600 -0.309

0.640 -0.250

0.700 -0.232

0.750 -0.005**

0.820 -0.176

0.870 -0.137

0.930 -0.082

0.960 -0.062

Lower Surface

0.020 0.319 0.020 0.478 0.020 0.535 0.020 0.752

0.110 0.014 0.060 0.331 0.060 0.377 0.060 0.843"*

0.230 0.003 0.090 0.244 0.090 0.474** 0.110 0.272

0.400 -0.032 0.120 0.152 0.120 0.197 0.250 0.033

0.490 -0.039 0.200 0.1 04 0.200 0.127 0.400 -0.016

0.630 0.950"* 0.260 0.036 0.250 0.041 0.490 -0.074

0.750 0.003 0.400 -0.020 0.400 -0.025 0.580 -0.144

0.850 0.039 0.490 -0.065 0.490 0.001 0.650 -0.039

0.900 0.120 0.580 -0.094 0.580 -0.106 0.750 0.170

0.960 0.103 0.640 0.057 0.650 -0.002 0.830 0.303

0.750 0.174 0.750 0.025 0.900 0.324

0.870 0.231 0.890 0.287 0.960 0.226

0.930 0.1 64 0.930 0.225

0.960 0. l I 1 0.960 -1.079"*

CN = 0.483 0.648 0.677 0.766

697
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 10-31-44-000, MINF = 0.796, Camber = 10/2, ALPT = 4.13, BETA = 0.63, QINF = 595.1,

RNPU = 4.9E+06, CNWP = 0.2126

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 0.588 0.000 0.055 0.000 0.466** 0.010 0.399

0.060 0.102 0.020 0.586 0.020 0.570 0.020 0.228

0.110 -0.282 0.040 0.355 0.060 0.609** 0.060 -0.304

0.200 -0.315 0.060 -0.008 0.090 -0.304 0.110 -0.672

0.230 -0.334 0.090 -0.252 0.110 -0.529 0.140 - 1.115

0.400 -0.199 0.130 -0.546 0.130 -2.256* * 0.190 -2.256"*

0.490 -0.184 0.150 -0.833 0.150 -0.973 0.250 -0.365

0.590 -0.217 0.200 -0.918 0.210 -0,977 0.400 -0.336

0.630 -0.222 0.250 -0.329 0.250 -0.323 0.490 -0.293

0.700 -0.221 0.260 -0.332 0.340 -0.336 0.580 -0.295

0.750 -0.231 0.280 -0.341 0.370 -0.346 0.650 -0.378

0.810 -0.211 0.290 -0.337 0.400 -0.309 0.700 -0.352

0.840 -0.218 0.310 -0.321 0.410 -1.036"* 0.750 -0.363

0.900 -0.122 0.320 -0.332 0.430 -0.332 0.800 -0.330

0.960 -0.006 0.340 -0.319 0.440 -0.324 0.830 -0.304

0.350 -0.199"* 0.460 -0.320 0.900 -0.200

0.370 -0.305 0.490 -0.299 0.960 -0.015

0.380 -0.312 0.500 -0.315

0.400 -0.278 0.520 -0.309

0.410 -0.294 0.540 -0.303

0.430 -0.272 0.550 -0.287

0.440 -0.267 0.580 -0.287

0.460 -0.277 0.600 -0.315

0.470 -0.290 0.610 -0.330

0.490 -0.282 0.650 -0.358

0.500 -0.274 0.700 -0.365

0.520 -0.273 0.750 -0.317

0.530 -0.271 0.820 -0.320

0.550 -0.293 0.890 -0.132

0,560 -0.290 0,900 -0.097

0.580 -0.260 0.960 0.019

0.590 -0.295

0.600 -0.287

0.640 -0.355

0.700 -0.305

0.750 -0.062**

0.820 -0.271

0.870 -0.234

0.930 -0.093

0.960 -0.026

Lower Surface

0.020 -0.995 0.020 -0.648 0.020 -0.850 0.020 -0.864

0.110 -0.396 0.060 -0.533 0.060 -0.680 0.060 -0.030

0.230 -0.116 0.090 -0.497 0.090 -0.487 0.110 -0.292

0.400 -0.069 0.120 -0.394 0.120 -0.331 0.250 -0.234

0.490 -0.045 0.200 -0.116 0.200 -0.109 0.400 -0.256

0.630 0.926** 0.260 -0.235 0.250 -0.150 0.490 -0.276

0.750 0.027 0.400 -0.127 0.400 -0.199 0.580 -0308

0.850 0.059 0.490 -0.110 0.490 -0.085 0.650 -0.153

0.900 0.134 0.580 -0.092 0.580 -0.199 0.750 0.113

0.960 0.135 0.640 0.019 0.650 -0.066 0.830 0.242

0.750 0.106 0.750 -0.041 0.900 0,293

0.870 0.167 0.890 0.272 0.960 0.252

0.930 0.175 0.930 0.221

0.960 0. t49 0.960 0.209

CN = 0.127 0.203 0.230 0.259

698
Table J-2. Continued.

Flight 211, Wing sweep = 26", Time = 10-32-11-500, MINF = 0.800, Camber = 10/2, ALPT = 5.00, BETA = 0.28, QINF = 597.9,

RNPU = 4.9E+06, CNWP = 0.2623

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.536 0,000 0.151 0.000 0.536"* 0.010 0.280

0.060 0.030 0.020 0.525 0.020 0.506 0.020 0.121

0.110 -0.322 0.040 0.299 0.060 0.573** 0,060 -0,430

0.200 -0.600 0.060 -0.064 0.090 -0.356 0.110 -0.734

0.230 -0.269 0.090 -0.308 0.110 -0.586 0.140 - 1.173

0.400 -0.222 0. 130 -0.580 0.130 -2.232 * * 0.190 -2.232 * *

0.490 -0.199 0.150 -0.877 0.150 - 1.025 0.250 -0.787

0.590 -0.238 0.200 -0.977 0.210 - 1.038 0.400 -0.349

0.630 -0.240 0.250 -0.870 0.250 -0,959 0.490 -0.316

0.700 -0.240 0.260 -0.461 0.340 -0.297 0.580 -0.315

0.750 -0.245 0.280 -0.336 0.370 -0.322 0.650 -0.398

0.810 -0.222 0.290 -0.284 0.400 -0.297 0,700 -0.368

0.840 -0.226 0.310 -0.269 0.410 -1.018"* 0.750 -0.377

0.900 -0.128 0.320 -0.282 0.430 -0.325 0.800 -0.330

0.960 -0.015 0.340 -0.284 0.440 -0.329 0.830 -0.309

0.350 -0.173"* 0.460 -0.326 0,900 -0.196

0.370 -0.290 0.490 -0,307 0.960 -0.016

0.380 -0.303 0,500 -0.329

0.400 -0,273 0.520 -0.326

0.410 -0.292 0.540 -0.317

0.430 -0.271 0.550 -0.299

0.440 -0.271 0.580 -0,296

0.460 -0.286 0.600 -0.326

0.470 -0.300 0.610 -0.350

0.490 -0.288 0.650 -0.387

0.500 -0.293 0,700 -0.392

0.520 -0.277 0.750 -0.329

0.530 -0,287 0.820 -0.332

0.550 -0.307 0.890 -0.136

0.560 -0,309 0.900 -0.103

0.580 -0,276 0.960 0.018

0.590 -0.304

0.600 -0.302

0.640 -0.376

0.700 -0.325

0.750 -0.059**

0.820 -0.289

0.870 -0.244

0,930 -0.094

0.960 -0,031

Lower Surface

0.020 - 1.120 0.020 -0.642 0.020 -0.730 0.020 -0.722

0.110 -0.299 0.060 -0.481 0,060 -0,492 0.060 -0.017

0.230 -0.081 0.090 -0.408 0.090 -0.271 0.110 -0.180

0.400 -0.042 0.120 -0.296 0.120 -0.167 0.250 -0.185

0.490 -0.042 0.200 -0.080 0.200 -0.079 0.400 -0.223

0.630 0.934** 0.260 -0.127 0.250 -0.114 0,490 -0.250

0.750 0.034 0.400 -0.105 0.400 -0.167 0.580 -0.292

0.850 0.061 0,490 -0.103 0,490 -0.078 0.650 -0.143

0.900 0.136 0.580 -0.1 04 0.580 -0.197 0.750 0.121

0.960 0.129 0.640 0.042 0.650 -0.063 0.830 0.253

0.750 0.129 0.750 -0.042 0.900 0.299

0.870 0.197 0.890 0.284 0.960 0.255

0.930 0.184 0.930 0.233

0.960 0.152 0.960 0.225

CN = 0.181 0.271 0.321 0.360

699
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 10-32-18-500, MINF = 0.791, Camber = 10/2, ALPT = 6.07, BETA = 0.37, QINF = 579.8,

RNPU = 4.8E+06, CNWP = 0.2747

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.468 0.000 0.279 0.000 0.588 ** 0.010 0.130

0.060 -0.053 0.020 0.467 0.020 0.403 0.020 -0.023

0.110 -0.396 0.040 0.211 0.060 0.475** 0.060 -0.603

0.200 - 1.108 0.060 -0.173 0.090 -0.454 0.110 -0.906

0.230 -0.522 0.090 -0.393 0.110 -0.678 0.140 - 1.270

0.400 -0.224 0.130 -0.676 0.130 -2.281 * * 0.190 -2.281 * *

0.490 -0.209 0.150 -0.968 0.150 - 1.104 0.250 -0.970

0.590 -0.238 0.200 - 1.068 0.210 - 1.144 0.400 -0.379

0.630 -0.246 0.250 - 1.084 0.250 -0.968 0.490 -0.332

0.700 -0.240 0.260 - 1.076 0.340 -0.418 0.580 -0.339

0.750 -0.239 0.280 - 1.086 0.370 -0.327 0.650 -0.402

0.810 -0.220 0.290 -0.915 0.400 -0.267 0.700 -0.376

0.840 -0.231 0.310 -0.483 0.410 - 1.029"* 0.750 -0,372

0.900 -0.137 0.320 -0.457 0.430 -0.298 0.800 -0.311

0.960 -0.027 0.340 -0.322 0.440 -0.299 0.830 -0.296

0,350 -0.157 ** 0.460 -0.299 0.900 -0.170

0.370 -0.240 0.490 -0.283 0.960 0.005

0.380 -0.244 0.500 -0.311

0.400 -0.222 0.520 -0.314

0.410 -0.246 0.540 -0.306

0.430 -0.243 0.550 -0.295

0.440 -0.244 0.580 -0.292

0.460 -0.260 0.600 -0.324

0.470 -0.276 0.610 -0.340

0.490 -0.275 0.650 -0.358

0.500 -0.277 0.700 -0.370

0.520 -0.268 0.750 -0.322

0.530 -0.276 0.820 -0.318

0.550 -0.303 0.890 -0.131

0.560 -0.302 0.900 -0.101

0.580 -0.272 0.960 0.017

0.590 -0.307

0.600 -0.298

0.640 -0.365

0.700 -0.318

0.750 -0.048"*

0.820 -0.281

0.870 -0.240

0.930 -0.096

0.960 -0.030

Lower Surface

0.020 - 1.049 0.020 -0.680 0.020 -0.740 0.020 -0.389

0.110 -0.165 0.060 -0.302 0.060 -0.099 0.060 -0.027

0,230 -0.053 0.090 -0.160 0.090 -0.035 0.110 -0.057

0.400 -0.042 0.120 -0.049 0.120 -0.040 0.250 -0.116

0.490 -0.041 0.200 -0.054 0.200 -0.054 0.400 -0.161

0.630 0.984** 0.260 -0.021 0.250 -0.067 0.490 -0.202

0.750 0.020 0.400 -0.083 0.400 -0.130 0.580 -0.247

0.850 0.055 0.490 -0.101 0.490 -0.064 0.650 -0. I 18

0.900 0.140 0.580 -0.114 0.580 -0.182 0.750 0.138

0.960 0.127 0.640 0.043 0.650 -0.050 0.830 0,265

0.750 0.155 0.750 -0.030 0.900 0.310

0.870 0.212 0.890 0.299 0.960 0.258

0.930 0.197 0.930 0.242

0.960 0.159 0.960 0.210

CN = 0.258 0.372 0.394 0.456

700
Table J-2. Continued.

Flight 211, Wing sweep = 26", Time = 10-32-35-500, MINF = 0.809, Camber = 10/2, ALPT = 7.98, BETA = 0.74, QINF = 606.2,

RNPU = 4.9E+06, CNWP = 0.4022

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x,/c CP

0.020 0.352 0.000 0.522 0.000 0.726** 0.010 -0.048

0.060 -0.171 0.020 0.292 0.020 0.207 0.020 -0.173

0.110 -0.462 0.040 -0.007 0.060 0.338** 0.060 -0.780

0.200 - 1.154 0.060 -0.296 0.090 -0.592 O. 110 - 1.085

0.230 -1.125 0.090 -0.490 0.110 -0.748 0.140 -1.386

0.400 -0.318 0.130 -0.748 0.130 -2.181"* 0.190 -2.181"*

0.490 -0.147 0.150 -1.010 0.150 -1.129 0.250 -1.391

0.590 -0.204 0.200 - 1.110 0.210 - I. 185 0.400 -0.819

0.630 -0.238 0.250 - 1.170 0.250 -0.926 0.490 -0.462

0.700 -0.230 0.260 - I. 155 0.340 - 1.227 0.580 -0.336

0.750 -0.249 0.280 - I. 134 0.370 - 1.225 0.650 -0.345

0.810 -0.231 0.290 - 1.134 0.400 - 1.165 0.700 -0.330

0.840 -0.25 l 0.310 -0.834 0.410 -0.984** 0.750 -0.309

0.900 -0.177 0.320 - 1.145 0.430 - 1.221 0.800 -0.233

0.960 -0.061 0.340 -0.889 0.440 - 1.017 0.830 -0.210

0.350 -0.514** 0.460 -0.696 0.900 -0.099

0.370 -0.957 0.490 -0.589 0.960 -0.009

0.380 - 1.176 0.500 -0.563

0.400 - 1.115 0.520 -0.544

0.410 -0.851 0.540 -0.507

0.430 - l. 105 0.550 -0.450

0.440 -0.787 0.580 -0.395

0.460 -0.734 0.600 -0.361

0.470 -0.544 0.610 -0.311

0.490 -0.469 0.650 -0.216

0.500 -0.421 0.700 -0.220

0.520 -0.388 0.750 -0.214

0.530 -0.323 0.820 -0.209

0.550 -0.280 0.890 -0.084

0.560 -0.238 0.900 -0.060

0.580 -0.193 0.960 0.034

0.590 -0.180

0.600 -0.152

0.640 -0.197

0.700 -0.205

0.750 -0.024**

0.820 -0.229

0.870 -0.201

0.930 -0.065

0.960 -0.015

Lower Surface

0.020 -0.559 0.020 -0.392 0.020 -0.216 0.020 0.006

0.110 -0.048 0.060 0.054 0.060 0.133 0.060 -0.025

0.230 0.005 0.090 0.043 0.090 0.108 0. l I 0 0.085

0.400 -0.029 0.120 0.092 0.120 0.078 0.250 -0.018

0.490 -0.047 0.200 0.000 0.200 -0.004 0.400 -0.085

0.630 0.942"* 0.260 0.048 0.250 0.018 0.490 -0.138

0.750 0.009 0.400 -0.037 0.400 -0.066 0.580 -0.202

0.850 0.042 0.490 -0.075 0.490 -0.036 0.650 -0.088

0.900 0.134 0.580 -0.108 0.580 -0.151 0.750 0.161

0.960 0.120 0.640 0.054 0.650 -0.025 0.830 0.285

0.750 0.167 0.750 -0.014 0.900 0.322

0.870 0.240 0.890 0.315 0.960 0.253

0.930 0.212 0.930 0.254

0.960 0.172 0.960 0.208

CN = 0.365 0.544 0.595 0.643

701
Table J-2. Continued.

Hight 211, Wing sweep = 26 °, Time = 10-32-37-000, MINF = 0.812, Camber = 10/2, ALPT = 8.05, BETA = 0.54, QINF = 611.8,

RNPU = 5.0E+06, CNWP = 0.4026

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.353 0.000 0.522 0.000 0.730** 0.010 -0.084

0.060 -0.164 0.020 0.281 0.020 0.206 0.020 -0.181

0.110 -0.457 0.040 -0.010 0.060 0.332" * 0.060 -0.772

0.200 - 1.149 0.060 -0.300 0.090 -0.607 O. 110 - 1.074

0.230 -1.123 0.090 -0.485 0.110 -0.745 0.140 -1.372

0.400 -0.344 O. 130 -0.744 O. 130 -2.168 ** O. 190 -2.168 **

0.490 -0.140 0.150 -1.006 0.150 -1.118 0.250 -1.385

0.590 -0.198 0.200 -1.102 0.210 -1.181 0.400 -0.837

0.630 -0.231 0.250 - 1.1 64 0.250 -0.924 0.490 -0.498

0.700 -0.222 0.260 - I. 150 0.340 - 1.222 0.580 -0.337

0.750 -0.238 0.280 - 1.130 0.370 - 1.213 0.650 -0.342

0.810 -0.221 0.290 - 1.130 0.400 - I. 161 0.700 -0.327

0.840 -0.241 0.310 -0.833 0.410 -0.981 ** 0.750 -0.302

0.900 -0.172 0.320 - 1.140 0.430 - 1.217 0.800 -0.226

0.960 -0.058 0.340 -0.887 0.440 - 1.209 0.830 -0.203

0.350 -0.508** 0.460 -0.709 0.900 -0.093

0.370 -0.955 0.490 -0.608 0.960 -0.004

0.380 - 1.172 0.500 -0.571

0.400 -1.115 0.520 -0.555

0.410 -0.850 0.540 -0.515

0.430 - 1.1 O0 0.550 -0.469

0.440 -0.786 0.580 -0.408

0.460 -0.966 0.600 -0.380

0.470 -0.599 0.610 -0.334

0.490 -0.486 0.650 -0.209

0.500 -0.443 0.700 -0.217

0.520 -0.403 0.750 -0.204

0.530 -0.342 0.820 -0.194

0.550 -0.303 0.890 -0.076

0.560 -0.259 0.900 -0.052

0.580 -0.210 0.960 0.038

0.590 -0.193

0.600 -0.157

0.640 -0.178

0.700 -0.186

0.750 -0.021"*

0.820 -0.217

0.870 -0.189

0.930 -0.066

0,960 -0.012

Lower Surface

0.020 -0.532 0.020 -0.379 0.020 -0.213 0.020 O. 101

O. 110 -0.048 0.060 0.052 0.060 O. 133 0.060 -0.031

0.230 0.006 0.090 0.043 0.090 O. 110 0.110 O. 119

0.400 -0.032 O. 120 0.092 O. 120 0.078 0.250 -0.018

0.490 -0.046 0.200 0.001 0.200 0.010 0.400 -0.087

0.630 0.927** 0.260 0.049 0.250 0.0 t 8 0.490 -0.140

0.750 0.006 0.400 -0,038 0.400 -0.065 0.580 -0.211

0.850 0.040 0.490 -0.075 0.490 -0.035 0.650 -0.090

0.900 O. 127 0.580 -0.108 0.580 -0.152 0.750 O.160

0.960 O. 119 0.640 0.049 0.650 -0.027 0.830 0.283

0.750 O. 162 0.750 -0.013 0.900 0.323

0.870 0.225 0.890 0.313 0.960 0.254

0.930 0.211 0.930 0.245

0.960 O. 171 0.960 0.209

CN = 0.363 0.542 0.597 0.646

702
Table J-2. Continued.

Flight 223, Wing sweep = 26", Time = 10-7-25-000, MINF = 0.691, Camber = 5/15, ALPT = 3.01, BETA = 0.66, QINF = 310.4,

RNPU = 2.8E+06. CNWP = 0.3089

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0,020 0.338 0.000 0.464 0.000 3.750* * 0.010 -0,086

0.060 0.011 0.020 0.196 0.020 0.162 0,020 -0,088

0.110 -0,039 0.040 0.050 0.060 -3.465"* 0.060 -0,424

0.200 -0.283 0.060 -0.176 0.090 -0.353 0.110 -0.575

0.230 -0.241 0.090 -0.287 0.110 -0,508 0.140 -0.544

0,400 -0.217 0.130 -0.419 0.130 -0.604 0.190 -2.994 * *

0.490 -0.256 0.150 -0.513 0.150 -0.562 0,250 -0.384

0.590 -0.374 0.200 -0.410 0.210 -0,485 0.400 -0.376

0,630 -0.407 0.250 -0.369 0.250 -0.357 0.490 -0.355

0.700 -0.559 0.260 -0.346 0.340 -0.405 0.580 -0.375

0.750 -0.748 0,280 -0.356 0.370 -0.418 0.650 -0.548

0.810 -0.686 0,299 -0.356 0.400 -0.335 0.700 -0.537

0.840 -0,727 0.310 -0.354 0.410 -1.584"* 0,750 -0.681

0.900 -0.284 0.320 -0.351 0.430 -0A28 0,800 -0,837"*

0.960 -0.269 0.340 -0.355 0.440 -0.403 0.830 -0.654

0.350 -0.211 ** 0.460 -0.411 0.900 -0.444

0.370 -0.322 0,490 -0.349 0.960 -0.439

0,380 -0,383 0.500 -0,435

0.400 -0.402 0.520 -0.433

0.410 -0.369 0.540 -0.451

0.430 -0.353 0.550 -0.389

0.440 -0.320 0.580 -0.405

0,460 -0,367 0.600 -0.493

0.470 -0.378 0.610 -0.488

0.490 -0,366 0.650 2,440**

0.500 -0,404 0.700 -0,638

0.520 -0.392 0,750 -0.692

0.530 -0.383 0.820 -0.627**

0.550 -0,431 0.890 -0.348

0.560 -0.436 0.900 -0.363

0.580 -0.419 0.960 -0.350

0,590 -0.487

0.600 -0.468

0.640 -0.606

0.700 -0.669

0.750 -0.022**

0.820 -0.65 l

0,870 -0.473

0.93O -0.328

0.960 -0.337

Lower Surface

0.020 -0,668 0,020 -0.534 0,020 -0.454 0,020 -0.262

0.110 -0.142 0.060 -0.135 0.060 -0.041 0.060 2.146"*

0.230 -0.035 0.090 -0, l 19 0.090 1.470** 0.110 -0.051

0.400 0.054 O. 120 -0.053 O. 120 -0.183 0.250 -0.135

0.490 0.108 0.200 -0.025 0.200 -0.036 0.400 -0.061

0.630 2.204** 0.260 -0.003 0.250 -0.054 0.490 -0,033

0.750 0.254 0.400 0.036 0.400 -0.006 0.580 0.030

0.850 0.307 0.490 0.066 0.490 -0.006 0,650 0.253

0.900 0.372 0.580 0.151 0.580 0.133 0.750 0.420

0,960 0.201 0.640 0.359 0.650 -0.041 0.830 0.535

0.750 0.425 0.750 0.001 0.900 0.570

0.870 0.470 0,890 0.517 0,960 0.397

0.930 0.393 0.930 0.430

0.960 0.250 0.960 - 1.668"*

CN = 0.416 0.570 0.483 0.570

703
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 8-54-32-000, MINF = 0.812, Camber = 10/2, ALFT = 4.28, BETA = 0.57, QINF = 613.4,

RNPU = 5.0E+06, CNWP = 0.1835

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.590 0.000 0.064 0.000 1.714 ** 0.010 0.430

0.060 0.105 0.020 0.588 0.020 0.584 0.020 0.269

0.110 -0.310 0.040 0.331 0.060 - 1.930"* 0.060 -0.242

0.200 -0.345 0.060 -0.001 0.090 -0.265 0.110 -0.617

0.230 -0.251 0.090 -0.218 0.110 -0.490 0.1 40 - 1.063

0.400 -0.187 0.130 -0.515 0.130 -0.804 0.190 -2.169"*

0.490 -0.179 0.150 -0.792 0.150 -0.928 0.250 -0.427

0.590 -0.226 0.200 -0.887 0.210 -0.933 0.400 -0.317

0.630 -0.222 0.250 -0.321 0.250 -0.410 0.490 -0.287

0.700 -0.230 0.260 -0.276 0.340 -0.304 0.580 -0.284

0.750 -0.244 0.280 -0.279 0.370 -0.325 0.650 -0.385

0.810 -0.213 0.290 -0.292 0.400 -0.315 0.700 -0.360

0.840 -0.216 0.310 -0.293 0.410 -2.655 ** 0.750 -0.371

0.900 -0.117 0.320 -0.299 0.430 -0.331 0.800 -0.325**

0.960 0.000 0.340 -0.299 0.440 -0.315 0.830 -0.308

0.350 -0.220** 0.460 -0.318 0.900 -0.202

0.370 -0.283 0.490 -0.276 0.960 -0.015

0.380 -0.304 0.500 -0.314

0.400 -0.246 0.520 -0.308

0.410 -0.291 0.540 -0.302

0.430 -0.272 0.550 -0.272

0.440 -0.258 0.580 -0.270

0.460 -0.277 0.600 -0.320

0.470 -0.287 0.610 -0.335

0.490 -0.278 0.650 1.044"*

0.500 -0.276 0.700 -0.383

0.520 -0.273 0.750 -0.333

0.530 -0.273 0.820 -0.331 **

0.550 -0.302 0.890 -0.128

0.560 -0.296 0.900 -0.086

0.580 -0.270 0.960 0.024

0.590 -0.307

0.600 -0.297

0.640 -0.374

0.700 -0.317

0.750 -0.066"*

0.820 -0.282

0.870 -0.239

0.930 -0.087

0.960 -0.025

Lower Surface

0.020 -0.922 0.020 -0.623 0.020 -0.757 0.020 -0.825

0.110 -0.454 0.060 -0.553 0.060 -0.643 0.060 0.903" *

0.230 -0.143 0.090 -0.516 0.090 0.567** 0.110 -0.153

0.400 -0.077 0.120 -0.429 0.120 -0.408 0.250 -0.235

0.490 -0.053 0.200 -0.160 0.200 -0.127 0.400 -0.263

0.630 0.925** 0.260 -0.282 0.250 -0.161 0.490 -0.287

0.750 0.033 0.400 -0.142 0.400 -0.206 0.580 -0.321

0.850 0.072 0.490 -0.111 0.490 -0.080 0.650 -0.142

0.900 0.139 0.580 -0.077 0.580 -0.186 0.750 0.102

0.960 0.143 0.640 0.016 0.650 -0.069 0.830 0.260

0.750 0.123 0.750 -0.040 0.900 0.300

0.870 0.172 0.890 0.256 0.960 0.259

0.930 0.174 0.930 0.217

0.960 0.1 40 0.960 -2.698 * *

CN = 0.111 0.187 0.208 0.260

704
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 8-54-38-500, MINF = 0,804, Camber = 10/2, ALPT = 5,18, BETA = 0,72, QINF = 601.2,

RNPU = 4.9E+06, CNWP = 0.2224

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.534 0.000 0,168 0.000 1.753"* 0.010 0.317

0.060 0.036 0,020 0,519 0.020 0.508 0,020 0.149

0,110 -0.295 0.040 0.259 0.060 - 1.965** 0.060 -0.389

0.200 - 1.014 0.060 -0,067 0.090 -0,342 0. I 10 -0.694

0.230 -0.308 0.090 -0.292 0.110 -0.568 0.140 - 1,130

0.400 -0,205 O. 130 -0.577 O. 130 -0.882 O, 190 -2.209"*

0.490 -0.194 O. 150 -0.873 O. 150 - 1.006 0.250 -0.844

0.590 -0,236 0.200 -0.975 0,210 - 1,024 0.400 -0,337

0.630 -0.232 0.250 -0,957 0.250 -0.964 0.490 -0.304

0.700 -0.234 0.260 -0.951 0.340 -0,288 0.580 -0.301

0,750 -0.241 0.280 -0.559 0.370 -0.288 0.650 -0.399

0.810 -0.214 0.290 -0.355 0.400 -0,277 0.700 -0,374

0.840 -0.217 0,310 -0.281 0.410 -2.705** 0.750 -0,371

0.900 -0.123 0.320 -0.273 0.430 -0.311 0,800 -0.324**

0,960 -0.011 0.340 -0.252 0,440 -0.304 0.830 -0.306

0.350 -0.173 ** 0.460 -0.313 0.900 -0.189

0.370 -0.244 0,490 -0.274 0,960 -0.009

0.380 -0,272 0.500 -0.316

0.400 -0,241 0.520 -0,310

0.410 -0.273 0.540 -0.311

0.430 -0.262 0,550 -0.276

0,440 -0.252 0.580 -0,280

0,460 -0.273 0.600 -0.328

0.470 -0.285 0,610 -0.337

0.499 -0.278 0.650 1.069"*

0.500 -0.275 0,700 -0.402

0.520 -0,278 0,750 -0.338

0.530 -0.275 0,820 -0.319"*

0,550 -0.304 0.890 -0,129

0.560 -0.304 0,900 -0.088

0.580 -0.275 0.960 0,018

0,590 -0.312

0.600 -0.304

0,640 -0,361

0.700 -0.317

0_750 -0.058**

0,820 -0,280

0,870 -0.240

0.930 -0.091

0.960 -0.029

Lower Surface

0,020 - 1.045 0.020 -0.617 0,020 -0.695 0.020 -0.581

0.110 -0.284 0.060 -0,497 0.060 -0.467 0.060 0.925"*

0.230 -0.082 0.090 -0.409 0,090 0,583"* 0.110 -0,061

0.400 -0,042 0,120 -0.272 O,120 -0.153 0,250 -0,174

0.490 -0,048 0,200 -0,081 0.200 -0,073 0.400 -0.207

0.630 0.947"* 0.260 -0.111 0.250 -0.102 0.490 -0.244

0.750 0.019 0.400 -0.096 0.400 -0.171 0.580 -0.284

0.850 0,064 0.490 -0.106 0.490 -0.068 0.650 -0.130

0.900 0,135 0.580 -0.099 0,580 -0.186 0.750 0,117

0,960 0.144 0,640 0,039 0.650 -0.063 0.830 0.274

0.750 0.146 0.750 -0.037 0.900 0,310

0.870 0,211 0.890 0.269 0,960 0,262

0.930 0.189 0.930 0,225

0.960 0.148 0.960 -2.749 * *

CN = 0.195 0,283 0.305 0.374

705
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 8-54-44-000, MINF = 0.801, Camber = 10/2, ALPT = 6.08, BETA = 0.63, QINF = 595.8,

RNPU = 4.9E+06, CNWP = 0.2493

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 0.497 0.000 0.242 0.000 1.771 ** 0.010 0.225

0.060 -0.006 0.020 0.486 0.020 0.454 0.020 0.058

0.110 -0.363 0.040 0.206 0.060 - 1.980** 0.060 -0.495

0.200 - 1.056 0.060 -0.120 0.090 -0.393 0.110 -0.789

0.230 -0.585 0.090 -0.344 0.110 -0.613 0.140 -1.180

0.400 -0.198 0.130 -0.609 0.130 -0.922 0.190 -2.226" *

0.490 -0.197 0.150 -0.916 0.150 - 1.069 0.250 -0.900

0.590 -0.221 0.200 - 1.017 0.210 - 1.078 0.400 -0.358

0.630 -0.237 0.250 - 1.013 0.250 -0.970 0.490 -0.311

0.700 -0.236 0.260 - 1.013 0.340 -0.436 0.580 -0.307

0.750 -0.239 0.280 -1.017 0.370 -0.317 0.650 -0.393

0.8 t0 -0.217 0.290 -0.998 0.400 -0.259 0.700 -0.368

0.840 -0.216 O.310 -0.619 0.410 -2.727 ** 0.750 -0.365

0.900 -0.127 0.320 -0.520 0.430 -0.274 0.800 -0.314"*

0.960 -0.012 0.340 -0.330 0.440 -0.272 0.830 -0.301

0.350 -0.178** 0.460 -0.288 0.900 -0.167

0.370 -0.217 0.490 -0.252 0.960 0.002

0.380 -0.228 0.500 -0.303

0.400 -0.184 0.520 -0.302

0.410 -0.225 0.540 -0.291

0.430 -0.223 0.550 -0.270

0.440 -0.216 0.580 -0.271

0.460 -0.249 0.600 -0.315

0.470 -0.255 0.610 -0.331

0.490 -0.252 0.650 1.081 **

0.500 -0.263 0.700 -0.370

0.520 -0.244 0.750 -0.330

0.530 -0.262 0.820 -0.314"*

0.550 -0.274 0.890 -0.124

0.560 -0.291 0.900 -0.083

0.580 -0.264 0.960 0.02 l

0.590 -0.307

0.600 -0.297

0.640 -0.360

0.700 -0.314

0.750 -0.049"*

0.820 -0.276

0.870 -0.240

0.930 -0.087

0.960 -0.025

Lower Surface

0.020 - 1.020 0.020 -0.583 0.020 -0.593 0.020 -0.358

0.110 -0.190 0.060 -0.408 0.060 -0.247 0.060 0.936**

0.230 -0.058 0.090 -0.280 0.090 0.591 * * 0.110 -0.012

0.400 -0.032 0.120 -0.133 0.120 -0.062 0.250 -0.129

0.490 -0.024 0.200 -0.060 0.200 -0.056 0.400 -0.166

0.630 0.959"* 0.260 -0.041 0.250 -0.068 0.490 -0.218

0.750 0.027 0.400 -0.074 0.400 -0.151 0,580 -0.264

0.850 0.074 0.490 -0.101 0.490 -0.054 0.650 -0.107

0.900 0.136 0.580 -0.098 0.580 -0.171 0.750 0.130

0.960 0.1 40 0.640 0.051 0.650 -0.050 0.830 0.279

0.750 0.165 0.750 -0.035 0.900 0.319

0.870 0.237 0.890 0.285 0.960 0.269

0.930 0.200 0.930 0.237

0.960 0.157 0.960 -2.771 **

CN = 0.248 0.347 0.355 0.424

706
Table J-2. Continued.

Flight 223, Wing sweep = 26", Time = 8-55-1-000, MINF = 0.804, Camber = 10/2, ALPT = 9.02, BETA = 0.66. QINF = 610.5.

RNPU = 5.0E+06, CNWP = 0.4424

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.264 0.000 0.622 0.003 1.691 ** 0.010 -0.176

0.060 -0.239 0.020 0.165 0.020 0.085 0.020 -0.238

0.110 -0.454 0.040 -0.057 0.060 - 1.970** 0.060 -0.821

0.200 -1.173 0.060 -0.411 0.090 -0.742 0.110 -1.140

0.230 - 1.130 0.090 -0.562 0. l 10 -0.868 0.140 - 1.397

0.400 -0.474 0.130 -0.812 0.130 - I. 123 0.190 -2.210"*

0.490 -0.152 0.150 -1.045 0.150 -1.182 0.250 -1.428

0.590 -0.213 0.200 -1.137 0.210 -1.179 0.400 -0.895

0.630 -0.237 0.250 - 1.188 0.250 -0.984 0.490 -0.555

0.700 -0.238 0.260 - 1.194 0.340 - 1.272 0.580 -0.339

0.750 -0.258 0.280 - 1.149 0.370 - 1.266 0.650 -0.328

0.810 -0.240 0.290 -1.149 0.400 -1.217 0.700 -0.313

0.840 -0.252 0.310 -0.859 0.410 -2.699** 0.750 -0.259

0.900 -0.192 0.320 - 1.153 0.430 - 1.260 0.800 -0.209"*

0.960 -0.073 0.340 -0.927 0.440 -0.946 0.830 -0.186

0.350 -0.542"* 0.460 -0.770 0.900 -0.091

0.370 -0.987 0.490 -0.624 0.960 -0.016

0.380 -1.184 0.500 -0.619

0.400 - 1.156 0.520 -0.606

0.410 -0.86 l 0.540 -0.586

0.430 - 1.143 0.550 -0.545

0.440 -0.769 0.580 -0.499

0.460 -0.818 0.600 -0.510

0.470 -0.609 0.610 -0.456

0.490 -0.538 0.650 1.018"*

0.500 -0.509 0.700 -0.285

0.520 -0.491 0.750 -0.256

0.530 -0.437 0.820 -0.176"*

0.550 -0.420 0.890 -0.066

0.560 -0.377 0.900 -0.040

0.580 -0.334 0.960 0.020

0.590 -0.309

0.600 -0.262

0.640 -0.193

0.700 -0.19 l

0.750 -0.015"*

0.820 -0.193

0.870 -0.169

0.930 -0.060

0.960 -0.010

Lower Surface

0.020 -0.304 0.020 -0.157 0.020 -0.064 0.020 0.239

0.110 -0.020 0.060 0.136 0.060 0.202 0.060 0.876**

0.230 0.036 0.090 0.096 0.090 0.539"* 0.110 0.193

0.400 -0.039 0.120 0.143 0.120 0.133 0.250 0.032

0.490 -0.031 0.200 0.030 0.200 0.034 0.400 -0.041

0.630 0.884** 0.260 0.088 0.250 0.064 0.490 -0.103

0.750 0.001 0.400 -0.006 0.400 -0.037 0.580 -0.171

0.850 0.04 1 0.490 -0.060 0.490 -0.016 0.650 -0.059

0.900 0.124 0.580 -0.091 0.580 -0.120 0.750 0.160

0.960 0.109 0.640 0.056 0.650 -0.0 l 6 0.830 0.300

0.750 0.178 0.750 0.007 0.900 0.328

0.870 0.238 0.890 0.296 0.960 0.247

0.930 0.20l 0.930 0.238

0.960 0.154 0.960 -2.742 * *

CN = 0.405 0.595 0.664 0.711

707
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 8-55-3-500, MINF = 0.793, Camber = 10/2, ALPT = 9.06, BETA = 0.69, QINF = 594.7,

RNPU = 4.9E+06, CNWP = 0.3973

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.257 0.000 0.632 0.000 1.731 ** 0.010 -0.189

0.060 -0.253 0.020 0.161 0.020 0.065 0.020 -0.253

0.110 -0.522 0.040 -0.074 0.060 -2.028"* 0.060 -0.862

0.200 - 1.202 0.060 -0.428 0.090 -0.749 0.110 - 1.168

0.230 - 1.131 0.090 -0.584 0.110 -0.889 0.140 - 1.433

0.400 -0.257 0.130 -0.838 0.130 - 1.152 0.190 -2.274 * *

0.490 -0.173 0.150 - 1.078 0.150 - 1.204 0.250 - 1.464

0.590 -0.244 0.200 - 1.168 0.210 - 1.216 0.400 -0.745

0.630 -0.247 0.250 - 1.218 0.250 - 1.016 0.490 -0.416

0.700 -0.245 0.260 - 1.220 0.340 - 1.297 0.580 -0.314

0.750 -0.259 0.280 - 1.185 0.370 - 1.286 0.650 -0.335

0.810 -0.232 0.290 - 1.185 0.400 - 1.002 0.700 -0.314

0.840 -0.249 0.310 -0.887 0.410 -2.776** 0.750 -0.272

0.900 -0.184 0.320 - 1.189 0.430 -0.693 0.800 -0.216**

0.960 -0.070 0.340 -0.957 0.440 -0.645 0.830 -0.193

0.350 -0.552** 0.460 -0.630 0.900 -0.103

0.370 - 1.019 0.490 -0.578 0.960 -0.025

0.380 - 1.221 0.500 -0.577

0.400 - 1.169 0.520 -0.548

0.410 -0.890 0.540 -0.510

0.430 -0.612 0.550 -0.449

0.440 -0.566 0.580 -0.396

0.460 -0.544 0.600 -0.385

0.470 -0.499 0.610 -0.331

0.490 -0.4.44 0.650 1.040**

0.500 -0.403 0.700 -0.258

0.520 -0.357 0.750 -0.237

0.530 -0.294 0.820 -0.189**

0.550 -0.269 0.890 -0.072

0.560 -0.242 0.900 -0.049

0.580 -0.213 0.960 0.019

0.590 -0.217

0.600 -0.195

0.640 -0.219

0.700 -0.221

0.750 -0.018"*

0.820 -0.219

0.870 -0.192

0.930 -0.069

0.960 -0.019

Lower Surface

0.020 -0.259 0.020 -0.156 0.020 -0.072 0.020 0.241

0.110 -0.012 0.060 0.126 0.060 0.196 0.060 0.894"*

0.230 0.035 0.090 0.100 0.090 0.548** 0.110 0.190

0.400 -0.008 0. 120 0.145 0.120 0.134 0.250 0.031

0.490 -0.049 0.200 0.029 0.200 0.033 0.400 -0.036

0.630 0.902** 0.260 0.092 0.250 0.067 0.490 -0.096

0.750 0.002 0.400 -0.004 0.400 -0.031 0.580 -0.1 64

0.850 0.042 0.490 -0.056 0.490 -0.015 0.650 -0.053

0.900 0.129 0.580 -0.086 0.580 -0.110 0.750 0.161

0.960 0.114 0.640 0.060 0.650 -0.018 0.830 0.301

0.750 0.189 0.750 0.007 0.900 0.326

0.870 0.247 0.890 0.295 0.960 0.250

0.930 0.199 0.930 0.239

0.960 0.154 0.960 -2.820**

CN = 0.387 0.585 0.629 0.694

708
Table J-2. Continued.

Hight 223, Wing sweep = 26 °, Time = 8-50-5-500, MINF = 0.801, Camber = 5/10, ALPT = 2.99, BETA = 0.83, QINF = 601.7,

RNPU = 4.9E+06, CNWP = 0.1594

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.468 0.000 0,352 0,000 1,729"* 0.010 O. 153

0.060 0.112 0.020 0.477 0.020 0.378 0.020 0.040

0.110 -0. l I 1 0.040 0.242 0.060 -3.696"* 0.060 -0.258

0.200 -0.216 0.060 0.016 0.090 -0.199 0.110 -0.463

0.230 -0.210 0.090 -0.114 0.110 -0.339 0.140 -0.666

0.400 -0.173 0.130 -0.267 0. 130 -0.520 0.190 -2.229**

0.490 -0.189 0.150 -0.411 0.150 -0.405 0.250 -0.321

0.590 -0.267 0.200 -0.324 0.210 -0.400 0.400 -0.303

0.630 -0.288 0.250 -0.266 0.250 -0.296 0.490 -0.283

0.700 -0.358 0.260 -0.261 0.340 -0.301 0.580 -0.295

0.750 - 1.006 0.280 -0.279 0.370 -0.317 0.650 -0.418

0.810 -0.864 0.290 -0.268 0.400 -0.300 0.700 -0.386

0.840 -0.946 0.310 -0.271 0,410 -2,726** 0.750 -0.430

0.900 -0.201 0.320 -0.278 0.430 -0.327 0.800 -2.630**

0.960 -0.157 0.340 -0.273 0.440 -0.309 0.830 -0.662

0,350 -0.219"* 0.460 -0.315 0,900 -0.403

0.370 -0.258 0.490 -0.261 0.960 -0.395

0.380 -0.278 0.500 -0.324

0.400 -0.228 0.520 -0,313

0.410 -0.281 0.540 -0.319

0.430 -0.255 0.550 -0.283

0.440 -0.255 0.580 -0.291

0.460 -0.273 0.600 -0.339

0.470 -0.282 0.610 -0.358

0.490 -0.274 0.650 1.046**

0.500 -0.294 0.700 -0.533

0.520 -0.284 0.750 -0.394

0.530 -0.283 0.820 -0.971 **

0.550 -0.313 0.890 -0.303

0.560 -0,323 0.900 -0.379

0.580 -0.302 0.960 -0.297

0.590 -0.343

0.600 -0.324

0.640 -0.469

0.700 -0.393

0,750 -0.063"*

0.820 -0.560

0.870 -0.387

0.930 -0.284

0.960 -0.273

Lower Surface

0.020 -0.926 0.020 -2.628 0.020 - 1.367 0.020 -0.395

0.110 -0.453 0.060 -0.694 0.060 -0.461 0.060 0.902**

0.230 -0.152 0.090 -0.501 0.090 0.553** 0.110 -0.250

0.400 -0.017 0.120 -0.273 0.120 -0.293 0.250 -0.292

0.490 0.030 0.200 -0.148 0.200 -0.149 0.400 -0.226

0.630 0.931 ** 0.260 -0.131 0.250 -0.209 0.490 -0.212

0.750 0.153 0.400 -0.079 0.400 -0.148 0.580 -0.15 I

0.850 0.204 0.490 -0.037 0.490 -0.068 0.650 0.069

0.900 0.278 0.580 0.035 0.580 -0.032 0.750 0.282

0.960 0.170 0.640 0.218 0.650 -0.078 0.830 0.414

0.750 0.286 0.750 -0.021 0.900 0.457

0.870 0.345 0.890 0.405 0.960 0.328

0.930 0.263 0.930 0.324

0.960 0.152 0.960 -2.769**

CN = 0.278 0.292 0.253 0.350

709
Table J-2. Continued.

Flight 223, Wing sweep = 26 °. Time = 8-50-31-000, MINF = 0.802, Camber = 5/10, ALPT = 5.00, BETA = 0.69, QINF = 609.5,

RNPU = 5.0E+06, CNWP = 0.2512

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP .r./c CP

0.020 0.300 0.000 0.609 0.000 1.686"* 0.010 -0.205

0.060 -0.048 0.020 0.176 0.020 0.105 0.020 -0.257

0.110 -0.287 0.040 0.024 0.060 - 1.981 ** 0.060 -0.614

0.200 -0.313 0.060 -0.221 0.090 -0.413 0.1 t 0 -0.735

0.230 -0.327 0.090 -0.333 0.110 -0.559 0.140 -0.943

0.400 -0.226 0.130 -0.532 0.130 -0.749 0.190 -2.222 * *

0.490 -0.225 0.150 -0.731 0.150 -0.841 0.250 -0.542

0.590 -0.296 0.200 -0.751 0.210 -0.844 0.400 -0.373

0.630 -0.315 0.250 -0.349 0.250 -0.364 0.490 -0.342

0.700 -0.370 0.260 -0.358 0.340 -0.372 0.580 -0.347

0.750 -0.798 0.280 -0.372 0.370 -0.388 0.650 -0.467

0.810 -0.767 0.290 -0.366 0.400 -0.366 0.700 -0.438

0.840 -0.863 0.310 -0.360 0.410 -2.712"* 0.750 -0.464

0.900 -0.253 0.320 -0.366 0.430 -0.394 0.800 -2.617"*

0.960 -0.219 0.340 -0.359 0.440 -0.375 0.830 -0.623

0.350 -0.198"* 0.460 -0.379 0.900 -0.416

0.370 -0.333 0.490 -0.336 0.960 -0.406

0.380 -0.354 0.500 -0.373

0.400 -0.297 0.520 -0.362

0.410 -0.343 0.540 -0.367

0.430 -0.317 0.550 -0.330

0.440 -0.309 0.580 -0.318

0.460 -0.330 0.600 -0.385

0.470 -0.340 0.610 -0.399

0.490 -0.334 0.650 1.012"*

0.500 -0.336 0.700 -0.626

0.520 -0.328 0.750 -0.492

0.530 -0.336 0.820 -0.979**

0.550 -0.362 0.890 -0.321

0.560 -0.367 0.900 -0.372

0.580 -0.336 0.960 -0.289

0.590 -0.381

0.600 -0.369

0.640 -0.668

0.700 -0.441

0.750 -0.030**

0.820 -0.573

0.870 -0.380

0.930 -0.283

0.960 -0.285

LowerSuff_e

0.020 -0.839 0.020 -0.830 0.020 -0.402 0.020 0.066

0.110 -0.165 0.060 -0.140 0.060 -0.064 0.060 0.869**

0.230 -0.039 0.090 -0.141 0.090 0.532" * 0.110 -0.053

0.400 0.001 0.120 -0.087 0.120 -0.144 0.250 -0.1 64

0.490 0.038 0.200 -0.035 0.200 -0.042 0.400 -0.141

0.630 0.899** 0.260 -0.054 0.250 -0.106 0.490 -0.1 44

0.750 0.184 0.400 -0.038 0.400 -0.089 0.580 -0.108

0.850 0.217 0.490 -0.017 0.490 -0.028 0.650 0.104

0.900 0.288 0.580 0.046 0.580 -0.003 0.750 0.321

0.960 0.149 0.640 0.248 0.650 -0.035 0.830 0.446

0.750 0.321 0.750 -0.006 0.900 0.493

0.870 0.421 0.890 0.453 0.960 0.335

0.930 0.312 0.930 0.363

0.960 0.193 0.960 -2.755**

CN = 0,382 0.490 0.440 0.535

710
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 8-50-40-000, MINF = 0.810, Camber = 5/10, ALPT = 6,02, BETA = 0.69, QINF = 619.2,

RNPU = 5.0E+06, CNWP = 0.2762

1] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.202 0.000 0.707 0.000 1.669"* 0.010 -0.388

0.060 -0.138 0.020 0.049 0.020 -0.060 0.020 -0,358

0.110 -0.370 0.040 -0.079 0.060 - 1.940** 0.060 -0.730

0.200 -0.795 0.060 -0.312 0.090 -0.486 0.110 -0.880

0.230 -0.272 0.090 -0.403 0.110 -0.624 0.140 - 1.079

0.400 -0.243 0.130 -0.595 0.130 -0.787 0.190 -2.177 **

0,490 -0.255 0.150 -0.780 0.150 -0,869 0,250 -0,755

0.590 -0.309 0.200 -0.817 0.210 -0.903 0.400 -0.395

0.630 -0.344 0.250 -0.870 0.250 -0.905 0.490 -0.359

0.700 -0.372 0.260 -0.859 0.340 -0.407 0.580 -0,364

0.750 -0.982 0.280 -0.862 0.370 -0.330 0.650 -0.478

0.810 -0.867 0.290 -0.852 0.400 -0.304 0.700 -0.446

0.840 -0,932 0.310 -0.496 0.410 -2.660** 0.750 -0.485

0.900 -0.277 0.320 -0.399 0.430 -0.338 0.800 -2.566**

0.960 -0.256 0.340 -0.272 0.440 -0.321 0.830 -0.701

0.350 -0.140"* 0.460 -0,335 0.900 -0.436

0.370 -0.240 0.490 -0.310 0.960 -0.396

0.380 -0.271 0.500 -0.349

0.400 -0.249 0.520 -0.344

0.410 -0.288 0.540 -0.349

0.430 -0.283 0.550 -0.317

0A40 -0.276 0.580 -0.313

0.460 -0.306 0.600 -0.378

0.470 -0.324 0.610 -0_397

0.490 -0.318 0.650 1.005"*

0.500 -0.324 0.700 -0.622

0.520 -0.323 0.750 -0,505

0.530 -0.330 0.820 -0.893**

0.550 -0.361 0.890 -0.318

0.560 -0.363 0.900 -0,380

0.580 -0.335 0.960 -0.308

0.590 -0.379

0.600 -0.370

0.640 -0.666

0.700 -0.510

0,750 -0.027**

0.820 -0.557

0.870 -0.400

0.930 -0.286

0,960 -0.294

Lower Surface

0.020 -0.530 0.020 -0.416 0.020 -0.211 0.020 0.214

0.110 -0.157 0.060 -0.071 0.060 0.021 0.060 0.865 **

0.230 -0.010 0.090 -0.070 0.090 0.533 ** 0.110 0.002

0.400 0.009 0.120 -0.034 0.120 -0.069 0.250 -0.118

0.490 0.054 0.200 -0.007 0.200 -0.001 0.400 -0.112

0.630 0.894** 0.260 -0.023 0.250 *0.059 0.490 -0. I 17

0.750 0.173 0.400 -0.018 0.400 -0.056 0.580 -0.089

0.850 0.218 0.490 -0.007 0.490 -0.021 0.650 O. 112

0.900 0.295 0.580 0,075 0.580 0,014 0.750 0.335

0.960 0.136 0.640 0.265 0,650 -0.033 0.830 0.453

0.750 0.324 0,750 -0.007 0.900 0.504

0.870 0.419 0.890 0.466 0.960 0.342

0.930 0.311 0.930 0.376

0.960 0.189 0.960 -2.702**

CN = 0.450 0.563 0.509 0.625

711
Table J-2. Continued.

Hight 223, Wing sweep = 26 °, Time = 8-50-45-000, MINF = 0.804, Camber = 5/10, ALPT = 7.08, BETA = 0.57, QINF = 608.2,

RNPU = 5.0E+06, CNWP = 0.3166

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.054 0.000 0.801 0.000 1.705" * 0.010 -0.750

0.060 -0.255 0.020 -0.121 0.020 -0.239 0.020 -0.626

0.110 -0.445 0.040 -0.227 0.060 -1.970** 0.060 -0.830

0.200 -0.885 0.060 -0.442 0.090 -0,710 0.110 - 1.025

0.230 -0.713 0.090 -0.511 0.110 -0.769 0.140 -1.189

0.400 -0.237 0.130 -0.674 0.130 -0.913 0.190 -2.211 **

0.490 -0.246 0.150 -0.862 0.150 -0.950 0.250 - 1.141

0.590 -0.322 0.200 -0.904 0.210 -0.975 0.400 -0.421

0.630 -0.346 0.250 -0.954 0.250 -0.924 0.490 -0.378

0.700 -0.388 0.260 -0.967 0.340 - 1.039 0.580 -0.377

0.750 -0.993 0.280 -0.975 0.370 - 1.026 0.650 -0.491

0.810 -0.882 0.290 -0.960 0.400 -0.482 0.700 -0.473

0.840 -0.943 0.310 -0.819 0.410 -2.702"* 0.750 -0.510

0.900 -0.318 0.320 -0.943 0.430 -0.360 0.800 -2.607"*

0.960 -0.279 0.340 -0.873 0.440 -0.311 0.830 - 1.03 l

0.350 -0.431 ** 0.460 -0.3 l0 0.900 -0.438

0.370 -0.803 0.490 -0.246 0.960 -0.314

0.380 -0.446 0.500 -0.317

0.400 -0.286 0.520 -0.320

0,410 -0.260 0.540 -0.323

0.430 -0.218 0.550 -0.292

0.440 -0.211 0.580 -0.326

0.460 -0.229 0,600 -0,367

0.470 -0.237 0.610 -0.385

0.490 -0.253 0.650 1.029**

0.500 -0.268 0.700 -0.602

0.520 -0.277 0.750 -0.484

0.530 -0.281 0.820 - 1.038"*

0.550 -0.325 0.890 -0.294

0.560 -0.332 0.900 -0.358

0.580 -0.322 0.960 -0.273

0.590 -0.369

0.600 -0.366

0.640 -0.661

0.700 -0.422

0.750 -0.029"*

0.820 -0.591

0.870 -0.506

0.930 -0.285

0.960 -0.289

Lower Surface

0.020 -0.307 0.020 -0.205 0.020 -0.040 0.020 0.310

0.110 -0.105 0.060 0.051 0.060 0.122 0.060 0.887**

0,230 0.035 0.090 0.018 0.090 0.549** 0.110 0.078

0.400 0.023 0,120 0.036 0.120 0.000 0.250 -0.059

0.490 0.047 0.200 0.040 0.200 0.044 0.400 -0.058

0.630 0.916"* 0.260 0.022 0.250 -0.007 0.490 -0.077

0.750 0.165 0.400 0.012 0.400 -0.019 0.580 -0.045

0.850 0.202 0.490 0.018 0.490 -0.019 0.650 0.142

0.900 0.292 0.580 0.086 0.580 0.034 0.750 0.361

0.960 0.126 0.640 0.279 0.650 -0.033 0.830 0.475

0.750 0.331 0.750 0.003 0.900 0.517

0.870 0.419 0.890 0.470 0.960 0.360

0.930 0.317 0.930 0.376

0.960 0.191 0.960 -2.745**

CN = 0.524 0.656 0.619 0,777

712
Table J-2. Continued,

Flight 223, Wing sweep = 26 °, Time = 8-50-49-500, MINF = 0.789. Camber = 5/10, ALPT = 8.00, BETA = 0.57. QINF = 584.2,

RNPU = 4.8E+06, CNWP = 0.3653

11 = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0,020 -0.149 0.000 0,847 0,000 1.779"* 0.010 -0,898

0.060 -0.399 0.020 -0.387 0.020 -0,475 0.020 -0,972

0.110 -0,523 0.040 -0,395 0,060 -2.047"* 0,060 -0.961

0,200 -0.963 0.060 -0.655 0.090 -0,894 0. 110 - 1.146

0.230 -0.835 0,090 -0.742 0. 110 -0,947 0.140 - 1.328

0.400 -0.251 0,130 -0.851 0.130 -1.072 0.190 -2.298**

0,490 -0.266 0.150 -0.968 0.150 - 1.080 0.250 - 1.298

0.590 -0.342 0.200 -0,983 0.210 - 1.130 0,400 -0.491

0.630 -0.369 0,250 - 1.061 0,250 -0,958 0,490 -0.397

0.700 -0.419 0.260 - 1.070 0.340 - 1.147 0.580 -0.400

0,750 - 1.030 0.280 - 1.089 0.370 -1.149 0,650 -0.516

0.810 -0.918 0,290 - 1.089 0.400 -0.729 0,700 -0.508

0,840 -0.978 0.310 -0.849 0.410 -2.809** 0,750 -0,577

0.900 -0.354 0.320 - 1.061 0,430 -0.479 0.800 -0.803"*

0,960 -0.334 0.340 -0.905 0.440 -0.410 0.830 -0.759

0.350 -0,461"* 0.460 -0.371 0,900 -0.251

0.370 -0.962 0.490 -0.311 0,960 -0.178

0.380 -0.977 0.500 -0.328

0.400 -0.495 0.520 -0.322

0.4 l0 -0.397 0.540 -0.328

0.430 -0.303 0.550 -0,306

0,440 -0.264 0,580 -0.310

0.460 -0,252 0.600 -0.377

0.470 -0.246 0.610 -0.396

0,490 -0.244 0,650 1.076**

0,500 -0.256 0,700 -0.525

0.520 -0.261 0,750 -0,464

0.530 -0.276 0.820 -0.906**

0.550 -0,318 0,890 -0,256

0.560 -0.336 0.900 -0.282

0.580 -0.320 0,960 -0.226

0.590 -0,364

0.600 -0.365

0.640 -0.519

0.700 -0.458

0.750 -0.021 **

0.820 -0.590

0,870 -0.465

0.930 -0.293

0.960 -0.292

Lower Surface

0,020 -0.184 0,020 0.013 0.020 0.129 0,020 0,469

0.110 -0.047 0,060 0,151 0,060 0.216 0,060 0.927**

0.230 0,087 0,090 0.105 0,090 0.575"* 0.110 0,155

0,400 0,046 0,120 0.101 0.120 0,077 0.250 0.001

0.490 0.060 0,200 0,090 0.200 0,088 0.400 -0.014

0.630 0,958"* 0.260 0.073 0.250 0.056 0,490 -0,030

0.750 0.161 0.400 0.047 0.400 0.022 0.580 -0.004

0,850 0.194 0,490 0,044 0.490 -0.005 0,650 0.164

0,900 0.273 0.580 0.113 0,580 0.066 0,750 0.377

0,960 0.106 0,640 0.285 0.650 -0.027 0.830 0.489

0.750 0.339 0.750 0.014 0.900 0,538

0.870 0,447 0.890 0.482 0.960 0.368

0.930 0.310 0.930 0,384

0.960 0.194 0,960 -2,854"*

CN = 0.594 0.750 0.698 0,847

713
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 10-28-38-500, MINF = 0.800, Camber = 5/10, ALPT = 3.03, BETA = 0.31, QINF = 601.9,

RNPU = 4.9E+06, CNWP = 0.2194

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x,/c CP x/c CP

0.020 0.473 0.000 0.360 0.000 0.558** 0.010 0.130

0.060 0.109 0.020 0.429 0.020 0.375 0.020 0.014

0.110 -0.130 0.040 0.276 0.060 0.576** 0.060 -0.302

0.200 -0.220 0.060 0.009 0.090 -0.221 0.110 -0.506

0.230 -0.249 0.090 -0.136 0.110 -0.365 0.140 -0.712

0.400 -0.180 0.130 -0.296 0.130 -2.234"* 0.190 -2.234**

0.490 -0.189 0.150 -0.411 0.150 -0.429 0.250 -0.347

0.590 -0.264 0.200 -0.338 0.210 -0.406 0.400 -0.3 l 2

0.630 -0.296 0.250 -0.278 0.250 -0.316 0.490 -0.282

0.700 -0.359 0.260 -0.277 0.340 -0.314 0.580 -0.306

0.750 -I .011 0.280 -0.284 0.370 -0.328 0.650 -0.420

0.810 -0.909 0.290 -0.284 0.400 -0.288 0.700 -0.400

0.840 -0.961 0.310 -0.265 0.410 -0.397 ** 0.750 -0.436

0.900 -0.174 0.320 -0.278 0.430 -0.326 0.800 -0.274

0.960 -0.134 0.340 -0.271 0.440 -0.314 0.830 -0.655

0.350 -0.193"* 0.460 -0.314 0.900 -0.392

0.370 -0.265 0.490 -0.294 0.960 -0.391

0.380 -0.283 0.500 -0.325

0.400 -0.249 0.520 -0.318

0.410 -0.270 0.540 -0.317

0.430 -0.265 0.550 -0.298

0.440 -0.255 0.580 -0.293

0.460 -0.276 0.600 -0.343

0.470 -0.283 0.610 -0.370

0.490 -0.287 0.650 -0.542

0.500 -0.281 0.700 -0.506

0.520 -0.276 0.750 -0.379

0.530 -0.292 0.820 -0.904

0.550 -0.314 0.890 -0.309

0.560 -0.324 0.900 -0.379

0.580 -0.297 0.960 -0.294

0.590 -0.337

0.600 -0.328

0.640 -0.478

0.700 -0.387

0.750 -0.067**

0.820 -0.554

0.870 -0.371

0.930 -0.266

0.960 -0.271

Lower Surface

0.020 -0.932 0.020 -0.279 0.020 - 1.382 0.020 -0.505

0.110 -0.434 0.060 -0.673 0.060 -0.439 0.060 -0.027

0.230 -0.141 0.090 -0.475 0.090 -0.274 0.110 -0.292

0.400 -0.011 0.120 -0.268 0.120 -0.300 0.250 -0.280

0.490 0.036 0.200 -0.138 0.200 -0.148 0.400 -0.236

0.630 0.911 ** 0.260 -0.122 0.250 -0.211 0.490 -0.211

0.750 0.169 0.400 -0.075 0.400 -0.152 0.580 -0.155

0.850 0.196 0.490 -0.027 0.490 -0.067 0.650 0.051

0.900 0.290 0.580 0.031 0.580 -0.042 0.750 0.293

0.960 0.173 0.640 0.228 0.650 -0.073 0.830 0.393

0.750 0.278 0.750 -0.021 0.900 0.460

0.870 0.347 0.890 0.420 0.960 0.317

0.930 0.273 0.930 0.332

0.960 0.177 0.960 0.260

CN = 0.295 0.300 0.313 0.355

714
Table J-2, Continued.

Flight 211, Wing sweep = 26 °, Time = 10-29-3-500, MINF = 0.794, Camber = 5/10, ALPT = 2.93, BETA = 0.54, QINF = 593.2,

RNPU = 4.9E+06, CNWP = 0.2350

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.470 0.000 0.355 0.000 0.568'* 0.010 0.117

0.060 0.096 0.020 0,437 0.020 0.370 0.020 0.009

0.110 -0.142 0.040 0.266 0.060 0.552** 0.060 -0.304

0.200 -0.231 0.060 0.012 0.090 -0.230 0.110 -0.508

0.230 -0.249 0.090 -0.140 0.110 -0.363 0.140 -0.629

0.400 -0.192 0.130 -0.301 0.130 -2.265 * * 0.190 -2.265 * *

0.490 -0.206 0.150 -0.414 0.150 -0.429 0.250 -0.350

0.590 -0.275 0.200 -0.335 0.210 -0.405 0.400 -0.317

0.630 -0.312 0.250 -0.273 0.250 -0.319 0.490 -0.291

0.700 -0.376 0.260 -0.282 0.340 -0.317 0.580 -0.315

0.750 -0.966 0.280 -0.286 0.370 -0.331 0.650 -0.424

0.810 -0.835 0.290 -0.286 0.400 -0.298 0.700 -0.404

0.840 -0.905 0,310 -0.273 0.410 -0.401 ** 0.750 -0.444

0.900 -0.193 0.320 -0.285 0.430 -0.329 0.800 -0.275

0.960 -0.130 0.340 -0.280 0.440 -0.318 0.830 -0.674

0.350 -0.196** 0.460 -0.317 0.900 -0.398

0.370 -0.273 0.490 -0.296 0.960 -0.383

0.380 -0.287 0.500 -0.318

0.400 -0.256 0.520 -0.324

0.410 -0.278 0.540 -0.320

0.430 -0.266 0.550 -0.307

0.440 -0.257 0.580 -0.311

0.460 -0.272 0.600 -0.352

0.470 -0.279 0.610 -0.380

0.490 -0.287 0.650 -0.519

0.500 -0.293 0.700 -0.487

0.520 -0.285 0.750 -0.389

0.530 -0.294 0.820 - 1.013

0.550 -0.319 0.890 -0.312

0.560 -0.329 0.900 -0.373

0.580 -0.299 0.960 -0.283

0.590 -0.340

0.600 -0.338

0.640 -0.477

0.700 -0,405

0.750 -0.064"*

0.820 -0.564

0.870 -0.383

0.930 -0.273

0.960 -0.268

Lower Surface

0.020 -0.986 0.020 -0.281 0.020 - 1.408 0.020 -0.507

0.110 -0.408 0.060 -0.652 0.060 -0.411 0.060 -0.018

0.230 -0.143 0.090 -0.445 0.090 -0.274 0.110 -0.301

0.400 -0.022 0.120 -0.255 0.120 -0.294 0.250 -0.286

0.490 0.020 0.200 -0.139 0.200 -0.145 0.400 -0.230

0.630 0.927** 0.260 -0.129 0.250 -0.208 0.490 -0.204

0.750 0.160 0.400 -0.083 0.400 -0.147 0.580 -0.150

0.850 0.192 0.490 -0.035 0.490 -0.073 0.650 0.052

0.900 0.285 0.580 0.023 0.580 -0.040 0.750 0.295

0.960 0.173 0.640 0.218 0.650 -0.072 0.830 0.391

0.750 0.269 0.750 -0.027 0.900 0.456

0.870 0.354 0.890 0.414 0.960 0.318

0.930 0.265 0.930 0.331

0.960 0.165 0.960 0.238

CN = 0.291 0.302 0.321 0.356

715
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 10-29-11-500, MINF = 0.798, Camber = 5/10, ALPT = 4.10, BETA = 0.80, QINF = 597.7,

RNPU = 4.9E+06, CNWP = 0.2996

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.381 0.000 0.517 0.000 0.637"* 0.010 -0.052

0.060 0.011 0.020 0.293 0.020 0.218 0.020 -0.179

0.110 -0.212 0.040 0.153 0.060 0.417 ** 0.060 -0.490

0.200 -0.291 0.060 -0.125 0.090 -0.364 0.110 -0.622

0.230 -0.320 0.090 -0.271 0.110 -0.508 0.140 -0.944

0.400 -0.221 0.130 -0.467 0.130 -2.244"* 0.190 -2.244" *

0.490 -0.214 0.150 -0.642 0.150 -0.790 0.250 -0.379

0.590 -0.286 0.200 -0.487 0.210 -0.433 0.400 -0.360

0.630 -0.320 0.250 -0.362 0.250 -0.390 0.490 -0.330

0.700 -0.374 0.260 -0.359 0.340 -0.372 0.580 -0.349

0.750 -0.947 0.280 -0.356 0.370 -0.385 0.650 -0.456

0.810 -0.874 0.290 -0.352 0.400 -0.348 0.700 -0.427

0.840 -0.962 0.310 -0.334 0.410 -0.394 ** 0.750 -0.452

0.900 -0.216 0.320 -0.343 0.430 -0.376 0.800 -0.270

0.960 -0.158 0.340 -0.336 0.440 -0.367 0.830 -0.650

0.350 -0.184** 0.460 -0.357 0.900 -0.403

0.370 -0.323 0.490 -0.336 0.960 -0.407

0.380 -0.334 0.500 -0.362

0.400 -0.298 0.520 -0.361

0.410 -0.323 0.540 -0.347

0.430 -0.300 0.550 -0.331

0.440 -0.295 0.580 -0.334

0.460 -0.313 0.600 -0.375

0.470 -0.325 0.610 -0.407

0.490 -0.322 0.650 -0.616

0.500 -0.321 0.700 -0.607

0.520 -0.311 0.750 -0.398

0.530 -0.322 0.820 -0.997

0.550 -0.338 0.890 -0.316

0.560 -0.353 0.900 -0.374

0.580 -0.323 0.960 -0.295

0.590 -0.360

0.600 -0.355

0.640 -0.636

0.700 -0.395

0.750 -0.037**

0.820 -0.568

0.870 -0.390

0.930 -0.287

0.960 -0.287

Lower Surface

0.020 - 1.04 1 0.020 -0.275 0.020 - 1.082 0.020 -0.203

0.110 -0.205 0.060 -0.245 0.060 -0.157 0.060 -0.022

0.230 -0.072 0.090 -0.203 0.090 -0.161 0.110 -0.156

0.400 -0.011 0.120 -0.137 0.120 -0.204 0.250 -0.210

0.490 0.027 0.200 -0.071 0.200 -0.076 0.400 -0.185

0.630 0.923 ** 0.260 -0.089 0.250 -0.149 0.490 -0.170

0.750 0.173 0.400 -0.054 0.400 -0.111 0.580 -0.125

0.850 0.203 0.490 -0.022 0.490 -0.047 0.650 0.072

0.900 0.282 0.580 0.031 0.580 -0.029 0.750 0.317

0.960 0.155 0.640 0.235 0.650 -0.047 0.830 0.417

0.750 0.298 0.750 -0.018 0.900 0.478

0.870 0.364 0.890 0.454 0.960 0.323

0.930 0.288 0.930 0.362

0.960 0.182 0.960 0.253

CN = 0.366 0.420 0.431 0.454

716
Table J-2. Continued.

Flight 21 l, Wing sweep = 26 °, Time = 10-29-15-500, MINF = 0,797, Camber = 5/10, ALPT = 5.15, BETA = 0.48, QINF = 595.9,

RNPU = 4.9E÷06. CNWP = 0.3278

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.277 0.000 0.633 0,000 0.682"* 0.010 -0.294

0.060 -0.082 0.020 0.152 0.020 0.049 0.020 -0.315

0.110 -0.323 0.040 0.028 0.060 0.335** 0.060 -0.712

0.200 -0.338 0,060 -0,239 0,090 -0,469 0.110 -0,833

0,230 -0.365 0.090 -0,374 0.110 -0.598 0.140 -0,972

0.400 -0.245 0.130 -0,564 0.130 -2,247"* 0.190 -2.247"*

0.490 -0.233 0.150 -0,763 0.150 -0,866 0,250 -0,526

0,590 -0.301 0.200 -0.791 0,210 -0.890 0,400 -0.389

0,630 -0.335 0.250 -0,353 0.250 -0.431 0,490 -0,358

0,700 -0.381 0.260 -0,356 0.340 -0.377 0.580 -0.371

0.750 -0.870 0,280 -0.373 0.370 -0.399 0,650 -0.477

0.810 -0.844 0.290 -0,365 0.400 -0.368 0,700 -0,454

0.840 -0.926 0.310 -0.362 0.410 -0.392** 0.750 -0,475

0,900 -0,255 0,320 -0,373 0.430 -0,400 0.800 -0,267

0.960 -0,230 0.340 -0.367 0,440 -0.394 0.830 -0.659

0,350 -0.181 ** 0,460 -0,383 0.900 -0.420

0.370 -0.354 0.490 -0.368 0,960 -0.397

0.380 -0.364 0.500 -0.385

0.400 -0.321 0,520 -0.377

0,410 -0.349 0.540 -0,372

0.430 -0.331 0.550 -0.358

0.440 -0.319 0,580 -0.352

0,460 -0.339 0.600 -0.403

0.470 -0.364 0.610 -0.421

0.490 -0.345 0.650 -0,638

0.500 -0.349 0.700 -0,628

0.520 -0.336 0,750 -0,457

0,530 -0.346 0.820 -0,907

0.550 -0.364 0.890 -0.308

0.560 -0.378 0,900 -0.364

0.580 -0,336 0.960 -0,289

0.590 -0,382

0.600 -0,362

0.640 -0.691

0.700 -0.411

0.750 -0,024**

0,820 -0.572

0.870 -0.406

0.930 -0.282

0,960 -0.288

Lower Surface

0.020 -0.657 0.020 -0.583 0,020 -0.353 0,020 0.100

0.110 -0.165 0,060 -0.106 0,060 -0,048 0,060 -0.018

0.230 -0.024 0.090 -0.116 0,090 -0,066 0.110 -0.054

0,400 0.004 0.120 -0.072 0.120 -0.127 0.250 -0.143

0.490 0.040 0.200 -0.020 0.200 -0.024 0.400 -0.138

0.630 0,930** 0.260 -0.052 0.250 -0.094 0.490 -0.133

0.750 0.177 0.400 -0,032 0.400 -0,075 0.580 -0.097

0.850 0.216 0.490 -0.005 0.490 -0,025 0.650 0.091

0,900 0.294 0.580 0,039 0.580 -0,007 0.750 0.334

0.960 0.146 0.640 0.258 0.650 -0.032 0.830 0.437

0,750 0.318 0.750 -0,007 0.900 0.494

0.870 0,402 0.890 0,467 0,960 0.329

0,930 0.315 0.930 0.370

0.960 0.197 0,960 0.269

CN = 0.410 0.505 0.509 0.547

717
Table J-2. Continued.

Flight 211, Wing sweep = 26", Time = 10-29-19-000, MINF = 0.796, Camber = 5/10, ALPT = 5.95, BETA -- 0.66, QINF = 593.9,

RNPU = 4.9E+06, CNWP = 0.3689

TI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 0.186 0.000 0,736 0.000 0.708"* 0.010 -0,444

0.060 -0.163 0.020 0.037 0,020 -0.091 0.020 -0.413

0.110 -0.391 0.040 -0.073 0,060 0,231 ** 0.060 -0.811

0.200 -0.331 0.060 -0,349 0.090 -0.541 0.110 -0.953

0.230 -0.348 0.090 -0.453 0.110 -0,674 0.140 - I. 142

0,400 -0.263 0.130 -0,639 0.130 -2.253 * * 0.190 -2.253 * *

0.490 -0.245 0.150 -0.825 0.150 -0.907 0.250 -0.655

0.590 -0.312 0.200 -0.862 0.210 -0.955 0.400 -0.413

0.630 -0,343 0.250 -0.916 0.250 -0.929 0.490 -0.379

0.700 -0,385 0.260 -0.896 0.340 -0.347 0.580 -0.390

0.750 - 1,007 0.280 -0.475 0.370 -0,355 0.650 -0.490

0,810 -0,899 0.290 -0,330 0.400 -0.345 0,700 -0.462

0,840 -0,948 0.310 -0.293 0.410 -0.391 ** 0.750 -0,497

0,900 -0.266 0.320 -0,298 0,430 -0.381 0.800 -0.266

0.960 -0.225 0,340 -0.304 0.440 -0.376 0.830 -0.675

0.350 -0.136** 0,460 -0,375 0.900 -0.394

0,370 -0.316 0,490 -0.363 0.960 -0.348

0.380 -0.340 0,500 -0.382

0.400 -0,308 0.520 -0.386

0.410 -0.333 0,540 -0,378

0.430 -0.323 0.550 -0.363

0.440 -0.314 0.580 -0.369

0.460 -0.334 0,600 -0,406

0,470 -0.346 0.610 -0,430

0,490 -0.349 0.650 -0,648

0.500 -0,350 0,700 -0,643

0.520 -0,344 0,750 -0,491

0,530 -0.351 0.820 -0.907

0,550 -0.375 0,890 -0.290

0.560 -0.389 0.900 -0.335

0,580 -0.352 0,960 -0.252

0.590 -0,390

0,600 -0.382

0.640 -0.700

0.700 -0.436

0.750 -0,017"*

0.820 -0,576

0,870 -0.487

0.930 -0.286

0.960 -0,282

Lower Surface

0.020 -0.352 0.020 -0,360 0.020 -0.181 0.020 0.225

0.110 -0.140 0,060 -0.016 0,060 0,040 0,060 -0.016

0.230 0.006 0.090 -0.053 0.090 0.009 0.110 0.026

0.400 0.011 0.120 -0.019 0.120 -0,064 0.250 -0.113

0,490 0.034 0,200 0.011 0.200 0.009 0.400 -0.107

0.630 0,935"* 0.260 -0.014 0,250 -0.049 0.490 -0.106

0.750 0.177 0.400 -0.012 0,400 -0.046 0,580 -0.073

0.850 0.205 0.490 -0.002 0.490 -0.020 0,650 0.111

0.900 0.297 0.580 0.042 0.580 0.002 0.750 0.354

0.960 0,147 0.640 0.264 0,650 -0.023 0.830 0,444

0.750 0.320 0,750 0.002 0.900 0.501

0.870 0.414 0.890 0,473 0.960 0.343

0.930 0.312 0.930 0.373

0,960 0.197 0.960 0.271

CN -- 0.441 0.570 0.573 0.618

718
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 10-29-28-500, MINF = 0.788, Camber = 5/10. ALPT = 8.t3, BETA = 0.74, QINF = 582.1,

RNPU = 4.8E+06, CNWP = 0.4656

1] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.178 0.000 0.856 0.000 0.660"* 0.010 -0.934

0.060 -0.456 0.020 -0.425 0.020 -0.527 0.020 - 1.040

0.110 -0.546 0.040 -0.063 0.060 0.064** 0.060 - 1.050

0.200 -0.994 0.060 -0.689 0.090 -0.937 0.110 - 1.219

0.230 -0.882 0.090 -0.793 0.110 -0.995 0.140 - 1.383

0.400 -0.261 0.130 -0.841 0.130 -2.303 * * 0.190 -2.303 **

0.490 -0.263 0.150 - 1.020 0.150 - 1.125 0.250 - 1.384

0.590 -0.334 0.200 - 1.030 0.210 - 1.178 0.400 -0.560

0.630 -0.372 0.250 - 1.098 0.250 -0.952 0.490 -0.429

0.700 -0.416 0.260 - 1.096 0.340 - 1.205 0.580 -0.431

0.750 - 1.002 0.280 - 1.124 0.370 - 1.198 0.650 -0.527

0.810 -0.905 0.290 - 1.124 0.400 - 1.144 0.700 -0.520

0.840 -0.971 0.310 -0.834 0.410 -0.403** 0.750 -0.589

0.900 -0.379 0.320 - 1.101 0.430 -0.611 0.800 -0.598

0.960 -0.361 0.340 -0.876 0.440 -0.523 0.830 -0.682

0.350 -0.430"* 0.460 -0.455 0.900 -0.219

0.370 -0.940 0.490 -0.369 0.960 -0.167

0.380 -1.131 0.500 -0.350

0.400 -0.967 0.520 -0.343

0.410 -0.569 0.540 -0.318

0.430 -0.388 0.550 -0.307

0.440 -0.335 0.580 -0.333

0.460 -0.294 0.600 -0.366

0.470 -0.268 0.610 -0.379

0.490 -0.242 0.650 -0.520

0.500 -0.245 0.700 -0.497

0.520 -0.234 0.750 -0.441

0.530 -0.249 0.820 -0.989

0.550 -0.282 0.890 -0.212

0.560 -0.308 0.900 -0.240

0.580 -0.293 0.960 -0.185

0.590 -0.336

0.600 -0.339

0.640 -0.500

0.700 -0.454

0.750 -0.002**

0.820 -0.578

0.870 -0.500

0.930 -0.287

0.960 -0.282

Lower Surface

0.020 -0.078 0.020 0.065 0.020 0.154 0.020 0.490

0.110 -0.032 0.060 0.185 0.060 0.235 0.060 0.023

0.230 0.108 0.090 0.130 0.090 0.180 0.110 0.198

0.400 0.046 0.120 0.111 0.120 0.090 0.250 0.016

0.490 0.058 0.200 0.110 0.200 0.110 0.400 -0.010

0.630 0.949"* 0.260 0.083 0.250 0.066 0.490 -0.017

0.750 0.166 0.400 0.054 0.400 0.039 0.580 0.007

0.850 0.189 0.490 0.060 0.490 0.001 0.650 0.167

0.900 0.274 0.580 0.086 0.580 0.063 0.750 0.396

0.960 0.102 0.640 0.295 0.650 -0.013 0.830 0.479

0.750 0.335 0.750 0.020 0.900 0.530

0.870 0.420 0.890 0.501 0.960 0.369

0.930 0.325 0.930 0.398

0.960 0.207 0.960 0.285

CN = 0.616 0.766 0.786 0.880

719
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 9-57-50-000, MINF = 0.798, Camber = 5/11, ALPT = 3.16, BETA = 0.25, QINF = 786.2,

RNPU = 6.5E+06, CNWP = 0.1765

= 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.496 0.000 0.318 0.000 0.526** 0.010 0,092

0.060 0.144 0.020 0.448 0,020 0.378 0.020 -0.013

0.110 -0.114 0.040 0.288 0.060 0.471 ** 0.060 -0.305

0.200 -0.211 0.060 0.037 0,090 -0.221 0.110 -0.508

0,230 -0.235 0.090 -0.100 0.110 -0.339 0.140 -0.684

0.400 -0.173 0.130 -0.269 0.130 -2.243 * * 0.190 -2.243 * *

0.490 -0.183 0.150 -0.388 0.150 -0.404 0.250 -0.343

0.590 -0.253 0.200 -0.316 0.210 -0.387 0.400 -0.312

0.630 -0.290 0.250 -0.260 0.250 -0.307 0.490 -0.286

0.700 -0.345 0,260 -0.261 0.340 -0.305 0,580 -0.304

0.750 -0.792 0.280 -0,268 0.370 -0.311 0.650 -0.417

0.810 -0.732 0,290 -0.268 0.400 -0.289 0.700 -0.392

0.840 -0.753 0.310 -0.255 0.410 -0.799"* 0.750 -0.407

0.900 -0.212 0,320 -0.261 0.430 -0.313 0.800 -0.721

0.960 -0.150 0.340 -0,262 0.440 -0.307 0.830 -0.719

0.350 -0.206** 0.460 -0.305 0.900 -0.406

0.370 -0.257 0.490 -0.274 0.960 -0.383

0.380 -0.264 0.500 -0.308

0.400 -0.232 0.520 -0.309

0.410 -0.265 0.540 -0.305

0.430 -0.251 0.550 -0.288

0.440 -0.246 0.580 -0.295

0.460 -0.256 0.600 -0.331

0.470 -0.280 0.610 -0,357

0.490 -0.267 0,650 -0,495

0.500 -0.274 0.700 -0.430

0.520 -0.270 0.750 -0.340

0.530 -0,278 0,820 -0.857

0.550 -0,302 0.890 -0.303

0.560 -0.311 0.900 -0.387

0.580 -0.283 0.960 -0.302

0,590 -0.318

0.600 -0.320

0.640 -0.450

0.700 -0.363

0.750 -0.080**

0.820 -0.595

0.870 -0.404

0.930 -0.295

0.960 -0.301

Lower Surface

0.020 -0.968 0.020 -0.741 0.020 - 1.402 0.020 -0,422

0.110 -0.485 0.060 -0.711 0.060 -0.515 0.060 -0.039

0.230 -0.169 0.090 -0,567 0.090 -0.299 0.110 -0.301

0.400 -0.030 0.120 -0.377 0.120 -0.274 0.250 -0.290

0.490 0.013 0.200 -0.176 0.200 -0.167 0.400 -0.248

0,630 0.344** 0.260 -0.153 0.250 -0.224 0.490 -0.219

0.750 0.154 0.400 -0.083 0.400 -0.165 0.580 -0.171

0.850 0.171 0.490 -0.036 0.490 -0.086 0.650 0.040

0.900 0.233 0.580 0.026 0.580 -0.053 0.750 0.285

0.960 0.138 0.640 0.220 0.650 -0.082 0.830 0.390

0.750 0.262 0.750 -0,036 0.900 0.445

0.870 0.330 0,890 0,420 0.960 0.314

0.930 0.257 0,930 0.335

0.960 0.160 0,960 0.262

CN = 0.232 0.270 0.283 0.363

720
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 9-58-1-500, MINF = 0.812, Camber = 5/10, ALPT = 5.23, BETA = 0.22, QINF = 811.0,

RNPU = 6.6E+06, CNWP = 0.3021

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.335 0.000 0.578 0.000 0.554** 0.010 -0.220

0.060 -0.031 0.020 0.239 0.020 0.127 0.020 -0.282

0.110 -0.286 0.040 0.049 0.060 0.254** 0.060 -0.666

0.200 -0.313 0.060 -0.174 0.090 -0.399 0.110 -0.789

0.230 -0.350 0.090 -0.314 0.110 -0.535 0.1 40 -0.952

0.400 -0.229 0.130 -0.511 0.130 -2.167"* 0.190 -2.167"*

0.490 -0.217 0.150 -0.703 0.150 -0.810 0.250 -0.645

0.590 -0.283 0.200 -0.734 0.210 -0.839 0.400 -0.367

0.630 -0.309 0.250 -0.305 0.250 -0.707 0.490 -0.342

0.700 -0.339 0.260 -0.321 0.340 -0.337 0.580 -0.357

0.750 -0.765 0.280 -0.339 0.370 -0.366 0.650 -0.452

0.8 l0 -0.676 0.290 -0.344 0.400 -0.343 0.700 -0.421

0.840 -0.728 0.310 -0.337 0.410 -0.767"* 0.750 -0.427

0.900 -0.243 0.320 -0.349 0.430 -0.377 0.800 -0.691

0.960 -0.227 0.340 -0.344 0.440 -0.366 0.830 -0.662

0.350 -0.186"* 0.460 -0.361 0.900 -0.429

0.370 -0.331 0.490 -0.325 0.960 -0.419

0.380 -0.341 0.500 -0.360

0.400 -0.304 0.520 -0.354

0.410 -0.330 0.540 -0.350

0.430 -0.309 0.550 -0.331

0.440 -0.299 0.580 -0.330

0.460 -0.320 0.600 -0.367

0.470 -0.330 0.610 -0.388

0.490 -0.323 0.650 -0.631

0.500 -0.320 0.700 -0.609

0.520 -0.314 0.750 -0.419

0.530 -0.322 0.820 -0.823

0.550 -0.342 0.890 -0.333

0.560 -0.346 0.900 -0.426

0.580 -0.313 0.960 -0.324

0.590 -0.347

0.600 -0.340

0.640 -0.639

0.700 -0.411

0.750 -0.046"*

0.820 -0.590

0.870 -0.412

0.930 -0.289

0.960 -0.293

Lower Surface

0.020 -0.921 0.020 -0.710 0.020 -0.551 0.020 0.063

0.110 -0.190 0.060 -0.231 0.060 -0.101 0.060 -0.025

0.230 -0.064 0.090 -0.171 0.090 -0.106 0.110 -0.082

0.400 -0.010 0.120 -0.109 0.120 -0.134 0.250 -0.181

0.490 0.015 0.200 -0.062 0.200 -0.060 0.400 -0.172

0.630 0.347"* 0.260 -0.079 0.250 -0.134 0.490 -0.166

0.750 0.1 64 0.400 -0.062 0.400 -0.1 04 0.580 -0.132

0.850 0.193 0.490 -0.029 0.490 -0.051 0.650 0.073

0.900 0.265 0.580 0.021 0.580 -0.038 0.750 0.318

0.960 0.131 0.640 0.238 0.650 -0.051 0. 830 0.418

0.750 0.292 0.750 -0.031 0.900 0.477

0.870 0.369 0.890 0.454 0.960 0.326

0.930 0.289 0.930 0.355

0.960 0.178 0.960 0.275

CN = 0.347 0.449 0.478 0.538

721
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 9-58-4-500, MINF -- 0.805, Camber -- 5/10, ALPT = 5.81, BETA = 0.43, QINF = 793.8,

RNPU = 6.5E+06, CNWP = 0.2369

rl = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0.254 0,000 0,660 0.000 0.582** 0,010 -0.380

0.060 -0.099 0,020 3,457 0.020 -0,016 0.020 -0,375

0.110 -0.346 0,040 -0.007 0.060 0.170* * 0.060 -0.745

0.200 -0.289 0.060 -2.914 0,090 -0,483 0.110 -0.895

0.230 -0.363 0.090 -0.391 0.110 -0.608 0.140 -1.086

0.400 -0.252 0.130 -0.582 0.130 -2.206"* 0.190 -2.206"*

0.490 -0.234 O. 150 -0.772 O. 150 -0.860 0.250 -0.611

0.590 -0.302 0.200 -0.803 0.210 -0.904 0.400 -0.399

0.630 -0.326 0.250 -0.841 0.250 -0.722 0.490 -0.360

0,700 -0,357 0,260 -0.767 0,340 -0,326 0.580 -0,387

0,750 -0,780 0,280 -0,348 0,370 -0.343 0.650 -0.470

0,810 -0.709 0.290 -0,289 0.400 -0.327 0,700 -0.443

0,840 -0,736 0.310 -0,279 0.410 -0,777"* 0,750 -0.450

0.900 -0.264 0,320 -0,294 0.430 -0,369 0.800 -0,699

0.960 -0.241 0.340 -0,308 0.440 -0,362 0.830 -0,742

0.350 -0.150** 0,460 -0,360 0,900 -0.444

0.370 -0.319 0,490 -0,341 0,960 -0.382

0.380 -0,335 0.500 -0.366

0.400 -0,299 0,520 -0,360

0.410 -0,325 0.540 -0.356

0,430 -0,308 0,550 -0.345

0.440 -0,305 0,580 -0.335

0,460 -0.324 0.600 -0.381

0,470 -0,352 0.610 -0.405

0.490 -0.336 0,650 -0,655

0.500 -0.337 0,700 -0.628

0.520 - 1.325 0.750 -0,432

0.530 -0.337 0,820 -0,833

0,550 1.061 0.890 -0.331

0.560 -0.360 0.900 0.068

0.580 -0,328 0.960 -0.303

0.590 -0.359

0,600 -0,350

0,640 -0,645

0.700 -0.415

0.750 -0.036**

0.820 -0,601

0,870 -0,438

0,930 -0,295

0.960 -0.297

Lower Surface

0.020 -0.754 0,020 -0,506 0.020 -0,280 0,020 0.014

0.1 t 0 -0.177 0,060 -0.096 0,060 -0,017 0,060 -0.732

0.230 -0,022 0.090 -0.106 0,090 -0,042 0,110 -0.008

0,400 -0,003 0.120 -0,066 0.120 -0,077 0.250 0,399

0,490 0.017 0.200 -0.030 0,200 -0,026 0.400 -0. t 40

0.630 0,361"* 0,260 -0.051 0.250 -0.092 0.490 -0.132

0,750 0.174 0,400 -0,044 0.400 -0.073 0.580 -0.101

0.850 0.204 0,490 -0.019 0.490 -0.039 0,650 0.096

0,900 0.282 0,580 0,030 0.580 -0,017 0.750 0,334

0.960 0.138 0.640 0,253 0.650 -0.050 0,830 0.435

0.750 0.304 0.750 -0.031 0.900 0.487

0.870 0.396 0.890 0,468 0.960 0.332

0,930 0,303 0.930 0,362

0,960 0.186 0.960 0.282

CN = 0.380 0,501 0.507 0,637

722
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-2-37-500, MINF = 0.856, Camber = 0/2, ALPT = 4.02, BETA = 0.54, QINF = 595.5,

RNPU = 4.7E+06, CNWP = 0.1865

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0,069 0,000 0.851 0.000 2.048** 0,010 -0,663

0.060 -0.096 0,020 -0.144 0.020 -0.271 0.020 -0.720

0.110 -0.180 0.040 -0.176 0.060 - 1.705 ** 0.060 -0.592

0.200 -0.187 0.060 -0.264 0.090 -0.533 0.110 -0.572

0,230 -0.251 0.090 -0.235 0.110 -0.228 0.140 -0.608

0.400 -0.179 0.130 -0,257 0.130 -0.286 0.190 -1.951"*

0,490 -0.181 0.150 -0.300 0.150 -0.310 0.250 -0.248

0.590 -0.244 0.200 -0.306 0.210 -0.397 0.400 -0.328

0.630 -0.271 0.250 -0,285 0,250 -0.402 0.490 -0.278

0.700 -0.233 0.260 -0.287 0.340 -0.281 0.580 -0.277

0.750 -0.241 0.280 -0.306 0.370 -0.316 0.650 -0.392

0.810 -0.207 0.290 -0.311 0.400 -0.323 0.700 -0.351

0.840 -0,213 0,310 -0.30l 0.410 -0.596** 0.750 -0.397

0,900 -0.084 0,320 -0.307 0.430 -0.323 0,800 -0.535**

0,960 0.040 0.340 -0.295 0,440 -0.312 0,830 -0.570

0.350 -0.296"* 0.460 -0,308 0.900 -0.150

0.370 -0.267 0,490 -0,241 0.960 0,024

0.380 -0.287 0.500 -0,301

0.400 -0.242 0.520 -0.297

0.410 -0.278 0,540 -0.283

0.430 -0,257 0.550 -0,245

0.440 -0.242 0,580 -0.239

0.460 -0.261 0,600 -0.286

0.470 -0.275 0.610 -0,303

0.490 -0.262 0.650 1.034"*

0.500 -0.263 0.700 -0.521

0,520 -0.263 0,750 -0.453

0,530 -0.271 0.820 -0.512**

0,550 -0,298 0.890 -0.081

0.560 -0.295 0.900 -0,041

0.580 -0.260 0.960 0.056

0.590 -0,302

0.600 -0.289

0.640 -0.510

0,700 -0,439

0,750 -0.068**

0.820 -0.264

0.870 -0.206

0,930 -0,058

0,960 0.007

Lower Surface

0,020 -0.892 0,020 -0,483 0.020 -0.197 0,020 0,222

0. | 10 -0.523 0.060 -0.207 0,060 -0,090 0,060 1.249**

0.230 -0.224 0.090 -0,232 0.090 0,867"* 0.110 -0,178

0.400 -0.115 0.120 -0.302 0.120 -0.215 0,250 -0.349

0.490 -0,092 0.200 -0,497 0,200 -0,354 0,400 -0.351

0,630 0.918"* 0.260 -0.347 0.250 -0,406 0,490 -0.410

0.750 0.048 0.400 -0.218 0.400 -0.302 0,580 -0.372

0.850 0.119 0.490 -0.197 0.490 -0,095 0.650 -0.145

0.900 0.206 0.580 -0.173 0.580 -0.256 0.750 0.109

0.960 0.197 0.640 0.030 0,650 -0.073 0,830 0,275

0.750 0.190 0.750 -0,054 0,900 0.318

0.870 0,269 0,890 0.311 0.960 0.282

0,930 0.232 0.930 0.263

0,960 0.188 0.960 -0.732"*

CN = 0,083 0.176 0,181 0.223

723
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time -- 9-2-45-000, MINF = 0.863, Camber = 0/2, ALPT = 5.21, BETA = 0.80, QINF = 605.2,

RNPU = 4.7E+06, CNWP = 0.2049

11 -- 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.149 0.000 0.876 0.000 2.015"* 0.010 -0.676

0.060 -0.377 0.020 -0.450 0.020 -0.441 0.020 -0.861

0.1 t 0 -0.407 0.040 -0.354 0.060 - 1.678"* 0.060 -0.777

0.200 -0.245 0.060 -0.536 0.090 -0.688 0.110 -0.736

0.230 -0.406 0.090 -0.564 0.110 -0.683 0.140 -0.774

0.400 -0.199 0.130 -0.581 0.130 -0.659 0.190 - 1.920"*

0.490 -0.204 0.150 -0.558 0.150 -0.604 0.250 -0.798

0.590 -0.254 0.200 -0.477 0.210 -0.642 0.400 -0.668

0.630 -0.280 0.250 -0.597 0.250 -0.668 0.490 -0.263

0.700 -0.276 0.260 -0.613 0.340 -0.725 0.580 -0.275

0.750 -0.243 0.280 -0.612 0.370 -0.739 0.650 -0.374

0.810 -0.230 0.290 -0.590 0.400 -0.699 0.700 -0.348

0.840 -0.222 0.310 -0.572 0.410 -0.587** 0.750 -0.383

0.900 -0.102 0.320 -0.581 0.430 -0.297 0.800 -0.519"*

0.960 0.021 0.340 -0.608 0.440 -0.218 0.830 -0.542

0.350 -0.389** 0.460 -0.194 0.900 -0.138

0.370 -0.443 0.490 -0.178 0.960 0.026

0.380 -0.231 0.500 -0.195

0.400 -0.116 0.520 -0.201

0.410 -0.164 0.540 -0.205

0.430 -0.157 0.550 -0.192

0.440 -0.160 0.580 -0.200

0.460 -0.188 0.600 -0.248

0.470 -0.214 0.610 -0.273

0.490 -0.215 0.650 1.016"*

0.500 -0.226 0.700 -0.491

0.520 -0.232 0.750 -0.423

0.530 -0.241 0.820 -0.539**

0.550 -0.274 0.890 -0.086

0.560 -0.280 0.900 -0.046

0.580 -0.257 0.960 0.053

0.59O -0.297

0.600 -0.285

0.640 -0.500

0.700 -0.436

0.750 -0.072"*

0.820 -0.299

0.870 -0.204

0.930 -0.064

0.960 -0.001

Lower Surface

0.020 -0.378 0.020 -0.194 0.020 -0.025 0.020 0.427

0.110 -0.368 0.060 -0.077 0.060 0.017 0.060 1.227" *

0.230 -0.119 0.090 -0.123 0.090 0.853" * 0.110 -0.068

0.400 -0.086 0.120 -0.201 0.120 -0.127 0.250 -0.275

0.490 -0.095 0.200 -0.241 0.200 -0.239 0.400 -0.277

0.630 0.903** 0.260 -0.267 0.250 -0.292 0.490 -0.352

0.750 0.030 0.400 -0.208 0.400 -0.276 0.580 -0.376

0.850 0.095 0.490 -0.196 0.490 -0.087 0.650 -0.141

0.900 O. 184 0.580 -0.178 0.580 -0.257 0.750 O. 113

0.960 0.175 0.640 0.025 0.650 -0.069 0.830 0.280

0.750 0.192 0.750 -0.051 0.900 0.323

0.870 0.265 0.890 0.309 0.960 0.275

0.930 0.235 0.930 0.261

0.960 0.184 0.960 -0.722"*

CN= 0.178 0.3_ 0.3_ 0.404

724
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-2-50-000, MINF = 0.860, Camber = 0/2, ALPT = 6.06, BETA = 0.77, QINF = 600.1,

RNPU = 4.7E+06, CNWP = 0.2962

q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.228 0.000 0.861 0,000 2,037"* 0.010 -0.81 l

0.060 -0.577 0.020 -0,467 0.020 -0.702 0.020 -0.884

O. 110 -0.555 0.040 -0,600 0.060 - 1.687"* 0.060 -0.882

0.200 -0.405 0.060 -0.651 0.090 -0.781 0.110 -0.825

0.230 -0.422 0.090 -0.654 0.110 -0.772 0.140 -0.855

0.400 -0.176 0.130 -0.694 0.130 -0.765 0.190 -1.931 **

0.490 -0.154 0.150 -0.682 0.150 -0.700 0.250 -0,886

0,590 -0.225 0.200 -0.606 0.210 -0.734 0.400 -0.716

0.630 -0.250 0.250 -0.704 0.250 -0.783 0.490 -0.570

0.700 -0.237 0.260 -0.707 0.340 -0.823 0.580 -0.465

0.750 -0.251 0.280 -0.725 0.370 -0.826 0.650 -0.330

0.810 -0.204 0,290 -0.733 0.400 -0.762 0.700 -0.309

0.840 -0.229 0.310 -0.715 0.410 -0.586** 0.750 -0.319

0.900 -0.126 0.320 -0.724 0.430 -0.819 0.800 -0.321 **

0.960 -0.001 0.340 -0.734 0.440 -0.809 0.830 -0.250

0.350 -0.408"* 0.460 -0.766 0.900 -0.116

0.370 -0.726 0.490 -0.780 0.960 0.038

0.380 -0.761 0.500 -0.838

0.400 -0.731 0.520 -0.828

0.410 -0.726 0.540 -0.718

0.430 -0.708 0.550 -0.405

0.440 -0.698 0.580 -0.223

0.460 -0.749 0.600 -0.208

0.470 -0.748 0.610 -0.182

0.490 -0.726 0.650 1.031 **

0.500 -0.402 0.700 -0.226

0.520 -0.233 0.750 -0.223

0.530 -0.146 0.820 -0.279"*

0.550 -0.130 0.890 -0.087

0.560 -0.128 0.900 -0.049

0.580 -0.114 0.960 0.054

0.590 -0.152

0.600 -0.144

0.640 -0.258

0.700 -0,251

0.750 -0.060**

0.820 -0.273

0.870 -0.231

0.930 -0.066

0.960 -0.002

Lower Surface

0.020 -0.178 0.020 -0.039 0.020 0.105 0.020 0.483

0.110 -0.250 0.060 0.005 0,060 0.099 0.060 1.244"*

0.230 -0,113 0.090 -0.049 0.090 0.866"* 0.110 0.008

0.400 -0.096 0.120 -0.132 0.120 -0.058 0.250 -0.207

0.490 -0.079 0.200 -0.128 0,200 -0.154 0.400 -0.219

0.630 0.916"* 0.260 -0.199 0.250 -0.212 0.490 -0.271

0.750 0.022 0.400 -0,174 0.400 -0.218 0.580 -0.346

0.850 0.085 0.490 -0. 175 0.490 -0,075 0.650 -0,124

0.900 0.172 0.580 -0.167 0,580 -0.228 0.750 0.129

0.960 0.161 0.640 0.036 0.650 -0.064 0.830 0.296

0.750 0.188 0.750 -0.046 0.900 0.334

0.870 0.269 0.890 0.319 0.960 0.283

0.930 0.232 0.930 0.269

0.960 0.186 0.960 -0.722**

CN = 0.215 0.412 0.420 0.488

725
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-2-53-500, MINF = 0.862, Camber = 0/2, ALPT = 7.29, BETA = 0.77, QINF --- 603.3,

RNPU = 4.7E+06, CNWP = 0.4023

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x,/c CP x/c CP

0.020 -0.713 0.000 0.830 0.000 2.027** 0.010 -0.890

0.060 -0.667 0.020 -0.747 0.020 -0.824 0.020 - 1.013

0.110 -0.672 0.040 -0.682 0.060 -1.677** 0.060 -0.992

0.200 -0.591 0.060 -0.778 0.090 -0.881 0.110 -0.908

0.230 -0.502 0.090 -0.778 0.110 -0.881 0.140 -0.930

0.400 -0.593 0.130 -0.810 0.130 -0.884 0.190 - 1.920"*

0.490 -0.437 0.150 -0.809 0.150 -0.813 0.250 -0.974

0.590 -0.184 0.200 -0.741 0.210 -0.832 0.400 -0.770

0.630 -0.212 0.250 -0.788 0.250 -0.864 0.490 -0.688

0.700 -0.206 0.260 -0.796 0.340 -0.923 0.580 -0.561

0.750 -0.234 0.280 -0.816 0.370 -0.926 0.650 -0.62 l

0.810 -0.210 0.290 -0.829 0.400 -0.897 0.700 -0.600

0.840 -0.220 0.310 -0.803 0.410 -0.583** 0.750 -0.622

0.900 -0.148 0.320 -0.819 0.430 -0.911 0.800 -0.189**

0.960 -0.029 0.340 -0.828 0.440 -0.899 0.830 -0.144

0.350 -0.421 ** 0.460 -0.762 0.900 -0.032

0.370 -0.819 0.490 -0.866 0.960 0.025

0.380 -0.870 0.500 -0.909

0.400 -0.808 0.520 -0.907

0.410 -0.841 0.540 -0.913

0.430 -0.813 0.550 -0.872

0.440 -0.820 0.580 -0.856

0.460 -0.845 0.600 -0.889

0.470 -0.843 0.610 -0.856

0.490 -0.830 0.650 1.025"*

0.500 -0.836 0.700 -0.374

0.520 -0.817 0.750 -0.233

0.530 -0.809 0.820 -0.131 **

0.550 -0.842 0.890 -0.022

0.560 -0.850 0.900 0.010

0.580 -0.825 0.960 0.078

0.590 -0.854

0.600 -0.702

0.640 -0.158

0.700 -0.127

0.750 -0.054**

0.820 -0. t 80

0.870 -0.173

0.930 -0.040

0.960 0.022

Lower Surface

0.020 -0.029 0.020 0.104 0.020 0.213 0.020 0.603

0.110 -0.189 0.060 0.091 0.060 0.177 0.060 1.237"*

0.230 -0.125 0.090 0.024 0.090 0.861 ** 0.110 0.068

0.400 -0.096 0.120 -0.059 0.120 0.011 0.250 -0.142

0.490 -0.086 0.200 -0.076 0.200 -0.078 0.400 -0.17 I

0.630 0.911 ** 0.260 -0.148 0.250 -0.149 0.490 -0.236

0.750 0.013 0.400 -0.147 0.400 -0.177 0.580 -0.334

0.850 0.065 0.490 -0.157 0.490 -0.063 0.650 -0.119

0.900 0.148 0.580 -0.156 0.580 -0.212 0.750 0.134

0.960 0.146 0.640 0.042 0.650 -0.056 0.830 0.299

0.750 0.187 0.750 -0.045 0.900 0.337

0.870 0.245 0.890 0.321 0.960 0.276

0,930 0.231 0.930 0.272

0.960 0.187 0.960 -0.718" *

CN = 0.325 0.537 0.568 0.609

726
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-2-57-500, MINF = 0.859, Camber = 0/2, ALPT = 8.07, BETA = 0.83, QINF = 601.1,

RNPU = 4.7E+06, CNWP = 0.4515

11 = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.790 0.000 0.795 0.000 2.026"* 0.010 -0.974

0.060 -0.782 0.020 -0.840 0.020 -0.905 0.020 - 1.087

0.110 -0.799 0.040 -0.793 0.060 - 1.692 ** 0.060 - 1.055

0.200 -0.706 0.060 -0.868 0.090 -0.969 0.110 -0.996

0.230 -0.601 0.090 -0.871 0.110 -0.959 0.140 - 1.039

0.400 -0.668 0.130 -0.883 0.130 -0.951 0.190 - 1.936 **

0.490 -0.598 0.150 -0.894 0.150 -0.882 0.250 - 1.051

0.590 -0.182 0.200 -0.835 0.210 -0.907 0.400 -0.834

0.630 -0.194 0.250 -0.873 0.250 -0.921 0.490 -0.719

0.700 -0.193 0.260 -0.876 0.340 - 1.003 0.580 -0.633

0.750 -0.226 0.280 -0.901 0.370 -0.998 0.650 -0.676

0.810 -0.205 0.290 -0.910 0.400 -0.964 0.700 -0.645

0.840 -0.219 0.310 -0.856 0.410 -0.593** 0.750 -0.589

0.900 -0.166 0.320 -0.895 0.430 -0.991 0.800 -0.211 **

0.960 -0.048 0.340 -0.902 0.440 -0.977 0.830 -0.141

0.350 -0.435** 0.460 -0.773 0.900 -0.048

0.370 -0.894 0.490 -0.931 0.960 -0.001

0.380 -0.943 0.500 -0.985

0.400 -0.869 0.520 -0.993

0.410 -0.880 0.540 -0.995

0.430 -0.895 0.550 -0.951

0.440 -0.829 0.580 -0.916

0.460 -0.930 0.600 -0.957

0.470 -0.910 0.610 -0.940

0.490 -0.903 0.650 1.021 **

0.500 -0.912 0.700 -0.431

0.520 -0.896 0.750 -0.336

0.530 -0.881 0.820 -0.128**

0.550 -0.913 0.890 -0.003

0.560 -0.923 0.900 0.026

0.580 -0.895 0.960 0.076

0.590 -0.943

0.600 -0.915

0.640 -0.249

0.700 -0.186

0.750 -0.040**

0.820 -0.130

0.870 -0.129

0.930 -0.017

0.960 0.035

Lower Surface

0.020 0.055 0.020 0.214 0.020 0.301 0.020 0.663

0.110 -0.140 0.060 0.163 0.060 0.225 0.060 1.234"*

0.230 -0.103 0.090 0.084 0.090 0.856 ** 0.110 0.142

0.400 -0.092 0.120 0.000 0.120 0.054 0.250 -0.096

0.490 -0.087 0.200 -0.032 0.200 0.001 0.400 -0.133

0.630 0.907** 0.260 -0.102 0.250 -0.097 0.490 -0.198

0.750 0.003 0.400 -0.117 0.400 -0.145 0.580 -0.295

0.850 0.054 0.490 -0.140 0.490 -0.050 0.650 -0.113

0.900 0.142 0.580 -0.149 0.580 -0.199 0.750 0.143

0.960 0.135 0.640 0.041 0.650 -0.043 0.830 0.301

0.750 0.187 0.750 -0.034 0.900 0.336

0.870 0.254 0.890 0.318 0.960 0.267

0.930 0.227 0.930 0.260

0.960 0.187 0.960 -0.729"*

CN = 0.387 0.614 0.650 0.685

727
TableJ-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-3-3-500, MINF = 0.857, Camber = 0/2, ALPT = 9.22, BETA = 0.83, QINF = 606.2,

RNPU = 4.8E+06, CNWP = 0.4920

"0= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.904 0.000 0.728 0.000 1.983** 0.010 - 1.1 O0

0.060 -0.919 0.020 -0.964 0.020 - 1.010 0.020 - 1.181

0.110 -0.862 0.040 -0.912 0.060 - 1.703"* 0.060 - 1.171

0.200 -0.798 0.060 -0.966 0.090 - 1.054 0.110 - 1.113

0.230 -0.696 0.090 -0.978 0.110 - 1.057 0.140 - 1.140

0.400 -0.742 0.130 -0.902 0.130 - 1.056 0.190 - 1.945" *

0.490 -0.703 0.150 -0.979 0.150 -0.977 0.250 - 1.148

0.590 -0.167 0.200 -0.922 0.210 -0.997 0.400 -0.902

0.630 -0.180 0.250 -0.956 0.250 -0.966 0.490 -0.769

0.700 -0.196 0.260 -0.961 0.340 - 1.096 0.580 -0.700

0.750 -0.256 0.280 -0.978 0.370 - 1.089 0.650 -0.731

0.810 -0.236 0.290 -0.991 0.400 - t .045 0.700 -0.697

0.840 -0.259 0.310 -0.875 0.410 - 1.009"* 0.750 -0.471

0.900 -0.205 0.320 -0.983 0.430 -1.099 0.800 -0.248**

0.960 -0.073 0.340 -0.929 0.440 - 1.076 0.830 -0.179

0.350 -0.454"* 0.460 -0.792 0.900 -0.100

0.370 -0.962 0.490 - 1.029 0.960 -0.044

0.380 - 1.036 0.500 - 1.066

0.400 -0.960 0.520 - 1.071

0.410 -0.899 0.540 - 1.071

0.430 -0.975 0.550 - 1.033

0.440 -0.848 0.580 - 1.020

0.460 - 1.018 0.600 - 1.064

0.470 - 1.008 0.610 -0.869

0.490 -0.987 0.650 0.987"*

0.500 -0.997 0.700 -0.405

0.520 -0.894 0.750 -0.400

0.530 -0.511 0.820 -0.290**

0.550 -0.474 0.890 -0.116

0.560 -0.446 0.900 -0.122

0.580 -0.416 0.960 -0.054

0.590 -0.429

0.600 -0.396

0.640 -0.345

0.700 -0.347

0.750 -0.037"*

0.820 -0.192

0.870 -0.162

0.930 -0.155

0.960 -0.1 44

Lower Surface

0.020 0.131 0.020 0.334 0.020 0.404 0.020 0.729

0.110 -0.086 0.060 0.229 0.060 0.301 0.060 1.197"*

0.230 -0.081 0.090 0.151 0.090 0.823" * 0.110 0.201

0.400 -0.092 0.120 0.059 0.120 0.123 0.250 -0.040

0.490 -0.092 0.200 0.021 0.200 0.087 0.400 -0.090

0.630 0.894 ** 0.260 -0.052 0.250 -0.04 1 0.490 -0.16 l

0.750 -0.015 0.400 -0.093 0.400 -0.105 0.580 -0.265

0.850 0.037 0.490 -0.127 0.490 -0.044 0.650 -0.105

0.900 0.126 0.580 -0.153 0.580 -0.188 0.750 0.142

0.960 0.115 0.640 0.028 0.650 -0.040 0.830 0.300

0.750 0.164 0.750 -0.025 0.900 0.329

0.870 0.246 0.890 0.294 0.960 0.249

0.930 0.168 0.930 0.231

0.960 0.106 0.960 -0.748 **

CN = 0.445 0.660 0.739 0.768

728
Table J-2. Continued.

Flight 223, Wing sweep = 26 °, Time = 9-3-15-000, MINF = 0.848, Camber = 0/2, ALPI" = 9.91, BETA = 0.66, QINF = 610.5,

RNPU = 4.8E+06, CNWP = 0.4793

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 - 1.042 0.000 0.636 0.000 1.913"* 0.010 - 1.216

0.060 - 1.023 0.020 - 1.087 0.020 - 1.152 0.020 - 1.275

0.110 - 1.032 0.040 -0.944 0.060 - 1.748 ** 0.060 - 1.265

0.200 -0.887 0.060 -1.081 0.090 -1.170 0.110 -1.216

0.230 -0.791 0.090 -1.079 0.1 t0 -1.147 0.140 -1.228

0.400 -0.848 0.130 -0.952 0.130 - 1.159 0.190 - 1.988" *

0.490 -0.285 0.150 - 1.047 0.150 - 1.074 0.250 - 1.233

0.590 -0.174 0.200 - 1.013 0.210 - 1.095 0.400 -0.949

0.630 -0.234 0.250 - 1.062 0.250 - 1.015 0.490 -0.796

0.700 -0.243 0.260 - 1.055 0.340 -1.170 0.580 -0.695

0.750 -0.277 0.280 - 1.078 0.370 - 1.177 0.650 -0.481

0.810 -0.269 0.290 - 1.091 0.400 - 1.135 0.700 -0.438

0.840 -0.290 0.310 -0.925 0.410 -1.059"* 0.750 -0.290

0.900 -0.204 0.320 - 1.069 0.430 -0.988 0.800 -0.191 **

0.960 -0.103 0.340 -0.864 0.440 -0.805 0.830 -0.182

0.350 -0.356"* 0.460 -0.699 0.900 -0.104

0.370 -0.914 0.490 -0.614 0.960 -0.067

0.380 -0.823 0.500 -0.596

0.400 -0.722 0.520 -0.592

0.410 -0.594 0.540 -0.582

0.430 -0.584 0.550 -0.556

0.440 -0.480 0.580 -0.539

0.460 -0.532 0.600 -0.554

0.470 -0.518 0.610 -0.532

0.490 -0.461 0.650 0.923"*

0.500 -0.490 0.700 -0.494

0.520 -0.457 0.750 -0.472

0.530 -0.455 0.820 -0,382**

0.550 -0.457 0.890 -0.283

0.560 -0.458 0.900 -0.282

0.580 -0.446 0.960 -0.221

0.590 -0.474

0.600 -0.435

0.640 -0.372

0.700 -0.400

0.750 -0.049"*

0.820 -0.281

0.870 -0.225

0.930 -0.223

0.960 -0.220

Lower Surface

0.020 0.250 0.020 0.411 0.020 0.471 0.020 0.761

0.110 -0.040 0.060 0.282 0.060 0.342 0.060 1.133"*

0.230 -0.064 0.090 0.201 0.090 0.761 ** 0.110 0.249

0.400 -0.086 0.120 0. ] 02 0.120 0.156 0.250 -0.005

0.490 -0.094 0.200 0.064 0.200 0.096 0.400 -0.057

0.630 0.832** 0.260 -0.009 0.250 0.001 0.490 -0.126

0.750 -0.036 0.400 -0.074 0.400 -0.070 0.580 -0.214

0.850 0.004 0.490 -0.120 0.490 -0.043 0.650 -0.084

0.900 0.089 0.580 -0.139 0.580 -0.172 0.750 0.151

0.960 0.082 0.640 0.005 0.650 -0.043 0.830 0.289

0.750 0.135 0.750 -0.014 0.900 0.314

0.870 0.183 0.890 0.255 0.960 0.227

0.930 0.108 0.930 0.179

0.960 0.040 0.960 -0.799**

CN = 0.461 0.652 0.744 0.792

729
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 15-2-25-000, MINF = 0.851, Camber = 0/2, ALPT = 4.10, BETA = -0.10, QINF -- 598.2,

RNPU = 4.7E+06, CNWP = 0.1806

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.017 0.000 0.847 0.000 0.422"* 0.010 -0.731

0.060 -0.153 0.020 -0.276 0.020 -0.404 0.020 -0.824

0.110 -0.223 0.040 -0.218 0.060 -0.251 0.060 -0.690

0.200 -0.211 0.060 -0.350 0.090 -0.640 0.110 -0.684

0.230 -0.301 0.090 -0.317 0.110 -0.545 0.140 -0.713

0.400 -0.215 0.130 -0.361 0.130 -0.295 0.190 -1.972"*

0.490 -0.201 0.150 -0.346 0.150 -0.301 0.250 -0.292

0.590 -0.261 0.200 -0.348 0.210 -0.405 0.400 -0.351

0.630 -0.277 0.250 -0.329 0.250 -0.443 0.490 -0.324

0.700 -0.249 0.260 -0.326 0.340 -0.305 0.580 -0.317

0.750 -0.258 0.280 -0.341 0.370 -0.353 0.650 -0.407

0.810 -0.227 0.290 -0.337 0.400 -0.353 0.700 -0.371

0.840 -0.241 0.310 -0,330 0.410 - 1.054** 0.750 -0.414

0.900 -0.113 0.320 -0.328 0.430 -0.343 0.800 -0.506

0.960 0.020 0.340 -0.310 0.440 -0.331 0.830 -0.492

0.350 -0.269"* 0.460 -0.326 0.900 -0.170

0.370 -0.302 0.490 -0.306 0.960 0.013

0.380 -0.314 0.500 -0.323

0.400 -0.271 0.520 -0.306

0.410 -0.305 0.540 -0.29l

0.430 -0.276 0.550 -0.288

0.440 -0.271 0.580 -0.301

0.460 -0.285 0.600 -0.391

0.470 -0.300 0.610 -0.328

0.490 -0.290 0.650 -0.666

0.500 -0.288 0.700 -0.549

0.520 -0.284 0.750 -0.483

0.530 -0.290 0.820 -0.355

0.550 -0.325 0.890 -0.111

0.560 -0.313 0.900 -0.071

0.580 -0.282 0.960 0.037

0.590 -0.323

0.600 -0.320

0.640 -0.548

0.700 -0.463

0.750 -0.071

0.820 -0.287

0.870 -0.237

0.930 -0.08 I

0.960 -0.012

Lower Surface

0.020 -0.779 0.020 -0.449 0.020 -0.175 0.020 0.231

0.110 -0.474 0.060 -0.189 0.060 -0.083 0.060 0.002

0.230 -0.195 0.090 -0.226 0.090 -0.122 0.110 -0.094

0.400 -0.116 0.120 -0.280 0.120 -0.220 0.250 -0.347

0.490 -0.109 0.200 -0.307 0.200 -0.345 0.400 -0.336

0.630 0.908** 0.260 -0.323 0.250 -0.358 0.490 -0.381

0.750 0.034 0.400 -0.226 0.400 -0.301 0.580 -0.400

0.850 0.091 0.490 -0.198 0.490 -0.112 0.650 -0.165

0.900 0.196 0.580 -0.186 0.580 -0.269 0.750 0.115

0.960 0,171 0.640 0.029 0.650 -0.075 0.830 0.251

0.750 0.168 0.750 -0.062 0.900 0.307

0.870 0,246 0.890 0.309 0.960 0.259

0.930 0.220 0.930 0.255

0.960 0.178 0.960 0.319

CN = 0.113 0.203 0.216 0.270

730
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 15-2-29-500, MINF = 0.853, Camber = 0/2, ALPT = 5.07, BETA = 0.31, QINF = 600.8,

RNPU = 4.7E+06, CNWP = 0.2395

rI = 0.93 0,76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.241 0.000 0,868 0.000 0.399* * 0.010 -0.732

0.060 -0.431 0.020 -0.547 0.020 -0.415 0.020 -0.932

0.110 -0.412 0.040 -0.386 0.060 -0.318 0.060 -0.872

0.200 -0.239 0,060 -0.609 0.090 -0.775 0.110 -0.819

0.230 -0.367 0.090 -0.640 0.110 -0.758 0.140 -0.855

0.400 -0.237 0.130 -0.659 0.130 -0.728 0.190 - 1.964 **

0.490 -0.218 0.150 -0.628 0.150 -0.674 0.250 -0.825

0.590 -0.268 0.200 -0.533 0.210 -0.707 0.400 -0.322

0.630 -0.300 0.250 -0.657 0.250 -0.737 0.490 -0.292

0.700 -0.256 0.260 -0.654 0.340 -0.673 0.580 -0.306

0.750 -0.260 0.280 -0.657 0.370 -0.262 0.650 -0.397

0.810 -0.234 0.290 -0.451 0.400 -0.216 0.700 -0.370

0.840 -0.252 0.310 -0.212 0.410 -1.050"* 0.750 -0.414

0.900 -0.120 0.320 -0.206 0.430 -0.241 0.800 -0.450

0.960 -0.006 0.340 -0.194 0.440 -0.244 0.830 -0.440

0,350 -0.184"* 0.460 -0.254 0.900 -0.161

0.370 -0.226 0.490 -0,261 0.960 0.013

0.380 -0.254 0,500 -0.273

0.400 -0,233 0.520 -0.277

0.410 -0,266 0,540 -0.270

0,430 -0.261 0,550 -0,269

0,440 -0.252 0,580 -0.285

0.460 -0.268 0.600 -0,384

0,470 -0.299 0.610 -0,324

0.490 -0,292 0,650 -0.661

0.500 -0,289 0,700 -0.547

0.520 -0.292 0.750 -0.484

0.530 -0.298 0.820 -0.342

0.550 -0.326 0.890 -0.108

0.560 -0.314 0.900 -0.072

0.580 -0.288 0.960 0.044

0.590 -0.330

0,600 -0.325

0.640 -0.545

0.700 -0.467

0.750 -0.066

0.820 -0.282

0.870 -0.235

0.930 -0.083

0.960 -0.012

Lower Surface

0.020 -0.316 0.020 -0.140 0.020 -0.005 0.020 0.431

0.110 -0.297 0.060 -0.067 0,060 0.018 0.060 0.002

0.230 -0.097 0.090 -0.111 0.090 -0.037 0.110 -0.011

0.400 -0.097 0.120 -0.180 0.120 -0.127 0,250 -0,269

0.490 -0,098 0.200 -0.149 0.200 -0.243 0.400 -0.270

0.630 0.903** 0.260 -0.247 0,250 -0.264 0.490 -0.309

0,750 0.031 0.400 -0.197 0,400 -0.252 0.580 -0.360

0.850 0.083 0.490 -0.186 0.490 -0.105 0.650 -0.154

0.900 0.177 0.580 -0.173 0.580 -0.250 0.750 0.125

0.960 0.164 0.640 0.026 0.650 -0.072 0.830 0.258

0.750 0.167 0.750 -0.059 0.900 0.314

0.870 0.249 0.890 0.318 0.960 0.267

0.930 0.222 0.930 0.257

0,960 0.183 0.960 0.320

CN = 0.197 0.308 0.329 0.395

731
Table J-2. Continued.

Flight 208, Wing sweep = 26", Time = 15-2-39-000, MINF = 0.857, Camber = 0/2, ALPT = 6.99, BETA = 0.25, QINF = 608.5,

RNPU = 4.8E+06, CNWP -- 0.3620

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x./c CP x/c CP

0.020 -0.718 0.000 0.819 0.000 0.403"* 0.010 -0.967

0.060 -0.735 0.020 -0.846 0.020 -0.883 0.020 - 1.093

0.110 -0.743 0.040 -0.697 0.060 -0.381 0.060 - 1.079

0.200 -0.670 0.060 -0.835 0.090 -0.958 0.110 -0.999

0.230 -0.548 0.090 -0.864 0.110 -0.942 0.140 - 1.005

0.400 -0.636 0.130 -0.863 0.130 -0.942 0.190 - 1.944**

0.490 -0.184 0.150 -0.877 0.150 -0.868 0.250 - 1.047

0.590 -0.189 0.200 -0.797 0.210 -0.900 0.400 -0.809

0.630 -0.225 0.250 -0.846 0.250 -0.926 0.490 -0.722

0.700 -0.214 0.260 -0.851 0.340 -0.970 0.580 -0.600

0.750 -0.245 0.280 -0.873 0.370 -0.964 0.650 -0.654

0.810 -0.225 0.290 -0.893 0.400 -0.943 0.700 -0.626

0.840 -0.247 0.310 -0.860 0.410 -1.042"* 0.750 -0.410

0.900 -0.166 0.320 -0.862 0.430 -0.965 0.800 -0.211

0.960 -0.049 0.340 -0.873 0.440 -0.952 0.830 -0.166

0.350 -0.436** 0.460 -0.762 0.900 -0.058

0.370 -0.872 0.490 -0.928 0.960 0.028

0.380 -0.920 0.500 -0.970

0.400 -0.862 0.520 -0.945

0.410 -0.871 0.540 -0.945

0.430 -0.870 0.550 -0.927

0.440 -0.821 0.580 -0.938

0.460 -0.899 0.600 -0.936

0.470 -0.896 0.610 -0.885

0.490 -0.878 0.650 -0.377

0.500 -0.881 0.700 -0.218

0.520 -0.863 0.750 -0.183

0.530 -0.854 0.820 -0.163

0.550 -0.889 0.890 -0.047

0.560 -0.826 0.900 -0.029

0.580 -0.436 0.960 0.070

0.590 -0.337

0.600 -0.242

0.640 -0.141

0.700 -0.133

0.750 -0.054

0.820 -0.206

0.870 -0.194

0.930 -0.056

0.960 0.013

Lower Surface

0.020 -0.037 0.020 0.138 0.020 0.216 0.020 0.602

0.110 -0.183 0.060 0.100 0.060 0.190 0.060 -0.003

0.230 -0.120 0.090 0.043 0.090 0.104 0.110 0.155

0.400 -0.094 0.120 -0.045 0.120 -0.015 0.250 -0.153

0.490 -0.092 0.200 -0.055 0.200 -0.078 0.400 -0.179

0.630 0.905 ** 0.260 -0.140 0.250 -0.1 40 0.490 -0.226

0.750 0.013 0.400 -0.143 0.400 -0.165 0.580 -0.314

0.850 0.054 0.490 -0.143 0.490 -0.073 0.650 -0.135

0.900 0.144 0.580 -0.152 0.580 -0.220 0.750 0.151

0.960 0.135 0.640 0.042 0.650 -0.055 0.830 0.281

0.750 0.182 0.750 -0.056 0.900 0.328

0.870 0.247 0.890 0.327 0.960 0.266

0.930 0.230 0.930 0.272

0.960 0.187 0.960 0.307

CN = 0.329 0.548 0.565 0.637

732
Table J-2. Continued.

Flight 208, Wing sweep = 26", Time = 15-2-48-500, MINF = 0,854, Camber = 0/2, ALPT = 8.06, BETA = 0.25, QINF = 610.5,

RNPU = 4.8E+06, CNWP = 0.4296

11 = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x./c CP x./c CP x/c CP

0.020 -0.835 0.000 0.754 0.000 0.330** 0.010 -1.086

0.060 -0.863 0.020 -0.930 0.020 -0.969 0.020 - 1.197

0.1 l0 -0.868 0.040 -0.840 0.060 -0.481 0.060 - 1.143

0.200 -0.768 0.060 -0.959 0.090 - 1.056 0.1 l0 - 1.125

0.230 -0.692 0.090 -0.963 0.110 - 1.050 0.140 - 1.141

0.400 -0.723 0.130 -0.888 0.130 -1.048 0.190 -1.961"*

0.490 -0.581 0.150 -0.966 0.150 -0.966 0.250 - 1.169

0.590 -0.175 0.200 -0.905 0.210 - 1.005 0.400 -0.873

0.630 -0.214 0.250 -0.956 0.250 -0.980 0.490 -0,757

0.700 -0.214 0.260 -0.948 0.340 - 1,071 0.580 -0,668

0,750 -0.254 0.280 -0.976 0.370 - 1,070 0.650 -0.697

0.810 -0.231 0.290 -0,992 0.400 - 1.045 0.700 -0,664

0.840 -0.257 0.310 -0,879 0.410 - 1.062"* 0.750 -0.408

0.900 -0.190 0.320 -0.959 0.430 - 1.069 0.800 -0.213

0.960 -0,069 0.340 -0.915 0,440 - 1.051 0,830 -0.138

0,350 -0,453** 0.460 -0.783 0,900 -0.047

0.370 -0,952 0.490 - 1.015 0.960 -0.008

0.380 - 1.012 0.500 - 1.050

0.400 -0.942 0.520 - 1,055

0.410 -0.892 0.540 - 1.057

0.430 -0.964 0.550 - 1.032

0.440 -0.842 0.580 - 1.029

0.460 - 1.001 0.600 - 1.046

0.470 -0,992 0.610 - 1.009

0.490 -0.973 0.650 -0.509

0.500 -0.978 0.700 -0.349

0.520 -0.968 0.750 -0.302

0.530 -0.929 0.820 -0.119

0.550 -0.987 0.890 -0.019

0.560 -0.991 0.900 0.009

0.580 -0,938 0.960 0.082

0.590 -0.630

0.600 -0.450

0,640 -0,238

0.700 -0.178

0.750 -0.034

0.820 -0.155

0.870 -0.140

0.930 -0.033

0.960 0.026

Lower Surface

0.020 0.083 0.020 0.266 0.020 0.313 0.020 0.670

0.110 -0.129 0,060 0.179 0.060 0.256 0.060 -0.027

0.230 -0.094 0,090 0.109 0.090 0,179 0.110 0.233

0.400 -0.083 0.120 0.022 0.120 0.054 0.250 -0,090

0.490 -0.084 0.200 -0,003 0,200 0.026 0_400 -0.136

0.630 0.878** 0.260 -0.093 0.250 -0,072 0,490 -0.182

0.750 0.008 0.400 -0.106 0.400 -0.126 0.580 -0.264

0,850 0.038 0.490 -0.124 0.490 -0.055 0.650 -0.114

0.900 0.137 0.580 -0.130 0.580 -0.187 0.750 0.147

0,960 0.124 0.640 0.047 0.650 -0.032 0.830 0.293

0.750 0.176 0.750 -0.030 0.900 0.333

0.870 0.239 0.890 0.327 0.960 0.254

0.930 0.229 0.930 0.269

0.960 0.187 0.960 0.305

CN = 0.428 0.637 0.670 0.724

733
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 15-2-57-000, MINF = 0.849, Camber = 0/2, ALPT = 9.11, BETA = 0.17, QINF = 619.4,

RNPU = 4.9E+06, CNWP = 0.4840

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.977 0.000 0.682 0.000 0.256** 0.010 - 1.220

0.060 -0.989 0.020 - 1.075 0.020 - 1.101 0.020 - 1.292

0.110 -0.974 0.040 -0.932 0.060 -0.586 0.060 - 1.300

0.200 -0.883 0.060 - 1.058 0.090 - 1.173 0.110 - 1.239

0.230 -0.800 0.090 -1.063 0.110 -1.141 0.140 -1.247

0.400 -0.831 0.130 -0.924 0.130 - 1.155 0.190 - 1.982" *

0.490 -0.648 0. ! 50 - 1.04 1 0.150 - 1.076 0.250 - 1.243

0.590 -0.152 0.200 - 1.002 0.210 - I. 100 0.400 -0.933

0.630 -0.215 0.250 - 1.062 0.250 - 1.015 0.490 -0.823

0.700 -0.219 0.260 - 1.044 0.340 -1.160 0.580 -0.731

0.750 -0.273 0.280 - 1.077 0.370 - 1.161 0.650 -0.656

0.810 -0.254 0.290 - 1.086 0.400 - 1.t 25 0.700 -0.597

0.840 -0.281 0.310 -0.915 0.410 - 1.095"* 0.750 -0.359

0.900 -0.219 0.320 - 1.062 0.430 - 1.187 0.800 -0.214

0.960 -0.094 0.340 -0.951 0.440 - 1.161 0.830 -0.160

0.350 -0.460** 0.460 -0.820 0.900 -0.096

0.370 -0.987 0.490 - 1.112 0.960 -0.035

0.380 -1.114 0.500 -1.137

0.400 - 1.042 0.520 - 1.147

0.410 -0.928 0.540 -1.013

0.430 -1.017 0.550 -0.687

0.440 -0.766 0.580 -0.563

0.460 -0.929 0.600 -0.566

0.470 -0.853 0.610 -0.529

0.490 -0.616 0.650 -0.586

0.500 -0.557 0.700 -0.447

0.520 -0.537 0.750 -0.434

0.530 -0.488 0.820 -0.311

0.550 -0.488 0.890 -0.135

0.560 -0.476 0.900 -0.145

0.580 -0.463 0.960 -0.065

0.590 -0.476

0.600 -0.442

0.640 -0.381

0.700 -0.365

0.750 -0.020

0.820 -0.196

0.870 -0.169

0.930 -0.113

0.960 -0.097

Lower Surface

0.020 0.210 0.020 0.393 0.020 0.419 0,020 0.742

0.110 -0.076 0.060 0.261 0.060 0.319 0.060 -0.075

0.230 -0.064 0.090 0.180 0.090 0.238 0.110 0.305

0.400 -0.073 0.120 0.083 0.120 0.115 0.250 -0.031

0.490 -0.089 0.200 0.053 0.200 0.087 0.400 -0.086

0.630 0.817** 0.260 -0.040 0.250 -0.030 0.490 -0.138

0.750 -0.002 0.400 -0.078 0.400 -0.084 0.580 -0.225

0.850 0.032 0.490 -0.107 0.490 -0.042 0.650 -0.096

0.900 0.127 0.580 -0.040 0.580 -0.172 0.750 0.160

0.960 0.112 0.640 0.035 0.650 -0.024 0.830 0.282

0.750 0.156 0.750 -0.017 0.900 0.330

0.870 0.205 0.890 0.309 0.960 0.244

0.930 0.171 0.930 0.234

0.960 0.1 t 3 0.960 0.237

CN = 0.496 0.668 0.746 0.797

734
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-57-18-000, MINF = 0.854, Camber = 10/2, ALPT = 4.00, BETA = 0.40, QINF = 600.1,

RNPU = 4.7E+06, CNWP = 0.1731

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.590 0.000 0.074 0.000 0.154"* 0.010 0.441

0.060 0.131 0.020 0,592 0.020 0.615 0.020 0.285

0.110 -0.234 0.040 0,409 0,060 0.298 0.060 -0.215

0.200 -0.914 0.060 0.040 0.090 -0.211 0.110 -0.568

0.230 -0.8 h5 0.090 -0.177 0.110 -0.426 0.140 -0.998

0.400 -0.159 0.130 -0.444 0.130 -0.709 0.190 - 1.959 * *

0.490 -0.176 0.150 -0.722 0.150 -0.865 0.250 -0.736

0,590 -0.238 0.200 -0.819 0.210 -0.866 0.400 -0.312

0.630 -0.248 0.250 -0.819 0.250 -0.834 0.490 -0.303

0.700 -0.235 0.260 -0.802 0.340 -0.410 0.580 -0.299

0.750 -0.252 0.280 -0.792 0.370 -0.282 0.650 -0.403

0.810 -0.227 0.290 -0.776 0.400 -0.246 0.700 -0.362

0.840 -0.241 0.310 -0.736 0.410 - 1.044 ** 0.750 -0.403

0.900 -0.121 0.320 -0.743 0.430 -0.253 0.800 -0.529

0.960 -0.013 0.340 -0.486 0.440 -0.251 0.830 -0.517

0.350 -0.263** 0.460 -0.265 0.900 -0.181

0.370 -0.223 0.490 -0.246 0.960 -0.002

0.380 -0.212 0.500 -0.270

0.400 -0.189 0.520 -0.261

0.410 -0.204 0.540 -0.260

0.430 -0.203 0.550 -0.256

0.440 -0.189 0.580 -0.267

0.460 -0.215 0.600 -0.314

0.470 -0.237 0.610 -0.307

0.490 -0.232 0.650 -0.645

0.500 -0.243 0.700 -0.528

0.520 -0.238 0.750 -0.462

0.530 -0,249 0.820 -0.330

0.550 -0.281 0.890 -0.118

0.560 -0.274 0.900 -0.081

0.580 -0.255 0,960 0.033

0.590 -0.299

0.600 -0.294

0.640 -0.535

0.700 -0.344

0.750 -0.080

0.820 -0.289

O.870 -0.239

0.930 -0.087

0.960 -0.020

Lower Surface

0.020 - 1.086 0,020 -0.873 0.020 - 1.565 0.020 -0.892

0.110 -0.498 0,060 -0.764 0.060 -0.928 0.060 0.054

0.230 -0.248 0.090 -0.655 0.090 -0.451 0.110 -0.393

0.400 -0.124 0.120 -0.552 0,120 -0.282 0.250 -0.285

0.490 -0.061 0.200 -0.222 0.200 -0.193 0.400 -0.332

0.630 1.010"* 0.260 -0.341 0.250 -0.217 0.490 -0.384

0.750 0.023 0.400 -0.170 0.400 -0.274 0.580 -0.417

0.850 0.058 0.490 -0.140 0.490 -0.116 0.650 -0.188

0.900 0.096 0.580 -0.108 0.580 -0.236 0.750 0.095

0.960 0.108 0.640 0.028 0.650 -0.076 0.830 0,236

0.750 0.100 0.750 -0.054 0.900 0.298

0.870 0.178 0.890 0.264 0.960 0.259

0.930 0.194 0.930 0.224

0.960 0.161 0,960 0.316

CN = 0.154 0.172 0.203 0.258

735
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-57-43-000, MINF = 0.851, Camber = t0/2, ALPT = 4.02, BETA = 0.45, QINF = 596.3,

RNPU = 4.7E+06, CNWP = 0.1775

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.585 0.000 0.074 0.000 0.162"* 0.010 0.436

0.060 0.116 0.020 0.590 0.020 0.607 0.020 0.283

0,1 I 0 -0.238 0.040 0.407 0.060 0.279 0.060 -0.223

0.200 -0.924 0.060 0.043 0.090 -0.223 0.110 -0.572

0.230 -0.822 0.090 -0.183 0.110 -0.437 0.140 - 1.001

0.400 -0.179 0.130 -0.454 0.130 -0.720 0.190 - 1.972**

0.490 -0.188 0.150 -0.734 0.150 -0.872 0.250 -0.741

0.590 -0.238 0.200 -0.827 0.210 -0.877 0.400 -0.318

0.630 -0.247 0.250 -0.834 0.250 -0.844 0.490 -0.297

0.700 -0.234 0.260 -0.811 0.340 -0.342 0.580 -0.301

0.750 -0,249 0.280 -0.802 0.370 -0.265 0.650 -0.397

0.810 -0,221 0.290 -0.788 0.400 -0.245 0.700 -0.361

0.840 -0.236 0.310 -0.741 0.410 - 1.051 ** 0.750 -0.406

0.900 -0.122 0.320 -0.742 0.430 -0.266 0.800 -0.519

0.960 -0.010 0.340 -0.329 0.440 -0.263 0.830 -0.496

0.350 -0.235"* 0.460 -0.272 0.900 -0.187

0.370 -0.214 0.490 -0.260 0.960 -0.005

0.380 -0.217 0.500 -0.282

0.400 -0.198 0.520 -0.268

0.410 -0.217 0.540 -0.269

0.430 -0.216 0.550 -0.267

0.440 -0.205 0.580 -0.257

0.460 -0.222 0.600 -0.322

0.470 -0.252 0.610 -0.316

0.490 -0.247 0.650 -0.658

0.500 -0.249 0.700 -0.535

0.520 -0.255 0.750 -0.464

0.530 -0.262 0.820 -0.331

0.550 -0.293 0.890 -0.127

0.560 -0.276 0.900 -0.084

0.580 -0.260 0.960 0.028

0.590 -0.307

0.600 -0,305

0.640 -0.537

0.700 -0.312

0.750 -0.078

0.820 -0.286

0.870 -0.237

0.930 -0.086

0.960 -0.020

Lower Surface

0.020 - 1.103 0.020 -0.845 0.020 - 1.575 0.020 -0.898

0.110 -0.489 0.060 -0.737 0.060 -0.827 0.060 0.054

0.230 -0.252 0.090 -0.639 0.090 -0.451 0.110 -0.401

0.400 -0.112 0.120 -0.534 0.120 -0.349 0.250 -0.288

0.490 -0.070 0.200 -0.229 0.200 -0.197 0.400 -0.327

0.630 1.016'* 0.260 -0.340 0.250 -0.204 0.490 -0.380

0.750 0.021 0.400 -0.165 0.400 -0.271 0.580 -0.397

0.850 0.054 0.490 -0.128 0.490 -0.117 0.650 -0.182

0.900 0.1 04 0.580 -0.102 0.580 -0.223 0.750 0.094

0.960 0.112 0.640 0.026 0.650 -0.080 0.830 0.240

0.750 0.102 0.750 -0.053 0.900 0.296

0.870 0.185 0.890 0.261 0.960 0.255

0.930 0.190 0.930 0.217

0.960 0.156 0.960 0.313

CN = 0.163 0.175 0.210 0.261

736
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-57-56-000, MINF = 0.851, Camber = 10/2, ALPT = 4.05, BETA = 0.45, QINF = 596.3,

RNPU = 4.7E+06, CNWP = 0.1789

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 0.585 0.000 0.087 0.000 0.190** 0.010 0.422

0.060 0.116 0.020 0.590 0.020 0.610 0.020 0.278

O. 110 -0.238 0.040 0.400 0.060 0.280 0.060 -0.223

0.200 -0.920 0.060 0.025 0.090 -0.230 0.110 -0.585

0.230 -0.835 0.090 -0.191 0.110 -0.441 0.140 - 1.001

0.400 -0.168 0.130 -0.457 0.130 -0.727 0.190 - 1.972"*

0.490 -0.188 0.150 -0.743 0.150 -0.875 0.250 -0.748

0.590 -0.242 0.200 -0.831 0.210 -0.885 0.400 -0.318

0.630 -0.249 0.250 -0.834 0.250 -0.854 0.490 -0.300

0.700 -0.240 0.260 -0.821 0.340 -0.425 0.580 -0.298

0.750 -0.248 0.280 -0.809 0.370 -0.288 0.650 -0.397

0.810 -0.218 0.290 -0.795 0.400 -0.244 0.700 -0.369

0.840 -0.232 0.310 -0.751 0.410 - 1.051 ** 0.750 -0.410

0.900 -0.123 0.320 -0.757 0.430 -0.255 0.800 -0.515

0.960 -0.010 0.340 -0.480 0.440 -0.256 0.830 -0.491

0.350 -0.254** 0.460 -0.267 0.900 -0.186

0.370 -0.223 0.490 -0.256 0.960 -0.008

0.380 -0.213 0.500 -0.276

0.400 -0.191 0.520 -0.259

0.410 -0.205 0.540 -0.266

0.430 -0.205 0.550 -0.258

0.440 -0.199 0.580 -0.269

0.460 -0.211 0.600 -0.320

0.470 -0.246 0.610 -0.313

0.490 -0.239 0.650 -0.670

0.500 -0.242 0.700 -0.535

0.520 -0.247 0.750 -0.462

0.530 -0.255 0.820 -0.329

0.550 -0.280 0.890 -0.125

0.560 -0.283 0.900 -0.081

0.580 -0.264 0.960 0.029

0.590 -0.301

0.600 -0.300

0.640 -0.536

0.700 -0.306

0.750 -0.078

0.820 -0.290

0.870 -0.239

0.930 -0.088

0.960 -0.015

Lower Surface

0.020 -0.888 0.020 -0.708 0.020 - 1.563 0020 -0.898

0.110 -0.706 0.060 -0.633 0.060 -0.830 0.060 0.054

0.230 -0.233 0.090 -0.593 0.090 -0.565 0.110 -0.396

0.400 -0.051 0.120 -0.516 0.120 -0.404 0. 250 -0.288

0.490 -0.029 0.200 -0.223 0.200 -0.201 0.400 -0.33 I

0.630 1.016"* 0.260 -0.380 0.250 -0.204 0.490 -0.359

0.750 0.033 0.400 -0.197 0.400 -0.268 0.580 -0.399

0.850 0.053 0.490 -0.143 0.490 -0.117 0.650 -0.186

0.900 0.116 0.580 -0.094 0.580 -0.234 0.750 0.095

0.960 0.119 0.640 0.005 0.650 -0.080 0.830 0.240

0.750 0.096 0.750 -0.056 0.900 0.289

0.870 0.139 0.890 0.269 0.960 0.251

0.930 0.164 0.930 0.221

0.960 0.143 0.960 0.316

CN = 0.152 0.172 0.210 0.264

737
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = t4-58-10-000, MINF = 0.854, Camber = 10/2, ALPT = 5.18, BETA = 0.34, QINF = 599.8,

RNPU = 4.7E+06, CNWP = 0.2939

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.543 0.000 0.201 0.000 0.281 ** 0.010 0.310

0.060 0.068 0.020 0.531 0.020 0.548 0.020 0.172

0.110 -0.281 0.040 0.343 0.060 0.271 0,060 -0.378

0.200 -0.951 0.060 -0.021 0.090 -0.283 0.110 -0.616

0.230 -0.899 0.090 -0.241 0.110 -0.497 0.140 - 1.057

0.400 -0. ! 21 0.130 -0.502 0.130 -0.778 0.190 - 1.959**

0.490 -0.120 0.150 -0.783 0.150 -0.916 0.250 -0.8 ! 1

0.590 -0.193 0.200 -0.875 0.210 -0.940 0.400 -0.651

0.630 -0.222 0.250 -0.904 0.250 -0.929 0.490 -0.412

0.700 -0.221 0.260 -0.892 0.340 -0.910 0.580 -0.378

0,750 -0.248 0.280 -0.900 0.370 -0.909 0.650 -0.424

0.810 -0.221 0.290 -0.878 0.400 -0.880 0.700 -0.399

0.840 -0.233 0.310 -0.835 0.410 - 1.044"* 0.750 -0.457

0.900 -0.128 0.320 -0.849 0.430 -0.883 0.800 -0.347

0.960 -0.014 0.340 -0.848 0.440 -0.866 0.830 -0,283

0.350 -0.460"* 0.460 -0.763 0.900 -0.167

0.370 -0.842 0.490 -0.355 0.960 0.012

0.380 -0.881 0.500 -0.307

0.400 -0.821 0.520 -0.261

0.410 -0.840 0.540 -0.246

0.430 -0.797 0.550 -0.231

0.440 -0.779 0.580 -0.237

0.460 -0.823 0.600 -0.289

0.470 -0.664 0.610 -0.259

0.490 -0.350 0.650 -0.534

0.500 -0.233 0.700 -0.377

0.520 -0.195 0.750 -0.296

0.530 -0.143 0.820 -0.318

0.550 -0.146 0.890 -0.114

0.560 -0.140 0.900 -0.074

0.580 -0.130 0.960 0.039

0.590 -0.166

0.600 -0.163

0.640 -0.270

0.700 -0.261

0.750 -0.062

0.820 -0.274

0.870 -0.233

0.930 -0.079

0.960 -0.012

Lower Surface

0.020 -0.863 0.020 -0.652 0.020 -0.771 0.020 -0.788

0.110 -0.575 0.060 -0.542 0.060 -0.579 0.060 -0.047

0.230 -0.115 0.090 -0.485 0.090 -0.415 0.110 -0.232

0.400 -0.035 0.120 -0.386 0.120 -0.290 0.250 -0.209

0.490 -0.029 0.200 -0.108 0.200 -0.104 0.400 -0.259

0.630 1.011 ** 0.260 -0.207 0.250 -0.136 0.490 -0.309

0.750 0.039 0.400 -0,124 0.400 -0.210 0.580 -0.358

0.850 0.063 0.490 -0. l 14 0.490 -0.093 0.650 -0.161

0.900 0.133 0.580 -0.098 0.580 -0.214 0.750 0.119

0.960 0.119 0.640 0.042 0.650 -0.064 0.830 0.261

0.750 0.125 0.750 -0.051 0.900 0.314

0.870 0.189 0.890 0.297 0.960 0.266

0.930 0.188 0.930 0.243

0.960 0.158 0.960 0.332

CN = 0.186 0.309 0.351 0.377

738
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-58-14-500, MINF = 0.853, Camber = 10/2, ALPT = 6.02, BETA = 0.19, QINF = 598.6,

RNPU = 4.7E+06, CNWP = 0.3008

rI = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.509 0.000 0.277 0.000 0.322** 0.010 0.225

0.060 0.027 0.020 0.471 0.020 0.483 0.020 0.087

O. 1 t 0 -0.308 0.040 0.295 0.060 0.253 0.060 -0.459

0.200 -0.987 0.060 -0.067 0.090 -0.333 O. I 10 -0.760

0.230 -0.942 0.090 -0.284 0.110 -0.546 0.140 - 1.107

0.400 -0.688 0.130 -0.547 0.130 -0.820 0.190 - 1.965"*

0.490 -0.111 0.150 -0.816 0.150 -0.959 0.250 - 1.090

0.590 -0.160 0.200 -0.918 0.210 -0.984 0.400 -0.785

0.630 -0.192 0.250 -0.955 0.250 -0.972 0.490 -0.503

0.700 -0.197 0.260 -0.942 0.340 -0.975 0.580 -0.463

0.750 -0.228 0.280 -0.962 0.370 -0.980 0.650 -0.526

0.810 -0.211 0.290 -0.945 0.400 -0.947 0.700 -0.500

0.840 -0.225 0.310 -0.865 0.410 -1.048"* 0.750 -0.547

0.900 -0.133 0.320 -0.909 0.430 -0.978 0.800 -0.259

0.960 -0.025 0.340 -0.911 0.440 -0.955 0.830 -0.243

0.350 -0.468"* 0.460 -0.767 0.900 -0.129

0.370 -0.901 0.490 -0.921 0.960 0.031

0.380 -0.944 0.500 -0.961

0.400 -0.878 0.520 -0.945

0.410 -0.871 0.540 -0.933

0.430 -0.884 0.550 -0.588

0.440 -0.824 0.580 -0.399

0.460 -0.900 0.600 -0.351

0.470 -0.900 0.610 -0.292

0.490 -0.881 0.650 -0.360

0.500 -0.880 0.700 -0.258

0.520 -0.862 0.750 -0.232

0.530 -0.857 0.820 -0.246

0.550 -0.622 0.890 -0.093

0.560 -0.361 0.900 -0.057

0.580 -0.253 0.960 0.052

0.590 -0.222

0.600 -0.169

0.640 -0.147

0.700 -0.161

0.750 -0.048

0.820 -0.226

0.870 -0.201

0.930 -0.052

0.960 0.004

Lower Surface

0.020 -0.787 0.020 -0.622 0.020 -0.682 0.020 -0.511

0.110 -0.435 0.060 -0.480 0.060 -0.395 0.060 -0.049

0.230 -0.075 0.090 -0.376 0.090 -0.178 0.110 -0.116

0.400 -0.032 0.120 -0.248 0.120 -0.106 0.250 -0.153

0.490 -0.041 0.200 -0.076 0.200 -0.086 0.400 -0.208

0.630 1.011 ** 0.260 -0.090 0.250 -0.102 0.490 -0.256

0.750 0.032 0.400 -0.096 0.400 -0.176 0.580 -0.324

0.850 0.060 0.490 -0.1 04 0.490 -0.081 0.650 -0.145

0.900 0.130 0.580 -0.113 0.580 -0.205 0.750 0.129

0.960 0.126 0.640 0.053 0.650 -0.056 0.830 0.268

0.750 0.163 0.750 -0.04 1 0.900 0.326

0.870 0.218 0.890 0.303 0.960 0.266

0.930 0.201 0.930 0.256

0.960 0.166 0.960 0.328

CN = 0.295 0.408 0.444 0.506

739
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-58-21-5000 M1NF = 0.856, Camber = 10/2, ALPT = 7.15, BETA = 0.22, QINF = 603.1,

RNPU = 4.7E+06, CNWP = 0.4154

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.464 0.000 0.381 0.000 0.382** 0.010 0.127

0.060 -0.022 0.020 0.426 0.020 0.410 0.020 -0.004

0.110 -0.342 0.040 0.237 0.060 0.138 0.060 -0.562

0.200 - 1.040 0.060 -0.132 0.090 -0.395 0.110 -0.874

0.230 -0.981 0.090 -0.327 0.110 -0.592 0.140 - 1.177

0.400 -0.792 0.130 -0.588 0.130 -0.865 0.190 - 1.951 **

0.490 -0.622 0.150 -0.844 0.150 -0.987 0.250 - 1.130

0.590 -0.154 0.200 -0.946 0.210 - 1.025 0.400 -0.810

0.630 -0.173 0.250 - 1.001 0.250 -0.965 0.490 -0.664

0.700 -0.167 0.260 -0.981 0.340 - 1.036 0.580 -0.557

0.750 -0.214 0.280 - 1.009 0.370 - 1.033 0.650 -0.599

0.810 -0.192 0.290 -0.996 0.400 - 1.003 0.700 -0.575

0.840 -0.217 0.310 -0.859 0.410 - 1.04 1 ** 0,750 -0.61 I

0.900 -0.151 0.320 -0.972 0.430 - 1.046 0.800 -0.275

0.960 -0.039 0.340 -0.917 0.440 - 1.029 0.830 -0.197

0.350 -0.475** 0.460 -0.762 0.900 -0.047

0.370 -0.955 0.490 -0.994 0.960 0.024

0.380 - 1.003 0.500 - 1.028

0.400 -0.947 0.520 - 1.027

0.410 -0.865 0.540 -1.024

0.430 -0.948 0.550 -0.998

0.440 -0.818 0.580 -0.990

0.460 -0.985 0.600 -0.994

0.470 -0.964 0,610 -0.969

0.490 -0.951 0.650 -0.530

0.500 -0.954 0.700 -0.368

0.520 -0.938 0.750 -0.286

0.530 -0.924 0.820 -0.154

0.550 -0.946 0.890 -0.034

0.560 -0.959 0.900 -0.007

0.580 -0.934 0.960 0.077

0.590 -0.985

0.600 -0.957

0.640 -0.283

0.700 -0.211

0.750 -0.039

0.820 -0.122

0.870 -0.122

0.930 -0.021

0.960 0.029

Lower Surface

0.020 -0.938 0.020 -0.532 0.020 -0.600 0.020 -0.250

0.110 -0.250 0.060 -0.322 0.060 -0.096 0.060 -0.038

0.230 -0.050 0.090 -0.193 0.090 -0.005 0.110 -0.021

0.400 -0.044 0.120 -0.073 0.120 -0.036 0.250 -0.092

0.490 -0.060 0.200 -0.053 0.200 -0.058 0.400 -0.1 64

0.630 1.003"* 0.260 -0.017 0.250 -0.059 0.490 -0.218

0.750 0.022 0.400 -0.081 0.400 -0.138 0.580 -0.300

0.850 0.051 0.490 -0.098 0.490 -0.067 0.650 -0.134

0.900 0.132 0.580 -0.113 0.580 -0.190 0.750 0.139

0.960 0.126 0.640 0.057 0.650 -0.045 0.830 0.288

0.750 0.171 0.750 -0.04 1 0.900 0.333

0.870 0.232 0.890 0.322 0.960 0.270

0.930 0.220 0.930 0.266

0.960 0.186 0.960 0.338

CN = 0.385 0.515 0.567 0.591

740
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-58-29-500, MINF = 0.849, Camber = 10/L ALPT = 8.06, BETA = 0.11, QINF = 597.3,

RNPU = 4.7E+06, CNWP = 0.4509

r I = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.403 0.000 0.481 0.000 0.407"* 0.010 0.012

0.060 -0.087 0.020 0.340 0.020 0.289 0.020 -0.098

0.110 -0,384 0.040 0.164 0.060 0.063 0.060 -0.661

0.200 - 1.068 0.060 -0.197 0,090 -0.452 0.110 -0,977

0.230 - 1.025 0.090 -0.406 0.110 -0.653 0.140 - 1.259

0.400 -0.859 0.130 -0.655 0. | 30 -0.936 0.190 - 1.984* *

0.490 -0.733 0.150 -0.916 0.150 - 1.045 0.250 - 1.270

0.590 -0.160 0.200 - 1.004 0.210 - 1.088 0.400 -0.879

0.630 -0.179 0.250 - 1.067 0.250 -0.988 0.490 -0.723

0.700 -0.173 0,260 - 1,053 0.340 - 1.122 0.580 -0.635

0.750 -0.211 0.280 - 1.075 0.370 - 1.111 0.650 -0.679

0.810 -0.208 0.290 - 1.083 0.400 - 1.077 0.700 -0.660

0.840 -0.230 0.310 -0.881 0.410 -1.065"* 0.750 -0.542

0.900 -0.176 0.320 - 1.045 0.430 - 1,128 0.800 -0.229

0.960 -0.056 0.340 -0.940 0.440 - 1.112 0.830 -0.167

0,350 -0.484** 0.460 -0.783 0.900 -0.060

0.370 -0.988 0.490 - 1.077 0.960 -0.002

0.380 -1.084 0.500 -1.110

0.400 - 1.022 0.520 - 1.099

0.410 -0.888 0.540 - 1.108

0.430 - 1.022 0.550 - 1.083

0.440 -0.840 0.580 - 1.082

0.460 - 1.057 0.600 - 1.098

0,470 - 1.047 0.610 - 1,059

0.490 - 1,033 0.650 -0,577

0.500 - 1.039 0.700 -0.433

0.520 - 1.019 0.750 -0.386

0.530 -0.953 0.820 -0.144

0,550 - 1.035 0.890 -0.025

0.560 - 1.029 0.900 0.001

0,580 - 1.012 0.960 0.080

0.590 - 1.056

0.600 - 1.027

0.640 -0.344

0.700 -0.293

0.750 -0.039

0,820 -0.106

0.870 -0.089

0.930 -0.009

0.960 0.029

Lower Surface

0.020 -0.798 0,020 -0.411 0.020 -0,342 0.020 -0.052

0. l 10 -0.062 0.060 -0.085 0.060 0.102 0.060 -0.035

0.230 -0.016 0,090 -0.014 0.090 0.074 0.1 I 0 0.067

0.400 -0.053 0.120 0.065 0.120 0.032 0.250 -0.039

0.490 -0.072 0.200 -0.029 0.200 -0.021 0,400 -0.111

0.630 0.999 ** 0.260 0.018 0.250 -0.012 0.490 -0.176

0.750 0.011 0.400 -0.057 0.400 -0.091 0.580 -0.253

0.850 0.045 0.490 -0,085 0.490 -0.057 0.650 -0.113

0.900 0.129 0.580 -0,109 0.580 -0.174 0.750 0.150

0.960 0.121 0.640 0.060 0.650 -0.031 0.830 0.281

0.750 O.181 0.750 -0.031 0.900 0.332

0.870 0.226 0.890 0.314 0.960 0.261

0.930 0.218 0.930 0.266

0.960 O. 179 0.960 0.342

CN = 0.445 0.595 0.652 0.684

741
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-58-32-000, MINF = 0.847, Camber = 10/2, ALPT = 7.97, BETA = 0.34, QINF = 596.2,

RNPU = 4.7E+06, CNWP = 0.4603

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.385 0.000 0.460 0.000 0.385** 0.010 0.011

0.060 -0.084 0.020 0.330 0.020 0.299 0.020 -0.085

0.110 -0.39 l 0.040 0.161 0.060 0.047 0.060 -0.671

0.200 - 1.068 0.060 -0.214 0.090 -0.474 0.110 -0.970

0.230 - 1.028 0.090 -0.408 0.110 -0.664 0.140 - 1.262

0.400 -0.853 0.130 -0.657 0.130 -0.938 0.190 - 1.992 **

0.490 -0.744 0.150 -0.919 0.150 - 1.053 0.250 - 1.273

0.590 -0.182 0.200 - 1.002 0.210 - 1.108 0.400 -0.88 l

0.630 -0.185 0.250 - 1.076 0.250 -0.995 0.490 -0.735

0.700 -0.178 0.260 - 1.056 0.340 - 1.126 0.580 -0.653

0.750 -0.221 0.280 - 1.089 0.370 - 1.119 0.650 -0.670

0.810 -0.206 0.290 - 1.101 0.400 - 1.091 0.700 -0.657

0.840 -0.246 0.310 -0.887 0.410 - 1.071 ** 0.750 -0.489

0.900 -0.176 0.320 - 1.051 0.430 - 1.136 0.800 -0.227

0.960 -0.073 0.340 -0.946 0.440 - 1.121 0.830 -0.182

0.350 -0.497"* 0.460 -0.789 0.900 -0.066

0.370 -0.994 0.490 - 1.083 0.960 -0.001

0.380 - 1.090 0.500 - 1.109

0.400 - 1.036 0.520 - 1.115

0.410 -0.894 0.540 -1.111

0.430 - 1.027 0.550 - 1.103

0.440 -0.846 0.580 - 1.103

0.460 - 1.066 0.600 - 1.101

0.470 - 1.040 0.610 - 1.069

0.490 - 1.045 0.650 -0.548

0.500 - 1.045 0.700 -0.418

0.520 - 1.014 0.750 -0.369

0,530 -0.960 0.820 -0.142

0.550 - 1.044 0.890 -0.027

0.560 - 1.044 0.900 -0.005

0.580 - 1.019 0.960 0.077

0.590 -1.078

0.600 -0.940

0.640 -0.333

0.700 -0.284

0.750 -0,028

0.820 -0.129

0.870 -0.101

0.930 -0.016

0.960 0.028

Lower Surface

0.020 -0.808 0.020 -0.406 0.020 -0.359 0.020 -0.077

0.110 -0.063 0.060 -0.114 0.060 0.095 0.060 -0.026

0.230 -0.017 0.090 -0.024 0.090 0.069 0.110 0.066

0.400 -0.054 0.120 0.068 0.120 0.016 0.250 -0.040

0.490 -0.066 0.200 -0.022 0.200 -0.026 0.400 -0.116

0.630 0.996"* 0.260 0.017 0.250 -0.010 0.490 -0.177

0.750 0.006 0.400 -0.056 0.400 -0.097 0.580 -0.255

0.850 0.042 0.490 -0.088 0.490 -0.058 0.650 -0.107

0.900 0.131 0.580 -0.120 0.580 -0.186 0.750 0.149

0.960 0.113 0.640 0.059 0.650 -0.032 0.830 0.270

0.750 0.179 0.750 -0.041 0.900 0.314

0.870 0.211 0.890 0.327 0.960 0.257

0.930 0.214 0.930 0.269

0.960 0.177 0.960 0.337

CN = 0.450 0.591 0.653 0.682

742
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-58-46-000, MINF = 0.841, Camber = 10/2, ALPT = 9.15, BETA = 0.72, QINF = 580.5,

RNPU = 4.6E+06, CNWP = 0.4966

_q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x./c CP x,/c CP x/c CP

0.020 0.324 0.000 0.606 0.000 0.402** 0.010 -0.138

0.060 -0.152 0.020 0.209 0.020 0.172 0.020 -0.203

0.110 -0.462 0.040 0.063 0.060 -0.027 0.060 -0.776

0.200 - 1.106 0.060 -0.331 0.090 -0.645 0.110 - 1.070

0.230 - 1.077 0.090 -0.500 0.110 -0.788 0.140 - 1.351

0.400 -0.939 0.130 -0.732 0.130 - 1.022 0.190 -2.018 * *

0.490 -0.566 0.150 -0.983 0.150 - 1.112 0.250 - 1.378

0.590 -0.181 0.200 - 1.069 0.210 - l. 159 0.400 -0.976

0.630 -0.216 0.250 - 1.140 0.250 -0.993 0.490 -0.815

0.700 -0.212 0.260 - 1.126 0.340 - 1.212 0.580 -0.734

0.750 -0.262 0.280 - 1.160 0.370 - 1.208 0.650 -0.636

0.810 -0.243 0.290 - 1.163 0.400 - 1.1 64 0.700 -0.575

0.840 -0.267 0.310 -0.883 0.410 -1.072** 0.750 -0.324

0.900 -0.203 0.320 - 1.124 0.430 - 1.210 0.800 -0.201

0.960 -0.087 0.340 -0.944 0.440 -I.199 0.830 -0.174

0.350 -0.497** 0.460 -0.782 0.900 -0.083

0.370 -0.993 0.490 - 1.173 0.960 -0.007

0.380 -1.176 0.500 -1.195

0.400 -1.100 0.520 -1.192

0.410 -0.865 0.540 - 1.180

0.430 - 1.002 0.550 -0.835

0.440 -0.819 0.580 -0.636

0.460 -0.943 0.600 -0.648

0.470 -0.867 0.610 -0.566

0.490 -0.619 0.650 -0.626

0.500 -0.614 0.700 -0.503

0.520 -0.539 0.750 -0.490

0.530 -0.539 0.820 -0.346

0.550 -0.515 0.890 -0.166

0.560 -0.499 0.900 -0.190

0.580 -0.488 0.960 -0.085

0.590 -0.504

0.600 -0.468

0.640 -0.398

0.700 -0.393

0.750 -0.025

0.820 -0.242

0.870 -0.213

0.930 -0.163

0.960 -0.142

Lower Surface

0.020 -0.708 0.020 -0.266 0.020 -0.143 0.020 0.213

0.110 -0.034 0.060 0.111 0.060 0.183 0.060 -0.005

0.230 0.029 0.090 0.080 0.090 0.151 0.110 0.159

0.400 -0.040 0.120 0.125 0.120 0.102 0.250 0.017

0.490 -0.062 0.200 0.023 0.200 0.015 0.400 -0.064

0.630 1.051 ** 0.260 0.060 0.250 0.045 0.490 -0.130

0.750 -0.012 0.400 -0.030 0.400 -0.052 0.580 -0.208

0.850 0.024 0.490 -0.077 0.490 -0.039 0.650 -0.089

0.900 0.118 0.580 -0.120 0.580 -0.153 0.750 0.164

0.960 0.108 0.640 0.035 0.650 -0.023 0.830 0.291

0.750 0.147 0.750 -0.016 0.900 0.333

0.870 0.200 0.890 0.307 0.960 0.254

0.930 0.154 0.930 0.236

0.960 0.091 0.960 0.296

CN = 0.482 0.599 0.731 0.764

743
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-58-50-500, MINF = 0.840, Camber = 10/2, ALPT = 10.26, BETA = 0.48, Q1NF = 582.8,

RNPU = 4.6E+06, CNWP = 0.4567

rl = 0.93 0.76 0.59 0,40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.223 0.000 0.716 0.000 0.407** 0.010 -0.281

0.060 -0.250 0.020 0.085 0.020 0.031 0.020 -0.303

0.110 -0.543 0.040 -0,053 0.060 -0.145 0.060 -0.849

0.200 - 1.142 0.060 -0.438 0,090 -0.761 0.110 - 1.154

0.230 - 1.094 0,090 -0.646 0.110 -0.891 0.140 - 1.409

0.400 -0.535 0.130 -0.820 0.130 - 1.116 0.190 -2.025"*

0.490 -0.34.4 0.150 - 1.043 0.150 - 1.187 0.250 - 1.450

0.590 -0.302 0.200 - 1.118 0.210 - 1.228 0.400 - 1.077

0.630 -0.303 0.250 - 1.114 0.250 - 1.005 0.490 -0.930

0,700 -0,302 0.260 -0,903 0.340 - 1.279 0.580 -0.607

0.750 -0.320 0,280 -1.007 0,370 -0.931 0.650 -0.372

0.810 -0.305 0.290 -0.926 0,400 -0.739 0.700 -0.328

0.840 -0.321 0.310 -0,700 0.410 - 1.083"* 0,750 -0.257

0.900 -0.236 0.320 -0.696 0,430 -0.717 0.800 -0.201

0.960 -0.142 0.340 -0.661 0.440 -0,686 0.830 -0.199

0.350 -0,324** 0.460 -0.683 0,900 -0.126

0.370 -0.603 0.490 -0.673 0.960 -0,067

0,380 -0,635 0.500 -0.658

0.400 -0.591 0.520 -0.635

0.410 -0.633 0.540 -0.641

0.430 -0.603 0,550 -0,617

0.440 -0.593 0.580 -0,640

0.460 -0.588 0.600 -0.661

0.470 -0.574 0.610 -0.571

0.490 -0.523 0.650 -0.670

0.500 -0.550 0.700 -0.546

0.520 -0.494 0.750 -0.533

0,530 -0.539 0.820 -0.483

0.550 -0,520 0.890 -0.418

0.560 -0.526 0.900 -0.397

0.580 -0.507 0,960 -0.350

0.590 -0.532

0,600 -0.492

0.640 -0.446

0.700 -0.449

0.750 -0.048

0.820 -0.349

0,870 -0,376

0.930 -0,339

0.960 -0.326

Lower Surface

0.020 -0,266 0.020 -0,076 0.020 -0.011 0.020 0,342

0.110 -0.017 0.060 0.193 0,060 0.246 0.060 -0.017

0,230 0.049 0.090 0.139 0.090 0.208 0.110 0.227

0.400 -0.037 0.120 0.163 0.120 0.152 0.250 0.057

0,490 -0.090 0,200 0.045 0.200 0,042 0,400 -0,035

0.630 1.032** 0.260 0,089 0.250 0,082 0.490 -0.108

0.750 -0.04 1 0.400 -0.024 0.400 -0.033 0.580 -0.200

0.850 -0,007 0,490 -0.082 0.490 -0.058 0.650 -0.094

0.900 0.085 0.580 -0,139 0.580 -0.159 0.750 0.153

0.960 0.061 0.640 0,003 0.650 -0.048 0.830 0,275

0.750 0.123 0.750 -0.009 0,900 0.309

O.870 O. 141 0.890 0.250 0.960 0.217

0.930 0.074 0.930 O. 154

0,960 -0.001 0.960 0.172

CN = 0,436 0.578 0.723 0.789

744
TabLe J-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 9-10-37-500, MINF = 0.847, Camber = 10/2, ALPT = 4.09, BETA = 0.57, QINF = 587.1,

RNPU = 4.6E+06, CNWP = 0.1963

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.609 0.000 0.080 0.000 3.160** 0.010 0.482

0.060 0.135 0.020 0.674 0.020 0.611 0.020 0,330

0.110 -0.228 0.040 0.377 0.060 -2.000"* 0.060 -0.182

0.200 -0.884 0.060 0.064 0.090 -0.182 0.110 -0.523

0.230 -0.771 0.090 -0.148 0.110 -0.387 0.140 -0.946

0.400 -0.156 0.130 -0.424 0.130 -0.687 0.190 - 1.994**

0.490 -0.173 0.150 -0.695 0,150 -0.841 0.250 -0.698

0.590 -0.225 0.200 -0.804 0.210 -0.836 0.400 -0.283

0.630 -0.223 0.250 -0.795 0.250 -0.798 0.490 -0.261

0.700 -0.216 0.260 -0.789 0.340 -0.271 0,580 -0.268

0.750 -0.230 0.280 -0.767 0.370 -0.246 0.650 -0.368

0.810 -0.203 0.290 -0.753 0.400 -0.237 0.700 -0,343

0.840 -0.194 0.310 -0.581 0.410 -0,764"* 0.750 -0.376

0,900 -0.106 0.320 -0.466 0.430 -0.260 0.800 -0,456

0.960 0.012 0.340 -0.240 0.440 -0.256 0.830 -0.408

0.350 -0.188"* 0.460 -0.263 0.900 -0.166

0.370 -0.180 0.490 -0.237 0.960 0.006

0.380 -0,202 0.500 -0.274

0.400 -0.155 0.520 -0.269

0.410 -0.211 0.540 -0.259

0.430 -0.206 0.550 -0.229

0.440 -0.199 0.580 -0.227

0.460 -0.215 0.600 -0.267

0.470 -0.242 0.610 -0.300

0.490 -0.230 0.650 2.460"*

0.500 -0.232 0.700 -0,527

0.520 -0.240 0.750 -0.417

0.530 -0.246 0.820 -0.327

0.550 -0.269 0.890 -0.104

0.560 -0.264 0.900 -0.063

0.580 -0.250 0.960 0.046

0.590 -0.281

0.600 -0,286

0.640 -0,490

0.700 -0.285

0,750 -0.064"*

0.820 -0.262

0.870 -0.213

0.930 -0,075

0.960 -0.012

Lower Surface

0,020 -0,757 0.020 -0.957 0.020 - 1,490 0.020 -0.890

0.110 -0.591 0.060 -0.979 0.060 -0.890 0.060 0.944"*

0.230 -0.189 0.090 -0.810 0.090 0.580"* 0.110 -0.244

0.400 -0.064 0.120 -0.543 0.120 -0.207 0.250 -0.259

0,490 -0.049 0.200 -0.162 0.200 -0.142 0.400 -0.30 I

0.630 0,968** 0.260 -0.165 0.250 -0.200 0.490 -0.337

0.750 0.040 0.400 -0.126 0.400 -0,244 0.580 -0.375

0.850 0.084 0.490 -0.121 0.490 -0,076 0.650 -0.155

0.900 0.142 0,580 -0.096 0.580 -0.205 0.750 0.108

0.960 0.149 0.640 0.051 0.650 -0,067 0.830 0.264

0.750 0.151 0.750 -0,041 0.900 0,312

0.870 0,213 0.890 0.258 0.960 0.272

0.930 0,172 0.930 0.220

0.960 0,147 0.960 -2.547 **

CN = 0.154 0.180 0.204 0.243

745
Table J-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 9-I 1-20-000, M1NF = 0.849, Camber = 10/2, ALPT = 8.01, BETA = 0.34, QINF = 587.7,

RNPU = 4.6E+06, CNWP = 0.4529

"8 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 0.426 0.000 0.442 0.000 3.166 ** 0.010 0.082

0.060 -0.060 0.020 0.400 0.020 0.334 0.020 -0.026

0.110 -0.388 0.040 0.155 0.060 - 1.989* * 0.060 -0.598

0.200 -0.985 0.060 -0.165 0.090 -0.400 0.110 -0.886

0.230 -0.933 0.090 -0.340 0.110 -0.604 0.140 - 1.147

0.400 -0.791 O. 130 -0.607 0.130 -0.888 0.190 - 1.983 **

0.490 -0.672 0.150 -0.865 0.150 -0.972 0.250 - 1.152

0.590 -0.185 0.200 -0.955 0.210 -0.989 0.400 -0.838

0.630 -0.165 0.250 -0.978 0.250 -0.980 0.490 -0.664

0.700 -0.162 0.260 -0.979 0.340 - 1.045 0.580 -0.588

0.750 -0.203 0.280 -0.999 0.370 - 1.045 0.650 -0.628

0.810 -0.194 0.290 -0.999 0.400 - 1.008 0.700 -0.612

0.840 -0.197 0.310 -0.864 0.410 -0.755" * 0.750 -0.580

0.900 -0.145 0.320 -0.978 0.430 - 1.040 0.800 -0.236

0.960 -0.030 0.340 -0.935 0.440 - 1.024 0.830 -0.155

0.350 -0.469"* 0.460 -0.757 0.900 -0.051

0.370 -0.957 0.490 -0.986 0.960 0.002

0.380 - 1.008 0.500 - 1.027

0.400 -0.933 0.520 - 1.026

0.410 -0.903 0.540 - 1.023

0.430 -0.939 0.550 -0.976

0.440 -0.851 0.580 -0.978

0.460 -0.969 0.600 -0.991

0.470 -0.959 0.610 -0.977

0.490 -0.942 0.650 2.467"*

0.500 -0.949 0.700 -0.461

0.520 -0.936 0.750 -0.355

0.530 -0.925 0.820 -0.137

0.550 -0.960 0.890 -0.010

0.560 -0.958 0.900 0.017

0.580 -0.934 0.960 0.082

0.590 -0.975

0.600 -0.959

0.640 -0.336

0.700 -0.270

0.750 -0.029**

0.820 -0.092

0.870 -0.085

0.930 -0.008

0.960 0.036

Lower Surface

0.020 -0.842 0.020 -0.447 0.020 -0.439 0.020 -0.099

0.110 -0.101 0.060 -0.186 0.060 0.073 0.060 0.953" *

0.230 -0.022 0.090 -0.066 0.090 0.588** 0.1 l0 0.116

0.400 -0.050 0.120 0.047 0.120 0.043 0.250 -0.040

0.490 -0.055 0.200 -0.027 0.200 -0.022 0.400 -0.113

0.630 0.939"* 0.260 0.029 0.250 -0.016 0.490 -0.177

0.750 0.019 0.400 -0.054 0.400 -0.101 0.580 -0.261

0.850 0.067 0.490 -0.089 0.490 -0.047 0.650 -0.101

0.900 0.127 0.580 -0.105 0.580 -0.166 0.750 0.143

0.960 0.129 0.640 0.065 0.650 -0.032 0.830 0.298

0.750 0.184 0.750 -0.024 0.900 0.330

0.870 0.248 0.890 0.315 0.960 0.267

0.930 0.211 0.930 0.263

0.960 0.180 0.960 -2.535"*

CN = 0.407 0.564 0.629 0.646

746
Table J-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 9-11-33-500, MINF = 0.859, Camber = 10/2. ALPT = 7.99, BETA = 0.25, QINF = 612.7,

RNPU = 4.8E+06. CNWP = 0.4575

rl = 0,93 0.76 0,59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 0,444 0.000 0.427 0.000 3.001 ** 0.010 0.115

0.060 -0.036 0,020 0.461 0.020 0.356 0.020 -0.002

0.110 -0.353 0.040 0.182 0.060 - 1.944"* 0.060 -0.578

0.200 - 1.022 0.060 -0.136 0.090 -0,373 0.110 -0,865

0.230 -0.928 0.090 -0.314 0. l 10 -0.577 0.140 - 1.133

0.400 -0.795 0,130 -0.587 0.130 -0.861 0,190 - 1.938 **

0.490 -0.682 0.150 -0.834 0. 150 -0.969 0.250 - 1.135

0.590 -0_243 0.200 -0.939 0.210 -0.975 0.400 -0.825

0.630 °0.157 0.250 -0.978 0,250 -0.976 0.490 -0.680

0,700 -0.143 0.260 -0.960 0.340 - 1.025 0.580 -0.584

0.750 -0,184 0.280 -0.981 0.370 - 1.029 0.650 -0.637

0.810 -0.176 0.290 -0.977 0,400 - 1.004 0.700 -0.622

0.840 -0.189 0,310 -0.865 0.410 -0.760** 0.750 -0,644

0.900 -0.146 0.320 -0.955 0.430 - 1.035 0.800 -0.301

0.960 -0.033 0.340 -0.933 0.440 -1.025 0.830 -0.201

0.350 -0.473"* 0.460 -0,762 0.900 -0.064

0.370 -0.937 0.490 - 1.006 0.960 -0.013

0.380 -0.988 0.500 - 1.021

0.400 -0,872 0.520 - 1.017

0.410 -0.903 0.540 - 1.012

0.430 -0.938 0.550 -0.974

0.440 -0.853 0.580 -0.955

0.460 -0.961 0.600 -0,989

0.470 -0.953 0.610 -0.965

0.490 -0.943 0,650 2.330**

0.500 -0.943 0.700 -0.669

0.520 -0.936 0.750 -0.431

0.530 -0.916 0.820 -0.175

0,550 -0.953 0.890 -0.026

0.560 -0.948 0.900 0.011

0.580 -0.937 0.960 0.067

0.590 -0.970

0.600 -0.957

0.640 -0.385

0.700 -0.340

0.750 -0.043**

0.820 -0.120

0.870 -0.080

0.930 -0.008

0.960 0.014

Lower Surface

0.020 -0.831 0,020 -0.462 0.020 -0.467 0.020 -0.109

0.110 -0.173 0,060 -0.243 0.060 0.016 0.060 0.877"*

0.230 -0,038 0.090 -0.121 0,090 0.528** 0.110 0.106

0.400 -0.050 0.120 0.016 0.120 0.028 0,250 -0.050

0.490 -0.064 0.200 -0.041 0.200 -0.036 0.400 -0.131

0,630 0.864"* 0.260 0,014 0.250 -0.031 0.490 -0.194

0.750 0.011 0.400 -0,067 0,400 -0.127 0.580 -0.295

0.850 0.060 0.490 -0.095 0,490 -0.046 0.650 -0.122

0.900 0.129 0.580 -0.122 0.580 -0.188 0.750 0.132

0.960 0.127 0.640 0.051 0.650 -0.042 0.830 0.298

0.750 0.171 0.750 -0.035 0.900 0.325

0,870 0.241 0,890 0.308 0.960 0.261

0.930 0.196 0.930 0.252

0.960 0.163 0.960 -2.468 * *

CN = 0.394 0.549 0,630 0.638

747
Table J-2. Continued.

Flight 208, Wing sweep = 26", Time = 14-52-18-000, MINF = 0.862, Camber = 5/10, ALPT = 3.07, BETA = 0.08, QINF = 611.4,

RNPU = 4.8E+06, CNWP = 0.1502

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 0.461 0.000 0.421 0.000 0.302"* 0.010 0.145

0.060 0.105 0.020 0.395 0.020 0.392 0.020 0.041

0.110 -0.157 0.040 0.288 0.060 0.265 0.060 -0.256

0.200 -0.238 0.060 0.012 0.090 -0.193 0.110 -0.443

0.230 -0.280 0.090 -0.136 0.110 -0.343 0.1 40 -0.747

0.400 -0.186 0.130 -0.315 0.130 -0.521 0.190 - 1.920* *

0.490 -0.191 0.150 -0.517 0.150 -0.640 0.250 -0.418

0.590 -0.253 0.200 -0.343 0.210 -0.619 0.400 -0.293

0.630 -0.296 0.250 -0.301 0.250 -0.271 0.490 -0.280

0.700 -0.395 0.260 -0.290 0.340 -0.289 0.580 -0.291

0.750 -0.819 0.280 -0.309 0.370 -0.324 0.650 -0.393

0.810 -0.747 0.290 -0.307 0.400 -0.304 0.700 -0.356

0.840 -0.819 0.310 -0.300 0.410 0.294** 0.750 -0.428

0.900 -0.272 0.320 -0.304 0.430 -0.316 0.800 -0.931

0.960 -0.267 0.340 -0.286 0.440 -0.298 0.830 -0.929

0.350 -0.256** 0.460 -0.300 0.900 -0.421

0.370 -0.272 0.490 -0.254 0.960 -0.414

0.380 -0.288 0.500 -0.303

0.400 -0.256 0.520 -0.279

0.410 -0.284 0.540 -0.269

0.430 -0.264 0.550 -0.264

0.440 -0.246 0.580 -0.268

0.460 -0.267 0.600 -0.288

0.470 -0.281 0.610 -0.302

0.490 -0.273 0.650 -0.664

0.500 -0.273 0.700 -0.524

0.520 -0.276 0,750 -0.478

0.530 -0.285 0.820 -0.969

0.550 -0.312 0.890 -0.44 1

0.560 -0.291 0.900 -0.499

0.580 -0.264 0.960 -0.451

0.590 -0.307

0.600 -0.302

0.640 -0.555

0.700 -0.482

0.750 -0.099

0.820 -0.565

0.870 -0.341

0.930 -0.315

0.960 -0.321

Lower Surface

0.020 - 1.343 0.020 -0.906 0.020 - 1.235 0.020 -0.455

0.110 -0.475 0.060 -0.975 0.060 -0.869 0,060 -0.058

0.230 -0.220 0.090 -0.771 0.090 -0.414 0.110 -0.358

0.400 0.002 0.120 -0.440 0.120 -0.437 0.250 -0.342

0.490 0.023 0.200 -0.220 0.200 -0.256 0,400 -0.316

0.630 0.908"* 0.260 -0.134 0.250 -0.303 0.490 -0.276

0.750 O. 167 0.400 -0.095 0.400 -0.192 0.580 -0.201

0.850 0.197 0.490 -0.049 0.490 -0.113 0.650 0.030

0.900 0.274 0.580 0.013 0.580 -0.047 0.750 0.269

0.960 0.122 0.640 0.240 0.650 -0.103 0.830 0.377

0.750 0.295 0.750 -0.050 0.900 0.449

0.870 0.365 0.890 0.415 0.960 0.305

0.930 0.283 0.930 0.328

0.960 0.163 0.960 0.333

CN = 0.271 0.253 0.268 0.350

748
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-53-36-000, MINF = 0.857, Camber = 5/10, ALl:q" = 3.00, BETA = 0.17, Q1NF = 598.7,

RNPU = 4.7E+06. CNWP = 0.1234

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.470 0.000 0.407 0.000 0.284"* 0.010 O. 163

0.060 O. 122 0.020 0,409 0.020 0.408 0.020 0.056

O. 110 -0.151 0.040 0.302 0.060 0.234 0.060 -0.247

0.200 -0.229 0.060 0.020 0.090 -0.191 O.110 -0.441

0.230 -0.252 0.090 -0.131 O. 110 -0.342 O. 140 -0.754

0.400 -0.186 0.130 -0.304 0.130 -0.524 0.190 -1.946"*

0.490 -0.182 O.150 -0.495 O. 150 -0.637 0.250 -0.257

0.590 -0.260 0.200 -0.387 0.210 -0.337 0.400 -0.295

0.630 -0.295 0.250 -0.292 0.250 -0.289 0.490 -0.282

0.700 -0.380 0.260 -0.278 0.340 -0.284 0.580 -0.287

0.750 -0.844 0.280 -0.297 0.370 -0.316 0.650 -0.384

0.810 -0.769 0.290 -0.294 0.400 -0.296 0.700 -0.350

0.840 -0.810 0.310 -0.284 0.410 -2.445 * * 0.750 -0.415

0.900 -0.235 0.320 -0.286 0.430 -0.304 0.800 -2.348

0.960 -0.237 0.340 -0.276 0.440 -0.289 0.830 -0.702

0.350 -0.255** 0.460 -0.299 0.900 -0.392

0.370 -0.264 0.490 -0.274 0.960 -0.412

0.380 -0.279 0.500 -0.298

0.400 -0.248 0.520 -0.277

0.410 -0.277 0.540 -0.274

0.430 -0.263 0.550 -0.264

0.440 -0.242 0.580 -0.278

0.460 -0.268 0.600 -0.313

0.470 -0.266 0.610 -0.304

0.490 -0.266 0.650 -0.653

0.500 -0.270 0.700 -0.540

0.520 -0.282 0,750 -0.473

0.530 -0.275 0.820 - 1.030

0.550 -0.308 0.890 -0.393

0.560 -0.289 0.900 -0.458

0.580 -0.268 0.960 -OAO0

0.590 -0.301

0.600 -0.286

0.640 -0.557

0.700 -0,475

0.750 -0.083

0.820 -0.557

0.870 -0.328

0.930 -0.284

0.960 -0.292

Lower Surface

0,020 - 1.346 0.020 -2.347 0.020 - 1.254 0.020 -0.476

O. 110 -0.463 0.060 -2.418 0.060 -0.885 0.060 -0.044

0.230 -0.215 0.090 -2.202 0.090 -0.421 O. 110 -0.375

0.400 0.000 O. 120 -0.413 O. 120 -0.447 0.250 -0.344

0.490 0.025 0.200 -0.213 0.200 -0.230 0.400 -0.319

0.630 0.928** 0.260 -0.132 0.250 -0.285 0.490 -0.270

0.750 O. 170 0.400 -0.091 0.400 -0.194 0.580 -0.194

0.850 0.202 0.490 -0.049 0.490 -0.098 0.650 0.031

0.900 0.275 0.580 0.013 0.580 -0.051 0.750 0.274

0.960 O. 131 0.640 0.241 0,650 -0.090 0.830 0.373

0.750 0.300 0.750 -0.042 0.900 0.448

0.870 0.361 0.890 0.413 0.960 0.309

0.930 0.273 0.930 0.328

0.960 O. 166 0.960 0.323

CN = 0.268 0.133 0.258 0.373

749
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-54-9-500, MINF = 0.852, Camber = 5/10, ALPT = 8.03, BETA = 0.40, QINF = 604.5,

RNPU = 4.8E+06, CNWP = 0.4939

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.039 0.000 0.829 0.000 0.336** 0.010 -0.704

0.060 -0.252 0.020 -0.173 0.020 -0.226 0.020 -0.745

0.110 -0.440 0.040 -0.173 0.060 -0.186 0.060 -0.795

0.200 -0.863 0.060 -0.442 0.090 -0.716 0.110 - 1.008

0.230 -0.810 0.090 -0.562 0.110 -0.779 0.140 - 1.176

0.400 -0.714 0.130 -0,658 0.130 -0.887 0.190 - 1.970* *

0.490 -0.600 0.150 -0.808 0.150 -0.937 0.250 - 1.184

0.590 -0.51 _ 0.200 -0.853 0.210 -0.982 0.400 -0.845

0.630 -0.350 0.250 -0.942 0.250 -0.966 0.490 -0.689

0.700 -0.400 0.260 -0.926 0.340 - 1.028 0.580 -0.588

0.750 -0.860 0.280 -0.953 0.370 - 1.033 0.650 -0.646

0.810 -0.809 0.290 -0.951 0.400 - 1.000 0.700 -0.621

0.840 -0.882 0.310 -0.877 0.410 -2.464 ** 0.750 -0.652

0.900 -0.471 0.320 -0.922 0.430 - 1.039 0.800 -0.626

0.960 -0.440 0.340 -0.914 0.440 - 1.017 0.830 -0.501

0.350 -0.398** 0.460 -0.784 0.900 -0.388

0.370 -0.921 0,490 -0.991 0.960 -0.324

0.380 -0.972 0.500 -1,032

0.400 -0.907 0,520 - 1.034

0.410 -0,894 0.540 - 1.035

0.430 -0.924 0.550 - 1.014

0.440 -0.844 0.580 - 1.020

0.460 -0.957 0.600 - 1.031

0.470 -0.939 0.610 - 1.0 ! 0

0.490 -0.928 0.650 -0.982

0.500 -0.934 0.700 -0.796

0.520 -0.915 0.750 -0.718

0.530 -0.906 0.820 -0.337

0.550 -0.936 0.890 -0.277

0.560 -0.945 0.900 -0.279

0.580 -0.918 0.960 -0.270

0.590 -0.961

0.600 -0.944

0.640 -0.893

0.700 -0.500

0.750 -0.031

0.820 -0.274

0.870 -0.264

0.930 -0.268

0.960 -0.263

Lower Surface

0.020 -0.275 0.020 -0.137 0.020 -0.011 0.020 0.369

0.110 -0.115 0.060 0.088 0.060 0.159 0.060 -0.04 1

0.230 0,045 0.090 0.044 0.090 0.103 0.110 0.116

0.400 0.011 0.120 0.044 0.120 -0.002 0.250 -0.045

0.490 0.022 0.200 0.046 0.200 0.035 0.400 -0.079

0.630 0.876** 0.260 0.018 0.250 0.000 0.490 -0.087

0.750 0.164 0.400 0.004 0.400 -0.012 0.580 -0.047

0.850 0.183 0.490 0.026 0.490 -0.04 1 0.650 0.144

0.900 0.277 0.580 0.064 0.580 0.029 0.750 0.388

0.960 0.101 0.640 0.284 0.650 -0.048 0.830 0.480

0.750 0.338 0.750 -0.044 0.900 0.529

0.870 0.417 0.890 0.495 0.960 0.350

0.930 0.333 0.930 0.398

0.960 0.212 0.960 0.400

CN = 0.643 0.766 0.803 0.864

750
Table J-2. Continued.

Flight 208, Wing sweep = 26 °, Time = 14-54-11-000, MINF = 0.851, Camber = 5/10, ALPT = 7.93, BETA = -0.24, QINF = 606.5,

RNPU = 4.8E+06, CNWP = 0.4625

11 = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x,/c CP x/c CP x/c CP

0.020 0.062 0.000 0.819 0.000 0.387 ** 0.010 -0.715

0.060 -0.236 0.020 -0.139 0.020 -0.201 0.020 -0.715

0.110 -0.424 0.040 -0.159 0.060 -0.189 0.060 -0.785

0.200 -0.860 0.060 -0.440 0.090 -0.691 0. ! 10 -0.982

0.230 -0.805 0.090 -0.531 0.110 -0.759 0.140 - 1.171

0.400 -0.701 0.130 -0.637 0.130 -0.866 0.190 - 1.971 **

0.490 -0.583 0.150 -0.800 0.150 -0.925 0.250 - 1.166

0.590 -0.451 0.200 -0.847 0.210 -0.960 0.400 -0.825

0.630 -0.334 0.250 -0.930 0.250 -0.969 0.490 -0.675

0.700 -0.373 0.260 -0.913 0.340 - 1.003 0.580 -0.564

0.750 -0.880 0.280 -0.949 0.370 - 1.018 0.650 -0.618

0.810 -0.838 0.290 -0.940 0.400 -0.979 0.700 -0.599

0.840 -0.906 0.310 -0.881 0.410 -2.463** 0.750 -0.628

0.900 -0.447 0.320 -0.915 0.430 - 1.020 0.800 -0.686

0.960 -0.417 0.340 -0.918 0.440 - 1.002 0.830 -0.534

0.350 -0.404** 0.460 -0.788 0.900 -0.444

0.370 -0.915 0.490 -0.972 0.960 -0.370

0.380 -0.965 0.500 - 1.029

0.400 -0.902 0.520 - 1.014

0.410 -0.898 0.540 - 1.028

0.430 -0.903 0.550 - 1.005

0.440 -0.848 0.580 -0.999

0.460 -0.936 0.600 - 1.004

0.470 -0.924 0.610 -0.974

0.490 -0.913 0.650 -0.887

0.500 -0.918 0.700 -0.719

0.520 -0.908 0.750 -0.675

0.530 -0.891 0.820 -0.346

0.550 -0.923 0.890 -0.277

0.560 -0.927 0.900 -0.276

0.580 -0.902 0.960 -0.262

0.590 -0.944

0.600 -0.942

0.640 -0.897

0.700 -0.783

0,750 -0.038

0.820 -0.253

0.870 -0.252

0.930 -0.247

0.960 -0.247

Lower Surface

0.020 -0.312 0.020 -0.171 0.020 -0.037 0.020 0.308

0.110 -0.124 0.060 0.072 0.060 0.132 0.060 -0.048

0.230 0.039 0.090 0.026 0.090 0.089 0.110 0.112

0.400 0.009 0.120 0.037 0.120 °0.020 0.250 -0.059

0.490 0.022 0.200 0.037 0.200 0.025 0.400 -0.083

0.630 0.866** 0.260 0.008 0.250 -0.003 0.490 -0.098

0.750 0.1 64 0.400 0.004 0.400 -0.020 0.580 -0.056

0.850 0.188 0.490 0.026 0,490 -0.044 0.650 0.137

0.900 0.275 0.580 0.066 0.580 0.026 0.750 0.383

0.960 0.097 0.640 0.297 0.650 -0.046 0.830 0.475

0.750 0.338 0.750 -0.049 0.900 0.531

0.870 0.423 0.890 0.501 0.960 0.358

0.930 0.335 0.930 0.393

0.960 0.218 0.960 0.398

CN = 0.630 0.772 0.778 0.853

751
Table J-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 9-7-47-000, MINF = 0.849, Camber = 5/10, ALPT = 3.03, BETA = 0.43, QINF = 588.2,

RNPU = 4.6E+06, CNWP = 0.1959

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.480 0.000 0.418 0.000 3.161 * * 0.010 0.202

0.060 O. 119 0.020 0.455 0.020 0.408 0.020 0.089

O.110 -0.155 0.040 0.259 0.060 -3.484** 0.060 -0.227

0.200 -0.223 0.060 0.038 0.090 -0.158 O. 110 -0.399

0.230 -0.247 0.090 -0.094 O. 110 -0.298 O. 140 -0.704

0.400 -0.161 O.130 -0.263 O. 130 -0.504 O. 190 - 1.984"*

0.490 -0.172 O.150 -0.388 O. 150 -0.606 0.250 -0.238

0.590 -0.250 0.200 -0.373 0.210 -0.291 0.400 -0.269

0.630 -0.283 0.250 -0.268 0.250 -0.272 0.490 -0.237

0.700 -0.330 0.260 -0.270 0.340 -0.287 0.580 -0.265

0.750 -0.683 0.280 -0.276 0.370 -0.304 0.650 -0.381

0.810 -0.532 0.290 -0.281 0.400 -0.280 0.700 -0.334

0.840 -0.558 0.310 -0.274 0.410 -0.757** 0.750 -0.402

0.900 -0.221 0.320 -0.275 0.430 -0.299 0.800 -0.929

0.960 -0.210 0.340 -0.266 0.440 -0.290 0.830 -0.705

0.350 -0.225** 0.460 -0.289 0.900 -0.389

0.370 -0.244 0.490 -0.254 0.960 -0.388

0.380 -0.267 0.500 -0.289

0.400 -0.208 0.520 -0.272

0.410 -0.259 0.540 -0.266

0.430 -0.245 0.550 -0.234

0.440 -0.234 0.580 -0.231

0.460 -0.244 0.600 -0.272

0.470 -0.258 0.610 -0.300

0.490 -0.248 0.650 2.463**

0.500 -0.248 0.700 -0.527

0.520 -0.262 0.750 -0.446

0.530 -0.261 0.820 -0.856

0.550 -0.295 0.890 -0.384

0.560 -0.281 0.900 -0.448

0.580 -0.253 0.960 -0.385

0.590 -0.285

0.600 -0.289

0.640 -0.542

0.700 -0.461

0.750 -0.073**

0.820 -0.530

0.870 -0.290

0.930 -0.283

0.960 -0.292

Lower Surface

0.020 - 1.343 0.020 -0.927 0.020 - 1.179 0.020 -0.392

O. 110 -0.441 0.060 -0.999 0.060 -0.655 0.060 0.949**

0.230 -0.183 0.090 -0.795 0.090 0.585"* O. 110 -0.268

0.400 0.005 O. 120 -0.300 O. 120 -0.363 0.250 -0.324

0.490 0.045 0.200 -0.189 0.200 -0.183 0.400 -0.278

0.630 0.972 ** 0.260 -0.108 0.250 -0.264 0.490 -0.231

0.750 O. 173 0.400 -0.066 0.400 -0.169 0.580 -0.179

0.850 0.216 0.490 -0.031 0.490 -0.063 0.650 0.064

0.900 0.267 0.580 0.035 0.580 -0.024 0.750 0.286

0.960 O. 139 0.640 0.249 0.650 -0.078 0.830 0.408

0.750 0.307 0.750 -0.027 0.900 0.469

0.870 0.386 0.890 0.415 0.960 0.333

0.930 0.276 0.930 0.332

0.960 O. 170 0.960 -2.536 * *

CN = 0.238 0.273 0.265 0.316

752
Table J-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 9-8-12-500, MINF = 0.858, Camber = 5/11, ALPT = 4.08, BETA = 0.28, QINF = 600.7,

RNPU = 4.7E+06, CNWP = 0.2656

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.419 0.000 0.507 0.000 3,095"* 0.010 0.078

0.060 0.056 0.020 0.370 0.020 0.320 0.020 -0,028

0.110 -0.204 0.040 0.191 0.060 -3.411 ** 0.060 -0,316

0.200 -0.184 0.060 -0.017 0.090 -0.212 0.110 -0.459

0.230 -0.260 0.090 -0.157 0.110 -0.351 0.140 -0.760

0.400 -0.176 0.130 -0.352 0.130 -0.541 0.190 -1.942"*

0.490 -0.18 L 0.150 -0.538 0.150 -0.647 0.250 -0.570

0.590 -0.248 0.200 -0.583 0.210 -0.651 0.400 -0.281

0,630 -0.279 0.250 -0.275 0.250 -0.641 0.490 -0.260

0.700 -0,388 0.260 -0.230 0.340 -0.243 0.580 -0.285

0.750 -0.688 0.280 -0.240 0.370 -0.293 0.650 -0.388

0.810 -0.610 0.290 -0.262 0.400 -0.281 0.700 -0.353

0.840 -0.634 0.310 -0.275 0.410 -0.741 ** 0.750 -0.429

0.900 -0.262 0.320 -0.282 0.430 -0.315 0.800 -0.909

0.960 -0.244 0.340 -0,282 0,440 -0.299 0.830 -0.808

0.350 -0.207** 0.460 -0.305 0.900 -0.399

0.370 -0.266 0.490 -0.275 0.960 -0.412

0.380 -0.289 0.500 -0.310

0.400 -0.236 0.520 -0.283

0.410 -0.281 0.540 -0.280

0.430 -0.263 0.550 -0.247

0.440 -0.252 0.580 -0,234

0,460 -0,259 0.600 -0.281

0.470 -0.271 0.610 -0.307

0.490 -0.267 0.650 2.411 **

0.500 -0,267 0.700 -0.525

0.520 -0.272 0.750 -0.45 l

0.530 -0.278 0.820 -0.894

0,550 -0.311 0.890 -0.426

0.560 -0.290 0.900 -0,478

0.580 -0.257 0.960 -0.428

0.590 -0.277

0.600 -0.286

0.640 -0.532

0.700 -0.465

0.750 -0,064"*

0.820 -0.532

0.870 -0.313

0.930 -0.298

0.960 -0.306

Lower Surface

0,020 - 1.278 0.020 -0.907 0.020 - 1.069 0.020 -0.186

0.110 -0.233 0.060 -0.978 0.060 -0.334 0.060 0.929"*

0.230 -0.143 0.090 -0.363 0.090 0.573** 0.110 -0.222

0.400 -0.006 0.120 -0.127 0.120 -0.253 0.250 -0.278

0.490 0.037 0.200 -0. 138 0.200 -0.148 0.400 -0.239

0.630 0.952** 0,260 -0.115 0.250 -0.229 0.490 -0.226

0.750 0.183 0.400 -0.057 0.400 -0.151 0.580 -0.168

0.850 0.215 0.490 -0.023 0,490 -0.054 0.650 0,074

0.900 0.272 0.580 0.044 0.580 -0.018 0.750 0.304

0,960 0.128 0.640 0.256 0.650 -0.069 0.830 0,431

0.750 0.317 0,750 -0.034 0,900 0,487

0.870 0.388 0.890 0.436 0.960 0.347

0.930 0.291 0.930 0.351

0.960 0.179 0.960 -2.483**

CN = 0.291 0.331 0,363 0.410

753
Table J-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 9-8-18-500, MINF = 0.858, Camber = 5/11, ALPT = 5.12, BETA = 0.22, QINF = 598.5,

RNPU = 4.7E+06, CNWP = 0.3537

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.335 0.000 0.598 0.000 3.114"* 0.010 -0.054

0.060 -0.036 0.020 0.264 0.020 0.201 0.020 -0.128

0.110 -0.296 0.040 0.105 0.060 -3.417** 0.060 -0.509

0.200 -0.705 0.060 -0.104 0.090 -0.294 0.110 -0.623

0.230 -0.551 0.090 -0.232 0.110 -0.427 0.140 -0.836

0.400 -0.155 0.130 -0.415 0.130 -0.619 0.190 -1.943"*

0.490 -0.180 0.150 -0.604 0.150 -0.710 0.250 -0.629

0.590 -0.252 0.200 -0.646 0.210 -0.718 0.400 -0.373

0.630 -0.281 0.250 -0.695 0.250 -0.734 0.490 -0.311

0.700 -0.398 0.260 -0.696 0.340 -0.765 0.580 -0.316

0.750 -0.861 0.280 -0.699 0.370 -0.767 0.650 -0.403

0.8I0 -0.724 0.290 -0.697 0.400 -0.530 0.700 -0.376

0.840 -0.768 0.310 -0.666 0.410 -0.737** 0.750 -0.439

0.900 -0.275 0.320 -0.672 0.430 -0.294 0.800 -0.906

0.960 -0.266 0.340 -0.672 0.440 -0.255 0.830 -0.776

0.350 -0.363** 0.460 -0.249 0.900 -0.393

0.370 -0.655 0.490 -0.216 0.960 -0.431

0.380 -0.683 0.500 -0.248

0.400 -0.395 0.520 -0.226

0.410 -0.232 0.540 -0.234

0.430 -0.157 0.550 -0.204

0.440 -0.147 0.580 -0.228

0.460 -0.143 0.600 -0.250

0.470 -0.162 0.610 -0.281

0.490 -0.166 0.650 2.427 **

0.500 -0.180 0.700 -0.504

0.520 -0.188 0.750 -0.420

0.530 -0.205 0.820 -1.036

0.550 -0.242 0.890 -0.421

0.560 -0.238 0.900 -0.479

0.580 -0.228 0.960 -0.426

0.590 -0.262

0.600 -0.270

0.640 -0.524

0.700 -0.446

0.750 -0.041"*

0.820 -0.565

0.870 -0.404

0.930 -0.301

0.960 -0.315

Lower Surface

0.020 - 1.211 0.020 -0.904 0.020 -0.887 0.020 -0.070

0. t 10 -0.148 0.060 -0.355 0.060 -0.114 0.060 0.940"*

0.230 -0.068 0.090 -0.191 0.090 0.582" * 0.110 -0.094

0.400 -0.003 0.120 -0.088 0.120 -0.162 0.250 -0.204

0.490 0.032 0.200 -0.073 0.200 -0.068 0.400 -0.190

0.630 0.963"* 0.260 -0.076 0.250 -0,158 0.490 -0.190

0.750 0.172 0.400 -0.048 0.400 -0.115 0.580 -0.1 40

0.850 0.215 0.490 -0.020 0.490 -0.034 0.650 0.096

0.900 0.270 0.580 0.047 0.580 -0.006 0.750 0.322

0.960 0.121 0.640 0.265 0.650 -0.049 0.830 0.453

0.750 0.328 0.750 -0.020 0.900 0.498

0.870 0.401 0.890 0.470 0.960 0.352

0.930 0.304 0.930 0.374

0.960 0.189 0.960 -2.485**

CN = 0.397 0.466 0.484 0.508

754
Table J-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 9-8-26-500, MINF = 0.855, Camber = 5/10, ALPT = 6.97, BETA = 0.22, QINF = 594.5,

RNPU = 4.7E+06, CNWP = 0.4279

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.198 0.000 0.752 0.000 3.136"* 0.010 -0.535

0.060 -0.129 0.020 0.047 0,020 -0.054 0,020 -0.256

0.110 -0.354 0.040 -0.061 0.060 -3.438"* 0,060 -0.680

0.200 -0.787 0.060 -0.267 0.090 -0.526 0.110 -0.84 I

0.230 -0.693 0.090 -0.354 0.110 -0.579 0.140 -1.011

0,400 -0.581 0.130 -0.528 0.130 -0.735 0.190 -1.954**

0,490 -0.442 0,150 -0.693 0.150 -0.811 0.250 -0.979

0.590 -0.293 0.200 -0.745 0.210 -0.818 0.400 -0.753

0.630 -0.281 0.250 -0.820 0.250 -0.853 0.490 -0.534

0,700 -0.295 0.260 -0,828 0.340 -0.906 0.580 -0.438

0.750 -0.885 0.280 -0,824 0,370 -0.909 0.650 -0.494

0.810 -0.832 0.290 -0.827 0.400 -0.886 0.700 -0.466

0.840 -0.889 0.310 -0.801 0.410 -0.740"* 0.750 -0.524

0.900 -0.341 0.320 -0.806 0.430 -0.909 0.800 -0.793

0.960 -0.335 0.340 -0.812 0.440 -0.895 0.830 -0.537

0.350 -0.383"* 0.460 -0.735 0.900 -0.435

0.370 -0.807 0.490 -0.870 0.960 -0.408

0.380 -0.849 0.500 -0.911

0.400 -0.783 0.520 -0.898

0.410 -0.822 0.540 -0.892

0.430 -0.785 0.550 -0,842

0.440 -0.777 0.580 -0.749

0.460 -0.817 0.600 -0.640

0.470 -0.805 0,610 -0.553

0.490 -0.798 0,650 2.445**

0.500 -0.803 0,700 -0.576

0.520 -0.775 0.750 -0.516

0.530 -0.788 0.820 -0.465

0.550 -0.819 0.890 -0,289

0.560 -0.819 0.900 -0.314

0.580 -0.796 0.960 -0.278

0.590 -0.840

0.600 -0.813

0.640 -0.861

0.700 -0.846

0.750 -0.025**

0.820 -0.624

0,870 -0,304

0.930 -0,220

0.960 -0.219

Lower Surface

0.020 -0.551 0.020 -0.381 0.020 -0.130 0.020 0.213

0,110 -0.146 0.060 -0.019 0.060 0,075 0.060 0.948"*

0,230 0.013 0.090 -0.04 1 0.090 0.587"* 0.110 0.059

0.400 0.007 0.120 -0.017 0.120 -0.024 0.250 -0.087

0.490 0,042 0.200 0.011 0.200 0.020 0.400 -0.106

0,630 0.970"* 0.260 -0.013 0.250 -0.049 0.490 -0.111

0.750 0.182 0+400 -0+005 0.400 -0.044 0.580 -0.091

0.850 0.227 0.490 0.014 0.490 -0.0 l 5 0.650 O. 134

0.900 0.290 0.580 0.066 0.580 0,025 0.750 0.359

0.960 O. 123 0.640 0.295 0,650 -0.029 0.830 0.481

0.750 0.350 0,750 -0.011 0.900 0.525

0.870 0,465 0.890 0.497 0.960 0.369

0.930 0.341 0.930 0.397

0.960 0,232 0.960 -2.500**

CN = 0.549 0.760 0.680 0.737

755
Table J-2. Continued.

Flight 224, Wing sweep = 26 °, Time = 9-8-31-000, MINF = 0.848, Camber = 5/10, ALPT = 8.00, BETA = 0.02, QINF = 583.5,

RNPU = 4.6E+06, CNWP = 0.4797

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x,/c CP x/c CP

0.020 0.066 0.000 0.818 0.000 3.198"* 0.010 -0.649

0.060 -0.230 0.020 -0.105 0.020 -0.212 0.020 -0.681

0.110 -0.412 0,040 -0.198 0.060 -2.031 * * 0.060 -0.755

0.200 -0.832 0.060 -0.404 0.090 -0.651 0.110 -0.935

0.230 -0.760 0,090 -0.496 0.110 -0.709 0.140 - 1.092

0.400 -0.664 0.130 -0.612 0.130 -0.843 0.190 - 1.988" *

0.490 -0.556 0.150 -0.767 0.150 -0.897 0.250 - 1.100

0.590 -0.394 0.200 -0.810 0.210 -0.921 0.400 -0,811

0.630 -0.313 0.250 -0.892 0.250 -0.929 0.490 -0.643

0.700 -0.323 0.260 -0.899 0.340 -0,974 0.580 -0.546

0.750 -0.879 0.280 -0.912 0.370 -0.984 0.650 -0.603

0.810 -0.831 0.290 -0.912 0.400 -0.988 0.700 -0.581

0.840 -0.888 0.310 -0.854 0.410 -0.751 ** 0.750 -0.613

0.900 -0.411 0.320 -0.894 0.430 -0.985 0.800 -0.64 1

0.960 -0.397 0.340 -0.897 0.440 -0.959 0.830 -0.507

0.350 -0.393"* 0.460 -0.746 0.900 -0.399

0.370 -0.885 0.490 -0.931 0,960 -0.35 I

0.380 -0.937 0.500 -0.989

0.400 -0.863 0.520 -0.990

0.410 -0.864 0.540 -0.976

0.430 -0.877 0.550 -0.949

0.440 -0.812 0.580 -0.923

0.460 -0.900 0.600 -0.946

0.470 -0.897 0.610 -0.913

0.490 -0.882 0.650 2.494**

0.500 -0.889 0.700 -0.729

0,520 -0.870 0.750 -0.651

0,530 -0,864 0.820 -0.336

0,550 -0.883 0.890 -0.259

0.560 -0.889 0,900 -0.259

0.580 -0.874 0.960 -0.241

0.590 -0.910

0.600 -0.894

0.640 -0.874

0.700 -0.898

0.750 -0.019* *

0.820 -0.237

0.870 -0.210

0.930 -0.227

0.960 -0.228

Lower Surface

0.020 -0.271 0.020 -0.1 64 0.020 0.007 0.020 0.334

0.110 -0.103 0.060 0.076 0.060 0.184 0.060 0.968"*

0.230 0.058 0.090 0.041 0.090 0.601 ** 0.110 0.126

0.400 0.026 0.120 0.053 0.120 0.028 0.250 -0.032

0.490 0.043 0.200 0.055 0.200 0.063 0.400 -0.057

0.630 0.991"* 0.260 0.034 0.250 0.007 0.490 -0.072

0.750 0.170 0.400 0.024 0.400 -0.007 0.580 -0.044

0.850 0.209 0.490 0.035 0.490 -0.009 0.650 0.160

0.900 0.278 0.580 0.078 0.580 0.047 0.750 0.379

0.960 0.111 0.640 0.300 0.650 -0.020 0.830 0.492

0.750 0.347 0.750 -0,020 0.900 0.537

0.870 0.443 0.890 0,501 0.960 0.368

0.930 0,335 0.930 0.396

0.960 0.221 0,960 -2.545**

CN = 0.618 0.802 0.784 0.844

756
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-53-1-500, MINF = 0.900, Camber = 012, ALPT = 3.52, BETA = 0.63, QINF = 601.5,

RNPU = 4.6E+06, CNWP = 0.1955

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x./c CP x./c CP

0.020 0.063 0.000 0.849 0.000 0.501 ** 0.010 -0.580

0.060 -0.114 0.020 -0.166 0.020 -0.171 0.020 -0.632

0.110 -0.222 0.040 -0.113 0.060 0.508"* 0.060 -0.557

0.200 -0.252 0.060 -0.256 0.090 -0.462 0.110 -0.551

0.230 -0.359 0.090 -0.236 0.110 -0.404 0.140 -0.590

0.400 -0.098 0.130 -0.291 0.130 - 1.763"* 0.190 - 1.763"*

0.490 -0.139 0.150 -0.371 0.150 -0.398 0.250 -0.531

0.590 -0.215 0.200 -0.296 0.210 -0.417 0.400 -0.559

0.630 -0.238 0.250 -0.442 0.250 -0.493 0.490 -0.210

0.700 -0.352 0.260 -0.439 0.340 -0.567 0.580 -0.245

0.750 -0.185 0.280 -0.454 0.370 -0.518 0.650 -0.345

0.810 -0.163 0.290 -0.454 0.400 -0.441 0.700 -0.323

0.840 -0.166 0.310 -0.438 0.410 -0.727** 0.750 -0.410

0.900 -0.064 0.320 -0.452 0.430 -0.481 0.800 -0.564

0.960 0.049 0.340 -0.474 0.440 -0.347 0.830 -0.534

0.350 -0.392** 0.460 -0.256 0.900 -0.137

0.370 -0.478 0.490 -0.215 0.960 0.031

0.380 -0.504 0.500 -0.251

0.400 -0.442 0.520 -0.235

0.410 -0.490 0.540 -0.232

0.430 -0.449 0.550 -0.221

0.440 -0.389 0.580 -0.218

0.460 -0.244 0.600 -0.233

0.470 -0.208 0.610 -0.249

0.490 -0.174 0.650 -0.518

0.500 -0.168 0.700 -0.435

0.520 -0.162 0.750 -0.412

0.530 -0.171 0.820 -0.542

0.550 -0.201 0.890 -0.061

0.560 -0.198 0.900 -0.017

0.580 -0.184 0.960 0.074

0.590 -0.215

0.600 -0.211

0.640 -0.430

0.700 -0.391

0.750 -0.088**

0.820 -0.354

0.870 -0.230

0.930 -0.080

0.960 -0.015

Lower Surface

0.020 -0.849 0.020 -0.508 0.020 -0.345 0.020 0.291

0.110 -0.559 0.060 -0.157 0.060 -0.109 0.060 -0.084

0.230 -0.556 0.090 -0.229 0.090 -0.136 0.110 -0.099

0.400 -0.060 0.120 -0.314 0.120 -0.255 0.250 -0.426

0.490 -0.076 0.200 -0.592 0.200 -0.419 0.400 -0.296

0.630 1.328"* 0.260 -0.463 0_250 -0.462 0.490 -0.446

0.750 0.051 0.400 -0.501 0.400 -0.401 0.580 -0.586

0.850 0.123 0.490 -0.544 0.490 -0.160 0.650 -0.462

0.900 0.216 0.580 -0.088 0.580 -0.606 0.750 -0.011

0.960 0.203 0.640 0.047 0.650 -0.094 0.830 0.121

0.750 0.185 0.750 -0.087 0.900 0.270

0870 0.246 0.890 0.259 0.960 0.281

0.930 0.240 0.930 0.253

0.960 0.196 0.960 0.343

CN = 0.043 0.132 0.163 0.200

757
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-53-16-000, MINF = 0.897, Camber = 0/3, ALPT = 3.99, BETA = -0.04, QINF = 595.2,

RNPU = 4.5E+06, CNWP = 0.2007

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0,020 0,032 0.000 0.837 0,000 0.510"* 0.010 -0.613

0.060 -0.128 0.020 -0.202 0.020 -0,225 0.020 -0.679

0.110 -0.238 0,040 -0.156 0.060 0.502 ** 0.060 -0.590

0,200 -0.264 0.060 -0,309 0,090 -0.505 0.110 -0.602

0,230 -0,373 0,090 -0.251 0.110 -0.450 0.140 -0.628

0.400 -0.116 0.130 -0.302 0.130 - 1.777" * 0.190 - 1.777 * *

0.490 -0.159 0.150 -0.389 0.150 -0.441 0.250 -0,553

0.590 -0.221 0.200 -0.308 0.210 -0.459 0,400 -0.585

0.630 -0,244 0.250 -0.468 0.250 -0.548 0.490 -0,246

0.700 -0,365 0.260 -0.461 0,340 -0.576 0.580 -0.243

0,750 -0.451 0,280 -0,468 0.370 -0.571 0.650 -0,337

0.810 o0.291 0.290 -0.472 0.400 -0,441 0,700 -0,323

0,840 -0.254 0.310 -0.461 0.410 -0.730* * 0.750 -0.410

0.900 -0.076 0,320 -0,464 0.430 -0.497 0,800 -0.573

0,960 0,049 0.340 -0.492 0.440 -0.497 0.830 -0.535

0.350 -0.400** 0,460 -0,388 0.900 -0.135

0.370 -0,487 0,490 -0.202 0.960 0.023

0.380 -0.510 0.500 -0.236

0.400 -0.449 0.520 -0.217

0.410 -0,508 0.540 -0,216

0.430 -0.478 0.550 -0,207

0.440 -0.449 0.580 -0.216

0.460 -0.261 0,600 -0.213

0.470 -0.190 0.610 -0,223

0,490 -0.163 0,650 -0.539

0.500 -0.158 0.700 -0,436

0.520 -0.1 64 0,750 -0.418

0.530 -0.1 64 0.820 -0,573

0.550 -0,208 0.890 -0.083

0.560 -0.196 0.900 -0,046

0.580 -0.175 0.960 0.047

0.590 -0,215

0.600 -0.214

0.640 -0.435

0.700 -0.396

0.750 -0,080"*

0.820 -0,371

0.870 -0.302

0,930 -0. t 21

0,960 -0,055

Lower Surface

0.020 -0.846 0.020 -0.391 0,020 -0.212 0,020 0.315

0.110 -0,556 0.060 -0.153 0.060 -0,079 0.060 -0.081

0.230 -0.560 0,090 -0.232 0,090 -0.127 0.110 -0.091

0.400 -0.070 0,120 -0,310 0.120 -0.245 0,250 -0.412

0.490 -0.080 0,200 -0.583 0,200 -0.390 0.400 -0.331

0.630 1.346** 0,260 -0.424 0.250 -0,430 0.490 -0.443

0.750 0.063 0.400 -0,462 0,400 -0,409 0.580 -0,573

0.850 0.126 0.490 -0.161 0.490 -0.150 0.650 -0.324

0.900 0.219 0.580 -0.105 0.580 -0,597 0.750 0.048

0.960 0.204 0.640 0.059 0,650 -0.091 0,830 0.186

0.750 0.191 0.750 -0.084 0.900 0.289

0.870 0.262 0.890 0.306 0.960 0,273

0.930 0.234 0.930 0.267

0.960 0.198 0.960 0.339

CN = 0.079 0.194 0.200 0,240

758
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-53-20-000, MINF = 0.898, Camber = 0/2, ALPT = 4.98, BETA = 0.57, QINF = 597.1,

RNPU = 4.5E+06, CNWP = 0.2452

rl = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.079 0.000 0.872 0.000 0.484"* 0.010 -0.597

0.060 -0.293 0.020 -0.370 0.020 -0.359 0.020 -0.765

0.110 -0.302 0.040 -0.224 0.060 0.439"* 0.060 -0.721

0.200 -0.371 0.060 -0.463 0.090 -0.605 0.110 -0.695

0.230 -0.379 0.090 -0.466 0.110 -0.595 0.140 -0.732

0.400 -0.475 0.130 -0.479 0.130 - 1.771 ** 0.190 - 1.771 * *

0.490 -0.386 0.150 -0.470 0.150 -0.548 0.250 -0.758

0.590 -0.216 0.200 -0.401 0.210 -0.567 0.400 -0.625

0.630 -0.200 0.250 -0.550 0.250 -0.610 0.490 -0.474

0.700 -0.175 0.260 -0.545 0.340 -0.672 0.580 -0.402

0.750 -0.228 0.280 -0.569 0.370 -0.679 0.650 -0.455

0.810 -0.218 0.290 -0.561 0.400 -0.655 0.700 -0.438

0.840 -0.215 0.310 -0.534 0.410 -0.728** 0.750 -0.492

0.900 -0.089 0.320 -0.541 0.430 -0.668 0.800 -0.648

0.960 0.029 0.340 -0.563 0.440 -0.658 0.830 -0.618

0.350 -0.403** 0.460 -0.678 0.900 -0.078

0.370 -0.575 0.490 -0.625 0.960 0.016

0.380 -0.603 0.500 -0.624

0.400 -0.531 0.520 -0.570

0.410 -0.573 0.540 -0.564

0.430 -0.554 0.550 -0.546

0.440 -0.538 0.580 -0.539

0.460 -0.589 0.600 -0.527

0.470 -0.593 0.610 -0.507

0.490 -0.589 0.650 -0.618

0.500 -0.599 0.700 -0.519

0.520 -0.579 0.750 -0.488

0.530 -0.585 0.820 -0.415

0.550 -0.612 0.890 -0.035

0.560 -0.623 0.900 -0.001

0.580 -0.600 0.960 0.073

0.590 -0.641

0.600 -0.640

0.640 -0.651

0.700 -0.554

0.750 -0.088**

0.820 -0.161

0.870 -0.167

0.930 -0.026

0.960 0.037

Lower Surface

0.020 -0.545 0.020 -0.328 0.020 -0.077 0.020 0.328

0.110 -0.491 0.060 -0.080 0.060 -0.007 0.060 -0.080

0.230 -0.483 0.090 -0.165 0.090 -0.056 0.110 -0.016

0.400 -0.1 04 0.120 -0.243 0.120 -0.195 0.250 -0.287

0.490 -0.098 0.200 -0.424 0.200 -0.284 0.400 -0.316

0.630 1.342** 0.260 -0.346 0.250 -0.364 0.490 -0.412

0.750 0.050 0.400 -0.406 0.400 -0.372 0.580 -0.508

0.850 0.109 0.490 -0.133 0.490 -0.149 0.650 -0.297

0.900 0.206 0.580 -0.149 0.580 -0.489 0.750 0.087

0.960 0.185 0.640 0.048 0.650 -0.087 0.830 0.238

0.750 O. 196 0.750 -0.083 0.900 0.308

0.870 0.271 0.890 0.323 0.960 0.263

0.930 0.256 0.930 0.278

0.960 0.218 0.960 0.357

CN = 0.147 0.340 0.339 0.392

759
Table J-2. Continued.

Flight 211. Wing sweep = 26 °, Time = 11-53-26-500. MINF = 0.897. Camber = 0/2, ALPT = 7.14, BETA = 0.28. QINF = 595.2.

RNPU = 4.5E+06. CNWP = 0.3855

rl = 0.93 0.76 0.59 0.40

Upper Surface

x,/c CP x/c CP x/c CP x/c CP

0.020 -0.469 0.000 0.855 0.000 0.359** 0.010 -0.818

0.060 -0.545 0.020 -0.543 0.020 -0.682 0.020 -0.915

0. 110 -0.565 0.040 -0.541 0.060 0.263** 0.060 -0.934

0.200 -0.589 0.060 -0.660 0.090 -0.785 0.110 -0.856

0.230 -0.497 0.090 -0.663 0.110 -0.781 0.140 -0.887

0.400 -0.587 0.130 -0.695 0.130 - 1.777 * * 0.190 - 1.777 * *

0.490 -0.522 0.150 -0.696 0.150 -0.736 0.250 -0.920

0.590 -0.538" 0.200 -0.608 0.210 -0.747 0.400 -0.725

0.630 -0.470 0.250 -0.726 0.250 -0.799 0.490 -0.649

0.700 -0.551 0.260 -0.713 0.340 -0.841 0.580 -0.524

0.750 -0.152 0.280 -0.749 0.370 -0.839 0.650 -0.572

0.810 -0.157 0.290 -0.752 0.400 -0.817 0.700 -0.561

0.840 -0.163 0.310 -0.719 0.410 -0.730"* 0.750 -0.607

0.900 -0.119 0.320 -0.733 0.430 -0.859 0.800 -0.745

0.960 -0.014 0.340 -0.751 0.440 -0.832 0.830 -0.740

0.350 -0.408" * 0.460 -0.821 0.900 -0.165

0.370 -0.748 0.490 -0.775 0.960 -0.123

0.380 -0.793 0.500 -0.851

0.400 -0.727 0.520 -0.844

0.410 -0.770 0.540 -0.847

0.430 -0.742 0.550 -0.826

0.440 -0.713 0.580 -0.823

0.460 -0.771 0.600 -0.820

0.470 -0.765 0.610 -0.814

0.490 -0.754 0.650 -0.846

0.500 -0.766 0.700 -0.724

0.520 -0.750 0.750 -0.720

0.530 -0.746 0.820 -0.267

0.550 -0.774 0.890 -0.110

0.560 -0.784 0.900 -0.094

0.580 -0.760 0.960 -0.053

0.590 -0.807

0.600 -0.789

0.640 -0.823

0.700 -0.741

0.750 -0.089**

0.820 -0.154

0.870 -0.114

0.930 -0.080

0.960 -0.057

Lower Surface

0.020 -0.150 0.020 0.021 0.020 0.150 0.020 0.513

0.110 -0.333 0.060 0.069 0.060 0.145 0.060 -0.096

0.230 -0.224 0.090 -0.03 l 0.090 0.072 0.110 0.136

0.400 -0.131 0.120 -0.112 0.120 -0.075 0.250 -0.172

0.490 -0.121 0.200 -0.106 0.200 -0.129 0.400 -0.215

0.630 1.346** 0.260 -0.257 0.250 -0.201 0.490 -0.327

0.750 0.002 0.400 -0.263 0.400 -0.259 0.580 -0.444

0.850 0.059 0.490 -0.197 0.490 -0.132 0.650 -0.238

0.900 0.169 0.580 -0.191 0.580 -0.245 0.750 0.111

0.960 0.146 0.640 0.039 0.650 -0.099 0.830 0.260

0.750 0.176 0.750 -0.099 0.900 0.309

0.870 0.234 0.890 0.3 l 3 0.960 0.232

0.930 0.209 0.930 0.241

0.960 0.152 0.960 0.299

CN = 0.319 0.529 0.567 0.587

76O
Table J-2. Continued.

Flight 211, Wing sweep = 26", Time = 11-53-30-500, MINF = 0.897, Camber = 0/2, ALPT = 8.10, BETA = 0.19, QINF = 600.0,

RNPU = 4.6E+06, CNWP = 0.4332

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.590 0.000 0.830 0.000 0.292** 0.010 -0.879

0.060 -0.627 0.020 -0.735 0.020 -0.765 0.020 - 1.009

0.110 -0.655 0.040 -0.586 0.060 0.178"* 0.060 -0.998

0.200 -0.689 0,060 -0.729 0.090 -0.855 0.110 -0.945

0.230 -0.555 0.090 -0,754 0.110 -0.856 0.140 -0.966

0.400 -0.647 0.I 30 -0.765 0.130 - 1.775"* 0.190 - 1.775"*

0.490 -0.584 0.150 -0.777 0.150 -0.811 0.250 - 1.007

0.590 -0.588 0.200 -0.708 0.210 -0.829 0.400 -0.764

0.630 -0.533 0.250 -0,780 0.250 -0.854 0.490 -0.662

0.700 -0,624 0.260 -0.769 0.340 -0.907 0.580 -0.585

0.750 -0.125 0.280 -0.808 0.370 -0.904 0.650 -0.628

0.810 -0.128 0.290 -0,808 0.400 -0.882 0.700 -0.599

0.840 -0.133 0.310 -0.780 0.410 -0,736"* 0.750 -0.639

0.900 -0.136 0.320 -0.786 0.430 -0.918 0.800 -0.751

0.960 -0.033 0.340 -0.813 0.440 -0.900 0.830 -0.767

0.350 -0.418"* 0.460 -0.827 0,900 -0.210

0.370 -0.805 0.490 -0.846 0.960 -0.160

0.380 -0.854 0.500 -0.917

0.400 -0.789 0.520 -0.910

0.410 -0.838 0.540 -0.920

0.430 -0.814 0.550 -0.890

0.440 -0.789 0.580 -0.875

0,460 -0,846 0.600 -0.883

0.470 -0.841 0.610 -0.866

0.490 -0.824 0.650 - 1.033

0,500 -0.828 0,700 -0.910

0.520 -0.819 0.750 -0.830

0.530 -0.808 0,820 -0,249

0.550 -0.842 0.890 -0.162

0.560 -0.846 0.900 -0.154

0.580 -0.822 0.960 -0,099

0.590 -0.861

0.600 -0.851

0.640 -0.380

0.700 -0.303

0,750 -0,087"*

0,820 -0.199

0.870 -0.185

0.930 -0.173

0.960 -0.158

Lower Surface

0,020 -0,071 0.020 0.136 0.020 0.237 0.020 0.633

0.110 -0,245 0.060 0.146 0.060 0.203 0.060 -0.092

0.230 -0.190 0.090 0.035 0.090 0.127 0.110 0.199

0.400 -0.146 0.120 -0.054 0.120 -0.025 0.250 -0.120

0.490 -0.1 44 0,200 -0.068 0.200 -0.021 0.400 -0.178

0.630 1.324"* 0.260 -0.205 0.250 -0.149 0.490 -0.280

0.750 -0.030 0.400 -0,243 0.400 -0.210 0.580 -0.398

0.850 0.030 0.490 -0.204 0.490 -0.113 0.650 -0.267

0.900 0.139 0.580 -0.217 0.580 -0.361 0.750 0.117

0.960 0.132 0.640 0.011 0.650 -0.092 0.830 0.26 l

0.750 0.148 0.750 -0.110 0,900 0.309

0.870 0.205 0.890 0.291 0.960 0.226

0.930 0.159 0.930 0.220

0.960 0,100 0.960 0.276

CN = 0.365 0.533 0.647 0.662

761
Table J-2. Continued.

Flight 211, Wing sweep = 26", Time = 11-53-32-000, MINF = 0,902, Camber = 0/2, ALPT = 8.11, BETA = 1.18, QINF = 610.3,

RNPU = 4.6E+06o CNWP = 0.4627

-q = 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 -0.600 0.000 0.847 0.000 0.303 * * 0.010 -0.885

0.060 -0.637 0.020 -0.737 0.020 -0.765 0.020 - 1.007

0.110 -0.677 0.040 -0.597 0.060 0.147"* 0.060 -0.985

0.200 -0.707 0.060 -0.729 0.090 -0.860 0.110 -0.962

0.230 -0.596 0.090 -0,759 0.110 -0.864 0.140 -0.981

0.400 -0.656 0.130 -0.776 0.130 - 1.757"* 0.190 -1.757"*

0.490 -0.604 0. i 50 -0.784 0.150 -0.819 0.250 - 1.020

0.590 -0.602 0.200 -0.718 0.210 -0.826 0.400 -0.780

0.630 -0.549 0.250 -0.790 0.250 -0.865 0.490 -0.674

0.700 -0.638 0.260 -0.777 0.340 -0.911 0.580 -0.611

0.750 -0.118 0.280 -0.812 0.370 -0.913 0.650 -0.630

0.810 -0.108 0.290 -0.821 0.400 -0.889 0.700 -0.616

0.840 -0.106 0.310 -0.790 0.410 -0.735** 0.750 -0.644

0.900 -0. ! 23 0.320 -0.797 0.430 -0.922 0.800 -0.753

0.960 -0.033 0.340 -0.812 0.440 -0.904 0.830 -0.768

0.350 -0,415"* 0.460 -0.825 0.900 -0.238

0.370 -0.813 0.490 -0.869 0.960 -0.197

0.380 -0.860 0.500 -0.920

0.400 -0.792 0.520 -0.916

0.410 -0.842 0,540 -0.915

0.430 -0.817 0,550 -0,898

0.440 -0.794 0.580 -0.898

0.460 -0.859 0.600 -0.899

0.470 -0.841 0.610 -0,889

0.490 -0.833 0.650 - 1.055

0.500 -0.845 0.700 -0,937

0.520 -0.821 0.750 -0.938

0.530 -0.818 0.820 -0.312

0.550 -0.851 0.890 -0.207

0.560 -0.858 0.900 -0.221

0.580 -0.832 0.960 -0.163

0.590 -0,876

0.600 -0.858

0.640 -0.346

0.700 -0,288

0.750 -0.094**

0.820 -0.221

0.870 -0.237

0.930 -0.218

0.960 -0.198

Lower Surface

0.020 -0.005 0.020 0.173 0.020 0.267 0.020 0.652

0.110 -0.226 0.060 0.165 0.060 0.231 0,060 -0.102

0.230 -0.217 0.090 0.053 0.090 0.146 0.110 0.220

0.400 -0.161 0.120 -0.036 0.120 -0.004 0.250 -0.102

0.490 -0.168 0.200 -0.057 0.200 0.001 0,400 -0.162

0.630 1.289'* 0.260 -0.199 0,250 -0.130 0.490 -0.273

0.750 -0.066 0.400 -0.249 0.400 -0.197 0,580 -0.386

0.850 0.002 0.490 -0.293 0.490 -0.123 0.650 -0.604

0.900 0.115 0.580 -0.261 0.580 -0.417 0.750 0.110

0.960 0.121 0,640 -0.022 0.650 -0.098 0.830 0.258

0.750 0,125 0.750 -0.120 0.900 0.305

0.870 0.183 0.890 0.269 0.960 0.217

0.930 0.139 0,930 0.197

0.960 0.073 0.960 0.247

CN = 0.357 0.526 0.670 0,651

762
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-48-2-000, MINF = 0.901, Camber = 10/2, ALPT = 4.00, BETA = 0.63, QINF = 599.9,

RNPU = 4.6E+06, CNWP = 0.2434

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 0.626 0.000 0.148 0.000 0.272** 0.010 0.473

0.060 0.175 0.020 0.585 0.020 0.655 0.020 0.329

0.110 -0.120 0.000 0.465 0.060 0.971 ** 0.060 -0,167

0.200 -0.842 0.060 0.109 0.090 -0.116 0.110 -0.470

0.230 -0.746 0.090 -0.092 0.110 -0.330 0.140 -0.866

0.400 -0.623 0.130 -0.327 0.130 - 1.759** 0.190 - 1.759"*

0.490 -0.494 0.150 -0.611 0.150 -0.750 0.250 -0.680

0.590 -0.078 0.200 -0.683 0.210 -0.744 0.400 -0.609

0.630 -0.107 0.250 -0.723 0.250 -0.728 0.490 -0.325

0.700 -0.108 0.260 -0.691 0.340 -0,718 0.580 -0.315

0.750 -0.184 0.280 -0.697 0.370 -0.718 0.650 -0.368

0.810 -0.184 0.290 -0.684 0.400 -0.699 0.700 -0.349

0.840 -0.177 0.310 -0.647 0.410 -0.549** 0.750 -0.432

0.900 -0.077 0.320 -0.657 0.430 -0.691 0.800 -0.611

0.960 0.032 0.340 -0.659 0.440 -0.674 0.830 -0.569

0.350 -0.479** 0.460 -0.686 0.900 -0.171

0.370 -0.652 0.490 -0,558 0.960 -0.022

0,380 -0.685 0.500 -0.498

0.400 -0.609 0.520 -0.360

0.410 -0.650 0.540 -0.314

0.430 -0.624 0.550 -0.277

0.440 -0.585 0.580 -0.260

0.460 -0.661 0.600 -0.264

0.470 -0.652 0.610 -0.280

0.490 -0.638 0.650 -0.551

0.500 -0.638 0.700 -0.454

0.520 -0.623 0.750 -0.451

0.530 -0.614 0.820 -0.590

0.550 -0.644 0.890 -0.040

0.560 -0.636 0.900 0.002

0.580 -0.624 0.960 0.074

0.590 -0.652

0.600 -0.619

0.640 -0.492

0.700 -0.433

0.750 -0.091 **

0.820 -0.151

0.870 -0.147

0.930 -0.020

0.960 0.039

Lower Surface

0.020 -0.865 0.020 -0.976 0.020 - 1.376 0.020 -0.774

0.110 -0.758 0.060 - 1.007 0.060 -0.937 0.060 -0.091

0.230 -0.409 0.090 -0.832 0.090 -0.684 0.110 -0.384

0.400 -0.246 0.120 -0.936 0.120 -0.561 0.250 -0.361

0.490 -0.135 0.200 -0.291 0.200 -0.256 0.400 -0.368

0.630 1.139** 0,260 -0.291 0.250 -0.282 0.490 -0.421

0.750 0.024 0.400 -0.287 0.400 -0.362 0.580 -0.529

0.850 0.074 0.490 -0.185 0,490 -0.156 0.650 -0.763

0.900 0.127 0.580 -0.137 0.580 -0.559 0.750 0.023

0.960 0.139 0.640 0.037 0.650 -0.101 0.830 0.187

0.750 0.175 0.750 -0.094 0.900 0.282

0.870 0.232 0.890 0.271 0.960 0.261

0.930 0.233 0.930 0.240

0,960 0.201 0.960 0.334

CN = 0.108 0.207 0.204 0,184

763
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-48-23-500, MINF = 0.892, Camber = 10/2, ALPT = 5.96, BETA = 0.34, QINF = 588.0,

RNPU = 4.5E+06, CNWP = 0.3356

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.562 0.000 0.291 0.000 0.295** 0.010 0.317

0.060 O. 113 0.020 0.504 0.020 0.548 0.020 O. 160

O. 110 -0.219 0.040 0.377 0.060 0.833 * * 0.060 -0.363

0.200 -0.923 0.060 0.006 0.090 -0.226 0.110 -0.658

0.230 -0.832 0.090 -0.182 0.110 -0.438 0.140 -0.984

0.400 -0.706 0.130 -0.433 0.130 - 1.796** 0.190 - 1.796**

0.490 -0.544 0.150 -0.704 0.150 -0.846 0.250 -0.965

0.590 -0.534 0.200 -0.777 0.210 -0.859 0.400 -0.691

0.630 -0.301 0.250 -0.846 0.250 -0.864 0.490 -0.584

0.700 -0.129 0.260 -0.807 0.340 -0.864 0.580 -0.454

0.750 -0.156 0.280 -0.829 0.370 -0.855 0.650 -0.501

0.810 -0.163 0.290 -0.826 0.400 -0.835 0.700 -0.476

0.840 -0.151 0.310 -0.774 0.410 -0.561 ** 0.750 -0.534

0.900 -0.089 0.320 -0.792 0.430 -0.875 0.800 -0.698

0.960 0.004 0.340 -0.792 0.440 -0.840 0.830 -0.664

0.350 -0.438 ** 0.460 -0.806 0.900 -0.135

0.370 -0.779 0.490 -0.802 0.960 -0.073

0.380 -0.831 0.500 -0.870

0.400 -0.764 0.520 -0.852

0.410 -0.804 0.540 -0.854

0.430 -0.776 0.550 -0.832

0.440 -0.742 0.580 -0.814

0.460 -0.805 0.600 -0.794

0.470 -0.786 0.610 -0.738

0.490 -0.773 0.650 -0.733

0.500 -0.787 0.700 -0.604

0.520 -0.761 0.750 -0.572

0.530 -0.769 0.820 -0.445

0.550 -0.796 0.890 -0.060

0.560 -0.802 0.900 -0.020

0.580 -0.772 0.960 0.038

0.590 -0.814

0.600 -0.805

0,640 -0.841

0.700 -0.872

0.750 -0.081 **

0.820 -0.161

0.870 -0.086

0.930 -0.014

0.960 0.020

Lower Surface

0.020 -0.757 0.020 - 1.011 0.020 -0.942 0.020 -0.518

0.110 -0.542 0.060 - 1.002 0.060 -0.519 0.060 -0.079

0.230 -0.151 0.090 -0.459 0.090 -0.303 0. I 10 -0.171

0.400 -0.088 0.120 -0.133 0.120 -0.228 0.250 -0.170

0.490 -0.059 0.200 -0.110 0.200 -0.1 [9 0.400 -0.244

0.630 1.161"* 0.260 -0.124 0.250 -0.141 0.490 -0.354

0.750 0.030 0.400 -0.167 0.400 -0.277 0,580 -0.480

0.850 0.085 0.490 -0.160 0.490 -0.112 0.650 -0.177

0.900 0.177 0.580 -0.134 0.580 -0.234 0.750 0.098

0.960 0.167 0.640 0.059 0.650 -0.089 0.830 0.248

0.750 0.163 0.750 -0.089 0.900 0.302

0.870 0.220 0.890 0.294 0.960 0.229

0.930 0.211 0.930 0.236

0.960 0.179 0.960 0.329

CN = 0.295 0.437 0.465 0.460

764
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-48-28-000, MINF = 0.895, Camber = 10/2, ALPT = 7.01, BETA = 0.25, QINF = 590.4,

RNPU = 4.5E+06, CNWP = 0.3709

11= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x./c CP x/c CP x/c CP

0.020 0.532 0.000 0.326 0.000 0.287** 0.010 0.233

0.060 0.071 0.020 0.439 0.020 0.505 0.020 0.108

0.110 -0.251 0.040 0.344 0.060 0.771 ** 0.060 -0.429

0.200 -0.935 0.060 -0.021 0.090 -0.264 O. 110 -0.719

0.230 -0.857 0.090 -0.212 O. 110 -0.460 O. 140 - 1.025

0.400 -0.738 0.130 -0.457 0.130 -1.785** 0.190 -1.785"*

0.490 -0.590 O. 150 -0.722 O. 150 -0.864 0.250 -0.987

0.590 -0.578 0.200 -0.801 0.210 -0.880 0.400 -0.709

0.630 -0.493 0.250 -0.871 0.250 -0.887 0.490 -0.633

0.700 -0.142 0.260 -0.831 0.340 -0.895 0.580 -0.509

0.750 -0.145 0.280 -0.863 0.370 -0.895 0.650 -0.542

0.810 -0.155 0.290 -0.854 0.400 -0.869 0.700 -0.523

0.840 -0.151 0.310 -0.810 0.410 -0.555** 0.750 -0.572

0.900 -0.099 0.320 -0.823 0.430 -0.910 0.800 -0.716

0.960 -0.007 0.340 -0.828 0.440 -0.887 0.830 -0.690

0.350 -0.445** 0.460 -0.799 0.900 -0.170

0.370 -0.814 0.490 -0.852 0.960 -0.118

0.380 -0.865 0.500 -0.904

0.400 -0.785 0.520 -0.896

0.410 -0.844 0.540 -0.895

0.430 -0.810 0.550 -0.868

0.440 -0.784 0.580 -0.855

0.460 -0.854 0.600 -0.855

0.470 -0.833 0.610 -0.838

0.490 -0.818 0.650 -0.866

0.500 -0.822 0.700 -0.758

0.520 -0.808 0.750 -0.719

0.530 -0.796 0.820 -0.323

0.550 -0.826 0.890 -0.100

0.560 -0.839 0.900 -0.072

0.580 -0.813 0.960 -0.025

0.590 -0.846

0.600 -0.843

0.640 -0.827

0.700 -0.385

0.750 -0.079"*

0.820 -0.214

0.870 -0.169

0.930 -0.143

0.960 -0.129

Lower Surface

0.020 -0.738 0.020 -0.716 0.020 -0.854 0.020 -0.405

0.110 -0.527 0.060 -0.494 0.060 -0.390 0.060 -0.067

0.230 -0.114 0.090 -0.452 0.090 -0.166 0.110 -0.095

0.400 -0.067 0.120 -0.302 0.120 -0.1 44 0.250 -0.129

0.490 -0.051 0.200 -0.100 0.200 -0.119 0.400 -0.214

0.630 1.160"* 0.260 -0.138 0.250 -0.114 0.490 -0.338

0.750 0.014 0.400 -0.136 0.400 -0.252 0.580 -0.448

0.850 0.068 0.490 -0.153 0.490 -0.119 0.650 -0.199

0.900 0.171 0.580 -0.149 0.580 -0.248 0.750 0.106

0.960 0.167 0.640 0.034 0.650 -0.085 0.830 0.255

0.750 0.141 0.750 -0.070 0.900 0.307

0.870 0.192 0890 0.282 0.960 0.229

0.930 O. 164 0.930 0.227

0.960 O. 118 0.960 0.310

CN = 0.333 0.446 0.526 0.519

765
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-48-29-000, MINF = 0.897, Camber = 1012, ALPT = 7.02, BETA = 0.34, Q1NF = 592.9,

RNPU = 4.5E+06, CNWP = 0.3783

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.534 0.000 0.344 0.000 0.279** 0.010 0.237

0.060 0.081 0.020 0.495 0.020 0.507 0.020 0.103

0.110 -0.238 0.040 0.339 0.060 0.764** 0.060 -0.437

0.200 -0.924 0.060 -0.021 0.090 -0.265 0.110 -0.721

0.230 -0.877 0.090 -0.210 0.110 -0.458 0.140 - 1.020

0.400 -0.734 0.130 -0.455 0.130 - 1.777"* 0.190 - 1.777"*

0.490 -0.603 0.150 -0.717 0.150 -0.860 0.250 -0.982

0.590 -0.585 0.200 -0.797 0.210 -0.873 0.400 -0.709

0.630 -0.506 0.250 -0.861 0.250 -0.881 0.490 -0.630

0.700 -0.155 0.260 -0.830 0.340 -0.891 0.580 -0.501

0.750 -0.123 0.280 -0.863 0.370 -0.895 0.650 -0.539

0.810 -0.129 0.290 -0.854 0.400 -0.869 0.700 -0.52 l

0.840 -0.125 0.310 -0.809 0.410 -0.552 ** 0.750 -0.573

0.900 -0.090 0.320 -0.824 0.430 -0.901 0.800 -0.713

0.960 0.004 0.340 -0.828 0.440 -0.888 0.830 -0.686

0.350 -0.440** 0.460 -0.795 0.900 -0.171

0.370 -0.8 t 2 0.490 -0.840 0.960 -0.121

0.380 -0.861 0.500 -0.907

0.400 -0.787 0.520 -0.892

0.410 -0.840 0.540 -0.891

0.430 -0.820 0.550 -0.870

0.440 -0.785 0.580 -0.856

0.460 -0.856 0.600 -0.857

0.470 -0.832 0.610 -0.830

0.490 -0.827 0.650 -0.866

0.500 -0.821 0.700 -0.771

0.520 -0.809 0.750 -0.734

0.530 -0.799 0.820 -0.323

0.550 -0.827 0.890 -0.099

0.560 -0.835 0.900 -0.074

0.580 -0.813 0.960 -0.023

0.590 -0.851

0.600 -0.842

0.640 -0.813

0.700 -0.374

0.750 -0.078**

0.820 -0.222

0.870 -0.181

0.930 -0.142

0.960 -0.126

Lower Surface

0.020 -0.818 0.020 -0.699 0.020 -0.835 0.020 -0.390

0.110 -0.507 0.060 -0.484 0.060 -0.369 0.060 -0.074

0.230 -0.090 0.090 -0.432 0.090 -0.143 0. I 10 -0,079

0.400 -0.059 0.120 -0.289 0.120 -0.126 0.250 -0.122

0.490 -0.075 0.200 -0.096 0.200 -0.111 0.400 -0.205

0.630 1.156"* 0.260 -0.126 0.250 -0.108 0.490 -0.332

0.750 0.009 0.400 -0.141 0.400 -0.246 0.580 -0.446

0.850 0.060 0.490 -0.156 0.490 -0.118 0.650 -0.262

0.900 0.1 64 0.580 -0.165 0.580 -0.250 0.750 0.106

0.960 0.158 0.640 0.025 0.650 -0.084 0.830 0.258

0.750 0.137 0.750 -0.077 0.900 0.310

0.870 0.182 0.890 0.277 0.960 0.231

0.930 0.158 0.930 0.223

0.960 0.1 l I 0.960 0.311

CN = 0.332 0.442 0.529 0.517

766
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-48-36-000, MINF = 0.902, Camber = 10/2, ALPT = 7.92, BETA = 0.40, QINF = 606.0,

RNPU = 4.6E+06, CNWP = 0.4400

r] = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.495 0.000 0.425 0.000 0.289** 0.010 0.151

0.060 0.035 0,020 0,422 0.020 0.437 0.020 0.029

0.110 -0.277 0.040 0.289 0.060 0,682** 0.060 -0.485

0.200 -0.948 0.060 -0.067 0.090 -0.301 0.110 -0.803

0.230 -0.910 0.090 -0.243 0.110 -0.508 0.140 - 1.071

0.400 -0.767 0.130 -0.493 0.130 - 1.754* * 0.190 - 1.754 **

0.490 -0.652 0.150 -0.745 0.150 -0.886 0.250 - 1.062

0,590 -0.630 0.200 -0.823 0.210 -0.909 0.400 -0.764

0.630 -0.573 0.250 -0.902 0.250 -0.920 0.490 -0.641

0.700 -0.459 0.260 -0.871 0.340 -0.939 0.580 -0.573

0.750 -0.159 0.280 -0.899 0.370 -0.942 0.650 -0.593

0.810 -0.149 0.290 -0.899 0,400 -0.917 0.700 -0.576

0.840 -0.147 0.310 -0.857 0.410 -0,556"* 0,750 -0.615

0.900 -0.140 0.320 -0.870 0.430 -0.964 0.800 -0.737

0.960 -0.045 0.340 -0.862 0.440 -0.938 0.830 -0,728

0.350 -0.454** 0.460 -0.794 0.900 -0,265

0.370 -0.856 0.490 -0.897 0.960 -0.198

0.380 -0.908 0.500 -0.950

0.400 -0.840 0.520 -0.947

0.410 -0.885 0,540 -0.948

0.430 -0.862 0.550 -0.928

0.440 -0.834 0.580 -0.922

0.460 -0.900 0.600 -0.926

0.470 -0.884 0.610 -0.908

0.490 -0.871 0.650 - 1.074

0.500 -0.878 0.700 -0.955

0.520 -0.864 0.750 -0.964

0.530 -0.853 0.820 -0.319

0.550 -0.878 0,890 -0.208

0.560 -0.882 0.900 -0.201

0.580 -0,860 0.960 -0.1 44

0.590 -0.891

0,600 -0.883

0.640 -0.394

0.700 -0.311

0.750 -0.099**

0.820 -0.235

0.870 -0.220

0.930 -0.224

0.960 -0.231

Lower Surface

0.020 -0.789 0.020 -0.574 0.020 -0,617 0.020 -0.181

0.110 -0.453 0.060 -0.363 0.060 -0.125 0.060 -0.088

0.230 -0.091 0.090 -0.288 0.090 0.013 0.110 0.003

0.400 -0.077 0.120 -0.133 0.120 -0.065 0.250 -0,074

0.490 -0.120 0.200 -0.089 0.200 -0.098 0.400 -0.169

0.630 1.115 ** 0.260 -0.068 0.250 -0.070 0.490 -0.293

0.750 -0.055 0.400 -0.159 0.400 -0.202 0.580 -0.412

0.850 0.003 0.490 -0.183 0.490 -0.127 0.650 -0.570

0.900 O.111 0.580 -0.204 0.580 -0.4 l 5 0.750 O. 103

0.960 O. 106 0.640 -0.004 0.650 -0.098 0.830 0.250

0.750 O. 114 0.750 -0.084 0.900 0.309

0.870 O. 154 0.890 0.263 0.960 0.217

0.930 0.110 0.930 0.195

0.960 0.042 0.960 0.287

CN = 0.362 0.457 0.615 0.570

767
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-48-38-500, MINF = 0.905, Camber = 10/2, ALPT = 8.01, BETA = 0.40, Q1NF = 613.1,

RNPU = 4.6E+06o CNWP = 0.4479

= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.497 0.000 0.428 0.000 0.274"* 0.010 0.148

0.060 0.035 0.020 0.422 0.020 0.424 0,020 0.024

0.110 -0.266 0.040 0.285 0.060 0.631 ** 0.060 -0.514

0.200 -0.945 0.060 -0.070 0.090 -0.304 0.110 -0.798

0.230 -0.904 0.090 -0.244 0.110 -0.502 0.140 - 1.058

0.400 -0.766 0.130 -0.489 0.130 - 1.745"* 0.190 - 1.745" *

0.490 -0.658 0.150 -0.742 0.150 -0.880 0.250 - 1.076

0.590 -0.642 0.200 -0.818 0.210 -0.903 0.400 -0.766

0.630 -0.578 0.250 -0.902 0.250 -0.917 0.490 -0.643

0.700 -0.624 0.260 -0.869 0.340 -0.940 0.580 -0.581

0.750 -0.152 0.280 -0.897 0.370 -0.939 0.650 -0.601

0.810 -0.141 0.290 -0.901 0.400 -0.918 0.700 -0.579

0.840 -0.135 0.310 -0.854 0.410 -0.561"* 0.750 -0.613

0.900 -0.144 0.320 -0.866 0.430 -0.958 0.800 -0.729

0.960 -0.050 0.340 -0.867 0.440 -0.939 0.830 -0.724

0.350 -0.456** 0.460 -0.796 0.900 -0.289

0.370 -0.855 0.490 -0.895 0.960 -0.216

0.380 -0.908 0.500 -0.957

0.400 -0.840 0.520 -0,940

0.410 -0.882 0.540 -0.948

0.430 -0.856 0.550 -0.927

0.440 -0.831 0.580 -0.924

0.460 -0.900 0.600 -0.928

0.470 -0.881 0.610 -0.902

0.490 -0.869 0.650 - 1.060

0.500 -0.877 0.700 -0.967

0.520 -0.858 0.750 -0.974

0.530 -0.854 0.820 -0.349

0.550 -0.881 0.890 -0.216

0.560 -0.882 0.900 -0.226

0.580 -0.861 0.960 -0.160

0.590 -0.897

0.600 -0.877

0.640 -0.442

0.700 -0.346

0.750 -0.106"*

0.820 -0.255

0.870 -0.247

0.930 -0.235

0.960 -0.227

Lower Surface

0.020 -0.749 0.020 -0.555 0.020 -0.598 0.020 -0.140

0.110 -0.442 0.060 -0.346 0.060 -0.096 0.060 -0.091

0,230 -0.090 0.090 -0.269 0.090 0.026 0.110 0.018

0.400 -0.073 0.120 -0.109 0.120 -0.053 0.250 -0.066

0.490 -0.131 0.200 -0.089 0.200 -0.104 0.400 -0.161

0.630 1.091 ** 0.260 -0.064 0.250 -0.065 0.490 -0.290

0.750 -0.058 0.400 -0.163 0.400 -0.194 0.580 -0.407

0.850 -0.003 0.490 -0.186 0.490 -0.132 0.650 -0.626

0.900 0.110 0.580 -0.209 0.580 -0.418 0.750 0.102

0.960 0.103 0.640 -0.005 0.650 -0.108 0.830 0.251

0.750 0.105 0.750 -0.094 0.900 0.303

0.870 0.152 0.890 0.263 0.960 0.217

0.930 0.1 04 0.930 0.192

0.960 0.037 0.960 0.262

CN = 0.370 0.465 0.618 0.574

768
TabLe J-2, Continued.

Flight 211, Wing sweep = 26 °, Time = 11-48-46-000, MINF = 0.908, Camber = 10/2, ALPT = 9.13, BETA = 0.19, QINF = 634.3,

RNPU = 4.8E÷06, CNWP = 0.4844

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x,/c CP x/c CP x/c CP

0.020 0.451 0.000 0.522 0.000 0.300"* 0.010 0.032

0.060 -0.006 0.020 0.336 0.020 0.351 0.020 -0.054

0.1 l0 -0.303 0.040 0.231 0.060 0.526** 0.060 -0.574

0.200 -0.967 0.060 -0.122 0.090 -0.415 O. 110 -0.864

0.230 -0.913 0.090 -0.295 O. 110 -0.563 O. 140 - 1.108

0.400 -0.794 O. 130 -0.526 O. 130 - 1.732"* O. 190 - 1.732"*

0.490 -0.697 0.150 -0.768 0.150 -0.909 0.250 - I. 133

0.590 -0.689 0.200 -0.849 0.210 -0.930 0.400 -0.827

0.630 -0.624 0.250 -0.932 0.250 -0.948 0.490 -0.679

0.700 -0.662 0.260 -0.899 0.340 -0.983 0.580 -0.619

0.750 -0.218 0.280 -0.930 0.370 -0.985 0.650 -0.642

0.810 -0.191 0.290 -0.939 0.400 -0.950 0.700 -0.626

0.840 -0.170 0.310 -0.880 0.410 -0.587"* 0.750 -0.634

0.900 -0.191 0.320 -0.906 0.430 - 1.000 0.800 -0.730

0.960 -0.120 0.340 -0.914 0.440 -0.982 0.830 -0.722

0.350 -0.449"* 0.460 -0.815 0.900 -0.386

0.370 -0.897 0.490 -0.951 0.960 -0.230

0.380 -0.947 0.500 -0.997

0.400 -0.871 0.520 -0.990

0.410 -0.896 0.540 -0.992

0.430 -0.900 0.550 -0.972

0.440 -0.848 0.580 -0.969

0.460 -0.944 0.600 -0.981

0.470 -0.922 0.610 -0.966

0.490 -0.911 0.650 - 1.104

0.500 -0.925 0.700 -0.994

0.520 -0.906 0.750 -0.765

0.530 -0.899 0.820 -0.476

0.550 -0.925 0.890 -0.382

0.560 -0.926 0.900 -0.382

0.580 -0.907 0.960 -0.317

0.590 -0.941

0.600 -0.928

0.640 -0.362

0.700 -0.347

0.750 -0.115"*

0.820 -0.302

0.870 -0.296

0.930 -0.292

0.960 -0.283

Lower Surface

0.020 -0.824 0.020 -0.427 0.020 -0.383 0.020 0.109

0.110 -0.163 0.060 -0.154 0.060 0.132 0.060 -0.113

0.230 -0.059 0.090 -0.077 0.090 0.097 0.110 0.095

0.400 -0.1 04 0.120 0.027 0.120 0.007 0.250 -0.014

0.490 -0.155 0.200 -0.061 0.200 -0.081 0.400 -0.119

0.630 1.009"* 0.260 -0.022 0.250 -0.018 0.490 -0.245

0.750 -0.111 0.400 -0.138 0.400 -0.154 0.580 -0.374

0.850 -0.070 0.490 -0.179 0.490 -0.130 0.650 -0.560

0.900 0.037 0.580 -0.228 0.580 -0.374 0.750 0.116

0.960 0.030 0.640 -0.017 0.650 -0.118 0.830 0.261

0.750 O. 103 0.750 -0.116 0.900 0.304

0.870 0.151 0.890 0.257 0.960 0.207

0.930 0.086 0.930 0.182

0.960 0.011 0.960 0.233

CN = 0.416 0.527 0.697 0.652

769
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-45-23-500, MINF = 0,896, Camber = 5/10, ALPT = 3.20, BETA = 0.17, QINF = 596.0,

RNPU = 4.5E+06, CNWP = 0.1808

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.463 0.000 0.488 0.000 0.370'* 0.010 0.156

0.060 0.129 0.020 0.363 0.020 0.413 0.020 0.067

0.110 -0.144 0.040 0.311 0.060 0.885"* 0.060 -0.265

0.200 -0.601 0,060 0.029 0.090 -0.140 0.110 -0.395

0.230 -0.479 0.090 -0.105 0.110 -0.298 0.140 -0.690

0.400 -0.159 0.130 -0.264 0.130 - 1.778 * * 0.190 - 1.778" *

0,490 -0.149 0.150 -0.457 0.150 -0.578 0.250 -0.534

0.590 -0.204 0.200 -0.489 0.210 -0.582 0.400 -0.247

0.630 -0.227 0.250 -0.526 0.250 -0.562 0.490 -0.229

0.700 -0.351 0.260 -0.503 0.340 -0.186 0.580 -0.245

0.750 -0.791 0.280 -0.491 0.370 -0.193 0.650 -0.321

0.810 -0.679 0.290 -0.361 0.400 -0.196 0.700 -0.301

0.840 -0.740 0.310 -0.192 0.410 -0.560* * 0.750 -0.391

0.900 -0.279 0.320 -0.180 0.430 -0.236 0.800 -0.953

0.960 -0.288 0.340 -0.168 0,440 -0.236 0.830 -0.917

0.350 -0.256** 0.460 -0.224 0.900 -0.428

0.370 -0.184 0.490 -0.191 0.960 -0,430

0.380 -0.214 0.500 -0.250

0.400 -0.186 0.520 -0.239

0.410 -0.264 0.540 -0.246

0.430 -0.251 0.550 -0.232

0.440 -0.239 0.580 -0.231

0.460 -0.297 0.600 -0.243

0.470 -0.279 0.610 -0.252

0.490 -0.252 0.650 -0.546

0.500 -0.218 0.700 -0.455

0.520 -0.215 0.750 -0.445

0.530 -0.229 0.820 -0.950

0.550 -0.267 0.890 -0.487

0.560 -0.259 0.900 -0.495

0.580 -0.230 0.960 -0.476

0.590 -0.250

0.600 -0.252

0.640 -0.469

0.700 -0.414

0.750 -0.099**

0.820 -0.530

0.870 -0.402

0.930 -0.328

0.960 -0.339

Lower Surface

0.020 - 1,262 0.020 -0,967 0.020 - 1.093 0.020 -0.351

0.110 -0.610 0.060 -0.963 0.060 -0.812 0.060 -0.069

0.230 -0.287 0,090 -0.822 0.090 -0.434 0.110 -0.306

0.400 0.060 0.120 -0.769 0.120 -0.467 0.250 -0.421

0.490 0.075 0.200 -0.364 0.200 -0.293 0.400 -0.367

0.630 I. 139 ** 0.260 -0.298 0.250 -0.418 0,490 -0.439

0.750 0.186 0.400 -0.043 0.400 -0.357 0,580 -0.173

0.850 0.229 0.490 -0.010 0.490 -0.113 0.650 0.062

0.900 0.317 0.580 0.060 0.580 -0.007 0.750 0.273

0.960 0.145 0.640 0.280 0.650 -0.112 0.830 0.385

0.750 0.323 0.750 -0.063 0.900 0.458

0.870 0.385 0.890 0.430 0.960 0.357

0.930 0,320 0.930 0.357

0.960 0.215 0.960 0.365

CN = 0.280 0,249 0.231 0.315

770
Table J-2. Continued,

Flight 211, Wing sweep = 26 °, Time = 11-45-51-500, MINF = 0.899, Camber = 5/11, ALPT -- 4.09, BETA = -0.10, QINF = 596.2,

RNPU = 4.5E+06, CNWP = 0.3033

rl = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0,428 0.000 0.545 0,000 0,396"* 0,010 0,056

0.060 0.081 0,020 0.321 0.020 0.356 0,020 -0.019

0.110 -0.183 0,040 0.273 0,060 0.838** 0.060 -0.359

0.200 -0.668 0.060 -0,024 0,090 -0.186 0.110 -0.485

0.230 -0.555 0,090 -0.137 0.110 -0.338 0.140 -0.735

0.400 -0.068 0.130 -0.309 0.130 - 1.769 ** 0.190 - 1.769"*

0.490 -0.098 0.150 -0.491 0.150 -0.610 0,250 -0.508

0.590 -0.195 0,200 -0.519 0.210 -0.613 0,400 -0.365

0.630 -0.234 0.250 -0,584 0.250 -0.618 0.490 -0,275

0.700 -0,340 0,260 -0.552 0.340 -0,628 0,580 -0.263

0,750 -0,859 0.280 -0.573 0,370 -0.641 0.650 -0.343

0.810 -0.803 0,290 -0.563 0.400 -0,562 0.700 -0.326

0,840 -0,845 0,310 -0.521 0.410 -0.551 ** 0.750 -0.415

0.900 -0,292 0,320 -0,528 0.430 -0.355 0.800 -0.960

0.960 -0.312 0.340 -0.529 0,440 -0.272 0.830 -0,922

0,350 -0.359** 0.460 -0.260 0.900 -0.424

0.370 -0.540 0,490 -0,201 0.960 -0,422

0.380 -0.574 0,500 -0.251

0.400 -0,498 0,520 -0.223

0.410 -0.533 0.540 -0.223

0,430 -0,497 0.550 -0.217

0.440 -0.448 0,580 -0.215

0.460 -0.365 0,600 -0.235

0,470 -0.247 0.610 -0,257

0.490 -0.216 0.650 -0.526

0,500 -0.177 0,700 -0,437

0,520 -0.179 0.750 -0.430

0.530 -0.171 0.820 -0.947

0,550 -0.181 0.890 -0.480

0.560 -0.166 0,900 -0.512

0.580 -0.1 44 0.960 -0,477

0.590 -0.170

0,600 -0.182

0.640 -0,432

0,700 -0.356

0.750 -0.082**

0.820 -0,564

0.870 -0,397

0.930 -0.347

0.960 -0.349

Lower Surface

0,020 - 1.221 0.020 -0,959 0.020 - 1.014 0,020 -0,223

0.110 -0.535 0,060 -0.906 0,060 -0.386 0,060 -0.061

0.230 -0.172 0.090 -0.814 0,090 -0,308 0.110 -0.216

0,400 0.051 0.120 -0.431 0.120 -0.411 0,250 -0.329

0,490 0,066 0.200 -0.167 0.200 -0.189 0.400 -0.347

0.630 1.147"* 0.260 -0.153 0.250 -0.330 0,490 -0.442

0,750 0.197 0,400 -0.061 0.400 -0.205 0.580 -0.167

0.850 0,222 0.490 -0,015 0.490 -0.093 0.650 0.056

0,900 0.305 0.580 0.045 0.580 -0,008 0.750 0.291

0.960 0. 137 0.640 0.286 0,650 -0.096 0.830 0.414

0,750 0,335 0,750 -0.064 0.900 0.472

0,870 0.407 0.890 0,438 0.960 0.350

0.930 0,340 0,930 0.358

0.960 0.214 0.960 0,359

CN = 0.318 0.354 0,366 0.379

771
Table J-2. Continued.

Flight 211. Wing sweep = 26 °, Time = 11-45-57-000, MINF = 0.900, Camber = 5/10, ALPT = 6.03, BETA = 0.02, QINF = 594.8,

RNPU = 4.5E+06, CNWP = 0.3696

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.335 0.000 0.665 0.000 0.444** 0.010 -0.136

0.060 0.002 0.020 0.194 0.020 0.175 0.020 -0.179

0.110 -0.241 0.040 0.153 0.060 0.674"* 0.060 -0.545

0.200 -0.741 0.060 -0.123 0.090 -0.286 0.110 -0.697

0.230 -0.634 0.090 -0.224 0.110 -0.436 0.140 -0.866

0.400 -0.539 0.130 -0.381 0.130 - 1.764"* 0.190 -1.764"*

0.490 -0.435 0.150 -0.571 0.150 -0.690 0.250 -0.856

0.590 -0.432 0.200 -0.596 0.210 -0.707 0.400 -0.641

0.630 -0.340 0.250 -0.698 0.250 -0.727 0.490 -0.464

0.700 -0.426 0.260 -0.665 0.340 -0.763 0.580 -0.403

0.750 -0.662 0.280 -0.691 0.370 -0.771 0.650 -0.449

0.810 -0.706 0.290 -0.680 0.400 -0.751 0.700 -0.429

0.840 -0.775 0.310 -0.655 0.410 -0.544"* 0.750 -0.484

0.900 -0.320 0.320 -0.663 0.430 -0.771 0.800 -0.954

0.960 -0.323 0.340 -0.671 0.440 -0.754 0.830 -0.964

0.350 -0.368"* 0.460 -0.765 0.900 -0.456

0.370 -0.666 0.490 -0.713 0.960 -0.452

0.380 -0.712 0.500 -0.787

0.400 -0.645 0.520 -0.772

0.410 -0.684 0.540 -0.758

0.430 -0.657 0.550 -0.669

0.440 -0.630 0.580 -0.555

0.460 -0.702 0.600 -0.532

0.470 -0.679 0.610 -0.529

0.490 -0.680 0.650 -0.628

0.500 -0.682 0.700 -0.535

0.520 -0.670 0.750 -0.521

0.530 -0.661 0.820 -0.829

0.550 -0.689 0.890 -0.416

0.560 -0.688 0.900 -0.439

0.580 -0.672 0.960 -0.405

0.590 -0.702

0.600 -0.713

0.640 -0.774

0.700 -0.789

0.750 -0.062"*

0.820 -0.361

0.870 -0.312

0.930 -0.337

0.960 -0.337

Lower Surface

0.020 - 1.138 0.020 -0.952 0.020 -0.770 0.020 0.076

0.110 -0.121 0.060 -0.315 0.060 -0.065 0.060 -0.067

0.230 -0.077 0.090 -0.184 0.090 -0.103 0.110 -0.066

0.400 -0.022 0.120 -0.124 0.120 -0.239 0.250 -0.187

0.490 0.009 0.200 -0.070 0.200 -0.097 0.400 -0.212

0.630 1.159"* 0.260 -0.119 0.250 -0.176 0.490 -0.287

0.750 0.175 0.400 -0.063 0.400 -0.128 0.580 -0.165

0.850 0.211 0.490 -0.024 0.490 -0.070 0.650 0.088

0.900 0.294 0.580 0.046 0.580 -0.017 0.750 0.344

0.960 0.123 0.640 0.278 0.650 -0.070 0.830 0.454

0.750 0.343 0.750 -0.070 0.900 0.517

0. 870 0.407 0.890 0.489 0.960 0.362

0.930 0.329 0.930 0.398

0.960 0.216 0.960 0.377

CN = 0.490 0.591 0.573 0.621

772
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time -- 11-46-1-000, M1NF -- 0.891, Camber = 5/10, ALPT -- 7.16, BETA = 0.05, QINF = 580.3,

RNPU = 4.4E+06, CNWP = 0,4117

lq = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0,239 0.000 0,747 0.000 0.414"* 0,010 -0.526

0.060 -0.086 0.020 0.025 0.020 0.014 0.020 -0,224

0.110 -0.306 0.040 0.038 0.060 0.601 ** 0.060 -0.650

0.200 -0,737 0.060 -0,235 0.090 -0.471 0.110 -0, 821

0.230 -0.676 0.090 -0.321 0.110 -0.563 0.140 -0.987

0.400 -0.628 0.130 -0.487 0.130 -1.798"* 0.190 -1.798"*

0.490 -0.517 0.150 -0.643 0,150 -0,773 0,250 -0.979

0,590 -0.511 0,200 -0,677 0.210 -0,787 0.400 -0.716

0,630 -0.418 0,250 -0.786 0.250 -0.810 0.490 -0.581

0,700 -0.485 0.260 -0.752 0,340 -0.846 0.580 -0,478

0.750 -0.570 0,280 -0.790 0,370 -0.860 0.650 -0,533

0.810 -0,600 0,290 -0,773 0.400 -0.863 0,700 -0.501

0.840 -0.656 0.310 -0.744 0.410 -0_547"* 0.750 -0.557

0,900 -0,360 0.320 -0.755 0,430 -0,872 0.800 -0.968

0.960 -0,375 0,340 -0.770 0.440 -0.847 0,830 -0.931

0,350 -0,382"* 0.460 -0.796 0,900 -0,489

0,370 -0.762 0.490 -0.817 0.960 -0.486

0.380 -0.807 0,500 -0.890

0,400 -0.740 0,520 -0.876

0.410 -0,785 0,540 -0.869

0.430 -0,746 0.550 -0,845

0.440 -0.721 0,580 -0,845

0.460 -0.799 0.600 -0,837

0.470 -0,781 0.610 -0,811

0.490 -0,771 0.650 -0.787

0,500 -0.759 0,700 -0.669

0.520 -0.760 0,750 -0.620

0.530 -0.755 0,820 -0.519

0.550 -0,796 0.890 -0,415

0.560 -0,789 0.900 -0.428

0.580 -0.770 0.960 -0.390

0.590 -0,800

0,600 -0,807

0,640 -0.848

0,700 -0.874

0.750 -0,050"*

0.820 -0.352

0,870 -0,308

0.930 -0.327

0,960 -0.322

Lower Surface

0.020 -0.963 0.020 -0,854 0.020 -0,200 0.020 0,195

0,110 -0.173 0.060 -0.004 0,060 0.057 0.060 -0,066

0,230 -0.020 0,090 -0.082 0.090 0.005 0.110 0.031

0.400 -0,016 0.120 -0.049 0,120 -0.158 0,250 -0.111

0.490 0.007 0.200 -0.019 0,200 -0,045 0.400 -0.151

0,630 1.198"* 0.260 -0,075 0,250 -0.076 0,490 -0,187

0.750 0.165 0.400 -0.046 0,400 -0,080 0,580 -0,126

0.850 0.191 0,490 -0.013 0.490 -0.062 0.650 0.112

0,900 0,276 0,580 0.040 0.580 -0.002 0.750 0,357

0.960 0.102 0,640 0,289 0.650 -0,073 0,830 0.460

0.750 0.337 0.750 -0,065 0.900 0,518

0.870 0.412 0.890 0.489 0.960 0,350

0.930 0,344 0,930 0.391

0.960 0.218 0,960 0.388

CN = 0.524 0.697 0,682 0.741

773
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-46-14-500, MINF = 0.894, Camber = 5/10, ALPT = 7.99, BETA = 0.22, QINF = 628.8,

RNPU = 4.8E+06, CNWP = 0.4275

"q= 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 0.204 0.000 0.795 0.000 0.424* * 0.010 -0.556

0.060 -0.108 0.020 -0.026 0.020 -0.042 0.020 -0.536

0. t 10 -0.307 0.040 -0.015 0.060 0.464"* 0.060 -0.644

0.200 -0.748 0.060 -0.271 0.090 -0.528 0.110 -0.873

0.230 -0.699 0.090 -0.340 0.110 -0.608 0.140 - 1.018

0.400 -0.650 0.130 -0.498 0.130 -1.788"* 0.190 -1.788**

0.490 -0.553 0.150 -0.665 0.150 -0.802 0,250 - 1.031

0.590 -0.545 0.200 -0.687 0.210 -0.817 0.400 -0.747

0.630 -0.459 0,250 -0.804 0.250 -0.848 0.490 -0.616

0.700 -0.527 0.260 -0.774 0.340 -0.877 0.580 -0.525

0.750 -0.542 0.280 -0.812 0.370 -0.882 0.650 -0.567

0.810 -0.576 0.290 -0.807 0.400 -0.870 0.700 -0.543

0.840 -0.642 0.310 -0,764 0.410 -0.633" * 0.750 -0.587

0.900 -0.398 0.320 -0.778 0.430 -0.901 0.800 -0.973

0.960 -0.431 0.340 -0.790 0.440 -0.880 0.830 -0.999

0.350 -0.377** 0.460 -0,862 0.900 -0.607

0.370 -0.782 0.490 -0.840 0.960 -0.519

0.380 -0.830 0.500 -0.909

0.400 -0.759 0.520 -0.902

0.410 -0.813 0.540 -0.908

0.430 -0.783 0.550 -0.890

0.440 -0.757 0,580 -0.887

0.460 -0.836 0.600 -0.883

0.470 -0.810 0.610 -0,870

0.490 -0.795 0.650 -0.989

0.500 -0.804 0.700 -0.841

0.520 -0.795 0.750 -0.738

0.530 -0.788 0.820 -0.523

0.550 -0.798 0.890 -0.443

0,560 -0.819 0.900 -0.444

0.580 -0.799 0.960 -0.429

0.590 -0.835

0.600 -0.833

0.640 -0.875

0.700 -0.888

0.750 -0.053**

0.820 -0.338

0.870 -0.331

0.930 -0.344

0.960 -0,339

Lower Surface

0.020 -0.853 0.020 -0.252 0.020 -0.134 0.020 0.357

0.1 I0 -0.169 0.060 0.040 0.060 0.103 0.060 -0.113

0.230 -0.005 0.090 -0.035 0.090 0.053 0.110 0.111

0.400 -0,010 0.120 -0.017 0.120 -0.100 0.250 -0.084

0,490 0.004 0.200 -0,002 0.200 -0.035 0.400 -0.131

0,630 0.977"* 0.260 -0.047 0.250 -0.053 0.490 -0.158

0.750 0.156 0.400 -0.026 0.400 -0.061 0,580 -0.104

0.850 0.189 0.490 -0.005 0.490 -0.064 0.650 0.129

0,900 0.273 0.580 0,047 0.580 0.002 0.750 0.381

0.960 0.091 0.640 0.294 0.650 -0.071 0.830 0.478

0.750 0,339 0.750 -0.185 0.900 0,535

0.870 0.426 0.890 0.500 0.960 0.361

0.930 0.349 0.930 0.401

0.960 0.225 0.960 0.397

CN = 0.546 0.731 0.732 0.813

774
Table J-2, Continued.

Flight 211, Wing sweep = 26 °, Time = 11-46-17-000, MINF = 0.898, Camber = 5/10. ALPT = 8.05, BETA = 0.05, QINF = 650.2,

RNPU = 4.9E+06, CNWP = 0.4384

1"1= 0.93 0.76 0.59 0.40

Upper Surface

x./c CP x/c CP x/c CP x/c CP

0.020 0,209 0.000 0.787 0,000 0.411 ** 0.010 -0.541

0.060 -0.111 0,020 -0,010 0.020 -0,044 0,020 -0,557

0. 110 -0,320 0.040 -0,006 0,060 0,402** 0.060 -0.671

0.200 -0,752 0.060 -0.270 0,090 -0.530 0.110 -0.859

0,230 -0.696 0,090 -0.331 0.110 -0.609 0.140 - 1.015

0,400 -0,654 0,130 -0.496 0.130 - 1.771 ** 0.190 - 1.771 * *

0.490 -0.543 0.150 -0.661 0.150 -0.796 0,250 - 1.026

0,590 -0.552 0.200 -0.683 0.210 -0.815 0.400 -0.738

0.630 -0,466 0,250 -0,788 0.250 -0.844 0.490 -0.612

0.700 -0.536 0.260 -0,764 0.340 -0.877 0,580 -0.527

0.750 -0.535 0.280 -0.805 0,370 -0.885 0.650 -0.561

0.810 -0,584 0.290 -0.801 0,400 -0.853 0,700 -0,540

0.840 -0,665 0.310 -0,754 0.410 -0.654** 0.750 -0.580

0.900 -0.415 0.320 -0.775 0,430 -0.887 0.800 -0.983

0.960 -0.436 0.340 -0.787 0.440 -0.868 0.830 - 1.018

0,350 -0,379"* 0.460 -0.876 0,900 -0,628

0.370 -0.779 0.490 -0.820 0.960 -0.564

0.380 -0.825 0,500 -0,901

0,400 -0.758 0.520 -0,888

0.410 -0.810 0.540 -0.900

0.430 -0,780 0.550 -0.884

0.440 -0,753 0,580 -0,879

0.460 -0.820 0.600 -0.882

0.470 -0.812 0.610 -0.870

0.490 -0.794 0.650 -0.993

0.500 -0.799 0.700 -0.854

0.520 -0.788 0.750 -0.735

0.530 -0.781 0.820 -0.561

0,550 -0_806 0,890 -0,468

0.560 -0.818 0.900 -0,460

0.580 -0.792 0,960 -0.454

0,590 -0.828

0.600 -0,825

0.640 -0.877

0.700 -0,889

0.750 -0.069"*

0.820 -0.354

0.870 -0.344

0.930 -0.358

0.960 -0.351

Lower Surface

0.020 -0.878 0.020 -0.245 0.020 -0.137 0,020 0,357

0.110 -0.180 0,060 0,033 0,060 0.105 0.060 -0.125

0,230 -0.016 0,090 -0.041 0.090 0.047 0.110 0,088

0.400 -0.022 0.120 -0.025 0.120 -0.102 0,250 -0,089

0.490 -0.004 0.200 -0.014 0.200 -0,047 0,400 -0.140

0,630 0.903** 0.260 -0.049 0.250 -0,059 0,490 -0.175

0.750 0.149 0.400 -0.031 0.400 -0.065 0.580 -0.105

0.850 0.183 0.490 -0.014 0.490 -0.075 0.650 0.127

0.900 0,264 0,580 0.038 0.580 -0,007 0.750 0.377

0,960 0.084 0,640 0,287 0,650 -0.083 0.830 0,479

0.750 0.331 0.750 -0.127 0.900 0,535

0.870 0.424 0.890 0.502 0.960 0,355

0,930 0,335 0,930 0.394

0.960 0.211 0,960 0,382

CN = 0,541 0,723 0.738 0.809

775
Table J-2. Continued.

Flight 231, Wing sweep = 26 °, Ttme= 13-33-23-000, MINF = 0,631, Camber = 7/-1, ALPT = 11.45, BETA = -0.27, QINF = 387.6,

RNPU = 3.8E+06, CNWP = 0.4439

11 = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x./c CP

0.020 - 1.210 0.000 0.317 0.000 3.008"* 0.010 -2.006

0,060 - 1.031 0.020 - 1,879 0,020 - 1.962 0,020 -2.035

0.110 -0.968 0.040 - 1.335" * 0.060 - 1.565" * 0.060 - 1.944

0.200 -0.718 0.060 - 1.436 0.090 - 1.861 0.110 - 1,447

0.230 -0.605 0.090 - 1.656 0.110 - 1.946 0.140 - 1.131

0.400 -0.389 0.130 - 1.202 0.130 -2.031 0.190 -3.585 * *

0.490 -0.372 0.150 - 1.519 0.150 - 1.455 0.250 -0.740

0.590 -0.366 0.200 - 1.186 0.210 - 1.258 0.400 -0.552

0.630 -0.344 0.250 -0.172** 0.250 -0.728 0.490 -0.461

0.700 -0.253 0.260 -0.653 0.340 -0.181 ** 0.580 -0.435

0.750 -0.257 0.280 0.748"* 0.370 0.407"* 0.650 -0.514

0.810 -0.249 0.290 -0.123"* 0.400 -0.548 0,700 -0.499

0.840 -0.226 0.310 0.179"* 0,410 -0.060** 0.750 -0.505

0.900 -0.247 0.320 -0.041 ** 0.430 -0.089** 0.800 -0.538

0.960 -0.156 0.340 0.407"* 0.440 -0.123"* 0.830 -0.391

0.350 -0.619"* 0.460 0.086** 0.900 -0.356

0.370 0.288** 0.490 -0.472 0.960 -0.326

0.380 -0.148"* 0.500 -0.010"*

0.400 -0,482 0.520 -0.069**

0,410 0,523** 0.540 0.146"*

0.430 0.411 ** 0.550 0.008**

0.440 -0.518 0.580 -0.452

0.460 -0.022 ** 0.600 -0.151 **

0.470 0.658** 0.610 0.213"*

0.490 -0.491 0.650 3.151 * *

0.500 0.599** 0.700 -0.564

0.520 0.765"* 0.750 -0.631

0.530 -0.469 0.820 -0.502

0.550 0.662** 0.890 -0.155

0.560 0.275** 0.900 -0.133

0.580 -0.471 0.960 -0.088

0,590 0,917"*

0.600 0.078**

0.640 -0.570

0.700 -0.600

0.750 -0.126**

0.820 -0.539

0.870 -0.164

0.930 -0.334

0.960 -0.249

Lower Surface

0.020 0.300 0.020 0.466 0.020 0.526 0.020 0.716

0.110 0.139 0.060 0.418 0.060 0.460 0.060 2.917 * *

0.230 0.158 0.090 0.327 0.090 0.797** 0.1 t0 0.380

0.400 0.054 0,120 0.315"* 0.120 0.209 0.250 0.188

0.490 0.024 0.200 0.147 0.200 0.121 0.400 0.149

0.630 0.769** 0.260 0,222 0.250 0.238 0.490 0.106

0.750 -0.072 0.400 0.122 0.400 0.125 0.580 0.074

0.850 -0.047 0,490 0.087 0.490 -0.010 0.650 0.179

0,900 0.012 0,580 0.072 0.580 0.133 0.750 0.371

0.960 -0.004 0.640 0.206 0.650 -0.086 0.830 0.437

0.750 0.097 0.750 0.057 0.900 0.488

0.870 0.069 0,890 0.440 0.960 0.284

0,930 0.031 0.930 0.361

0.960 -0.014 0.960 -0.127"*

CN = 0.471 0.827 0.843 0.929

776
Table J-2. Continued.

Flight 211, Wing sweep = 26 °, Time = 11-38-33-000, MINF = 0.850, Camber = 0/2, ALPT = 5.51, BETA = 0.08, Q1NF = 253.3,

RNPU = 2.0E+06, CNWP -- 0.2692

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.526 0.000 0.847 0.000 0.375"* 0.010 -0.950

0.060 -0.622 0.020 -0.783 0.020 -0.762 0.020 -0.958

0.110 -0.575 0.040 -0.574 0.060 1.527"* 0.060 -0.952

0.200 -0.264 0.060 -0.784 0.090 -0.815 0.110 -0.898

0.230 -0.354 0.090 -0.735 0.110 -0.884 0.140 -0.914

0.400 -0.239 0.130 -0.735 0.130 - 1.975"* 0.190 - 1.975" *

0.490 -0.215 0.150 -0.732 0.150 -0.784 0.250 -0.930

0.590 -0.293 0.200 -0.585 0.210 -0.773 0.400 -0.704

0.630 -0.289 0.250 -0.791 0.250 -0.788 0.490 -0.315

0.700 -0.234 0.260 -0.736 0.340 -0.799 0.580 -0.310

0.750 -0.271 0.280 -0.761 0.370 -0.836 0.650 -0.359

0.810 -0.276 0.290 -0.779 0.400 -0.744 0.700 -0.351

0.840 -0.231 0.310 -0.731 0.410 0.891"* 0.750 -0.424

0.900 -0.156 0.320 -0.729 0.430 -0.347 0.800 -0.406

0.960 -0.030 0.340 -0.746 0.440 -0.249 0.830 -0.310

0.350 -0.389** 0.460 -0.219 0.900 -0.154

0.370 -0.414 0.490 -0.152 0.960 0.0l 5

0.380 -0.271 0.500 -0.215

0.400 -0.113 0.520 -0.207

0.410 -0.183 0.540 -0.235

0.430 -0.154 0.550 -0.223

0.440 -0.109 0.580 -0.260

0.460 -0.197 0.600 -0.238

0.470 -0.185 0.610 -0.252

0.490 -0.212 0.650 -0.707

0.500 -0.254 0.700 -0.493

0.520 -0.213 0.750 -0.470

0.530 -0.235 0.820 -0.360

0.550 -0.313 0.890 -0.107

0.560 -0.277 0.900 -0.076

0.580 -0.265 0.960 0.080

0.590 -0.323

0.600 -0.330

0.640 -0.462

0.700 -0.340

0.750 -0.021"*

0.820 -0.273

0.870 -0.240

0.930 -0.096

0.960 -0.041

Lower Surface

0.020 -0.207 0.020 -0.019 0.020 0.090 0.020 0.412

O.110 -0.234 0.060 0.079 0.060 O. 1O0 0.060 -0.046

0.230 -0.079 0.090 -0.072 0.090 -0.015 O. 110 -0.003

0.400 -0.090 O. 120 -0.127 O.120 -0.319 0.250 -0.225

0.490 -0.071 0.200 -0.140 0.200 -0.195 0.400 -0.258

0.630 4.888** 0.260 -0.254 0.250 -0.197 0.490 -0.315

0.750 0.011 0.400 -0.184 0.400 -0.213 0.580 -0.325

0.850 0.085 0.490 -0.189 0.490 -0.048 0.650 -0.14 l

0.900 O. 186 0.580 -0.178 0.580 -0.226 0.750 0.095

0.960 O. 129 0.640 0.016 0.650 -0.053 0.830 0.260

0.750 0.1 64 0.750 -0.035 0.900 0.321

0.870 0.234 0.890 0.294 0.960 0.244

0.930 0.208 0.930 0.259

0.960 0.196 0.960 0.402

CN = 0.238 0.381 0.413 0.466

777
Table J-2. Concluded.

Hight 211, Wing sweep = 26 °, Time = 11-39-16-000, MINF -- 0.850, Camber = 0/2, ALPT = 5.60, BETA = 0.11, QINF = 252.9,

RNPU = 2.0E+06, CNWP = 0.2661

"q = 0.93 0.76 0.59 0.40

Upper Surface

x/c CP x/c CP x/c CP x/c CP

0.020 -0.565 0.000 0.844 0.000 0.292 ** 0.010 -0.984

0.060 -0.657 0.020 -0.892 0.020 -0.790 0.020 -0.960

0.110 -0.593 0.040 -0.592 0.060 1.529** 0.060 -0.996

0.200 -0.279 0.060 -0.785 0.090 -0.853 0.110 -0.923

0.230 -0.376 0.090 -0.764 0.110 -0.903 0.140 -0.936

0.400 -0.231 0.130 -0.728 0.130 -1.978"* 0.190 -1.978"*

0.490 -0.228 0.150 -0.762 0.150 -0.803 0.250 -0.957

0.590 -0.2"]6 0.200 -0.618 0.210 -0.803 0.400 -0.739

0.630 -0.285 0.250 -0.789 0.250 -0.820 0.490 -0.316

0.700 -0.230 0.260 -0.728 0.340 -0.854 0.580 -0.311

0.750 -0.267 0.280 -0.791 0.370 -0.837 0.650 -0.372

0.810 -0.241 0.290 -0.791 0.400 -0.815 0.700 -0.352

0.840 -0.249 0.310 -0.748 0.410 0.892 * * 0.750 -0.424

0.900 -0.135 0.320 -0.741 0.430 -0.383 0.800 -0.395

0.960 -0.030 0.340 -0.746 0.440 -0.268 0.830 -0.300

0.350 -0.390** 0.460 -0.257 0.900 -0.154

0.370 -0.614 0.490 -0.161 0.960 0.015

0.380 -0.337 0.500 -0.237

0.400 -0.165 0.520 -0.208

0.410 -0.205 0.540 -0.210

0.430 -0.154 0.550 -0.223

0.440 -0.102 0.580 -0.260

0.460 -0.201 0.600 -0.256

0.470 -0.177 0.610 -0.252

0.490 -0.203 0.650 -0.659

0.500 -0.222 0.700 -0.480

0.520 -0.241 0.750 -0.453

0.530 -0.245 0.820 -0.361

0.550 -0.296 0.890 -0.107

0.560 -0.288 0.900 -0.073

0.580 -0.258 0.960 0.068

0.590 -0.287

0.600 -0.324

0.640 -0.427

0.700 -0.345

0.750 -0.017"*

0.820 -0.269

0.870 -0.227

0.930 -0.070

0.960 -0.024

Lower Surface

0.020 -0.225 0.020 -0.007 0.020 0.072 0.020 0.421

0.110 -0.219 0.060 0.070 0.060 0.097 0.060 -0.028

0.230 -0.052 0.090 -0.083 0.090 -0.010 0.110 0.003

0.400 -0.103 0.120 -0.119 0.120 -0.320 0.250 -0.217

0.490 -0.062 0.200 -0.114 0.200 -0.172 0.400 -0.250

0.630 4.896** 0.260 -0.246 0.250 -0.189 0.490 -0.306

0.750 0.011 0.400 -0.162 0.400 -0.202 0.580 -0.307

0.850 0.090 0.490 -0.185 0.490 -0.044 0.650 -0.155

0.900 0.168 0.580 -0.160 0.580 -0.226 0.750 0.119

0.960 0.142 0.640 0.016 0.650 -0.053 0.830 0.270

0.750 0.202 0.750 -0.053 0.900 0.329

0.870 0.256 0.890 0.290 0.960 0.244

0.930 0.208 0.930 0.254

0.960 0.170 0.960 0.408

CN = 0.247 0.401 0.427 0.486

778
APPENDIX K

Boundary-Layer Data

Leading-edge wing sweep is 26 °. Table K-1 contains a summary of the data listing in table K-2. Camber is either

_)LE/'TEor _)LE./1/M/O"Refer to Nomenclature for definitions.

Table K-1. Summary of data.

Flight/Time QINE Ib/ft 2 MINF ALPT, deg BETA, deg THETA, in. Camber

229/11.17.26.000 304. 0.605 6.47 0.40 0.163 0/2

229/11.17.30.000 305. 0.606 6.51 0.51 0.171 0/2

229/11.17.40.000 306. 0.606 6.50 0.46 0.164 0/2

229/11.17.49.000 307. 0.607 6.25 0.51 0.1 64 0/2

229/11.18.00.000 309. 0.609 6.28 0.48 0.167 0/2

229/11.18.00.500 309. 0.609 6.29 0.54 0.166 0/2

229/11.18.01.000 309. 0.609 6.28 0.51 0.166 0/2

229/11.18.01.500 309. 0.610 6.28 0.54 0.149 0/2

229/11.18.02.000 309. 0.610 6.28 0.48 0.162 0/2

229/11.18.11.500 311. 0.611 6.28 0.22 0.169 0/2

229/11.18.12.000 310. 0.610 6.29 0.02 0.170 0/2

229/11.18.12.500 310. 0.610 6.29 -0.15 0.166 0/2

229/11.18.17.500 308. 0.608 7.03 -0.33 0.174 0/2

229/11.18.34.000 301. 0.603 8.08 -0.09 0.218 0/2

229/11.18.42.000 303. 0.605 8.99 0.14 0.430 0/2

229/11.18.51.500 296. 0.599 10.11 0.34 0.542 0/2

229/11.18.59.000 298. 0.598 10.15 0.17 0.556 0/2

229/11.18.03.500 309. 0.610 6.28 0.46 0.165 0/2

229/11.18.11.500 311. 0.611 6.28 0.22 0.169 0/2

229/11.18.17.500 308. 0.608 7.03 -0.33 0.174 0/2

229/11.18.20.500 306. 0.607 7.74 0.34 0.189 0/2

229/11.18.21.000 306. 0.607 8.03 0.25 0.207 0/2

229/11.18.24.000 303. 0.604 7.83 0.28 0. i 92 0/2

229/11. i 8.26.000 303. 0.604 7.81 0.25 0.196 0/2

229/11.18.34.000 301. 0.603 8.08 -0.09 0.218 0/2

229/11.18.36.500 301. 0.603 8.08 -0.15 0.199 0/2

229/11.18.41.500 303. 0.605 8.95 0.08 0.431 0/2

229/11.18.42.000 303. 0.605 8.99 0.14 0.430 0/2

229/11.18.42.500 303. 0.606 9.18 0.37 0.389 0/2

229/11.18.45.000 302. 0.605 9.50 0.22 0.506 0/2

229/11.18.46.500 299. 0.602 9.50 0.14 0.518 0/2

779
TableK-1.Continued.

Flight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

229/11.18.49.000 300. 0.603 10.02 0.05 0.557 0/2

229/11.18.51.000 296. 0.599 10.03 0.22 0.579 0/2

229/11.20.09.000 299. 0.600 6.50 0.34 O.157 5/2

229/11.20.23.500 301. 0.602 6.50 0.34 O.169 5/2

229/11.20.26.000 302. 0.603 6.50 0.37 O.161 5/2

229/11.20.34.000 302. 0.603 6.50 0.11 0.161 5/2

229/11.20.40.000 302. 0.604 6.54 0.08 O.156 5/2

229/11.20.47.000 304. 0.606 6.50 0.34 O.157 5/2

229/11.20.55.500 306. 0.607 6.81 -0.09 O.168 5/2

229/11.20.56.000 306. 0.607 7.08 0.02 O.169 5/2

229/11.21.09.000 301. 0.604 7.96 -0.33 0.188 5/2

229/11.21.13.500 297. 0.600 8.01 -0.18 0.182 5/2

229/11.21.14.000 296. 0.600 8.08 O.19 O.182 5/2

229/11.21.15.500 297. 0.601 8.95 0.19 0.196 5/2

229/11.21.16.500 299. 0.602 8.89 O.11 O.190 5/2

229/11.21.17.000 300. 0.603 9.19 0.11 0.203 5/2

229/11.21.24.000 304. 0.606 10.04 -0.04 0.215 5/2

229/11.21.24.500 304. 0.606 10.02 -0.01 0.212 5/2

229/11.21.31.500 302. 0.602 10.10 -0.12 0.202 5/2

229/11.21.33.000 302. 0.602 10.07 -0.15 0.213 5/2

229/11.26.48.500 302. 0.800 5.90 0.14 0.184 0/2

229/11.27.10.500 304. 0.802 7.12 0.02 O.194 0/2

229/11.27.17.000 297. 0.793 8.04 -0.09 0.222 0/2

229/11.28.05.500 297. 0.798 8.03 -0.27 0.224 0/2

229/11.31.02.500 301. 0.801 5.97 0.02 O.184 5/2

229/11.31.08.000 299. 0.800 6.06 -0.85 0.190 5/2

229/11.31.11.500 298. 0.799 7.03 -0.04 0.206 5/2

229/11.31.13.000 297. 0.798 7.20 O.14 0.208 5/2

229/11.31.17.500 295. 0.796 8.05 -0.07 0.212 5/2

229/11.31.22.500 288. 0.789 8.05 -0.09 0.214 5/2

229/11.31.25.500 288. 0.790 8.05 -0.30 0.216 5/2

229/11.31.34.500 297. 0.805 9.16 0.02 0.429 5/2

229/11.31.42.500 302. 0.809 10.09 -0.18 0.435 5/2

229/11.31.43.500 303. 0.810 10.04 -0.18 0.654 5/2

229/12.37.03.000 301. 0.801 6.07 -0.67 O.180 0/2

229/12.37.18.500 302. 0.800 8.01 -0.07 O.192 0/2

229/12.38.26.500 302. 0.803 6.01 -0.15 O.182 5/2

78O
TableK-1.Continued.

Flight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

229/12.38.35.500 302. 0.802 5.98 -0.30 0.174 5/2

229/12.38.57.000 291. 0.791 7.93 -0.18 0.211 5/2

229/12.40.24.500 305. 0.805 5.97 0.11 0.230 10/2

229/12.40.27.500 305. 0.805 5.93 -0.07 0.193 10/2

229/12.41.01.500 312. 0.809 8.42 -0.21 0.398 10/2

229/12.41.02.500 314. 0.811 8.43 -0.01 0.413 10/2

229/12.41.03.000 316. 0.812 8.43 0.02 0.418 10/2

229/12.41.03.500 317. 0.814 8.42 -0.04 0.433 10/2

229/12.43.14.000 306. 0.806 8.01 -0.15 0.245 5/2

229/i2.44.02.500 301. 0.802 5.01 -0.24 0.346 5/6

229/12.44.04.500 300. 0.801 5.01 -0.33 0.310 5/6

229/12.44.14.500 301. 0.801 5.10 -0.30 0.334 5/6

229/11.28.13.000 299. 0.803 8.98 0.08 0.391 0/2

229/11.28.13.500 299. 0.803 9.04 0.05 0.384 0/2

229/11.28.20.000 298. 0.803 9.98 0.14 0.573 0/2

229/11.28.24.500 298. 0.803 9.97 0.19 0.510 0/2

229/11.31.34.000 296. 0.804 8.91 0.05 0.380 5/2

229/11.31.44.000 304. 0.810 9.98 -0.09 0.746 5/2

229/11.31.45.500 307. 0.812 10.04 0.37 0.625 5/2

229/11.31.50.000 314. 0.817 10.03 -0.38 0.779 5/2

229/11.31.16.500 296. 0.797 7.94 -0.24 0.243 5/2

229/11.31.21.000 289. 0.790 7.98 -0.12 0.211 5/2

229/11.31.21.500 289. 0.790 8.04 -0.15 0.215 5/2

229/11.31.23.000 288. 0.789 8.07 -0.12 0.231 5/2

229/11.31.26.000 288. 0.791 8.04 -0.47 0.220 5/2

229/11.31.33.500 296. 0.803 8.75 0.14 0.360 5/2

229/11.31.35.000 298. 0.806 9.22 0.11 0.485 5/2

229/11.31.41.500 302. 0.809 9.97 -0,01 0.720 5/2

229/11.31.44.500 305. 0.811 10.03 -0.04 0.710 5/2

229/11.31.45.000 306. 0.812 10.05 0.19 0.657 5/2

229/11.31.46.000 308. 0.813 9.98 0.37 0.614 5/2

229/12.40.44.500 303. 0.801 7.91 -0.36 0.310 10/2

229/12.40.45.500 302. 0.800 8.06 -0.18 0.344 10/2

229/12.40.46.000 301. 0.799 8.06 -0.09 0.353 10/2

229/12.40.50.500 296. 0.793 7.90 -0.36 0.306 10/2

229/12.40.53.000 296. 0.792 8.07 -0.30 0.346 10/2

229/12.40.55.000 297. 0.793 8.06 -0.27 0.369 10/2

781
TableK-1.Continued.

Flight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA, in. Camber

229/12.41.01.000 311. 0.808 8.42 -0.21 0.377 10/2

229/12.41.02.000 313. 0.810 8.34 -0.09 0.390 10/2

229/12.41.04.000 318. O.814 8.40 -0.07 0.415 10/2

229/12.44.01.000 301. 0.802 5.01 -0.27 0.298 5/6

229/12.44.01.500 301. 0.802 4.98 -0.30 0.308 5/6

229/12.44.03.500 301. 0.801 5.04 -0.36 0.343 5/6

229/12.44.04.000 300. 0.801 5.04 -0.30 0.336 5/6

229/12.44.09.000 300. 0.801 4.50 -0.30 0.278 5/6

229/12.44.09. 500 300. O.801 4.55 -0.04 O.299 5/6

229/12.44.13.000 301. 0.802 4.99 -0.15 0.299 5/6

229/12.36.46.000 298. 0.798 5.66 -0.04 O. 169 0/2

229/12.36.53.500 299. 0.798 5.65 -0.15 0.184 0/2

229/12.37.02.500 300. 0.800 6.04 -0.41 0.175 0/2

229/12.37.05.000 301. 0.801 6.09 -0.88 0.173 0/2

229/12.37.10.000 302. 0.802 7.05 -0.07 0.173 0/2

229/12.37.11.000 302. 0.802 7.18 -0.36 0.170 0/2

229/12.37.17.500 301. 0.800 8.03 -0.24 0.180 0/2

229/12.37.19.500 302. 0.800 8.03 -0.30 0.200 0/2

229/12.38.21.000 301. 0.801 5.98 -0.21 0.174 5/2

229/12.38.26.000 302. 0.802 6.01 -0.15 0.183 5/2

229/12.38.41.000 301. 0.802 5.99 -0.91 0.182 5/2

229/12.38.45.500 302. 0.803 6.98 -0.09 0.201 5/2

229/12.38.46.000 302. 0.803 7.20 -0.07 O.182 5/2

229/12.38.58.500 290. 0.790 8.06 -0.27 0.208 5/2

229/12.38.59.500 290. 0.790 8.10 -0.33 0.224 5/2

229/12.40.17.500 304. O.803 5.97 -0.21 0.218 10/2

229/12.40.19.500 304. 0.803 5.97 0.05 O.191 10/2

229/12.40.38.000 307. 0.806 6.95 -0.18 0.213 10/2

229/12.40.38.500 307. 0.806 7.07 -0.04 0.219 10/2

229/12.40.39.000 307. O.806 7.29 -0.12 0.226 10/2

229/12.40.45.000 302. 0.800 8.02 -0.36 0.320 10/2

229/12.40.46.500 301. 0.798 8.01 0.08 0.333 10/2

229/12.40.52.500 296. 0.792 8.00 -0.12 0.341 10/2

229/12.40.57.500 302. 0.798 8.01 -0.21 0.374 10/2

229/12.42.27.500 305. 0.804 5.52 0.08 O.178 5/2

229/12.42.29.000 305. 0.805 5.66 O. 14 O.180 5/2

229/12.42.42.500 306. 0.807 5.94 -0.09 O.188 5/2

782
TableK-1.Continued.

Flight/Time QINEIb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

229/12.42.44.500 306. 0.806 5.97 0.11 0.185 5/2

229/12.42.52.500 306. 0.808 5.98 -0.88 0.183 5/2

229/12.42.55.500 307. 0.808 6.95 0.02 0.200 5/2

229/12.42.56.000 307. 0.808 7.06 0.08 0.193 5/2

229/12.42.57.500 307. 0.809 7.19 -0.09 0.207 5/2

229/12.43.12.000 304. 0.805 7.97 -0.24 0.241 5/2

229/12.43.14.500 306. 0.807 8.01 -0.07 0.247 5/2

229/12.44.08.500 300. 0.801 4.54 -0.36 0.316 5/6

229/12.44.10.000 300. 0.801 4.50 -0.30 0.293 5/6

229/12.44.12.500 301. 0.802 4.95 -0.27 0.314 5/6

229/12.44.13.500 301. 0.802 4.97 -0.30 0.288 5/6

229/12.44.19.000 299. 0.799 5.02 -0.15 0.342 5/6

229/12.44.30.500 298. 0.797 5.83 -0.56 0.342 5/6

229/12.44.31.000 298. 0.797 5.96 -0.56 0.368 5/6

229/12.44.31.500 298. 0.797 6.11 -0.53 0.444 5/6

229/12.44.38.000 293. 0.791 6.91 -0.47 0.477 5/6

229/12.44.39.000 292. 0.790 6.99 -0.38 0.455 5/6

229/12.44.39.500 292. 0.789 7.04 -0.30 0.494 5/6

229/12.44.52.000 299. 0.799 8.07 -0.30 0.484 5/6

229/12.44.52.500 300. 0.799 8.05 -0.30 0.495 5/6

229/12.44.53.000 300. 0.800 8.04 -0.38 0.484 5/6

229/12.52.48.500 303. 0.802 5.61 0.08 0.175 0/2

229/12.53.53.000 308. 0.807 3.13 0.14 0.146 0/2

229/12.53.53.500 310. 0.809 3.14 -0.04 0.151 0/2

229/12.53.54.000 312. 0.811 3.19 0.08 0.152 0/2

229/12.54.01.500 346. 0.837 8.08 0.11 0.273 0/2

229/13.03.57.500 298. 0.796 5.04 -0.07 0.202 1/4

229/13.03.59.000 297. 0.796 5.04 -0.01 0.202 1/4

229/13.04.07.500 296. 0.795 5.04 -0.21 0.205 1/4

229/13.04.14.000 303. 0.802 3.01 -0.27 0.163 0/2

229/13.04.14.500 305. 0.804 3.00 -0.27 0.141 0/2

229/13.04.17.500 320. 0.818 3.01 0.08 0.157 0/2

229/13.04.18.000 323. 0.820 3.00 -0.18 0.158 0/2

229/13.04.23.500 353. 0.842 7.95 -0.07 0.334 2/6

229/13.04.24.500 353. 0.840 8.56 -0.12 0.463 3/6

229/13.04.25.000 351. 0.837 8.65 -0.27 0.617 3/6

229/13.04.29.000 323. 0.808 8.88 -0.07 0.360 4/7

783
TableK-1.Continued.

Flight/Time QINF,lb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

229/13.04.29.500 318. O.803 8.96 -0.01 0.430 4/7

229/13.04.30.000 312. 0.797 8.88 -0.18 0.477 4/7

229/13.22.42.000 305. 0.804 5.17 0.25 0.206 1/4

229/13.22.42.500 305. 0.804 5.17 0.22 0.213 1/4

229/13.22.45.000 305. 0.804 5.17 0.08 0.204 1/4

229/13.23.09.000 307. 0.807 5.17 0.02 0.212 1/4

229/13.23.19.500 307. 0.806 6.02 -0.70 0.240 1/5

229/13.23.20.000 306. 0.806 5.81 -0.56 0.262 1/5

229/13.23.20.500 306. 0.806 6.05 -0.53 0.233 1/5

229/13.23.28.000 305. 0.800 7.06 -0.27 0.525 2/6

229/13.23.28.500 306. 0.800 7.12 -0.18 0.561 2/6

229/13.23.30.500 315. 0.806 7.94 O.17 0.669 3/6

229/13.23.31.000 319. 0.810 8.12 0.28 0.567 3/6

229/12.54.02.500 345. 0.835 9.06 0.08 0.441 0/2

229/12.54.03.000 343. 0.832 9.47 O.11 0.537 0/2

229/11.34.59.500 295. 0.847 5.16 0.22 O.188 0/2

229/11.35.01.500 295. 0.847 5.20 O.19 O.190 0/2

229/11.35.09.500 298. 0.849 5.89 O.19 O.188 0/2

229/11.35.36.500 300. 0.852 6.02 -0.04 0.193 0/2

229/11.35.42.000 302. 0.855 7.01 -0.27 0.216 0/2

229/11.35.51.000 293. 0.845 8.01 0.02 0.309 0/2

229/11.35.52.000 295. 0.847 8.01 -0.04 0.324 0/2

229/11.37.34.000 298. 0.844 5.70 0.05 0.191 5/2

229/11.37.40.000 297. O.844 5.70 -0.01 O.180 5/2

229/11.38.11.500 297. 0.845 6.00 -0.53 O.197 5/2

229/11.38.12.500 298. 0.846 6.02 -0.44 0.207 5/2

229/11.38.18.500 300. 0.849 7.10 -0.33 0.246 5/2

229/11.38.22.000 300. 0.850 8.01 -0.41 0.395 5/2

229/11.38.25.000 299. 0.850 8.01 -0.04 0.386 5/2

229/11.38.28.500 299. 0.850 8.01 -0.18 0.430 5/2

229/11.38.33.500 299. 0.851 9.02 -0.07 0.866 5/2

229/11.35.07.500 297. 0.849 5.72 0.28 O.190 0/2

229/11.35.10.500 298. 0.849 5.71 O.19 O.192 0/2

229/11.35.11.500 298. 0.849 5.72 0.25 O.181 0/2

229/11.35.23.000 296. 0.848 5.52 O.11 O.192 0/2

229/11.35.28.500 297. 0.848 5.49 0.08 O.197 0/2

229/11.35.29.000 297. 0.848 5.49 O.19 O.191 0/2

784
TableK-1.Continued.

Flight/Time QINElb/fl2 MINF ALPT,deg BETA,deg THETA,in. Camber

229/11.35.29.500 297. 0.848 5.49 0.22 O.186 0/2

229/11.35.37.000 300. 0.852 6.02 0.02 O.191 0/2

229/11.35.37.500 301. 0.852 6.07 -0.01 O.188 0/2

229/11.35.41.500 302. 0.855 6.96 -0.33 0.218 0/2

229/11.35.42.500 301. 0.854 7.06 -0.33 0.226 0/2

229/11.35.50.000 292. 0.844 7.92 O.19 0.292 0/2

229/11.35.50.500 293. 0.844 7.92 0.02 0.278 0/2

229/11.36.01.500 310. 0.860 8.58 0.66 0.701 0/2

229/11.36.02.000 312. 0.861 8.67 0.75 0.821 0/2

229/11.36.24.500 314. 0.860 9.15 -0.15 0.915 0/2

229/11.37.33.500 298. 0.845 5.70 0.02 0.218 5/2

229/11.37.37.000 297. 0.844 5.56 0.02 O.192 5/2

229/11.37.38.000 297. 0.844 5.53 0.02 O.187 5/2

229/11.37.38.500 297. 0.844 5.53 -0.04 O.188 5/2

229/11.37.55.000 297. 0.844 5.71 -0.01 O.195 5/2

229/11.37.55.500 297. 0.844 5.71 -0.01 O.192 5/2

229/11.38.10.500 297. 0.845 5.91 -0.64 O.194 5/2

229/11.38.11.000 297. 0.845 5.91 -0.56 O.199 5/2

229/11.38.12.000 297. 0.845 5.96 -0.53 0.200 5/2

229/11.38.13.500 297. 0.845 6.11 -0.38 0.212 5/2

229/11.38.17.500 299. 0.848 6.91 -0.44 0.237 5/2

229/11.38.18.000 300. 0.849 6.98 -0.38 0.233 5/2

229/11.38.19.000 300. 0.850 7.27 -0.44 0.266 5/2

229/11.38.22.500 300. 0.850 8.04 -0.36 0.396 5/2

229/11.38.24.000 299. 0.850 8.04 -0.21 0.429 5/2

229/11.38.25.500 299. 0.850 8.01 -0.07 0.390 5/2

229/11.38.27.000 299. 0.849 8.01 -0.09 0.420 5/2

229/11.38.28.000 298. 0.849 8.01 -0.12 0.387 5/2

229/11.38.31.000 299. 0.851 8.20 -0.09 0.448 5/2

229/11.38.31.500 299. 0.851 8.38 -0.04 0.588 5/2

229/11.38.32.000 299. 0.851 8.78 O.11 0.780 5/2

229/11.38.32.500 299. 0.851 8.85 0.05 0.877 5/2

229/11.38.33.000 299. 0.851 8.90 0.08 0.879 5/2

229/11.38.34.000 299. 0.851 9.08 -0.09 0.865 5/2

229/12.31.28.000 302. 0.902 5.70 -0.12 0.257 0/2

229/12.31.28.500 302. 0.902 5.70 0.28 0.256 0/2

229/I2.31.37.000 301. 0.899 5.70 0.22 0.247 0/2

785
TableK-1.Continued.

Flight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

229/12.31.42.000 302. 0.898 6.03 O.11 0.269 0/2

229/12.31.44.500 301. 0.897 6.11 -0.01 0.267 0/2

229/12.31.58.000 300. 0.895 6.70 -0.47 0.310 0/2

229/12.31.59.000 300. 0.895 7.27 -0.33 0.542 0/2

229/12.32.01.000 299. 0.893 7.60 -0.41 0.952 0/2

229/12.32.01.500 298. 0.892 7.58 -0.53 0.938 0/2

229/12.32.03.000 298. O.892 7.23 -0.15 0.650 0/2

229/12.32.03.500 298. 0.893 7.32 0.05 0.704 0/2

229/12.32.04.000 298. 0.893 7.35 0.31 0.770 0/2

229/12.32.05.500 299. 0.895 7.58 0.25 0.951 0/2

229/12.32.59.000 324. 0.901 6.98 0.05 0.800 0/2

229/12.33.43.500 300. 0.896 6.45 0.05 0.585 5/2

229/12.33.44.000 300. 0.896 6.43 -0.04 0.694 5/2

229/12.33.50.000 300. 0.897 5.83 -0.15 0.355 5/2

229/12.33.50.500 300. 0.897 5.83 -0.21 0.345 5/2

229/12.33.51.500 300. 0.898 5.71 -0.04 0.319 5/2

229/12.33.52.500 301. 0.899 5.83 -0.04 0.367 5/2

229/12.33.53.000 301. 0.899 5.79 -0.01 0.367 5/2

229/12.33.58.000 302. 0.901 6.06 0.02 0.608 5/2

229/12.34.06.000 304. 0.904 6.38 -0.18 0.904 5/2

229/12.34.07.000 304. 0.904 6.33 -0.07 0.894 5/2

229/12.34.07.500 304. 0.904 6.42 -0.36 0.874 5/2

229/12.34.12.500 304. 0.904 6.33 -0.24 0.903 5/2

229/12.34.13.500 304. 0.904 6.32 0.46 0.861 5/2

229/12.34.22.000 303. 0.904 6.33 -0.62 0.767 5/2

229/12.34.22.500 303. 0.904 6.59 -0.47 0.914 5/2

229/12.34.23.000 303. O.903 6.80 -0.38 O.968 5/2

229112.31.41.500 302. 0.898 6.00 -0.04 0.276 0/2

229/12.31.45.500 301. 0.896 6.02 -0.27 0.262 0/2

229/12.31.58.500 300. 0.895 6.99 -0.12 0.373 0/2

229/12.33.38.500 299. 0.895 6.06 -0.09 0.399 5/2

229/12.33.39.500 299. 0.896 5.98 -0.21 0.385 5/2

229/12.33.49.500 299. 0.896 6.00 -0.01 0.409 5/2

229/12.34.02.000 304. 0.903 6.02 O.14 0.664 5/2

229/12.34.15.500 304. 0.904 6.00 -0.09 0.623 5/2

229/12.34.23.500 303. 0.903 6.92 -0.44 0.895 5/2

229/12.31.46.000 301. 0.896 5.93 -0.09 0.252 0/2

786
TableK-1.Continued.

Flight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

229/12.31.54.000 301. 0.895 5.97 0.11 0.260 0/2

229/12.31.57.000 300. 0.896 6.02 -0.64 0.245 0/2

229/12.33.57.000 302. 0.901 6.08 -0.15 0.559 5/2

229/12.33.59.000 302. 0.902 5.97 -0.27 0.542 5/2

229/12.34.01.000 303. 0.903 5.97 -0.09 0.576 5/2

229/12.34.01.500 303. 0.903 6.02 0.08 0.607 5/2

229/11.42.02.500 302. 0.951 6.50 0.22 0.594 0/2

229/11.42.03.000 301. 0.950 6.47 0.34 0.608 0/2

229/11.42.03.500 301. 0.950 6.36 0.37 0.621 0/2

229/11.42.04.000 301. 0.950 6.14 0.25 0.611 0/2

229/11.42.04.500 301. 0.950 6.10 0.34 0.646 0/2

229/11.42.05.000 301. 0.950 6.00 0.22 0.628 0/2

229/11.42.05.500 301. 0.950 5.98 0.25 0.627 0/2

229/11.42.06.500 301. 0.950 6.10 0.22 0.624 0/2

229/11.42.07.000 301. 0.950 6.07 0.28 0.624 0/2

229/11.42.15.500 300. 0.949 6.06 0.22 0.689 0/2

229/11.42.16.500 300. 0.949 6.10 0.31 0.697 0/2

229/11.42.28.000 301. 0.950 6.38 -0.15 0.682 0/2

229/11.42.28.500 301. 0.950 6.44 -0.12 0.698 0/2

229/11.42.29.000 301. 0.950 6.61 -0.07 0.701 0/2

229/11.42.29.500 301. 0.949 6.56 -0.01 0.709 0/2

229/11.42.31.000 301. 0.949 6.86 0.05 0.739 0/2

229/11.42.31.500 301. 0.949 6.95 0.05 0.713 0/2

229/11.42.32.000 301. 0.949 7.08 0.05 0.730 0/2

229/11.42.32.500 301. 0.949 7.16 0.02 0.732 0/2

229/14.04.24.500 450. 0.802 3.95 0.34 0.172 0/2

229/14.04.25.000 449. 0.802 4.01 0.22 O.175 0/2

229/14.04.26.000 450. 0.802 4.04 0.25 0.174 0/2

229/14.04.27.000 450. O.803 4.01 0.28 O.175 0/2

229/14.04.36.500 452. 0.804 4.04 0.37 O.176 0/2

229/14.04.38.000 452. 0.804 3.95 0.31 O.173 0/2

229/14.04.38.500 452. 0.804 4.01 0.34 O.174 0/2

229/14.04.46.500 452. 0.804 4.01 0.31 O.173 0/2

229/14.05.12.000 454. 0.805 4.94 0.02 O.185 0/2

229/14.05.12.500 455. 0.805 5.07 0.25 0.240 0/2

229/I4.05.13.000 455. 0.805 5.14 O.11 O.188 0/2

229/14.05.16.000 457. 0.807 6.04 0.05 0.247 0/2

787
TableK-1.Continued.

Flight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

229/14.05.16.500 457. 0.807 6.09 0.05 0.200 0/2

229/14.05.18.000 456. 0.807 6.20 -0.07 O.197 0/2

229/14.05.21.000 455. 0.805 6.96 0.37 0.227 0/2

229/14.05.21.500 455. 0.805 7.02 O.37 O.226 0/2

229/14.05.22.000 455. 0.805 7.08 0.34 0.218 0/2

229/14.05.22.500 455. 0.805 7.01 O.17 0.224 0/2

229/14.05.23.000 455. 0.804 7.01 0.25 0.238 0/2

229/14.05.26.5O0 460. O.808 7.93 O.28 O.247 0/2

229/14.05.27.000 460. 0.808 8.02 0.22 0.237 0/2

229/14.05.27.500 460. 0.808 7.97 0.25 0.253 0/2

229/14.05.28.000 461. 0.808 8.01 O.25 0.246 0/2

229/14.05.28.500 461. 0.808 8.02 0.34 0.251 0/2

229/14.05.36.500 472. 0.813 8.52 0.19 0.335 0/2

229/14.05.37.000 473. 0.813 8.52 0.17 0.331 0/2

229/14.05.37.500 473. 0.813 8.48 0.08 0.327 0/2

229/14.05.38.000 473. O.813 8.63 O.14 O.340 0/2

229/14.05.38.500 473. 0.813 8.75 0.22 0.370 0/2

229/14.05.39.000 472. 0.812 8.75 0.28 0.393 0/2

229/14.05.39.500 472. 0.812 8.93 0.37 0.430 0/2

229/14.05.40.000 471. 0.811 9.14 0.25 0.444 0/2

229/14.05.43.000 462. 0.804 9.97 0.11 0.744 0/2

229/14.05.46.000 455. 0.797 9.97 0.05 0.639 0/2

229/14.07.12.500 451. O.801 4.18 O.28 O.181 5/2

229/14.07.14.000 450. 0.800 4.19 0.34 O.183 5/2

229/14.07.19.500 450. 0.800 4.19 0.19 0.183 5/2

229/14.07.20.000 450. 0.801 4.18 0.43 O.181 5/2

229/14.07.34.500 452. 0.801 4.18 0.28 O.180 5/2

229/14.07.35.000 452. 0.801 4.19 0.34 O.183 5/2

229/14.07.42.500 454. O.801 4.84 -0.85 O.192 5/2

229/14.07.43.000 454. 0.801 5.00 -1.25 0.229 5/2

229/14.07.43.500 454. 0.801 5.21 -1.31 O.194 5/2

229/14.07.44.500 454. 0.801 5.83 -0.38 0.200 5/2

229/14.07.45.000 454. 0.801 6.11 0.08 0.203 5/2

229/14.07.45.500 454. 0.801 6.33 0.43 0.217 5/2

229/14.07.46.500 453. 0.800 6.69 0.48 0.211 5/2

229/14.07.47.000 452. 0.799 6.96 0.40 0.233 5/2

229/14.07.47.500 451. 0.798 7.05 0.25 0.263 5/2

788
TableK-1.Continued.

Hight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

229/14.07.48.000 451. 0.798 7.08 O. 17 0.225 5/2

229/14.07.50.500 451. 0.798 7.60 0.34 0.232 5/2

229/14.07.51.000 45 I. 0.798 7.57 0.31 0.240 5/2

229/14.07.51.500 452. 0.798 7.63 0.31 0.226 5/2

229/14.07.52.000 452. 0.798 7.92 0.40 0.273 5/2

229/14.07.52.500 452. 0.798 8.00 0.31 0.271 5/2

229/14.07.53.500 452. 0.798 8.11 0.02 0.283 5/2

229/14.07.54.000 453. 0.798 8.11 0.28 0.274 5/2

229/14.07.57.500 458. 0.802 7.99 0.46 0.244 5/2

229/14.07.58.000 460. 0.803 7.96 0.34 0.264 5/2

229/14.07.58.500 460. 0.804 8.05 0.28 0.261 5/2

229/14.08.05.000 475. 0.813 9.09 0.28 0.445 5/2

229/14.08.05.500 476. 0.813 9.11 0.25 0.473 5/2

229/14.08.06.000 476. O.814 9.08 0.22 0.461 5/2

229/14.08.14.500 467. 0.802 9.99 0.05 0.681 5/2

230/08.53.04.500 511. 0.780 2.82 0.72 0.201 0/2

230/08.53.06.000 505. 0.778 2.82 0.46 O.194 0/2

230/08.53.06.500 502. 0.777 2.82 0.54 O. 190 0/2

230/08.53.09.000 498. 0.775 2.79 0.60 O. 154 0/2

230/08.53.09.500 499. 0.775 2.85 0.60 O. 160 0/2

230/08.53.15.500 516. 0.785 3.97 0.63 0.215 0/2

230/08.53.16.000 518. 0.786 4.06 0.57 O. 175 0/2

230/08.53.17.000 524. 0.789 4.03 0.63 0.214 0/2

230/08.54.44.500 514. 0.783 4.20 0.66 O.188 0/3

230/08.54.46.000 513. 0.783 4.20 0.66 O.185 0/3

230/08.54.47.500 513. 0.783 4.19 0.60 O.185 0/3

230/08.54.48.500 513. 0.783 4.19 0.54 O.183 0/3

230/08.54.54.500 512. 0.782 5.80 0.66 0.214 1/4

230/08.54.55.000 511. 0.781 5.99 0.60 0.253 1/4

230/08.54.55.500 509. 0.780 6.02 0.66 0.223 1/4

230/08.54.56.000 507. 0.779 6.21 0.63 0.229 1/4

230/08.54.57.000 500. 0.775 6.70 0.46 0.258 2/5/4/5

230/08.54.57.500 496. 0.772 6.70 0.51 0.262 2/5

230/08.54.58.000 492. 0.770 6.59 0.60 0.272 2/5

230/08.55.05.500 444. 0.747 2.63 0.69 O.154 0/2

230/08.55.06.500 442. 0.746 2.62 0.77 O.148 0/2

230/08.55.07.500 440. 0.745 2.62 0.75 O.152 0/2

789
TableK-1.Continued.

Flight/Time QINF,lb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

230/08.55.09.500 441. 0.746 3.10 0.77 O.159 0/2

230/08.55.12.000 448. 0.751 3.10 0.80 0.163 0/3/2/2

230/08.55.13.500 455. 0.755 3.10 0.77 O.160 0/2

230/08.55.26.500 551. 0.804 6.29 0.60 0.258 1/4

230/08.55.27.000 552. 0.804 6.28 0.66 0.259 1/5/4/4

230/08.55.27.500 554. 0.805 6.24 0.72 0.266 1/5/4/4

230/08.55.34.000 558. 0.805 6.21 0.63 0.234 1/4

230/08.55.42.000 509. 0.783 2.57 0.57 O.193 0/2

230/08.55.43.000 503. 0.780 2.59 0.66 O.155 0/2

230/08.55.44.000 498. 0.778 2.59 0.75 O.190 0/2

230/08.55.46.000 494. 0.776 2.96 0.69 O.196 0/2

230/08.55.46.500 494. 0.775 3.02 0.66 O.163 0/2

230/08.55.47.000 494. 0.776 3.01 0.75 O.162 0/2

230/08.55.54.000 524. 0.792 3.96 0.66 0.220 0/3

230/08.55.54.500 527. 0.794 3.98 0.66 O.185 0/3

230/08.56.00.000 564. 0.813 4.00 0.60 0.218 0/3

230/08.56.01.500 571. O.815 3.97 0.63 0.219 0/3

230/09.00.30.000 513. 0.783 4.01 0.66 0.186 0/3

230/09.00.30.500 514. 0.785 4.02 0.57 O.180 0/3

230/09.00.31.000 514. 0.784 3.98 0.75 0.187 0/3

230/09.00.31.500 513. 0.784 4.02 0.46 0.228 0/3

230/09.00.35.000 510. 0.781 4.17 0.63 O.192 0/3

230/09.00.36.500 512. 0.783 4.18 0.63 O.186 0/3

230/09.00.45.500 513. 0.785 7.89 0.34 0.518 3/6

230/09.00.46.000 510. 0.782 8.37 0.34 0.594 3/6

230/09.00.46.500 506. 0.780 7.80 0.43 0.632 3/6

230/09.00.56.000 511. 0.783 8.11 0.86 0.555 3/6

230/09.00.56.500 509. 0.782 8.22 0.75 0.659 3/6

230/09.00.57.000 506. 0.780 8.46 0.69 0.736 3/6

230/09.00.57.500 503. 0.777 8.44 0.60 0.722 3/6

230/09.01.04.500 497. 0.775 5.77 0.98 0.211 1/4

230/09.01.05.000 498. 0.776 6.65 0.83 0.228 1/4

230/09.01.08.500 485. 0.766 9.05 0.14 0.714 4/7

230/09.01.09.000 481. 0.763 9.10 0.25 0.691 4/7

230/09.01.19.000 454. 0.745 9.18 0.63 0.453 4/7

230/09.01.19.500 450. 0.742 8.88 0.75 0.606 4/7

230/09.01.20.000 447. O.740 8.65 O.83 0.584 4/7

790
TableK-1.Continued.

Flight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

230/09.01.20.500 443. 0.737 8.87 0.83 0.556 4/7

230/09.01.21.000 440. 0.734 9.10 0.80 0.490 4/7

230/09.01.21.500 437. 0.732 8.87 0.86 0.537 4/7

230/09.01.24.000 434. 0.731 4.87 -1.51 0.194 1/4

230/09.01.25.000 435. 0.731 5.02 -0.56 0.193 1/4

230/09.01.28.500 433. 0.732 3.09 0.80 0.164 0/3

230/09.01.29.000 434. 0.733 3.01 0.72 0.167 0/3

230/09.01.29. 500 437. 0.715 3.06 0.75 0.161 0/3

230/09.01.35.500 449. 0.746 4.19 0.63 0.180 1/3

230/09.01.36.500 453. 0.749 4.23 0.66 0.179 1/3

230/09.01.37.500 456. 0.751 4.24 0.63 0.182 1/3

230/09.01.39.000 464. 0.757 4.24 0.63 0.184 1/3

230/09.01.39.500 465. 0.758 4.24 0.57 0.185 1/3

230/09.01.41.500 473. 0.764 4.21 1.29 0.182 1/3

230/09.04.26.500 478. 0.767 4.97 1.90 0.199 1/4/3/3

230/09.04.27.000 478. 0.766 4.94 1.53 0.197 1/4/3/3

230/09.04.27.500 478. 0.767 5.00 1.47 0.253 1/4/3/3

230/09.04.35.000 450. 0.747 4.91 0.40 0.206 1/4/5/5

230/09.04.35.500 450. 0.747 5.16 -0.64 0.213 1/4/5/5

230/09.04.36.000 451. 0.748 4.96 -1.11 0.211 1/4/5/5

230/09.07.50.000 519. 0.788 4.12 0.08 0.195 0/3/4/4

230/09.07.50.500 520. 0.789 4.13 -0.38 0.229 0/3/4/4

230/09.07.51.000 521. 0.790 4.22 -0.62 0.194 0/3/4/4

230/09.07.56.500 524. 0.792 6.69 0.46 0.266 2/5/4/5

230/09.07.57.000 523. 0.791 6.75 0.63 0.261 2/5

230/09.08.17.500 254. 0.595 6.13 0.69 0.184 3/5/5/6

230/09.08.18.000 247. 0.589 6.07 0.43 0.191 3/5

230/09.08.18.500 241. 0.583 6.02 0.22 0.174 3/5

230/09.08.19.000 235. 0.578 5.67 0.22 0.164 3/5

230/09.08.28.000 161. 0.500 5.12 0.57 0.117 2/4

230/09.08.28.500 159. 0.498 5.19 0.54 0.110 2/4

230/09.08.29.000 158. 0.496 5.17 0.40 0.111 2/4/4/5

230/09.08.29.500 156. 0.494 5.14 0.25 0.110 2/4/4/5

230/09.08.30.000 154. 0.492 5.18 0.22 0.130 2/4

230/09.08.34.000 148. 0.484 5.54 0.66 0.104 2/5

230/09.08.34.500 147. 0.484 5.53 0.69 0.124 2/5

230/09.08.35.000 147. 0.484 5.49 0.75 0.111 2/5

791
TableK-1.Continued.

Flight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA, in. Camber

230/09.08.35.500 148. 0.485 5.54 0.83 O.132 2/5

230/09.11.18.000 524. 0.791 7.33 0.25 0.385 2/5/5/-1

230/09.11.18.500 523. 0.790 7.01 0.31 0.430 2/5/5/- 1

230/09.11.19.000 521. 0.789 7.14 0.48 0.410 2/515/-1

230/09.11.19.500 519. 0.787 7.32 0.40 0.414 2/5/5/- 1

230/08.46.19.000 597. 0.796 3.98 0.51 0.224 0/2

230/08.46.20.500 593. 0.793 4.02 0.60 0.233 0/2

230/08.46.25.500 589. 0.791 4.06 0.43 0.218 0/2

230/08.46.26.500 588. 0.791 4.05 0.48 0.219 0/2

230/08.46.27.500 587. 0.790 4.01 0.60 0.220 0/2

230/08.46.44.500 609. 0.806 3.52 0.28 0.393 5/6

230/08.46.45.000 609. 0.807 3.52 0.31 0.354 5/6

230/08.46.46.500 608. 0.806 3.53 0.22 0.375 5/6

230/08.46.48.000 606. 0.804 3.53 0.40 0.356 5/6

230/08.46.49.500 605. 0.804 3.53 0.34 0.380 5/6

230/08.46.55.000 603. 0.802 3.53 0.40 0.372 5/6

230/08.47.24.000 605. 0.803 4.02 0.63 0.220 0/2

230/08.47.32.500 602. 0.800 4.03 0.75 0.222 0/2

230/08.48.03.500 601. 0.799 4.02 0.66 0.221 0/2

230/08.48.18.000 600. 0.795 5.25 1.15 0.227 0/2

230/08.48.18.500 600. 0.795 4.92 0.98 0.219 0/2

230/08.48.19.000 599. 0.795 4.84 1.00 0.225 0/2

230/08.48.20.000 597. 0.793 5.06 0.83 0.227 0/2

230/08.48.27.500 573. 0.783 5.89 0.80 0.235 0/2

230/08.48.28.000 571. 0.782 5.98 0.95 0.257 0/2

230/08.48.28.500 568. 0.781 5.96 0.92 0.234 0/2

230/08.48.29.000 565. 0.779 5.86 0.75 0.230 0/2

231/13.03.14.500 601. 0.799 4.01 0.48 0.170 0/2

231/13.03.30.000 596. 0.795 4.01 0.48 0.169 0/2

231/13.03.31.500 593. 0.794 4.02 0.40 0.171 0/2

231 /13.03.32.500 593. 0.793 4.02 0.40 O. 171 0/2

231/13.03.42.000 598. 0.796 3.04 0.48 O. 161 0/2

231/13.03.43.000 597. 0.795 3.02 0.48 O. 156 0/2

231/13.03.47.000 616. 0.804 3.06 0.31 0.162 0/2

231/13.03.47.500 619. 0.805 3.07 0.37 O. 159 0/2

231 / 13.03.49.500 640. O.814 5.95 0.51 O. 197 0/2

231/13.03.50.000 642. 0.815 6.40 0.40 0.208 0/2

792
TableK-1.Concluded.

Flight/Time QINElb/ft2 MINF ALPT,deg BETA,deg THETA,in. Camber

231/13.03.50.500 643. 0.814 6.86 0.40 0.216 0/2

231/13.03.51.000 641. 0.813 7.20 0.51 0.221 0/2

231/13.03.51.500 639. 0.811 7.43 0.60 0.244 0/2

231/13.03.52.000 635. 0.808 7.69 0.57 0.250 0/2

23 Ill 3.03.52.500 628. 0.805 8.08 0.66 0.252 0/2

231/13.03.54.000 605. 0.792 8.66 0.51 0.303 0/2

231/13.03.54.500 597. 0.787 8.59 0.60 0.297 0/2

231 l13.03.55.000 587. 0.782 8.75 0.51 0.309 0/2

231 l13.05.56.500 600. 0.801 3.98 0.37 0.180 0/3

231/13.06.08.500 605. 0.804 3.98 0.34 0.182 0/3

231/13.06.22.000 600. 0.801 3.98 0.46 0.182 0/3

231/13.06.58.000 599. 0.800 3.01 0.40 0.159 0/2

231/13.06.59.500 603. 0.801 3.03 0.46 0.159 0/2

23 l/13.07.01.000 613. 0.807 3.03 0.57 0.154 0/2

231 /13.07.02.500 625. 0.813 3.46 0.46 0.166 0/2

231/13.07.03.000 629. 0.815 3.95 0.40 0.168 0/2

231/13.07.04.000 635. 0.817 5.04 0.37 0.197 0/3

231/13.07.04.500 637. 0.818 5.50 0.48 0.212 0/3

231/I 3.07.06.000 635. 0.815 6.39 0.37 0.245 1/4

231/13.07.06.500 632. 0.813 6.62 0.34 0.259 1/4

231/13.07.09.000 609. 0.800 7.01 0.37 0.358 2/5

231/13.07.09.500 601. 0.796 7.04 0.40 0.392 2/5

231/13.07.10.500 581. 0.786 6.92 0.37 0.328 2/5

231/13.07.11.500 558. 0.773 5.05 0.34 0.229 2/5

231/13.08.43.500 609. 0.805 3.91 0.02 0.183 0/3

231/13.08.44.000 609. 0.805 3.99 -0.01 0. i 83 0/3

231/13.08.44.500 610. 0.806 3.95 -0.04 0.183 0/3

231 / 13.08.45.000 611. 0.806 4.07 -0.04 0.183 0/3

231/13.08.47.000 613. 0.807 4.66 -0.04 0.199 0/3

231 /13.08.47.500 613. 0.807 4.85 -0.09 0.200 0/3

231 / 13.08.48.000 613. 0.807 5.16 0.05 0.208 0/3

231/13.08.49.500 611. 0.805 5.86 -0.07 0.219 I/4

231/13.08.50.500 610. 0.804 6.04 -0.24 0.237 1/4

231/13.09.02.000 629. 0.801 5.09 0.60 0.210 1/4

231/13.09.02.500 629. 0.800 4.77 0.37 0.206 1/4

793
TableK-2.Listingof data.

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:17:26.000 11:17:30.000 11:17:40.000 11:17:49.000 11:18:00.000

Camber 0/2

QINF = 303.7

MINF = 0.605

ALPT = 6.47

BETA = 0.40

H = 15150.

TINF = 17.2

RNPU -- 2.7E+06

PSUR = 1168.4

MTOP -- 0.62

Y, in. U/UTOP W/UTOP

0.240 0.6606 -0.2293

0.470 0.7765 -0.0660

0.970 0.8983 0.0564

1.470 0.9877 -0.1889

1.960 1.0189 -0.1914

2.330 0.9875 -0.1416

2.990 0.9956 -0.2241

3.490 1.0068 -0.1209

3.990 1.0040 -0.1370

4.960 1.0000 -0.0893

Camber 0/2

QINF = 305.2

MINF = 0.606

ALPT = 6.51

BETA = 0.51

H= 15141.

TINF = 17.4

RNPU = 2.7E+06

PSUR = 1168.4

MTOP = 0.63

U/UTOP W/UTOP

0.6623 -0.2280

0.7732 -0.0581

0.8891 0.0567

0.9789 -0.1874

1.0206 -0.1938

0.9895 -0.1427

0.9984 -0.2210

1.0038 -0.127 t

0.9988 -0.1479

1.0000 -0.0906

Camber 0/2

QINF = 305.9

MINF = 0.606

ALPT = 6.50

BETA = 0.45

H= 15119.

TINF = 17.0

RNPU = 2.7E+06

PSUR = 1168.4

MTOP -- 0.62

U/UTOP W/UTOP

0.6642 -0.2088

0.7809 -0.0554

0.8955 0.0577

0.9852 -0.1811

1.0266 -0.1879

0.9920 -0.1375

0.9987 -0.2130

1.0065 -0.1288

1.0015 -0.1422

1.0000 -0.0880

Camber 0/2

QINF = 306.9

MINF = 0.607

ALPT = 6.25

BETA = 0.51

H = 15120.

TINF = 18.3

RNPU = 2.7E+06

PSUR = 1169.5

MTOP = 0.62

U/UTOP W/LrrOP

0.6650 -0.2270

0.7730 -0.0676

0.8953 0.0591

0.9896 -0.1821

1.0225 -0.1913

0.9920 -0.1386

1.0016 -0.2166

1.0068 -0.1322

1.0015 -0.1439

1.0000 -0.0880

Camber

QINF =

MINF =

ALPT =

BETA --

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6578

0.7713

0.8932

0.9854

1.0223

0.9924

1.0025

1.0087

1.0045

1.0000

0/2

308.8

0.609

6.28

0.48

15111.

17.7

2.7E+06

1169.5

0.63

W/UTOP

-0.2169

-0.0674

0.0575

-0.1834

-0.1900

-0.1375

-0.2203

-0.1219

-0.1356

-0.0936

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:18:00.500 11:18:01.000 11:18:01.500 11:18:02.000 11:18:11.500

Camber 0/2

QINF = 308.8

MINF = 0.609

ALPT = 6.29

BETA = 0.54

H= 15111.

TINF = 18.4

RNPU = 2.7E+06

PSUR = 1168.4

MTOP = 0.63

Y,in. U/UTOP W/UTOP

0.240 0.6589 -0.2175

0.470 0.7707 -0.0608

0.970 0.8975 0.0487

1.470 0.9839 -0.1809

1.960 1.0220 -0.1966

2.330 0.9929 -0.1300

2.990 1.0011 -0.2200

3.490 1.0096 -0.1167

3.990 1.0009 -0.1429

4.960 1.0000 -0.0898

Camber 0/2

QINF = 309.1

M1NF = 0.609

ALPT = 6.28

BETA = 0.51

H= 15111.

TINF = 18.4

RNPU = 2.7E+06

PSUR = 1168.4

MTOP = 0.63

U/UTOP W/UTOP

0.6668 -0.2472

0.7707 -0.0594

0.8922 0.0560

0.9881 -0.1798

1.0210 -0.1912

0.9937 -0.1376

1.0013 -0.2205

1.0068 -0.1472

0.9972 -0.1360

1.0000 -0.0898

Camber 0/2

QINF = 309.3

MINF = 0.610

ALPT = 6.28

BETA = 0.54

H= 15111.

TINF = 18.4

RNPU = 2.7E+06

PSUR -- t 168.4

MTOP = 0.62

U/UTOP W/UTOP

0.6729 -0.2297

0.7888 -0.0649

0.9101 0.0575

1.0018 -0.1865

1.0349 -0.1954

1.0047 -0.1458

1.0144 -0.2234

1.0073 -0.1450

1.0165 -0.1388

1.0000 -0.0987

Camber 0/2

QINF -- 309.3

MINF = 0.610

ALPT = 6.28

BETA = 0.48

H = 15122.

TINF = 18.7

RNPU = 2.7E+06

PSUR = 1168.4

MTOP = 0.63

U/UTOP W/UTOP

0.6652 -0.2271

0.7797 -0.0642

0.8937 0.0576

0.9921 -0.1816

1.0256 -0.1934

0.9930 -0.1419

1.0015 -0.2214

1.0116 -0.1267

0.9878 -0.1496

1.000O -0.0918

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6559

0.7671

0.8941

0.9818

1.0184

0.9887

0.9973

1.0050

0.9960

1.0000

0/2

310.5

0.611

6.28

0.22

15124.

18.2

2.7E+06

I 168.4

0.63

W/UTOP

-0.2164

-0.0577

0.0565

-0.1817

-0.1883

-0.1326

-0.2173

-0.1196

-0.1403

-0.0852

794
TableK-2.Continued.

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:18:12.000 11:18:12.500 11:18:17.500 11:18:34.000 11:18:42.000

Camber 0/2

QINF= 310.0

MINF= 0.610

ALPT = 6.29

BETA -- 0.02

H = 15123.

TINF = 17.9

RNPU = 2.7E+06

PSUR = 1169.5

MTOP = 0.63

Y, in. U/UTOP W/UTOP

0.240 0.6534 -0.2268

0.470 0.7684 -0.0578

0.970 0.8906 0.0591

1,470 0.9837 -0.1767

1.960 1.0211 -0.1861

2.330 0.9915 -0.1318

2.990 1.0001 -0.2173

3.490 1.0049 -0.1119

3.990 1.0009 -0.1318

4.960 1.0000 -0.0891

Camber 0/2

QINF = 309.5

MINF= 0.610

ALPT = 6.29

BETA = -0.15

H= 15123.

TINF = 18.0

RNPU = 2.7E+06

PSUR = 1168,4

MTOP = 0.63

U/UTOP W/UTOP

0.6555 -0.2275

0.7699 -0.0579

0.8976 0.0599

0.9840 -0.1736

1.0214 -0.1854

0.9918 -0.1287

0.9979 -0.2060

1.0062 -0.1216

1.0042 -0.1282

1.0000 -0.0821

Camber 0/2

QINF = 307.8

MINF = 0.608

ALPT = 7.03

BETA = -0.33

H= 15132,

TINF = 17.5

RNPU = 2.7E+06

PSUR = 1166.3

MTOP = 0.63

U/UTOP wRYroP

0.6544 -0.2309

0.7674 -0.0519

0.8830 0.0452

0.9798 -0.1746

1.0230 -0.1947

0.9948 -0.1389

1.0016 -0.2166

1.0067 -0.1322

1.0036 -0.1350

1.0000 -0.0880

Camber 0/2

QINF = 301.0

MINF = 0.603

ALPT = 8.08

BETA = -0.10

H = 15237.

TINF = 17.7

RNPU = 2.7E+06

PSUR = 1164.1

MTOP = 0.62

U/UTOP W/UTOP

0.6200 -0.2144

0.7306 -0.0352

0.8425 0.0304

0.9333 -0.1823

1.0087 -0.1864

0.9913 -0.1467

1.0018 -0.2226

1.0049 -0.1333

1.0046 -0.1541

1.00(X) -0.0967

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5384

0.6417

0.7469

0.8206

0.8866

0.9092

0.9538

0.9799

0.9834

1.0000

0/2

302.9

0.605

8.99

0.14

15294.

17.8

2.7E+06

1157.6

0.63

W/UTOP

-0.1904

0.0296

-0.0040

-0.1528

-0.1492

-0.1143

-0.2093

-0.1247

-0.1487

-0.0986

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:18:51.500 11:18:59.000 11:18:03.500 11:18:11,500 11:18:17,500

Camber 0/2

QINF = 296.5

MINF = 0.599

ALPT = 10.11

BETA = 0.34

H = 15266.

T1NF = 18.5

RNPU = 2.6E+06

PSUR= 1164.1

MTOP = 0.54

Y, in. U/UTOP W/UTOP

0,240 0.5731 -0.1205

0.470 0.7075 0.0844

0.970 0.7707 -0.0121

1,470 0.8159 -0.1287

1.960 0.8553 -0.1097

2.330 0.8478 -0.0684

2.990 0.8811 -0.1956

3,490 0.9300 -0.0519

3.990 0.9350 -0.0956

4.960 1.0000 -0.0774

Camber 0/2

QINF = 297.8

MINF = 0.598

ALPT= 10.15

BETA = 0.17

H = 15068.

TINF= 19.0

RNPU = 2.6E+06

PSUR = 1171.7

MTOP = 0.56

U/UTOP W/UTOP

0.5618 -0.1406

0.6929 0.0690

0.7629 -0.0128

0.8081 -0.1347

0.8375 -0.1145

0.8398 -0.0779

0.8772 -0.1924

0.9181 -0.0592

0.9453 -0.0983

1.0000 -0.0869

Camber 0/2

QINF = 309.3

MINF= 0.610

ALPT = 6.28

BETA = 0.48

H = 15122.

TI NF = 18.4

RNPU = 2.7E+06

PSUR = 1169.5

MTOP = 0.63

U/UTOP W/UTOP

0.6626 -0.2262

0.7702 -0.0673

0.8981 0.0599

0.9858 -0.1803

1.0211 -0.1906

0.9934 -0.1354

1.0000 -0.2130

1.0073 -0.1217

1.0035 -0.1394

1.0000 -0.0898

Camber 0/2

QINF= 310.5

MINF = 0.611

ALPT = 6.28

BETA = 0.22

H = 15124.

TINF = 18.2

RNPU = 2.7E+06

PSUR = 1168.4

MTOP = 0.63

U/UTOP W/UTOP

0.6559 -0.2164

0.7671 -0.0577

0.8941 0.0565

0.9818 -0.1817

1.0184 -0.1883

0.9887 -0.1326

0.9973 -0.2173

1.0050 -0.1196

0.9960 -0.1403

1.0000 -0.0852

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6544

0.7674

0.8830

0.9798

1.0230

0.9948

1.0016

1.0067

1.0036

1.0000

0/2

307.8

0.608

7.03

-0.33

15132.

17.5

2.7E+06

1166.3

0,63

W/UTOP

-0.2309

-0.0519

0.0452

-0.1746

-0.1947

-0.1389

-0.2166

-0.1322

-0.1350

-0.0880

795
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:18:20.500 11:18:21,000 11:18:24,000 11:18:26.000 11:18:34.000

Camber 0/2

QINF = 305.9

MINF = 0.607

ALPT = 7.74

BETA = 0.34

H -- 15141.

TINF = 17.7

RNPU = 2.7E+06

PSUR = 1165.2

MTOP = 0.63

Y, in. U/UTOP W/UTOP

0.240 0.6488 -0,2321

0.470 0.7566 -0.0630

0,970 0.8693 0.0366

1.470 0.9631 -0.1917

1,960 1.0151 -0.1959

2.330 0.9892 -0.1493

2.990 0.9993 -0.2301

3.490 1.0037 -0.1401

3,990 1.0026 -0.1619

4.960 1.00(_ -0.1020

Camber 0/2

QINF = 305.9

MINF = 0.607

ALPT = 8.03

BETA = 0.25

H= 15141.

TINF = 17.7

RNPU = 2.7E+06

PSUR = 1165.2

MTOP = 0.63

U/Lr'I'OP W/UTOP

0.6390 -0.2460

0.7373 -0.0517

0.8511 0.0276

0.9461 -0.1928

1.0052 -0.1965

0.9913 -0.1528

0.9999 -0.2316

1.0052 -0.1669

1.0032 -0.1537

1.0000 -0.1027

Camber 0/2

QINF = 303.2

MINF = 0.604

ALPT = 7.83

BETA = 0.28

H= 15161.

T1NF = 17.2

RNPU = 2.7E+06

PSUR = 1166.3

MTOP = 0.62

U/UTOP W/UTOP

0.6506 -0.2327

0.7551 -0.0555

0.8671 0.0389

0.9606 -0.1913

1.0104 -0.1980

0.9915 -0.1476

1.0014 -0.2271

1.0088 -0.1371

1.0050 -0.1646

1.0000 -0.1010

Camber 0/2

QINF = 302.7

MINF = 0.604

ALPT = 7.8l

BETA -- 0.25

H = 15172.

TINF = 17.3

RNPU = 2.7E+06

PSUR = 1160.8

MTOP = 0.63

U/UTOP W/UTOP

0.6375 -0.2345

0.7512 -0.0565

0.8678 0.0282

0.9538 -0.1879

1.0083 -0.1932

0.9904 -0.1458

0.9940 -0.2364

0,9994 -0.1344

0.9938 -0.1516

1.0000 -0,0981

Camber

QINF =

MlNF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP --

U/UTOP

0.6200

0.7306

0.8425

0.9333

1.0087

0.9913

1.0018

1.0049

1.0046

1.0000

0/2

301.0

0,603

8.08

-0.10

15237.

17.7

2.7E+06

1164.1

0.62

W/UTOP

-0.2144

-0.0352

0.0304

-0.1823

-0.1864

-0.1467

-0.2226

-0.1333

-0.1541

-0.0967

F111/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:18:36.500 11:18:41.500 11:18:42.000 11:18:42.500 11:18:45,000

Camber 0/2

QINF = 301.2

MINF = 0,603

ALFr = 8.08

BETA = -0.15

H = 15259.

TINF = 17.7

RNPU = 2.7E+06

PSUR = 1157.6

MTOP = 0.63

Y,in. U/UTOP W/UTOP

0,240 0.6372 -0.2247

0,470 0.7483 -0.0404

0.970 0.8626 0,0348

1,470 0.9520 -0.1827

1.960 1.0104 -0.1932

2.330 0.9937 -0.1457

2,990 1.0010 -0.2205

3.490 1.0066 -0.1451

3.990 1.0054 -0.1505

4.960 1.0000 -0.0960

Camber 0/2

QINF = 302.9

MINF = 0.605

ALPT = 8.95

BETA = 0.08

H = 15294.

TINF = 17.4

RNPU = 2.7E+06

PSUR = 1163.0

MTOP = 0.62

U/UTOP W/UTOP

0.5361 -0.2085

0.6467 0.0057

0.7404 0.0127

0.8276 -0.1453

0.8865 -0.1405

0.9145 -0.1214

0.9625 -0.2209

0.9809 -0.1298

0.9696 -0.1579

1.0000 -0.0966

Camber 0/2

QINF = 302.9

MINF = 0.605

ALPT = 8.99

BETA = 0.14

H = 15294.

TINF = 17.8

RNPU = 2.7E+06

PSUR = 1157.6

MTOP = 0.63

U/UTOP W/LrI'OP

0.5384 -0.1904

0.6417 0.0296

0.7469 -0.0040

0.8206 -0.1528

0.8866 -0.1492

0.9092 -0.1143

0.9538 -0.2093

0.9799 -0.1247

0.9834 -0.1487

1.0000 -0.0986

Camber 0/2

QINF = 303.4

MINF = 0.606

ALP'r= 9.18

BETA = 0.37

H -- 15294.

TINF= 18.t

RNPU = 2.7E+06

PSUR = 1156.5

MTOP = 0.62

U/UTOP W/UTOP

0.5393 -0.1751

0,6616 0.0237

0.7579 -0.0008

0.8325 -0.1777

0.8985 -0.1496

0.9252 -0.1194

0.9642 -0.2232

0.9900 -0.1213

0.9992 -0.1472

1.0000 -0.1081

Camber

QINF =

MINI: --

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5208

0.6356

0.7278

0.8000

0.8569

0.8789

0.9185

0.9607

0.9574

1.0000

0/2

302.2

0,605

9,50

0.22

15293.

17.9

2.7E+06

1158.8

0.62

W/UTOP

-0.1761

0.0259

-0.0035

-0.1564

-0.1277

-0.1078

-0.2005

-0.1023

-0.1328

-0.0956

796
Table K-2. Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:18:46.500 11:18:49.000 11:18:51.000 11:20:09.000 1t:20:23.500

Camber 0/2

QINF = 299.1

MINF = 0.602

ALP'l" = 9.50

BETA = 0.14

H = 15290.

TINF= 18.2

RNPU = 2.6E+06

PSUR = 1161.9

MTOP = 0.61

Y, in. U/UTOP W/UTOP

0.240 0.5448 -0.1773

0,470 0.6601 0.0474

0,970 0.7510 0,0100

1.470 0.8084 -0.1392

1.960 0.8675 -0.1289

2,330 0.8672 -0.0952

2,990 0.9055 -0.1978

3,490 0.9401 -0.0794

3.990 0.9499 -0.1273

4,960 1.0000 -0.0927

Camber 0/2

QINF = 300.0

MINF = 0.603

ALPT = 10.02

BETA = 0.05

H = 15291.

TINF = 17,7

RNPU = 2.7E+06

PSUR = 1161.9

MTOP = 0.58

U/UTOP W/UTOP

0.5501 -0.1914

0.6698 0.0731

0.7483 -0.0020

0.7922 -0.1332

0.8367 -0.1157

0.8475 -0.0774

0.8875 -0.1909

0.9322 -0.0956

0.9396 -0.1109

1.0000 -0.0835

Camber 0/2

QINF = 296.2

MINF = 0.599

ALPT = 10.03

BETA = 0.22

H = 15277.

TINF = 18.2

RNPU = 2.6E+06

PSUR = 1163.0

MTOP = 0.57

U/UTOP W/UTOP

0.5538 -0.1183

0.6804 0.0893

0.7435 -0.0065

0.7902 -0.1327

0.8381 -0.1089

0.8417 -0.0771

0.8793 -0.1881

0.9206 -0,0578

0.9219 -0.1103

1.0000 -0.0845

Camber 5/2

QINF= 299.2

MINF = 0.600

ALPT = 6.50

BETA = 0.34

H = 15102.

TINF= 18.1

RNPU = 2.7E+06

PSUR = 1168.4

MTOP = 0.62

U/UTOP W/UTOP

0.6751 -0.2699

0.7889 -0.0547

0,8981 0.0549

0.9935 -0.1824

1.0217 -0.1932

0.9923 -0.1473

1.0033 -0.2108

1.0133 -0.1454

1.0094 -0.1313

1.13000 -0.0904

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

O6611

0.7801

0.8948

0.9769

1.0183

0.9890

0.9930

1.0063

1.0017

1.0000

5/2

301.4

0.602

6.50

0.34

15115.

18.2

2.7E+06

1168.4

0.63

WPUTOP

-0.2182

-0.0405

0.0533

-0.1859

-0.1797

-0.1351

-0.2212

-0.1234

-0.1276

-0.0893

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:20:26.000 11:20:34.000 11:20:40.000 I 1:20:47,000 11:20:55.500

Camber 5/2

QINF = 302. I

MINF = 0.603

ALPT = 6.50

BETA = 0.37

H = 15127.

TINF= 18.1

RNPU = 2.7E+06

PSUR = 1168.4

MTOP = 0.62

Y, in. U/UTOP W/UTOP

0.240 0.6582 -0.1917

0,470 0,7787 -0.0585

0.970 0.9006 0.0475

1.470 0.9895 -0.1830

1.960 1.0220 -0.1898

2.330 0.9935 -0.1390

2.990 1.0011 -0.2188

3,490 1.0035 -0.0906

3.990 1.0032 -0.1534

4.960 1.0000 -0.0886

Camber 5/2

QINF = 301.6

MINF = 0,603

ALPT = 6,50

BETA = 0.11

H = 15160.

TINF = 17,7

RNPU = 2.7E+06

PSUR = 1165.3

MTOP = 0.62

U/UTOP W/UTOP

0.6649 -0.2434

0.7736 -0.0523

0.9024 0.0537

0.9888 -0.1763

1.0196 -0.1892

0.9935 -0.1357

1.0012 -0.2189

1.0079 -0.1531

1.0036 -0.1279

1.0000 -0.0871

Camber 5/2

QINF = 302.3

MINF = 0.604

ALPT = 6.54

BETA = 0.08

H = 15182.

TI NF = 18.0

RNPU = 2.7E+06

PSUR = 1165.3

MTOP = 0.62

U/UTOP W/UTOP

0.6678 -0.2051

0.7845 -0.0590

0.9062 0.0581

0.9907 -0.1809

1.0183 -0.1793

0,9973 -0.1373

0.9990 -0.2254

1.0090 -0.1185

1.0024 -0.1308

1.0000 -0.0834

Camber 5/2

QINF = 304.2

MINF = 0.606

ALPT = 6.50

BETA = 0.34

H = 15195.

TINF = 17.4

RNPU = 2.7E+06

PSUR = 1163.0

MTOP = 0.62

U/UTOP W/UTOP

0.6778 -0.2242

0.7787 -0.0460

0.8953 0.0559

0.9981 -0.1822

1.0278 -0.1976

1.0016 -0.1435

1.0069 -0.2099

1.0092 -0.1140

1.0038 -0.1349

1.0000 -0.0939

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6621

0.7720

0.8949

0.9821

1.0161

0.9884

0.9970

1.0027

0.9990

1.0000

5/2

305.6

0.607

6.8t

-0.10

15186.

17.6

2.7E+06

1167.3

0.62

W/UTOP

-0.1943

-0.0552

0.0597

-0.1833

-0.1860

-0.1337

-0,2248

-0.1180

-0.1303

-0.0837

797
TableK-2.Continued.

FI I 1/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:20:56.000 11:21:09.000 11:21:13.500 11:21:14.000 11:21:15.500

Camber 5/2

QINF = 3O5.6

MINF = 0,607

ALPT = 7.08

BETA = 0.02

H = 15174.

TINF= 17.3

RNPU = 2.7E+06

PSUR = 1161.9

MTOP = 0.63

Y,in. U/UTOP W/UTOP

0.240 0.6585 -0.2933

0.470 0.7725 -0.0618

0,970 0.8916 0.0438

1,470 0.9819 -0.1866

1.960 1.0156 -0.1890

2,330 0.9863 -0.1471

2.990 0.9954 -0.2269

3.490 1.0032 -0.1674

3,990 1.0053 -0.1408

4.960 1.0000 -0.0942

Camber 5/2

QINF = 301.2

MINF = 0,604

ALPT = 7.96

BETA = -0.33

H = 15303.

TINF = 17.6

RNPU = 2.7E+06

PSUR = 1156.5

MTOP = 0.63

U/UTOP W/UTOP

0,6411 -0.2257

0.7516 -0.0588

0.8709 0.0343

0.9687 -0.1873

1.0171 -0.1944

0.9906 -0.1499

0.9988 -0.2266

1.0049 -0.1315

1.0175 -0.1344

1.0000 -0.0949

Camber 5/2

QINF = 296.6

MINF = 0.600

ALPT = 8.01

BETA = -0.18

H = 15355.

TINF = 17.3

RNPU = 2.6E+06

PSUR = 1157.6

MTOP = 0.62

U/UTOP W/UTOP

0.6516 -0.2377

0.7626 -0.0643

0.8723 0.0275

0.9748 -0.1937

1.0236 -0.1996

0.9980 -0.1500

1.0051 -0.2270

1.0083 -0.1397

1.0078 -0.1471

1.0000 -0.0989

Camber 5/2

QINF = 296.4

MINF = 0,600

ALPT = 8.08

BETA = 0.19

H = 15355.

TINF = 17.0

RNPU = 2.6E+06

PSUR = 1152.2

MTOP = 0.63

U/UTOP W/UTOP

0.6488 -0.2729

0.7654 -0.0554

0.8750 0.0269

0.9720 4).1870

1.0111 -0.1916

0.9901 -0.1557

0.9979 -0.2337

1.0005 -0.1338

0.9983 -0.1536

1.0000 -0.1018

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/LrI'OP

0.6434

0.7492

0.8614

0.9589

1.0125

0.9901

0.9985

1.0037

1.0002

1.0000

5/2

297.3

0.601

8.95

0.19

15344.

17.3

2.6E+06

1154.3

0.63

W/UTOP

-0.2502

-0.0710

0.0074

-0.2028

-0.2014

-0.1601

-0.2373

-0.1590

-0.1591

-0.1092

F111/MAW BOUNDARY LAYER DATA. FLT 229

Time 11:21:16,500 11:21:17.000 11:21:24.000 11:21:24,500 11:21:31.500

Camber 5/2

QINF = 299.0

MINF = 0,602

ALPT = 8.89

BETA = 0.11

H = 15324.

TINF= 17.5

RNPU = 2.7E+06

PSUR = 1154.3

MTOP = 0.62

Y, in. U/UTOP W/UTOP

0.240 0.6462 -0.2393

0.470 0.7584 -0.0673

0.970 0.8631 0.0149

1.470 0.9659 -0.2064

1.960 1.0164 -0.2016

2.330 0.9945 -0.1595

2,990 1.0055 -0.2473

3.490 1.0101 -0.1557

3,990 1.0014 -0.1563

4,960 1.0000 -0.1091

Camber 5/2

QINF = 300.5

MINF = 0.603

ALPT = 9.19

BETA = 0.11

H = 15325.

T1NF = 17.3

RNPU = 2.7E+06

PSUR = 1157.6

MTOP = 0.63

U/UTOP W/UTOP

0.6437 -0.2386

0.7387 -0.0700

0.8580 0.0053

0.9488 -0.1997

1.0054 -0.2015

0.9856 -0.1577

0.9970 -0.2313

1.0013 -0.1221

1.0147 -0.1424

1.0000 -0.1025

Camber 5/2

QINF = 304.2

MINF = 0.606

ALPT = 10.04

BETA = -0.04

H = 15217.

TINF = 17.4

RNPU = 2.7E+06

PSUR = 1158.6

MTOP = 0.63

U/UTOP W/UTOP

0.6248 -0.2454

0.7330 -0.0661

0.8393 -0.0029

0.9402 -0.2025

1.0027 -0.2014

0.9900 -0.1595

0.9984 -0.2384

1.0005 -0.1599

1.0010 -0.1617

1.0000 -0.1123

Camber 5/2

Q1NF = 303.9

MINF = 0,606

ALPT = 10.02

BETA = -0.01

H = 15217.

TINF = 17.4

RNPU = 2.7E+06

PSUR = 1160.8

MTOP = 0.63

U/LrTOP W/UTOP

0.6295 -0.2553

0.7340 -0.0778

0.8476 -0.0029

0.9397 -0,2013

1.0079 -0.1996

0.9941 -0.1643

1.0032 -0.2385

1.0050 -0.1674

1.0049 -0.1637

1.0000 -0.1115

Camber

QINF --

M1NF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6420

0.7461

0.8549

0.9516

1.0137

1.0058

1.0151

1.0259

1.0188

1.0000

5/2

301.8

0,602

10.10

-0.12

15127.

17.8

2.7E+06

1162.9

0.62

W/UTOP

-0.2251

-0.0571

-0.0071

-0.2009

-0.2038

-0.1610

-0.2458

-0.1527

-0.1569

-0.1194

798
TableK-2.Continued.

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:21:33,000 11:26:48.500 11:27:10,500 11:27:17.000 11:28:05.500

Camber 512

QINF = 301.6

MINF = 0.602

ALPT = I 0.07

BETA -- -0.15

H= 15104.

TINF -- 17.5

RNPU = 2.7E+06

PSUR = 1168.3

MTOP = 0.63

Y, in. U/UTOP W/UTOP

0.240 0.6328 -0.2439

0.470 0.7333 -0.0466

0,970 0.8416 -0.0012

1.470 0.9431 -0.1995

1.960 1.0098 -0.1945

2,330 0.9863 -0.1646

2.990 1.0000 -0.2325

3.490 1.0070 -0.1601

3.990 0.9957 -0.1615

4.960 1.0000 -0.1084

Camber 0/2

QINF = 301.8

MINF = 0,800

ALPT = 5.90

BETA= 0.14

H = 28440,

TINF = -36.5

RNPU = 2.4E+06

PSUR = 661.6

MTOP = 0.81

U/UTOP W/UTOP

0.6132 °0.2222

0.7367 -0.0401

0.8701 0.0727

0.9772 -0.1812

1.0198 -0.1918

0.9921 -0.1409

1.0004 -0.2230

1.0067 -0.1327

0.9973 -0,1397

1.0000 -0.0903

Camber 0/2

QINF = 304.1

MINF = 0,802

ALPT= 7.12

BETA = 0.02

H = 28388.

TINF = -36.1

RNPU = 2.4E+06

PSUR = 659.4

MTOP = 0.81

U/UTOP W/UTOP

0.6374 -0.2277

0.7523 -0.0529

0.8688 0.0543

0.9474 -0.2071

1.0037 -0.2034

0.9927 -0.1540

1.0012 -0.2357

1.0060 -0.1504

1.0028 -0.1542

1.0000 -0.1033

Camber 0/2

QINF = 297.0

MINF = 0,793

ALPT = 8,04

BETA = -0.10

H = 28421.

TINF= -36.4

RNPU = 2.3E+06

PSUR = 658.3

MTOP = 0.79

U/UTOP W/UTOP

0.6931 -0.2284

0.7893 -0.0544

0.8598 0.0436

0.9286 -0.1996

0.9688 -0.1929

0.9723 -0.1612

0.9999 -0.2398

1.0131 -0.1569

1.0015 -0,1580

1.0000 -0.1086

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6866

0.7928

0.8693

0.9307

0.9659

0.9656

0.9974

1.0201

1.0069

1.0000

0/2

297. I

0,798

8.03

-0.27

28723.

°38.3

2.3E+06

651.7

0.79

W/UTOP

-0.2256

-0.0489

0.0437

-0.1971

-0.1927

-0.1532

-0.2492

-0,1938

-0.1656

-0.1072

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:31:02,500 11:31:08.000 11:31:11.500 11:31:13,000 11:31:17,500

Camber 5/2

QINF = 300.8

MINF = 0.801

ALPT = 5.97

BETA = 002

H = 28606.

TINF = -37.4

RNPU = 2.4E+06

PSUR = 658.2

MTOP = 0.80

Y, in. U/UTOP W/UTOP

0.240 0.6380 -0.2081

0.470 0.7595 -0.0458

0.970 0.8757 0.0725

1.470 0.9635 -0.1755

1.960 1.0115 -0.1975

2.330 0.9960 -0.1488

2.990 1.0025 -0.2287

3.490 1.0187 -0.1196

3.990 1.0023 -0.1395

4.960 1.0000 -0.0925

Camber 5/2

QINF = 299.2

MINF = 0.800

ALPT = 6.06

BETA = -0.85

H = 28649.

TINF = -37.2

RNPU = 2.3E+06

PSUR = 657.1

MTOP = 0.80

U/UTOP W/UTOP

0.6234 -0.1956

0.7480 -0.0246

0.8734 0.0766

0.9577 -0.1684

1.0109 -0.1846

0.9939 -0,1263

0.9994 -0.2123

1.0076 -0.0863

1.0192 -0.1235

1.0000 -0.0773

Camber 5/2

QINF = 298.1

MINF = 0.799

ALPT = 7.03

BETA = -0.04

H = 28658.

TINF = -37.0

RNPU = 2.3E+06

PSUR = 655.0

MTOP = 0.80

U/UTOP W/UTOP

0.6586 -0.2330

0.7677 -0.0553

0.8652 0.0565

0.9369 -0.1838

0.9895 -0.1913

0.9899 -0.1512

1.0052 -0.2375

1.0078 -0.1333

1.0089 -0.1480

1,0000 -0.0991

Camber 5/2

QINF = 297.2

MINF = 0.798

ALPT = 7.20

BETA = 0.14

H = 28668.

TINF = -37.2

RNPU = 2.3E+06

PSUR = 653.8

MTOP = 0.80

U/UTOP W/UTOP

0.6699 -0.3262

0.7798 -0.0514

0.8641 0.0620

0.9338 -0.1968

0.9852 -0.1928

0.9876 -0.1563

1.0043 -0.2391

1.0116 -0.1527

0.9973 -0.1543

1.0000 -0.1007

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6860

0.7883

0.8657

0.9348

0.9768

0.9799

1.0123

1.0306

1.0153

1.0000

5/2

294,9

0.796

8.05

-0.07

28753.

-37.4

2.3E+06

647.2

0.79

W/UTOP

-0.2385

-0.0568

0.0408

-0.1909

-0.1939

-0.1613

-0.2492

-0.1455

-0.1604

-0.1071

799
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:31:22.500 11:31:25.500 11:31:34.500 l 1:31:42.500 11:31:43,500

Camber 5/2

QINF = 288.0

MINF = 0.789

ALPT = 8.05

BETA = -0.10

H = 28888.

T1NF = -37.9

RNPU = 2.3E+06

PSUR = 646.1

MTOP = 0.78

Y, in. U/LrrOP W/UTOP

0.240 0.6826 -0.2322

0.470 0.7966 -0.0474

0.970 0.8681 0.0410

1.470 0.9326 -0.1968

1.960 0.9730 -0.1898

2.330 0.9763 -0.1618

2.990 1.0087 -0.2497

3.490 1.0274 -0.1513

3.990 1.0109 -0.1631

4.960 1.0000 -0.1107

Camber 5/2

QINF = 287.8

MINF = 0.790

ALPT = 8.05

BETA = -0.30

H = 28966.

TINF = -38.3

RNPU = 2.3E+06

PSUR -- 643.9

MTOP = 0.79

U/UTOP W/UTOP

0.6810 -0.2129

0.7912 -0.0390

0.8633 0.0448

0.9330 -0.1888

0.9765 -0.1899

0.9731 -0.1493

1.0125 -0.2426

1.0217 -0.1578

1.0064 -0.1653

1.0000 -0.1014

Camber 5/2

QINF = 297.1

MINF = 0.805

ALPT= 9.16

BETA = 0.02

H = 29083.

TINF = -39.1

RNPU = 2.3E+06

PSUR = 641.7

MTOP = 0.81

U/UTOP W/UTOP

0.6380 -0.1891

0.7282 -0.0209

0.8057 0.0247

0.8373 -0.1768

0.8701 -0.1581

0.8818 -0.1621

0.9218 -0.2266

0.9658 -0.1682

0.9807 -0.1648

1.0000 -0.1167

Camber 5/2

QINF = 302.2

MINF = 0.809

ALPT = 10.09

BETA = -0.18

H = 28946.

TINF= -38.3

RNPU = 2.3E+06

PSUR = 656.0

MTOP = 0.73

U/UTOP W/UTOP

0.6487 -0.0081

0.7714 0.0992

0.8043 0.0491

0.8448 -0.0987

0.8915 -0.1036

0.8631 -0.0061

0.9027 -0.1823

0.9616 -0.0505

0.9781 -0.0998

1.0000 -0.0650

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP --

U/LrFOP

0.7371

0.6951

0.7518

0.7536

0.7401

0.7972

0.8377

0.9074

0.8723

1.0000

5/2

303.3

0.810

10.04

-0.18

28903.

-38.4

2.4E+06

634.1

0.67

W/UTOP

0.3999

0.2528

-0.0045

-0.0991

-0.0542

-0.1064

-0.2071

-0.0019

-0.0725

-0.0792

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:37:03.000 12:37:18,500 12:38:26.500 12:38:35.500 12:38:57.000

Camber 0/2

QINF = 300.6

MINF = 0.801

ALPT = 6.07

BETA = -0.67

H = 28584.

TINF = -38.3

RNPU = 2.4E+06

PSUR = 656.0

MTOP = 0.82

Y, in. U/UTOP W/UTOP

0.240 0.5940 -0.2062

0.470 0.7365 0.0026

0.970 0.8834 0.0876

1.470 0.9771 -0.1781

1.960 1.0205 -0.1892

2.330 0.9882 -0.1366

2.990 0.9898 -0.2308

3.490 1.0063 -0.1145

3.990 0.9957 -0. 1258

4.960 1.0000 -0.0845

Camber 0/2

Q1NF = 301.9

MINI: = 0.800

ALPT = 8.01

BETA = -0.07

H = 28474.

TINF = -37.9

RNPU = 2.4E+06

PSUR = 656.0

MTOP = 0.80

U/UTOP W/UTOP

0.6811 -0.2282

0.8068 -0.0354

0.8861 0.0466

0.9536 -0.2043

0.9806 -0.1923

0.9783 -0.1648

0.9999 -0.2635

1.0190 -0.1556

1.0011 -0.1603

1.0000 -0.1157

Camber 5/2

QINF = 302.4

MINF = 0.803

ALPT = 6.01

BETA = -0.15

H = 28575.

TINF = -37.2

RNPU = 2.4E+06

PSUR = 657.1

MTOP = 0.81

U/UTOP W/UTOP

0.6347 -0.2322

0.7616 -0.0144

0.8779 0.0710

0.9638 -0.1849

1.0128 -0.1915

0.9927 -0.1469

0.9941 -0.2332

1.0093 -0.1295

1.0124 -0.1299

10000 -0.0935

Camber 5/2

QINF = 301.7

MINF = 0.802

ALPT = 5.98

BETA = -0.30

H = 28574.

TINF = -36.5

RNPU = 2.3E+06

PSUR = 656.0

MTOP = 0.81

U/UTOP

0.6413

0.7696

0.8933

0.9670

1.0195

1.0011

1.0011

1.0137

1.0060

1.0000

W/UTOP

-0.2359

-0.0145

0.0791

-0.1938

-0.1924

-0.1433

-0.2378

-0.1277

-0.1380

-0.0978

Camber

QINF =

MINF =

ALPT --

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6841

0.7977

0.8738

0.9341

0.9746

0.9735

1.0037

1.0181

1.0042

1.0000

5/2

291.4

0.791

7.93

-0.18

28770.

-37.5

2.3E+06

648.3

0.79

W/UTOP

-0.2494

-0.0219

0.0449

-0.2145

-0.1812

-0.1733

-0.2622

-0.1541

-0.1510

-0.1011

800
TableK-2.Continued.

Time 12:40:24,500

F11 l/MAW BOUNDARY LAYER DATA, FLT 229

Camber 10/2

QINF = 3O5.2

MINF = 0,805

ALPT = 5.97

BETA = 0.11

H = 28468.

T1NF = -35.5

RNPU = 2.4E+06

PSUR = 660.4

MTOP = 0.81

Y, in. U/LrI'OP W/UTOP

0.240 0.6594 -0.1921

0.470 0.7813 -0.0162

0.970 0.8821 0.0825

1.470 0.9352 -0.1855

1.960 0.9838 -0.1804

2.330 0.9803 -0.1430

2.990 0.9889 -0.2330

3.490 0.9984 -0.1270

3.990 0.9747 -0.1407

4.960 1.0000 -0.0884

12:40:27.500

Camber 10/2

QINF = 305.2

MINF = 0.805

ALPT = 5.93

BETA = -0.07

H = 28479.

TINF = -35.5

RNPU = 2.4E+06

PSUR = 660.4

MTOP = 0.81

U/UTOP W/krrOP

0.6590 -0.2029

0.7858 -0,0060

0.8867 0.0791

0.9510 -0.1777

0.9887 -0.1779

0.9869 -0.1403

0.9956 -0.2332

1.0102 -0.1199

0.9966 -0.1358

1.0000 -0.0909

12:41:01.500

Camber 10/2

QINF = 311.9

MINF= 0.809

ALPT = 8.42

BETA = -0,21

H = 28209.

TINF = -34.7

RNPU = 2.4E+06

PSUR = 673.8

MTOP = 0.81

U/UTOP W/LrroP

0.6559 -0.1880

0.7610 0.0051

0.8072 0.0362

0.8421 -0.2072

0.8896 -0.1606

0.8936 -0.1525

0.9332 -0.2418

0.9774 -0.1258

0.9828 -0.1754

1.0000 -0.1101

12:41:02.500

Camber 10/2

QINF = 314.5

MINF = 0.811

ALPT = 8.43

BETA = -0.01

H = 28158.

TINF = -34.6

RNPU = 2.4E+06

PSUR = 674.9

MTOP = 0.81

U/UTOP W/UTOP

0.6433 -0.2091

0.7510 -0.0057

0.8006 0.0328

0.8449 -0.1938

0.8726 -0.1621

0.8858 -0.1422

0.9259 -0.2386

0.9748 -0.1489

0.9845 -0.1574

1.0000 -0.1161

12:41:03.000

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP --

U/UTOP

0.6436

0.7426

0.8000

0.8373

0.8866

0.8893

0.9263

0.9672

0.9784

1.0000

10/2

315.9

0.812

8.43

0.02

28137.

-34.1

2.4E+06

674.9

0.81

W/UTOP

-0.1738

-0.0060

0.0370

-0.1878

-0.1544

-0.1534

-0.2467

-0.1508

-0.1611

-0.1123

FI 1 I/MAW BOUNDARY LAYER DATA. FLT 229

Time 12:41:03.500 12:43:14.000 12:44:02.500 12:44:04.500 12:44:14.500

Camber 10/2

QINF = 317.0

MINF= 0.814

ALPT = 8.42

BETA = -0.04

H= 28117,

TINF = -34.6

RNPU = 2.4E+06

PSUR = 673.8

MTOP = 0.82

Y, in. U/UTOP W/UTOP

0.240 0.6477 -0.1825

0.470 0.7417 0.0055

0.970 0.7921 0.0377

1.470 0.8373 -0.1824

1,960 0.8770 -0.1560

2.330 0.8831 -0.1446

2,990 0.9230 -0.2477

3,490 0,9690 -0.1504

3.990 0.9687 -0.1715

4.960 1.000{3 -0.1107

Camber 5/2

QINF = 305.6

MINF = 0,806

ALPT = 8.01

BETA = -0.15

H = 28536.

TINF = -37.3

RNPU = 2.4E+06

PSUR = 657.2

MTOP = 0.81

U/UTOP W/UTOP

0.6801 -0.2283

0.7939 -0.0278

0.8606 0.0483

0.9088 -0.2183

0.9582 -0.1831

0.9596 -0.1601

0.9907 -0.2593

1,0223 -0.1658

1.0071 -0.1572

1.0000 -0.1064

Camber 5/6

QINF = 301.0

MINF = 0.802

ALPT = 5.01

BETA = -0.24

H = 28640.

TINF = -37.5

RNPU = 2.4E+06

PSUR = 603.3

MTOP = 0.89

U/UTOP W/UTOP

0.6550 -0.2039

0.7602 -0.0067

0.8395 0.0416

0.8896 -0.1746

0.9205 -0.1528

0.9263 -0.1443

0.9429 -0.2337

0.9781 -0.1545

0.9761 -0.1738

1.0000 -0.1209

Camber 5/6

QINF = 30O.3

MINF = 0.801

ALPT = 5.01

BETA = -O.33

H = 28639.

TINF = -37.4

RNPU = 2.3E+06

PSUR = 617,6

MTOP = 0.86

U/UTOP W/UTOP

0.6300 -0.1994

0.7516 0.0049

0.8372 0_0465

0.8963 -0.1732

0.9468 -0.1503

0.9409 -0.1377

0.9543 -0.2312

0.9819 -0.1482

0.9962 -0.1633

1.0000 -0.1258

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6414

0.7565

0.8338

0.9011

0.9339

0.9324

0.9497

0.9778

0.9773

1.0000

5/6

300.6

0.801

5.10

-0.30

28628.

-37.0

2.3E+06

612.1

0.87

W/UTOP

-0.1927

-0.0137

0.0431

-0.1653

-0.1481

-0.1425

-0.2295

-0.1542

-0.1774

-0.1219

801
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:28:13,000 11:28:13.500 11:28:20,000 11:28:24.500 11:31:34.000

Camber 0/2

QINF = 298.6

MINF = 0.803

ALPT = 8.98

BETA = 0.08

H = 28850.

TINF = -38.5

RNPU = 2.3E+06

PSUR = 652.8

MTOP = 0.79

Y, in. U/UTOP W/UTOP

0,240 0.6571 -0.2443

0.470 0.7592 -0.0341

0.970 0.8200 0.0301

1.470 0.8602 -0.1866

1.960 0.9012 -0.1757

2.330 0.8919 -0.1421

2.990 0.9341 -0.2470

3.490 0.9692 -0.1425

3.990 0.9805 -0.1645

4.960 1.0600 -0.1153

Camber 0/2

QINF = 298.8

MINF = 0,803

ALPT = 9.04

BETA = 0.05

H = 28850.

TINF = -38.6

RNPU = 2.3E+06

PSUR = 648.3

MTOP = 0.80

U/UTOP W/UTOP

0.6736 -0.1968

0.7680 -0.0225

0.8120 0.0264

0.8606 -0.1946

0.8970 -0.1579

0.8919 -0.1348

0.9319 -0.2332

0.9590 -0.1582

0.9988 -0.1630

1.6060 -0.1129

Camber 0/2

QINF = 297.6

MINF = 0.803

ALPT -- 9.98

BETA = 0.14

H = 28915.

TINF = -39.2

RNPU = 2.3E+06

PSUR = 646.2

MTOP = 0.63

U/U'TOP W/UTOP

0.7020 -0.6099

0.7452 0.2683

0.7685 0.0606

0.7793 -0.0442

0.8178 -0.0484

0.8247 -0.0222

0.8576 -0.1752

0.9416 0.0172

0.9118 -0.0512

1.6000 -0.0726

Camber 0/2

QINF = 298.3

MINF = 0,803

ALPT = 9.97

BETA = 0.19

H = 28905.

TINF = -39.3

RNPU = 2.3E+06

PSUR = 639.5

MTOP = 0.66

U/UTOP W/UTOP

0.6120 0.2405

0.7573 0.2111

0.8017 0.0778

0.8153 -0.0767

0.8658 -0.0652

0.8496 -0.0165

0.8815 -0.1673

0.9433 -0.0132

0.9356 -0.0823

1.0060 -0.0622

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR --

MTOP =

U/UTOP

0.6585

0.7494

0.8091

0.8559

0.8912

0.8_2

0.9391

0.9730

1.6058

1.0060

5/2

296.5

0.804

8.91

0.05

29082.

-39.0

2.3E+06

647.2

0.81

W/UTOP

-0.2026

-0.0287

0.0284

-0.1868

-0.1667

-0.1502

-0.2364

-0.1 403

-0.1602

-0.1124

F111/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:31:44.000 11:31:45.560 11:31:50.000 11:31:16.560 11:31:21.000

Camber 5/2

QINF = 304.1

MINF = 0.810

ALPT = 9.98

BETA = -0.10

H = 28870.

TINF = -38.1

RNPU = 2.4E+06

PSUR = 645.1

MTOP = 0.54

Y, in. U/UTOP W/UTOP

0.240 0.4646 -0.1815

0,470 0.7196 0.3114

0.970 0.6987 -0.2270

1.470 0.7032 -0.1526

1.960 0.7573 -0.0062

2,330 0.7484 -0.0632

2,990 0,7803 -0.1898

3,490 0.9033 0.0437

3.990 0.8264 -0.1229

4.960 1.6000 -0.0756

Camber 5/2

QINF = 306.6

MINF= 0,812

ALPT = 10.04

BETA= 0.37

H = 28784.

TINF = -37.7

RNPU = 2.4E+06

PSUR = 630.8

MTOP = 0.51

U/UTOP W/UTOP

0.5378 -0.0957

0.7798 0.3807

0.8778 -0.8296

0,8050 -0.2135

0.8121 -0.0129

0.7746 -0.0312

0.8024 -0.2914

0.9273 0.0709

0.8312 -0.0761

1.0060 -0.0790

Camber 5/2

QINF = 314.1

MINF = 0.817

ALP'I" = 10.03

BETA = -0.38

H = 28494.

TINF = -36.6

RNPU = 2.4E+06

PSUR = 632.0

MTOP = 0.60

U/UTOP W/UTOP

0.4551 -0.0734

0.7003 0.2365

0.7386 -0.7369

0.6949 -0.1596

0.7048 0.0009

0.7261 -0.1401

0.7553 -0.2048

0.8589 0.0403

0.8189 -0.0731

1.0000 -0.0831

Camber 5/2

QINF = 296.2

MINF = 0,797

ALPT = 7.94

BETA = -0.24

H = 28722.

TINF = -37.5

RNPU = 2.3E+06

PSUR = 653.8

MTOP = 0.80

U/UTOP W/UTOP

0.6676 -0.2687

0.7749 -0.0545

0.8585 0.0370

0.9159 -0.1829

0.9630 -0.1794

0.9565 -0.1726

0.9973 -0.2471

1.0138 -0.1617

1.0038 -0.1575

1.0600 -0.0979

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.6797

0.7870

0.8646

0.9393

0.9794

0.9771

1.0049

1.0135

1.0069

1.0000

5/2

289.3

0.790

7.98

-0.12

28845.

-37.7

2.3E+06

648.3

0.79

W/UTOP

-0.2963

-0.0468

0.0292

-0.1848

-0.2002

-0.1556

-0.2441

-0.1548

-0.1589

-0.1029

802
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:31:21,500 11:31:23.000 11:31:26,000 11:31:33.500 11:31:35,000

Camber 5/2

QINF = 288.9

MINF = 0,790

ALPT = 8.04

BETA = -0.15

H = 28856.

T1NF= -37.6

RNPU = 2.3E+06

PSUR = 647.2

MTOP = 0.79

Y,in. U/UTOP W/UTOP

0,240 0.6813 -0.2410

0.470 0.7828 -0.0498

0.970 0.8687 0.0409

1.470 0.9290 -0.196 l

1.960 0.9762 -0.1870

2.330 0.9782 -O.1627

2.990 1.0092 -0.2522

3.490 1.0195 -0.1605

3.990 1.0128 -0.1574

4.960 1.0000 -0.1 045

Camber 5/2

QINF= 287.9

MINF = 0.789

ALPT = 8.07

BETA = -0.12

H = 28899.

TINF = -38.2

RNPU = 2.3E+06

PSUR = 647.2

MTOP = O.79

U/UTOP W/UTOP

0.6747 -0.2088

0.7832 -0.0398

0,8559 0.0425

0.9183 -0.2058

0.9645 -0.1909

0.9734 -0.1570

1.0047 -0.2403

1.0169 -0.1440

1.0003 -0.1622

1.0000 -0.1110

Camber 5/2

QINF= 2880

MINF = 0,791

ALPT = 8.04

BETA = -0.47

H = 28989.

TINF= -37.8

RNPU = 2.3E+06

PSUR = 642.8

MTOP = 0.79

U/UTOP W/U-FOP

0.6628 -0.2203

0.7753 -0.0420

0.8631 0.0445

0.9357 -0.1826

0.9720 -0.1859

0.9757 -0.1558

1.0076 -0.2471

1.0136 -0.1355

1.0042 -0.1811

1.0000 -0.0980

Camber 5/2

QINF= 295.6

MINF = 0.803

ALPT = 8.75

BETA = 0.14

H = 29080.

T1NF = -39.5

RNPU = 2.3E+06

PSUR = 646.1

MTOP = 0.81

U/UTOP W/UTOP

0.6666 -0.2157

0.7501 -0.0617

0.8154 0.0319

0.8696 -0.1926

0.9062 -0,1692

0.9093 -0.1527

0.9453 -0.2487

0.9860 -0.1774

0.9904 -0.1676

1.0000 -0.1159

Camber

QINF =

MINF=

ALPT =

BETA =

H--

TINF --

RNPU =

PSUR --

MTOP =

U/UTOP

0.6194

0.7205

0.7703

0.8136

0.8483

0.8550

0.9002

0.9512

0.9729

1.0000

5/2

297.8

0,806

9.22

0.11

29073,

-38.9

2.3E+06

649.4

0.79

W/UTOP

-0.1509

0.0173

0.0167

-0.1739

-0.1427

-0.1354

-0.2258

-0.1213

-0.1426

-0.1064

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:31:41.500 11:31:44.500 11:31:45.000 11:31:46.000 12:40:44.500

Camber 5/2

QINF = 301.7

MINF = 0.809

ALPT = 9.97

BETA = -0.01

H = 28978.

TINF = -38.6

RNPU = 2.3E+06

PSUR = 638.4

MTOP = 0.63

Y, in. U/UTOP W/UTOP

0.240 0.4786 -0.3262

0.470 0.6817 0.2734

0.970 0.7102 -0.0069

1.470 0.7093 -0,1135

1.960 0.7460 -0.0344

2.330 0.7549 -0.0476

2.990 0.7937 -0.1743

3.490 0.8941 0.0085

3.990 0.8697 -0.0962

4.960 1.0000 -0.0804

Camber 5/2

QINF = 304.8

MINF = 0.811

ALPT = 10.03

BETA = -0.04

H = 28849.

TINF = -37.9

RNPU = 2.4E+06

PSUR = 634.1

MTOP = 0.52

U/UTOP W/UTOP

0.4785 -0.1253

0.7476 0.3681

0.7685 -0.2331

0.7422 -0.1509

0.7654 0.0592

0.7473 -0.0253

0.7925 -0.4382

0.9443 0,0063

0.7968 -0.0773

1.0000 -0.0682

Camber 5/2

QINF = 305.7

M1NF= 0.812

ALPT = 10.05

BETA = 0.19

H = 28817.

TINF = -38.0

RNPU = 2.4E+06

PSUR = 636.3

MTOP = 0.45

U/UTOP W/UTOP

0.4782 -0.0415

0.8000 0.4329

0.5427 0.1952

0.7859 -0.1962

0.7821 -0.0140

0.7671 -0.0565

0.8368 -0,8186

0.9643 0.1017

0.8688 -0.0433

1.0000 -0.0782

Camber 5/2

QINF = 3O7.6

MINF= 0,813

ALPT = 9.98

BETA = 0.37

H = 28752.

TINF = -37.8

RNPU = 2.4E+06

PS UR = 631.9

MTOP = 0.50

U/UTOP W/UTOP

0.5336 -0.1243

0.7946 0.3677

0.8576 -0.7605

0.8073 -0.1689

0.8132 -0.0016

0.7727 -0.0182

0.8039 -0.4281

0.9345 0.0857

0.8552 -0.0773

1.0000 -0.0754

Camber

QINF =

MINF=

ALl:r[ =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6831

0.7794

0.8463

0.8967

0.9350

0.9214

0.9510

0.9922

0.9970

1.0000

10n

303.1

0.801

7.91

-0.36

28431.

-35.4

2.4E+06

661.6

0.81

W/UTOP

-0.2340

-0.0183

0.0371

-0.1856

-0.1459

-0.1565

-0.2396

-0.1363

-0.1682

-0.1017

803
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:40:45.500 12:40:46.000 12:40:50.500 12:40:53.000 12:40:55.000

Camber 10/2

QINF = 301.8

MINF= 0.800

ALPT = 8.06

BETA = -0.18

H = 28440.

TINF = -35,2

RNPU = 2.3E+06

PSUR = 660.5

MTOP = 0.81

Y, in, U/UTOP W/UTOP

0.240 0.6668 -0.1839

0.470 0.7775 -0.0112

0.970 0.8392 0.0424

1,470 0.8772 -0.1934

1.960 0.9171 -0.1678

2.330 0.9158 -0.1517

2.990 0.9448 -0.2420

3.490 0.9852 -0.1495

3.990 0.9857 -0.1539

4.960 1.0000 -0.1064

Camber 10/2

QINF = 301.1

MINF = 0.799

ALPT = 8.06

BETA = -0.10

H = 28450.

TINF -- -35. l

RNPU = 2.3E+06

PSUR -- 656.0

MTOP = 0.82

U/UTOP W/UTOP

0.6684 -0.2126

0.7743 0.0060

0.8291 0.0439

0.8723 -0.2056

0.9127 -0.1682

0.9109 -0.1456

0.9487 -0.2469

0.9827 -0.1487

0.9838 -0.1529

1.0000 -0.1068

Camber 10/2

QINF -- 296.4

MINF = 0.793

ALPT = 7.90

BETA = -0.36

H = 28498.

TINF = -35.4

RNPU = 2.3E+06

PSUR = 656.0

MTOP = 0.80

U/UTOP W/UTOP

0.6703 -0.2130

0.7875 0.0053

O.8499 0.0410

0.8903 -0.1922

0.9258 -0.1695

0.9321 -0.1400

0.9579 -0.2530

0.9952 -0.1500

0.9953 -0.1549

1.0000 -0.1051

Camber 10/2

QINF = 295.8

MINF = 0.792

ALPT = 8.07

BETA = -0.30

H = 28475.

TINF = -35.0

RNPU = 2.3E+06

PSUR = 660.5

MTOP = 0.80

U/UTOP W/UTOP

0.6667 -0.1879

0.7785 -0.0086

0.8352 0.0405

0.8803 -0.1874

0.9155 -0.1622

0.9124 -0.1441

0.9432 -0.2427

0.9838 -0.1434

0.9883 -0.1585

1.0000 -0.1063

Camber

QINF =

MINF =

ALPT =

BETA=

H=

TINF =

RNPU =

PSUR =

MTOP --

U/UTOP

0.6605

0.7681

0.8314

0.8741

0.9097

0.9051

0.9369

0.9757

0.9788

1.0000

10/2

296.9

0.793

8.06

-0.27

28443.

-35.1

2.3E+06

662.7

0.81

W/UTOP

-0.2147

-0.0058

0.0403

-0.1913

-0.1572

-0.1336

-0.2434

-0.1440

-0.1533

-0.1060

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:41:01.000 12:41:02.000 12:41:04.000 12:44:01.000 12:44:01.500

Camber 10/2

QINF = 310.8

MINF = 0.808

ALPT = 8.42

BETA = -0.21

H = 28230.

TINF = -34.2

RNPU = 2.4E+06

PSUR = 674.9

MTOP = 0.80

Y,in. U/UTOP W/UTOP

0.240 0.6578 -0.1543

0.470 0.7536 0.0052

0.970 0.8188 0.0347

1.470 0.8532 -0.1841

1.960 0.9078 -0.1559

2.330 0.9045 -0.1460

2.990 0.9425 -0.2472

3.490 0.9750 -0.1530

3.990 0.9856 -0.1625

4.960 1.0000 -0.1106

Camber 10/2

QINF= 313.1

MINF = 0.810

ALPT = 8.34

BETA = -0.10

H = 28189.

TINF = -34.5

RNPU = 2.4E+06

PSUR = 676.0

MTOP = 0.81

U/UTOP W/UTOP

0.6564 -0.1834

0.7590 -0.0119

0.8149 0.0346

0.8536 -0.1930

0.8890 -0.1491

0.8963 -0.1451

0.9339 -0.2481

0.9786 -0.1439

0.9835 -0.1545

1.0000 -0.1092

Camber 10/2

QINF = 318.0

MINF = 0.814

ALPT = 8.40

BETA -- -0.07

H = 28085.

TINF = -34.4

RNPU = 2.4E+06

PSUR = 674.9

MTOP = 0.82

U/UTOP W/UTOP

0.6449 -0.1817

0.7468 0.0052

0.8027 0.0297

0.8371 -0.1803

0.8781 -0.1589

0.8839 -0.1525

0.9209 -0.2467

0.9697 -0.1514

0.9896 -0.1562

1.0000 -0.1130

Camber 5/6

QINF = 301.2

MINF = 0.802

ALPT = 5.01

BETA = -0.27

H = 28641.

TINF = -37.2

RNPU = 2.3E+06

PSUR -- 617.6

MTOP = 0.87

U/UTOP W/UTOP

0.6364 -0.1999

0.7580 -0.0092

0.8518 0.0527

0.9025 -0.1748

0.9572 -0.1681

0.9490 -0.1315

0.9593 -0.2290

0.9809 -0.1608

0.9879 -0.1798

1.0000 -0.1202

Camber

QINF =

MINF =

ALPT --

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.6518

0.7583

0.8496

0.9085

0.9457

0.9433

0.9564

0.9830

0.9805

1.0000

5/6

301.2

0.802

4.98

-0.30

28641.

-37.5

2.4E+06

605.5

0.89

W/UTOP

-0.2029

-0.0122

0.0468

-0.1681

-0.1600

-0.1377

-0.2354

-0.1 442

-0.1713

-0.1188

804
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:44:03.500 12:44:04.000 12:44:09.000 12:44:09.500 12:44:13.000

Camber 5/6

QINF = 300,5

MINF= 0.801

ALPT = 5.04

BETA = -0.36

H = 28640.

TINF = -37.4

RNPU = 2.3E+06

PSUR = 617.6

MTOP = 0.87

Y, in. U/UTOP W/UTOP

0.240 0.6354 -0.1983

0.470 0.7490 -0.0120

0.970 0.8340 0.0430

1.470 0.8884 -0.1704

1.960 0.9232 -0.1349

2.330 0.9343 -0.1402

2.990 0.9501 -0.2322

3,490 0.9808 -0.1519

3.990 0.9751 -0.1846

4.960 1.0000 -0.1203

Camber 5/6

QINF = 300.3

MINF = 0.801

ALPT = 5.04

BETA = -O.3O

H = 28639.

T1NF = -37.4

RNPU = 2.3E+06

PSUR = 612.1

MTOP = 0.88

U/UTOP W/UTOP

0.6435 -0.2322

0.7463 0.0024

0.8307 0,0454

0.8890 -0.1695

0.9348 -0.1500

0.9395 -0.1363

0.9538 -0.2243

0.9769 -0.1154

0.9773 -0.1698

1.0000 -0.1225

Camber 5/6

QINF = 299,6

MINF= 0.801

ALPT = 4.50

BETA = -0.30

H = 28660.

TINF = -37.6

RNPU = 2.3E+06

PSUR = 622.0

MTOP = 0.87

U/UTOP W/UTOP

0.6348 -0,2018

0.7530 -0.0120

0.8494 0.0603

0,9123 -0.1716

0.9691 -0.1575

0.9586 -0.1323

0.9682 -0.2279

0,9868 -0.1494

0.9904 -0.1686

1.0000 -0.1151

Camber 5/6

QINF = 299,6

MINF = 0.801

ALPT = 4.55

BETA = -0.04

H = 28660.

TINF= -37.3

RNPU = 2,3E+06

PSUR = 617.6

MTOP = 0.87

U/UTOP W/UTOP

0.6386 -0.1915

0.7549 -0.0092

0.8508 0.0496

0.9069 -0.1712

0.9532 -0.1534

0.9477 -0.1394

0,9596 -0.2310

0.9857 -0.1288

0.9849 -0,1725

1.0000 -0.1214

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.6269

0.7_2

0.8412

0.9009

0.9585

0.9_7

0.9_3

0.9866

0.9888

1.0000

5/6

301.0

0,802

4.99

-0.15

28640.

-37.1

2.3E+06

620,9

0.86

W/UTOP

-0.1951

-0,0061

0.0543

-0.1712

-0.1545

-0.1356

-0.2257

-0.1512

-0.1661

-0.1188

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:36:46,000 12:36:53.500 12:37:02.500 12:37:05.000 12:37:10.000

Camber 0/2

QINF = 297.9

MINF = 0.798

ALPT = 5.66

BETA = -0.04

H = 28624,

TINF = -38.3

RNPU = 2.3E+06

PSUR = 653.8

MTOP = 0.81

Y,in. U/UTOP W/UTOP

0,240 0.6110 -0.2636

0,470 0.7509 -0.0061

0.970 0.8938 0.0804

1.470 0.9873 -0,1834

1.960 1.0261 -0,1915

2.330 0.9940 -0.1398

2.990 0.9957 -0.2332

3.490 1.0102 -0.1229

3.990 0.9990 -0.1321

4.960 1.0000 -0.0914

Camber 0/2

QINF = 298.6

MINF = 0.798

ALPT = 5.65

BETA= -0.15

H = 28614.

TINF = -38.0

RNPU = 2.3E+06

PSUR = 653.8

MTOP = 0.83

U/UTOP W/UTOP

0.6076 -0.2504

0.7437 -0.0140

0.8821 0.0819

0.9660 -0.1828

1.0059 -0.1883

0.9746 -0.1393

0.9777 -0.2335

0.9925 -0.1219

0.9819 -0.1279

1.0000 -0.0829

Camber 0/2

QINF = 300.4

MINF= 0.800

ALPT = 6.04

BETA = -0.65

H = 28583.

TINF = -38.2

RNPU = 2.4E+06

PSUR = 652.7

MTOP = 0.82

U/UTOP W/UTOP

0.6051 -0.2437

0.7411 0.0026

0.8899 0.0758

0.9792 -0.1829

1.0166 -0.1953

0.9896 -0.1379

0.9923 -0.2304

1.0080 -0.1208

0.9904 -0.1408

1.0000 -0.0881

Camber 0/2

QI NF = 301.1

MINF= 0.801

ALPT = 6.09

BETA = -0.79

H = 28584,

TINF = -38.0

RNPU = 2.4E+06

PSUR = 654.9

MTOP = 0.81

U/UTOP W/UTOP

0.6084 -0.2054

0.7420 0.0026

0.8903 0.0786

0.9828 -0.1791

1.0257 -0.1872

0.9936 -0.1326

0.9954 -0.2237

1.0119 -0.1121

1.0016 -0.1288

1.0000 -0.0887

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6390

0.7691

0.8836

0.9760

1.0120

0.9878

0.9859

1.0027

0.9872

1.0000

0/2

301.8

0.802

7,05

-0.07

28563.

-38.1

2.4E+06

652.7

0,82

W/UTOP

-0.1950

-0.0230

0.0609

-0.1994

-0.1944

-0.1529

-0.2448

-0.1405

-0.1540

-0.1047

8O5
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:37:11.000 12:37:17.500 12:37:19,500 12:38:21.000 12:38:26.000

Camber 0/2

QINF = 301.8

MINF -- 0.802

ALPT = 7.18

BETA = -0.36

H = 28563.

TINF = -38.1

RNPU = 2.4E+06

PSUR = 652.7

MTOP = 0.81

Y,in. U/UTOP W/UTOP

0,240 0.6410 -0.2674

0.470 0.7657 -0.0192

0.970 0.8986 0.0592

1.470 0.9733 -0.2002

1.960 1.0172 -0.2019

2,330 0.9942 -0.1606

2,990 0.9981 -0.2476

3.490 1.0089 -0.1414

3.990 0.9905 -0.1588

4.960 1.0000 -0.1059

Camber 0/2

QINF = 301.2

MINF = 0.800

ALPT = 8.03

BETA = -0.24

H = 28495.

TINF = -37.8

RNPU = 2.4E+06

PSUR = 656.0

MTOP = 0.80

U/UTOP W/UTOP

0.6802 -0.2420

0.8012 -0.0375

0.8940 0.0476

0.9517 -0.2145

0.9922 -0.1968

0.9904 -0.1670

1.0044 -0.2587

1.0189 -0.1587

1.0030 -0.1619

1.0000 -0.1124

Camber 0/2

QINF = 302.2

MINF = 0.800

ALPT -- 8.03

BETA = -0.30

H = 28441.

TINF = -37.6

RNPU = 2.4E+06

PSUR = 657. l

MTOP = 0.80

U/UTOP W/UTOP

0.6754 -0.2002

0.7966 -0.0373

0.8900 0.0506

0.9415 -0.2152

0.9836 -0.2031

0.9781 -0.1647

0.9958 -0.2545

1.0114 -0.1187

1.0012 -0.1836

1.0000 -0.1096

Camber 5/2

QINF = 301.3

MINF = 0.801

ALPT = 5.98

BETA = -0.21

H = 28574.

TINF = -36.7

RNPU = 2.3E+06

PSUR = 657.1

MTOP = 0.80

U/UTOP W/UTOP

0.6462 -0.2496

0.7694 -0.0034

0.8938 0,0771

0.9660 -0.1950

1.0210 -0.1927

1.0006 -0.1470

1.0035 -0.2368

1.0087 -0.1297

1.0072 -0.1364

1.0000 -0.0998

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP --

U/UTOP

0.6324

0.7654

0.8860

0.9540

1.0141

0.9928

0.9923

1.0091

0.9947

1.0000

5/2

302.2

0.802

6.01

-0.21

28575.

-37.2

2.4E+06

657.1

0.81

W/UTOP

-0.2426

-0.0032

0.0841

-0.1941

-0.1950

-0.1457

-0.2357

-0.1233

-0.1410

-0.0922

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:38:41.000 12:38:45.500 12:38:46,000 12:38:58.500 12:38:59.500

Camber 5/2

QINF = 301.3

MINF = 0,802

ALPT = 5.99

BETA = -0.91

H = 28596.

TINF = -36.8

RNPU = 2.3E+06

PSUR = 657.1

MTOP = 0.81

Y,in. U/UTOP W/UTOP

0.240 0.6146 -0.2073

0.470 0.7561 0.0025

0.970 0.8872 0.0780

1.470 0.96 l0 -0.1786

1,960 1.0168 -0.1850

2.330 0.9943 -0.1318

2.990 0.9951 -0.2324

3,490 1.0114 -0,1181

3.990 1.0167 -0,1178

4,960 1.0000 -0.0764

Camber 5/2

QINF = 302.4

MINT = 0.803

ALPT = 6.98

BETA = -0.10

H = 28587.

TINF -- -36.9

RNPU = 2.4E+06

PSUR = 656.0

MTOP = 0.81

U/UTOP W/UTOP

0.6579 -0.3589

0.7661 -0.0118

0.8758 0.0597

0.9385 -0.2099

0.9886 -0.1848

0.9914 -0.1569

1.0001 -0.2475

1.0089 -0.1420

0.9991 -0.1600

1.0000 -0,1062

Camber 5/2

QINF = 302.4

MINF = 0.803

ALPT = 7.20

BETA = -0.07

H = 28587.

TINT = -36.9

RNPU = 2.4E+06

PSUR = 656.0

MTOP = 0.80

U/UTOP W/UTOP

0.6773 -0.2412

0.7908 -0.0296

0,8857 0.0580

0.9460 -0.2152

0.9970 -0.1917

0.9990 -0.1673

1.0105 -0.2672

1.0254 -0.1461

1.0076 -0,1583

1.0000 -0.1001

Camber 5/2

QINF -- 290.1

MINF = 0.790

ALPT = 8.06

BETA = -0.27

H = 28791.

TINF = -37.3

RNPU = 2.3E+06

PSUR = 649.4

MTOP = 0.79

U/UTOP W/UTOP

0.6719 -0.2236

0.7963 -0.0184

0.8797 0.0476

0.9330 -0.1988

0.9768 -0.1819

0.9780 -0.1670

0.9999 -0.2570

1.0211 -0.1418

0.9997 -0.1674

1.0000 -0.1065

Camber

QINF =

MINF --

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6734

0.7971

0.8742

0.9257

0.9680

0.9673

0.9948

1.0212

1.0028

1.0000

512

289.8

0,790

8.10

-0.33

28790,

-37.0

2.3E+06

650.5

0.79

W/UTOP

-0.2863

-0.0140

0.0048

-0.2049

-0.1783

-0.1629

-0.2593

-02006

-0.1537

-0.1040

806
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:40:17.500 12:40:19.500 12:40:38.000 12:40:38.500 12:40:39.000

Camber 10/2

QINF = 303,7

MINF = 0.803

ALPT = 5.97

BETA = -0.21

H = 28465.

TINF = -35.6

RNPU = 2.4E+06

PSUR = 659.3

MTOP = 0,81

Y, in, U/LrrOP W/UTOP

0.240 0.6633 -0.1933

0,470 0.7847 -0.0059

0.970 0.8790 0.0793

1.470 0.9344 -0.1889

1,960 0,9863 -0.1773

2,330 0.9818 -0.1385

2.990 0.9903 -0.2368

3.490 0.9992 -0.1242

3.990 0,9888 -0.1389

4,960 1.0000 -0.0867

Camber 10/2

QINF= 304.1

MINF = 0.803

ALPT = 5,97

BETA = 0,05

H = 28466

T1NF = -35.6

RNPU = 2.4E+06

PSUR = 659.3

MTOP = 0.81

U/UTOP W/UTOP

0,6658 -0.2003

0,7895 -0.0060

0,8896 0,0753

0.9407 -0.1835

0.9930 -0.1821

0.9905 -0.1420

0.9971 -0.2365

1.0008 -0.1252

1.0049 -0.1287

1.0000 -0.0861

Camber 10/2

QINF = 306,9

MINF= 0,806

ALPT = 6,95

BETA = -0.18

H = 28426.

TINF = -35.3

RNPU = 2,4E+06

PSUR = 663.8

MTOP = 0.80

U/UTOP W/UTOP

0.6814 -0.2064

0.7903 -0.0148

0.8771 0.0562

0.9419 -0.1872

0.9678 -0.1824

0.9712 -0.1516

0.9976 -0.2473

1.0217 -0.1484

1.0033 -0.1489

1.0000 -0,1016

Camber 10/2

QINF = 306.9

MINF = 0.806

ALPT = 7.07

BETA = -0.04

H = 28415,

TINF = -35.3

RNPU = 2.4E+06

PSUR = 663.8

MTOP = 0,80

U/UTOP W/UTOP

0.6862 -0.2019

0,7944 -0.0291

0.8727 0,0601

0.9260 -0.2004

0.9700 -0.1818

0.9706 -0,1461

1,0005 -0.2399

1.0267 -0,1486

1.0061 -0.1567

1.0000 -0.1009

Camber

QINF =

MINF =

ALPT =

BETA ---

H=

TINF -

RNPU --

PSUR =

MTOP =

U/UTOP

0.6814

0.7983

0.8764

0.9242

0.9640

0.9646

0.9944

1.0283

1,0093

1.0000

10/2

306.9

0.806

7,29

-0.12

28415.

-35.3

2.4E+06

659.3

0.81

W/UTOP

-0,2602

-0.0155

0,0427

-0.2048

-0.1840

-0.1579

-0.2467

-0.1718

-0.1608

-0.1043

FI I I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:40:45.000 12:40:46,500 12:40:52,500 12:40:57.500 12:42:27,500

Camber 10/2

QINF = 302.4

MINF = 0.800

ALPT = 8,02

BETA = -0.36

H = 28441.

TINF= -35.3

RNPU = 2.4E+06

PSUR = 660.5

MTOP = 0,81

Y,in. U/UTOP W/UTOP

0,240 0.6646 -0.1978

0.470 0.7774 -0.0112

0,970 0.8402 0.0554

1.470 0.8807 -0.1951

1.960 0.9187 -0.1643

2.330 0.9179 -0,1480

2,990 0.9505 -0.2412

3,490 1.0014 -0.1324

3.990 0.9853 -0.1523

4,960 1,0000 -0.1080

Camber 1012

QINF= 300.6

MINF = 0.798

ALPT = 8.01

BETA = 0.08

H = 28460.

TINF = -35.1

RNPU = 2.3E+06

PSUR = 660,5

MTOP = 0.81

U/UTOP W/UTOP

0.6736 -0.1983

0.7860 -0.0086

0.8399 0.0376

0.8792 -0.1992

0,9158 -0.1702

0.9174 -0.1540

0.9498 -0.2510

0.9888 -0.1510

0.9898 -0.1538

1.0000 -0.1099

Camber 10/2

QINF = 295,8

MINF= 0.792

ALPT = 8.00

BETA = -0.12

H = 28486.

TINF = -35.3

RNPU = 2.3E+06

PSUR = 659.4

MTOP = 0.81

U/UTOP W/UTOP

0.6611 -0.2150

0.7771 -0.0032

0.8399 0.0416

0.8813 -0.1899

0.9176 -0.1609

0.9110 -0.1411

0.9440 -0.2568

0.9919 -0.1369

0.9858 -0.1627

1.0000 -0.1067

Camber 10/2

QINF= 301.7

MINF= 0.798

ALPT = 8.01

BETA = -0,2 I

H = 28372.

TINF= -35.4

RNPU = 2,4E+06

PSUR = 663.8

MTOP = 0.82

U/UTOP W/UTOP

0,6544 -0.1843

0.7632 -0.0031

0.8283 0.0424

0.8685 -0.1884

0.9021 -0.1617

0.9006 -0.1404

0.9345 -0.2412

0,9894 -0.1293

0.9756 -0.1508

1.0000 -0.1011

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP --

U/UTOP

0.6349

0.7694

0.8855

0.9649

1.0236

0.9987

1.0007

1,0035

1.0018

1.0000

5/2

305.0

0.804

5.52

0.08

28468.

-36.4

2.4E+06

660.4

0.81

W/UTOP

-0.2335

-0,0021

0.0866

-0,1915

-0.1900

-0.1439

-0.2385

-0,1258

-0.1604

-0.0871

807
TableK-2.Continued.

Time 12:42:29.000

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

Y, in, U/LrI'OP

0.240 0.6345

0.470 0.7637

0,970 0.8859

1.470 0.9617

1.960 1.0173

2.330 0.9987

2.990 0.9943

3.490 1.0094

3.990 0.9987

4.96O 1.0000

F111/MAW BOUNDARY LAYER DATA, FLT 229

12:42:42.500

5/2 Camber

305.5 QINF =

0.805 MINF =

5.66 ALPT =

0.14 BETA =

28468. H =

-36.5 TINF =

2.4E+06 RNPU =

658.2 PSUR =

0.82 MTOP =

W/UTOP U/UTOP

-0.1896 0.6350

-0.0221 0.7556

0.0848 0.8781

-0.1864 0.9522

-0.1920 1.0116

-0.1486 0.9880

-0.2311 0.9868

-0.1240 1.0023

-0.1324 0.9981

-0.0914 1.0000

5/2

306.3

0.807

5.94

-0.10

28503.

-36.7

2.4E+06

661.6

0.82

W/UTOP

-0.1897

-0.0022

0.0765

-0.1972

-0.1891

-0.1467

-0.2333

-0.1302

-0.1364

-0.0872

12:42:44.500

Camber 5/2

QINF = 306.0

MINF = 0.806

ALPT = 5.97

BETA = 0.11

H = 28514.

TINF = -36.7

RNPU = 2.4E+06

PSUR = 661.6

MTOP = 0.81

U/UTOP W/UTOP

0.6265 -0.2455

0.7600 -0.0084

0.8837 0.0806

0.9546 -0.1977

1.0158 -0.1920

0.9941 -0.1538

0.9936 -0,2397

1.0076 -0.1287

0.9979 -0.1239

1.0000 -0.0922

12:42:52.500

Camber 5/2

QINF = 306.4

MINF = 0.808

ALPT = 5.98

BETA = -0.88

H = 28571.

TINF = -37.2

RNPU = 2.4E+06

PSUR = 658.2

MTOP = 0.82

U/UTOP W/UTOP

0.6229 -0.1992

0.7620 0.0162

0.8896 0.0850

0.9543 4). 1741

1.0108 -0.1769

0.9902 -0.1274

0.9905 -0.2196

1.0079 -0.1011

0.9887 -0.1353

1.0000 -0.0806

12:42:55.500

Camber

QINF =

MINF =

ALPT =

BETA=

14=

TINF =

RNPU --

PSUR =

MTOP --

U/UTOP

0.6646

0.7832

0.8756

0.9384

0.9872

0.9894

1.0010

1.0172

0.9992

1.0000

5/2

306.9

0.808

6.95

0.02

28549.

-37.2

2.4E+06

656.0

0.82

W/UTOP

-0.2367

-0.0274

0.0625

-0.2023

-0.1899

-0.1622

-0.2472

-0.1499

-0.1534

-0.1028

F111/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:42:56.000 12:43:12.000 12:43:14.500 12:44:08.500

Y,in.

0.240

0.470

0.970

1.470

1.960

2.330

2.990

3.490

3.990

4.960

Camber

QINF =

MINF =

ALPT =

BETA --

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6636

0.7884

0.8839

0.9416

0.9877

0.9911

1.0087

1.0192

0.9992

1.0000

12:42:57.500

5/2 Camber

306.9 QINF =

0.808 MINF =

7.06 ALPT =

0.08 BETA =

28549. H =

-37.2 TINF =

2.4E+OS RNPU --

656.0 PSUR =

0.81 MTOP =

W/UTOP U/UTOP

-0.2264 0.6700

-0.0276 0.7875

0.0594 0.8731

-0.2112 0.9349

-0.1851 0.9808

-0.1619 0.9829

-0.2480 1.0059

-0.1450 1.0129

-0.1424 0.9997

-0.1140 1.0000

5/2

307.3

0.809

7.19

-0.10

28550.

-37.0

2.4E+06

653.8

0.82

W/UTOP

-0.2386

-0.0276

0.0606

-0.2050

-0.1863

-0.1610

-0.2539

-0.1399

-0.1545

-0.1036

Camber 5/2

QINF = 303.7

MINF -- 0.805

ALPT = 7.97

BETA = -0.24

H = 28578.

TINF = -37.4

RNPU = 2.4E+06

PSUR = 658.3

MTOP = 0.81

U/UTOP W/UTOP

0.6760 -0.1963

0.7864 -0.0275

0.8662 0.0325

0.9195 -0.1983

0.9609 -0.1775

0.9578 -0.1709

0.9889 -0.2710

1.0187 -0.1551

0.9854 -0.1755

1.0000 -0.1099

Camber 5/2

QINF = 306,2

MINF = 0.807

ALPT = 8.01

BETA = -0.07

H = 28526.

TINF = -37.4

RNPU = 2.4E+06

PSUR = 657.2

MTOP = 0.81

U/UTOP W/UTOP

0.6706 -0.1993

0.7878 -0.0394

0.8552 0.0474

0.9116 -0.2123

0.9573 -0.1858

0.9596 -0.1627

0.9916 -0.2592

1.0250 -0.1607

1.0116 -0.1642

1.0000 -0.1132

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP --

U/UTOP

0.6334

0.7531

0.8430

0.9038

0.9516

0.9454

0.9535

0.9798

0.9769

1.0000

5/6

299.6

0.801

4.54

-0.36

28660.

-37.3

2.3E+06

620.9

0.87

W/UTOP

-0.2128

-0.0165

0.0563

-0.1727

-0.1630

-0.1363

-0.2265

-0.1505

-0.1683

-0.1142

808
TableK-2.Continued.

Time 12:44:10.000

Camber 5/6

QINF = 299.8

MINF = 0.801

ALPT = 4.50

BETA = -0.30

H = 28661.

TINF = -37.3

RNPU = 2.3E+06

PSUR = 603.3

MTOP = 0.89

Y, in. U/UTOP W/UTOP

0.240 0.6545 -0.2322

0.470 0.7618 -0.0199

0.970 0.8531 0.0608

1.470 0.9121 -0.1659

1.960 0.9543 -0.1562

2.330 0.9518 -0.1444

2.990 0.9648 -0.2340

3.490 0.9821 -0.1128

3.990 0.9818 -0.1612

4.960 1.0000 -0.1178

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

12:44:12.500 12:44: l 3.500 12:44:19.000 12:44:30.500

Camber 5/6

QINF= 300.7

MINF = 0.802

ALPT = 4.95

BETA = -0.27

H = 28651.

TINF = -37.1

RNPU = 2.3E+06

PSUR = 605.5

MTOP = 0.90

U/UTOP W/UTOP

0.6369 -0.2007

0.7529 -0.0025

0.8348 0.0502

0.8965 -0.1725

0.9461 -0.1556

0.9409 -0,1347

0.9543 -0.2330

0.9796 -0.1478

0.9913 -0.1589

1.0000 -0.1067

Camber 5/6

QINF = 301.0

MINF = 0.802

ALPT = 4.97

BETA = -0.30

H = 28640.

TINF = -37.1

RNPU = 2.3E+06

PSUR = 617.6

MTOP = 0.86

U/UTOP W/UTOP

0.6356 -0.1978

0.7497 -0.0025

0.8472 0.0539

0.9066 -0.1711

0,9611 -0.1517

0.9518 -0.1342

0.9674 -0.2289

0.9913 -0.1490

0.9869 -0.1729

1.0000 -0.1260

Camber 5/6

QINF = 299.2

MINF = 0.799

ALPT = 5.02

BETA = -0.15

H = 28626.

T1NF = -37.2

RNPU = 2.3E+06

PSUR = 621.0

MTOP = 0.87

U/UTOP W/UTOP

0.6247 -0.1836

0.7346 -0.0141

0.8398 0.0439

0.8891 -0.1774

0.9395 -0.1539

0.9258 -0.1468

0.9495 -0.2316

0.9724 -0.1563

0.9801 -0.1866

1.0000 -0.1256

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.6396

0.7558

0.8379

0.8897

0.9242

0.9245

0.9496

0.9777

0.9794

1.0000

5/6

297.7

0.797

5.83

-0.56

28612.

-37.2

2.3E+06

607.8

0.88

W/UTOP

-0.1978

0.0072

0.0290

-0.1783

-0.1455

-0.1357

-0.2246

-0.1420

-0.1798

-0.1241

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:44:31.000 12:44:31,500 12:44:38.000 12:44:39.000 12:44:39.500

Camber 5/6

QINF = 297.8

MINF = 0.797

ALPT = 5.96

BETA = -0.56

H = 28601,

TINF= -36.9

RNPU = 2.3E+06

PSUR = 604.5

MTOP = 0.88

Y,in. U/UTOP W/UTOP

0,240 0.6482 -0.1916

0.470 0.7562 -0.0023

0.970 0.8332 0.0328

1.470 0.8731 -0.1869

1.960 0.9041 -0.1215

2.330 0.9162 -0.1477

2.990 0.9378 -0.2314

3.490 0.9778 -0.1507

3.990 0.9752 -0.1590

4.960 1.0000 -0.1244

Camber 5/6

QINF = 297.5

MINF = 0.797

ALPT= 6.11

BETA = -0.53

H = 28601.

TINF = -37.2

RNPU = 2.3E+06

PSUR = 601.2

MTOP = 0.88

U/UTOP W/UTOP

0.6450 -0.2644

0.7460 -0.0055

0.8150 0.0237

0.8483 -0.1818

0.8641 -0.1371

0.8880 -0.1456

0.9089 -0.2475

0.9650 -0.1522

0.9486 -0.1866

1.0000 -0.1284

Camber 5/6

QINF = 293.0

MINF = 0.791

ALPT = 6.91

BETA = -0.47

H = 28604.

TINF = -37.1

RNPU = 2.3E+06

PSUR = 601.2

MTOP = 0.86

U/UTOP W/UTOP

0.6625 -0.2330

0.7571 -0.0289

0.8084 -0.0119

0.8363 -0.2048

0.8332 -0.1305

0.8487 -0.1494

0.8861 -0.2490

0.9513 -0.1546

0.9620 -0.2312

1.0000 -0.1408

Camber 5/6

QINF = 292.3

MINF = 0.790

ALPT = 6.99

BETA = -0.38

H = 28603.

TINF = -36.7

RNPU = 2.3E+06

PSUR = 595.7

MTOP = 0.86

U/UTOP W/UTOP

0.6715 -0.2282

0.7653 -0.0140

0.8067 -0.0126

0.8388 -0.2067

0.8563 -0.1200

0.8575 -0.1484

0.8981 -0.2352

0.9529 -0.1471

0.9684 -0.2121

1.0000 -0.1534

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6577

0.7484

0.7981

0.8265

0.8261

0.8533

0.8819

0.9545

0.9485

1.0000

5/6

291.7

0.789

7.04

-0.30

28602.

-37.2

2.3E+06

601,2

0.86

W/UTOP

-0.2349

-0.0270

-0.0188

-0.2142

-0.1249

-0.1527

-0.2677

-0.1544

-0,1904

-0.1491

809
Table K-2. Continued.

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:44:52,000 12:44:52,500 12:44:53.000 12:52:48.500 12:53:53,000

Camber 5/6

QINF = 299.3

MINF = 0.799

ALPT = 8.07

BETA = -0.30

H = 28570.

TINF = -36.7

RNPU = 2.3E+06

PSUR = 603.4

MTOP = 0.88

Y, in. U/UTOP W/UTOP

0.240 0.6755 -0.2734

0.470 0.7558 -0.0674

0.970 0.7941 -0.0373

1,470 0.8319 -0.2298

1,960 0.8289 -0.1255

2.330 0.8428 -0.1472

2,990 0.8869 -0.2853

3,490 0.9463 -0.1799

3.990 0.9639 -0.2253

4.960 1.0000 -0.1543

Camber 5/6

QINF = 300.O

MINF = 0,799

ALPT = 8.05

BETA = -0.30

H = 28560.

TINF = -36.5

RNPU = 2.3E+06

PSUR = 602.3

MTOP = 0.89

U/UTOP W/UTOP

0.6896 -0,2541

0.7662 -0.0665

0.8028 -0.0314

0.8255 -0.2227

0.8250 -0.1291

0.8384 -0.1649

0.8768 -0.2450

0.9322 -0.1918

0.9603 -0.2199

1.0000 -0.1659

Camber 5/6

QINF = 300.5

MINF = 0,800

ALPT = 8.04

BETA = -0.38

H = 28550.

TINF = -36.5

RNPU = 2.3E+06

PSUR = 611.2

MTOP = 0.88

U/UTOP W/UTOP

0.6690 -0.2608

0.7518 -0.0661

0.7909 -0.0403

0.8401 -0.2344

0.8411 -0.1472

0.8482 -0.1664

0.8860 -0.2693

0.9362 -0.1988

0.9627 -0.2210

1.0000 -0.1577

Camber 0/2

QINF = 302.8

M1NF -- 0,802

ALPT = 5.61

BETA = 0.08

H = 28498.

TINF = -36.1

RNPU = 2.4E+06

PSUR = 659.3

MTOP = 0.82

U/UTOP W/UTOP

0.6058 -0.2345

0.7416 -0.0150

0.8834 0.0769

0.9850 -0.1833

1.0215 -0.1912

0.9876 -0.1372

0.9908 -0.2312

1.0085 -0.1274

0.9942 -0.1349

1.0000 -0.0928

Camber

QINF =

MINF =

ALPT ---

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6219

0.7735

0.9309

0.9952

1.0212

0.9895

0.9917

1.0045

0.9987

1.0000

0/2

308.1

0,807

3.13

0.14

28372.

-35.7

2.4E+06

664.8

0.82

W/UTOP

-0.2165

0.0132

0.1293

-0.1472

-0.1633

-0.1083

-0.2031

-0.1217

-0.0956

-0.0637

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:53:53,500 12:53:54.000 12:54:01,500 13:03:57.500 13:03:59.000

Camber 0/2

QINF= 310.1

MINF = 0.809

ALPT = 3.14

BETA = -0.04

H = 28330,

TINF = -35.6

RNPU = 2.4E+06

PSUR = 664.8

MTOP = 0.83

Y, in. U/UTOP W/UTOP

0.240 0.6179 -0.2149

0.470 0.7605 0.0051

0.970 0.9290 0.1271

1.470 0.9906 -0.1317

1,960 1.0229 -0.1764

2.330 0.9888 -0.0977

2,990 0.9857 -0.2109

3,490 1.0079 -0.1212

3.990 0.9821 -0,0998

4.960 1.0000 -0.0587

Camber 0/2

QINF = 312.4

MINF = 0.811

ALPT = 3.19

BETA = 0.08

H = 28289.

TINF = -35.6

RNPU = 2.4E+06

PSUR = 669.3

MTOP = 0.82

U/UTOP W/UTOP

0.6212 -0.1834

0.7537 0.0097

0.9254 0.1273

0.9935 -0.1467

1.0185 -0.1607

0.9900 -0.1007

0.9874 -0,1996

1.0163 -0.0753

1.0156 -0.0895

1.0000 -0.0650

Camber 0/2

QINF = 346.4

MINF = 0.837

ALPT = 8.08

BETA = 0.11

H = 27423.

TINF = -32.7

RNPU = 2.6E+06

PSUR = 693.7

MTOP = 0.84

U/UTOP W/UTOP

0.6775 -0.2143

0.7734 -0.0737

0.8367 0.0421

0,8961 -0.2191

0.9426 -0.1929

0.9546 -0.1835

0.9824 -0.2530

1.0073 -0.1843

0.9977 -0.1706

1.0000 -0.1110

Camber 1/4

QINF = 298.1

MINF = 0.796

ALl:q" = 5.04

BETA = -0.07

H = 28535.

TINF = -37.1

RNPU = 2.3E+06

PSUR = 651.7

MTOP = 0.83

U/UTOP W/UTOP

0.5369 -0.4042

0.6735 0.0173

0.8521 0.0704

0.9721 -0.2044

1.0243 -0.1932

0.9936 -0.1502

0.9939 -0.2415

1.0104 -0.1419

0.9770 -0.1692

1.0000 -0.0991

Camber

QINF --

MINF =

ALPT --

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.5373

0.6745

0.8527

0.9725

1.0245

0.9935

0.9937

1.0111

0.9960

1.0000

1/4

297.4

0,796

5.04

-0.01

28545.

-37.3

2.3E+06

651.7

0.82

W/UTOP

-0.3838

0.0032

0.0655

-0.1997

-0.1952

-0.1577

-0.2364

-0.1304

-0.1547

-0.0973

810
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FIT 229

Time 13:04:07.500 13:04:14.000 13:04:14.500 13:04:i7.500 13:04:18.000

Camber 1/4

QINF = 296.5

MINF = 0.795

ALPT = 5.04

BETA = -0.21

H = 28577.

TINF = -36.9

RNPU = 2.3E+06

PSUR = 647.3

MTOP = 0.83

Y,in. U/UTOP W/UTOP

0.240 0.5437 -0.4960

0.470 0.6709 0.0071

0.970 0.8522 0.0743

1.470 0.9661 -0.2047

1,960 1.0184 -0.1927

2.330 0.9875 -0.1553

2.990 0.9862 -0.2376

3.490 1.0017 -0.1384

3.990 0.9924 -0.1484

4.960 1.0000 -0.0942

Camber 0/2

QINF = 303.2

MINF = 0.802

ALPT = 3.01

BETA = -0.27

H = 28476.

TINF = -36.5

RNPU = 2.4E+06

PSUR = 662.6

MTOP = 0.83

U/UTOP W/UTOP

0.6046 -0.1759

0.7567 0.0102

0.9108 0.1264

0.9841 -0.1425

1.0057 -0.1709

0.9765 -0.0905

0.9755 -0.2025

0,9951 -0.0879

0.9850 -0.1149

1.0000 -0.0598

Camber 0/2

QINF = 304.8

MINF= 0.804

ALPT = 3.00

BETA = -0.27

H = 28445.

TINF = -36.7

RNPU -- 2.4E+06

PSUR = 662.6

MTOP = 0.81

U/UTOP W/UTOP

0.6196 -0.1802

0.7682 0.0192

0.9393 0.1323

1.0109 -0.1491

1.0401 -0.1683

1.0015 -0.1038

1.0011 -0.2026

1.0284 -0.0867

1.0110 -0.1027

1.0000 -0.0673

Camber 0/2

QINF = 319.9

MINF= 0,818

ALPT = 3.01

BETA = 0.08

H = 28144.

TINF= -35.4

RNPU = 2.4E+06

PSUR = 672.6

MTOP = 0.84

U/UTOP W/UTOP

0.6046 -0.1541

0.7527 0.0090

0.9194 0.1275

0.9902 -0.1443

1.0167 -0.1764

0.9862 -0,0971

0.9848 -0.1993

1.0041 -0.0834

0.9916 -0.0998

1.0000 -0.0638

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6078

0.7503

0.9130

0.9930

1.0212

0.9873

0.9820

1.0187

0.9891

1,0000

0/2

322.7

0,820

3.00

-0.18

28081.

-34.8

2.4E+06

677.0

0.84

W/UTOP

-0.1673

-0.0041

0.1325

-0.1457

-0.1761

-0.0913

-0.2039

-0.0883

-0.0973

-0.0659

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

Time 13:04:23.500 13:04:24.500 13:04:25.000 13:04:29.000 13:04:29.500

Camber 2/6

QINF= 353.4

MINF= 0.842

ALPT = 7.95

BETA = -0.07

H = 27221.

TINF = -31.0

RNPU = 2.6E+06

PSUR = 700.4

MTOP = 0.85

Y,in. U/UTOP W/UTOP

0.240 0.3831 0.2196

0.470 0.5489 0.1037

0.970 0.6798 0.0347

1.470 0.8110 -0.2057

1.960 0.9377 -0.1879

2.330 0.9908 -0.1760

2.990 1.0049 -0.2605

3.490 1.0199 -0.1837

3.990 1.0052 -0.1833

4.960 1,000(3 -0.1253

Camber 3/6

QINF = 352.6

MINF = 0,840

ALPT = 8.56

BETA = -0.12

H = 27141.

TINF = -31.0

RNPU = 2.6E+06

PSUR = 698.3

MTOP = 0.83

U/UTOP W/UTOP

0.3252 -0.1072

0.5349 0.2921

0.5804 0.0505

0.6704 -0.1106

0.7940 -0.0985

0.8992 -0.1602

0.9848 -0.2159

1.0326 -0.1463

1.0237 -0.1569

1.0000 -0.0961

Camber 3/6

QINF= 351.3

MINF = 0.837

ALPT = 8.65

BETA = -0.27

H= 27117.

TINF = -31.1

RNPU = 2.6E+06

PSUR = 689.5

MTOP = 0.87

U/UTOP W/UTOP

0.2455 -0.0705

0.4869 0.3095

0.4898 0.0094

0.5236 -0.0983

0.6396 -0.0366

0.7492 -0.1354

0.8550 -0.1831

0.9641 -0.1121

0.9922 -0.1444

1.0000 -0.0828

Camber 4/7

QINF = 323.4

MINF = 0.808

ALPT = 8.88

BETA = -0.07

H = 27364.

TINF = -32.0

RNPU = 2.5E+06

PSUR = 647.7

MTOP = 0.89

U/UTOP W/UTOP

0.6231 -0.3865

0.6886 -0.0924

0.7675 -0.0543

0.8531 -0.2595

0.8954 -0.1963

0.9289 -0.2405

0.9632 -0.2826

0.9981 -0.2206

0.9995 -0.2357

1.0000 -0.1601

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF=

RNPU =

PSUR =

MTOP =

U/UTOP

0.6247

0.7014

0,7698

0.8509

0.8726

0.8963

0.9219

0.9711

0.9732

1.0000

4/7

318.1

0.803

8.96

-0.0 I

27445.

-32.0

2.4E+06

643,3

0.90

W/UTOP

-0.3426

-0.1035

-0.0456

-0.2418

-0.1694

-0.2309

-0.2701

-0.2361

-0.2294

-0.1538

811
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

Time 13:04:30.000 13:22:42.000 13:22:42.500 13:22:45.000 13:23:09.000

Camber 4/7

QINF= 312.1

MINF -- 0.797

ALPT = 8.88

BETA = -0.18

H = 27537.

TINF = -32.6

RNPU = 2.4E+06

PSUR -- 626.7

MTOP = 0.89

Y,in. U/UTOP W/UTOP

0.240 0.6664 -0.2278

0.470 0.7446 -0.0673

0.970 0.7898 -0.0642

1.470 0.8243 -0.2237

1.960 0.8284 -0.1300

2.330 0.8638 -0.2339

2.990 0.8869 -0.2488

3.490 0.9479 -0.2193

3.990 0.9705 -0.2206

4.960 1.0000 -0.1615

Camber 1/4

QINF = 304.8

MINF = 0.804

ALPT = 5.17

BETA = 0.25

H = 28478.

TINF = -36.4

RNPU -- 2.4E+06

PSUR = 655.0

MTOP = 0.82

U/IYroP W/UTOP

0.5306 -0.3124

0.6572 0.0135

0.8478 0.0706

0.9707 -0.2118

1.0308 -0.2016

0.9967 -0.1751

1.0051 -0.2550

1.0108 -0.1571

1.0003 -0.1422

1.00(10 -0.1016

Camber 1/4

QINF = 304.8

MINF = 0.804

ALPT = 5.17

BETA = 0.22

H = 28478.

TINF = -36.7

RNPU = 2.4E+06

PSUR = 655.0

MTOP = 0.83

U/UTOP W/UTOP

0.5302 -0.4205

0.6544 0.0148

0.8319 0.0726

0.9668 -0.2137

1.0213 -0.2047

0.9909 -0.1566

0.9982 -0.2376

1.0122 -0.1508

1.0014 -0.1488

1.0(100 -0.1019

Camber 1/4

QINF = 305.0

MINF = 0.804

ALPT = 5.17

BETA -- 0.08

H = 28479.

TINF = -36.8

RNPU = 2.4E+06

PSUR = 653.9

MTOP = 0.83

U/UTOP W/UTOP

0.5421 -0.5206

0.6672 -0.0001

0.8410 0.0711

0.9771 -0.2061

1.0275 -0.2035

0.9944 -0.1690

1.0024 -0.2478

1.0174 -0.1587

1.0075 -0.1588

1.0000 -0.1033

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.5571

0.6587

0.8315

0.9_2

1.0260

0.9916

0.9924

1.0138

1.0006

1.0000

1/4

307.0

0.807

5.17

0.02

28471.

-36.7

2.4E+06

650.6

0.84

W/UTOP

-0.4055

0.0182

0.0730

-0.2016

-0.2007

-0.1561

-0.2406

-0.1493

-0.1747

-0.1005

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 13:23:19.500 13:23:20.000 13:23:20.500 13:23:28.000 13:23:28.500

Camber 1/5

QINF -- 306.6

MINF = 0.806

ALPT = 6.02

BETA = -0.70

H = 28459.

TINF = -37.0

RNPU = 2.4E+06

PSUR = 629.8

MTOP = 0.87

Y.in. U/UTOP W/UTOP

0.240 0.5816 -0.3376

0.470 0.6792 -0.0197

0.970 0.8204 0.0443

1.470 0.9278 -0.2001

1.960 0.9954 -0.1848

2.330 0.9887 -0.1553

2.990 0.9923 -0.2364

3.490 1.0093 -0.1502

3.990 1.0000 -0.1654

4.960 1.0000 -0.1056

Camber 1/5

QINF = 306.4

MINF = 0.806

ALPT = 5.81

BETA = -0.56

H = 28459.

TINF = -36.9

RNPU -- 2.4E+06

PSUR = 630.9

MTOP = 0.88

U/UTOP W/UTOP

0.5887 -0.3430

0.6883 -0.0248

0.8166 0.0497

0.9221 -0.1990

0.9921 -0.1871

0.9810 -0.1562

0.9845 -0.2346

0.9917 -0.1654

0.9921 -0.1641

1.0000 -0.1059

Cam ber 1/5

QINF = 306.1

M1NF = 0.806

ALPT = 6.05

BETA = -0.53

H = 28458.

T1NF = -36.9

RNPU = 2.4E+06

PSUR = 625.4

MTOP = 0.88

U/UTOP W/UTOP

0.6126 -0.3005

0.7078 -0.0328

O.8254 O.0438

0.9418 -0.1968

0.9924 -0.1917

0.9844 -0.1616

0.9899 -0.2444

1.0078 -0.1652

0.9916 -0.1802

1.0000 -0.1159

Camber 2/6

QINF = 305.0

MINF = 0.800

ALPT -- 7.06

BETA = -0.27

H = 28221.

TINF = -35.6

RNPU = 2.4E+06

PSUR = 615.6

MTOP = 0.86

U/UTOP W/UTOP

0.6471 -0.2125

0.7476 -0.0190

0.7864 -0.0109

0.8106 -0.1967

0.8257 -0.0937

0.8315 -0.1335

0.8644 -0.2156

0.9370 -0.1506

0.9467 -0.1937

1.0000 -0.1447

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6423

0.7263

0.7782

0.8020

0.7945

0.8175

0.8578

0.9200

0.9355

1.0000

2/6

306.2

0.800

7.12

-0.18

28166.

-35.6

2.4E+06

611.2

0.87

W/UTOP

-0.2107

-0.0081

-0.0505

-0.1897

-0.1005

-0.1581

-0.2408

-0.1285

-0.2062

-0.1423

812
Table K-2. Continued.

FI 1 I/MAW BOUNDARY LAYER DATA. FLT 229

Time 13:23:30.500 13:23:31.000 12:54:02.500 12:54:03.000 I 1:34:59.500

Camber 3/6

QINF = 314.8

MINF = 0.806

ALPT = 7.94

BETA = 0,17

H = 27878.

TINF = -34, I

RNPU = 2.4E+06

PSUR = 603.5

MTOP = 0.87

Y.in. U/UTOP W/UTOP

0.240 0.6645 -0.2246

0.470 0.7347 -0.0225

0.970 0.7531 -0.0697

1.470 0.7542 -0.2049

1.960 0.7382 -0.0781

2.330 0,7546 -0,1474

2.990 0,7925 -0.2367

3.490 0.8708 -0,1358

3.990 0,8912 -0.2050

4.960 1.0000 -0,1560

Camber 3/6

QINF = 318.5

MINF = 0,810

ALPT = 8.12

BETA = 0.28

H = 27794,

TINF = -34.1

RNPU = 2.4E+06

PSUR = 627.8

MTOP = 0.88

U/UTOP W/UTOP

0.6918 -0.2523

0.7643 -0.0571

0.7775 -0.0469

0.7957 -0.2210

0.7968 -0.1114

0,7887 -0.1232

0,8380 -0.2320

0,9166 -0.1925

0.9382 -0.2310

1.0000 -0.1603

Camber 0/2

QINF = 345.1

MINF = 0.835

ALPT = 9.06

BETA = 0.08

H = 27365.

TINF = -32.3

RNPU = 2.5E+06

PSUR = 702.5

MTOP = 0.84

U/UTOP W/UTOP

0.6340 -0.1841

0.7179 -0,0370

0.7722 0,0374

0.8137 -0.2103

0.8697 -0.1699

0.8842 -0.1830

0.9250 -0.2414

0.9718 -0.1704

0.9793 -0,1699

1.0000 -0,1197

Camber 0/2

QINF= 343.5

MINF = 0.832

ALPT = 9,47

BETA = 0.11

H = 27351.

T1NF= -32,1

RNPU = 2.5E+06

PSUR = 699.2

MTOP = 0.83

U/UTOP W/UTOP

0.5910 -0.1348

0.6861 0.0384

0.7394 0.0446

0.7821 -0,1644

0.8236 -0.1321

0.8515 -0,1739

0.8919 -0.2203

0,9461 -0.1449

0.9435 -0.1388

1.0000 -0.1093

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP --

U/UTOP

0.6057

0,7253

0.8744

0.9660

1.0171

0,9945

0.9985

1.0032

0.9949

1.0000

0/2

295.0

0.847

5.16

0.22

31472.

-50.4

2.3E+06

571.5

0.87

W/UTOP

-0,2641

-0.0236

0.0865

-0.1836

-0A935

-0.1422

-0.2263

-0,1176

-0.1326

-0.0852

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 1 1:35:01.500 11:35:09.500 11:35:36.500 11:35:42,000 11:35:51,000

Camber 0/2

QINF = 295.0

MINF = 0,847

ALPT = 5.20

BETA = 0,19

H = 31461,

T1NF = -50.4

RNPU = 2.3E÷06

PSUR = 578,2

MTOP = 0,86

Y.in. U/UTOP W/UTOP

0.240 0.6010 -0,2498

0.470 0.7253 -0,0217

0.970 0.8717 0,0933

1.470 0.9662 -0.1789

1.960 1.0218 -0.1944

2.330 0.9944 -0.1444

2.990 0.9997 -0.2314

3.490 1.0076 -0.1225

3.990 1,0021 -0.1357

4.960 1.0000 -0,0855

Camber 0/2

QINF = 297.7

MINF = 0,849

ALPT = 5.89

BETA = 0.19

H = 31376.

TINF = -50.0

RNPU = 2.3E+06

PSUR = 577.0

MTOP = 0,86

U/UTOP W/UTOP

0.6357 -0.2287

0.7517 -0.0356

0.8744 0.0834

0.9547 -0.1956

1,0078 -0,2014

0,9979 -0.1494

1.0030 -0.2385

1,0058 -0,1426

0.9913 -0.1502

1.0000 -0,0917

Camber 0/2

QINF = 300.1

MINF = 0,852

ALPT = 6.02

BETA = -0.04

H = 31358.

TINF = -50.4

RNPU = 2.3E+06

PSUR = 577.0

MTOP = 0.86

U/UTOP W/UTOP

0.6399 -0.2051

0.7471 -0.0354

0.8660 0.0821

0.9515 -0,1971

1.0059 -0.2000

0.9940 -0.1500

1,0012 -0.2305

1.0081 -0.1 445

1.0104 -0,1410

1.0000 -0.0952

Camber 0/2

QINF= 301,5

MINF= 0.855

ALPT = 7.01

BETA = -0,27

H = 31394.

TINF = -50.0

RNPU = 2.3E+06

PSUR = 580.3

MTOP = 0.85

U/UTOP W/UTOP

0.6751 -0.2312

0.7758 -0.0588

0.8533 0.0688

0.9242 -0.2043

0.9799 -0.1963

0,9894 -0.1582

1.0140 -0,2494

1,0250 -0,1338

1,0049 -0,1559

1,0000 -0.1044

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6710

0.7530

0.8137

0.8688

0.9252

0.9388

0.9796

1.0124

1.0076

1.0000

O/2

293.2

0.845

8,01

0,02

31514.

-50.2

2.3E+06

578.2

0.84

W/UTOP

-0.1980

-0.0528

0.0486

-0.2131

-0.1844

-0.1636

-0,2630

-0.1826

-0.1788

-0.1124

813
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:35:52,000 11:37:34,000 11:37:40.000 11:38:11.500 11:38:12,500

Camber 0/2

QINF = 294.7

MINF = 0.847

ALPT -- 8.01

BETA = -0.04

H = 31494.

TINT = -50.1

RNPU = 2.3E+06

PSUR = 580.3

MTOP = 0.84

Y, in. U/UTOP W/UTOP

0.240 0.6574 -0.2843

0.470 0.7468 -0.0474

0.970 0.8011 0.0553

1,470 0.8651 -0.2008

1,960 0.9143 -0.1869

2.330 0.9346 -0.1714

2,990 0.9738 -0.2526

3.490 1.0077 -0.1631

3,990 1.0067 -0.1633

4.960 1.0000 -0.1163

Camber 5/2

QINF = 297.5

M1NF = 0.844

ALPT = 5.70

BETA = 0.05

H = 31162.

TINF = -49.1

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.85

U/UTOP W/UTOP

0.6500 -0.2018

0.7655 -0.0338

0.8729 0.0894

0.9430 -0.1857

1.0013 -0.1920

0.9978 -0.1439

1.0093 -0.2336

1.0122 -0.1301

1.0023 -0.1336

1.0000 -0.0947

Camber 5/2

QINF = 297.3

MINF = 0.844

ALPT = 5.70

BETA = -0.01

H = 31173.

TI NF = -49.1

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.83

U/UTOP W/UTOP

0.6664 -0.2441

0.7760 -0.0340

0.8839 0.0842

0.9540 -0.1905

1.0155 -0.1943

1.0094 -0.1470

1.0213 -0.2388

1.0303 -0.1285

1.0158 -0.1326

1.0000 -0.0981

Camber 5/2

QINF = 297.2

MINF = 0,845

ALPT = 6.00

BETA = -0.53

H = 31206.

TINT = -48.9

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.84

U/UTOP W/UTOP

0.6568 -0.2143

0.7669 -0.0336

0,8731 0.0806

0.9375 -0.1836

0.9924 -0.1920

0.9974 -0.1429

1.0099 -0.2250

1.0182 -0.1270

1.0045 -0.1372

1.0000 -0.0889

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.6548

0.7_5

0.8_5

0.9293

0.9901

0.9916

1.0090

1.0159

1.0086

1.0000

5/2

297.6

0.846

6.02

-0.44

31207.

-48.9

2.3E+06

580.4

0.85

W/UTOP

-0.2207

-0.0436

0.0846

-0.1820

-0.1855

-0.1460

-0.2390

-0.1135

-0.1379

-0.0867

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:38:18,500 11:38:22.000 11:38:25.000 11:38:28,500 11:38:33.500

Camber 5/2

QINF = 300.1

MINF = 0.849

ALPT = 7.10

BETA = -0.33

H = 31223.

TINF = -49.1

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.84

Y, in. U/UTOP W/UTOP

0.240 0.6715 -0.2318

0.470 0.762 t -0.0466

0.970 0.8426 0.0653

1.470 0.9026 -0.1979

1.960 0.9591 -0.1885

2.330 0.9756 -0.1566

2.990 1.0081 -0.2474

3.490 1.0291 -0.1445

3,990 1.0228 -0.1539

4.960 1.0000 -0.1044

Camber 5/2

QINF = 300.3

MINF = 0.850

ALPT = 8.01

BETA = -0.41

H = 31257.

TINF = -48.9

RNPU = 2.3E+06

PSUR = 589.3

MTOP = 0.85

U/UTOP W/UTOP

0.5744 -0.1723

0.6824 0.0018

0.7458 0.0724

0.8096 -0.1865

0.8798 -0.1711

0.9097 -0.1602

0.9671 -0.2395

0.9933 -0.1594

0.9991 -0.1719

1.0000 -0. l 143

Camber 5/2

QINF = 299.3

MINF = 0,850

ALPT = 8.01

BETA = -0.04

H = 31300.

TINF = -49.1

RNPU = 2.3E+06

PSUR = 587.1

MTOP = 0.85

U/UTOP W/UTOP

0.5951 -0.1755

0.6833 0.0135

0.7458 0.0589

0.8142 -0.1947

0.8803 -0.1689

0.9150 -0.1651

0.9697 -0.2455

1.0030 -0.1579

1.0017 -0.1747

1.0000 -0.1174

Camber 5/2

QINF = 298.6

MINF = 0,850

ALPT = 8.01

BETA = -0.18

H = 31344.

TINF = -49.4

RNPU = 2.3E+06

PSUR = 583.7

MTOP = 0.87

U/UTOP W/UTOP

0.5793 -0.2275

0.6776 0.0102

0.7381 0.0601

0.7944 -0.1975

0.8639 -0.1563

0.8935 -0.1622

0.9492 -0.2415

0.9866 -0.1416

0.9908 -0.1676

1.0000 -0.0974

Camber

Q1NF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.3587

0.6040

0.5879

0.6058

0.6377

0.6281

0.6797

0.8174

0.8225

1.0000

5/2

299.0

0,851

9.02

-0.07

31367.

-49.2

2.3E+06

559.6

0.66

W/UTOP

-0.0175

0.3736

-0.0828

-0.1941

-0.0014

-0.0744

-0.2382

-0.0176

-0.1236

-0.0974

814
TableK-2.Continued.

FI l I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:35:07.500 l 1:35:10,500 11:35:11,500 11:35:23.000 11:35:28,500

Camber 0/2

QINF = 297.4

MINF = O.849

ALPT = 5.72

BETA = 0.28

H = 31398.

TINF = -50.3

RNPU = 2.3E+06

PSUR = 578.2

MTOP = 0.85

Y, in. U/LrroP W/UTOP

0.240 0.6217 -0.2323

0.470 0.7437 -0.0379

0,970 0.8720 0.0827

1.470 0.9564 -0.1867

1,960 1.0140 -0,2051

2,330 0.9990 -0.1461

2.990 1.0026 -0.2335

3.490 1.0049 -0,1417

3.990 1.0077 -0.1397

4.960 1.0000 -0.0923

Camber 0/2

QINF = 297,7

MINF = 0.849

ALPT = 5.71

BETA = 0.19

H = 31376.

TINF = -50,0

RNPU = 2.3E+06

PSUR = 577,0

MTOP = 0.86

U/UTOP W/UTOP

0.6270 -0.2385

0.7494 -0.0355

0.8715 0,0819

0,9512 -0,1900

1.0061 -0.1982

0,9948 -0,1502

0.9999 -0.2377

1.0051 -0,1470

0.9984 -0.1450

1.0000 -0.0934

Camber 0/2

QINF= 298.1

MINF = 0.849

ALPT = 5.72

BETA = 0.25

H = 31365,

TINF = -50.4

RNPU = 2.3E+06

PSUR = 576.0

MTOP = 0.86

U/UTOP W/UTOP

0.6298 -0.2506

0.7620 -0,0445

0.8787 0.0830

0.9651 -0.1937

1.0145 -0.2004

0.9987 -0.1484

1.0069 -0.2265

1.0l 17 -0.1243

1.0057 -0.1544

1,0000 -0.0988

Camber 0/2

QINF = 296.3

MINF = 0,848

ALPT = 5.52

BETA = 0. l 1

H = 31419.

T1NF -- -50.2

RNPU = 2.3E+06

PSUR = 578.2

MTOP = 0.86

U/UTOP W/UTOP

0.6128 -0.2275

0.7344 -0.0247

0.8668 0.0934

0.9599 -0.1858

1.0179 -0,1987

0,9955 -0.1457

1.0020 -0.2388

1,0097 -0.1358

1.0052 -0,1553

1.0O00 -0.0889

Camber

QINF =

MINF =

ALPT =

BETA -

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0,6087

0.7312

0.8690

0.9478

1.0221

0.9928

0.9982

1,0049

0.9789

1.0000

0/2

296.8

0.848

5.49

0.08

31397,

--49.9

2,3E+06

578.2

0.86

W/UTOP

-0.2357

-0.0190

0.0930

-0,1925

-0.1909

-0,1369

-0.2355

-0.1287

-0.1504

-0.0870

F111/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:35:29.000 11:35:29,500 l 1:35:37,000 11:35:37.500 11:35:41.500

Camber 0/2

QINF = 296.8

MINF = 0.848

ALPT = 5.49

BETA = 0.19

H = 31397.

TINF = -49.9

RNPU = 2.3E+06

PSUR = 578.2

MTOP = 0.86

Y, in. U/UTOP W/UTOP

0.240 0.6096 -0.2360

0.470 0.7323 -0.0246

0.970 0,8691 0.0866

1,470 0,9616 -0.1860

1,960 1.0183 -0.1956

2.330 0,9944 -0.1383

2,990 0.9982 -0.2315

3.490 1.0026 -0.1357

3,990 1.0007 -0,1373

4,960 1.0000 -0.0876

Camber 0/2

QINF = 297.0

MINF = 0.848

ALPT = 5.49

BETA = 0,22

H = 31397,

TINF = -49,9

RNPU = 2.3E+06

PSUR = 578,2

MTOP = 0.86

U/UTOP W/UTOP

0.6086 -0,2356

0.7315 -0.0349

0.8749 0,0918

0,9690 -0.1740

1.0161 -0.1928

0.9971 -0.1323

0.9961 -0.2295

1.0055 -0.1385

0.9825 -0.1599

1.0000 -0,0883

Camber 0/2

QINF = 300,3

MINF= 0,852

ALPT = 6.02

BETA = 0.02

H = 31358.

TINF = -50.1

RNPU = 2.3E+06

PSUR = 580.3

MTOP = 0.86

U/UTOP W/UTOP

0.6390 -0.2225

0.7527 -0.0428

0.8767 0.0775

0.9452 -0.1913

1.0013 -0.2000

0.9957 -0.1514

1.0039 -0,2378

1.0094 -0.1380

1.0023 -0,1456

1,0000 -0.0928

Camber 0/2

QINF = 300.5

MINF= 0.852

ALPT = 6.07

BETA = -0.01

H = 31347.

TI NF = -50.1

RNPU = 2.3E+06

PSUR = 578,2

MTOP = 0.86

U/UTOP W/UTOP

0.6438 -0.2245

0.7654 -0.0541

0.8748 0.0788

0.9487 -0.1930

1.0022 -0,2014

0,9969 -0,1565

1.0087 -0.2438

1.0145 -0.1399

1.0053 -0.1460

1.0O0O -0,0928

Camber

QINF =

MINF =

ALPT =

BETA

H=

TINF=

RNPU =

PSUR =

MTOP --

U/UTOP

0.6732

0.7754

0.8600

0.9172

0,9759

0.9906

1.0141

1.0227

0,9910

1.0000

0/2

301.9

0.855

6.96

-0.33

31384.

-50.4

2.3E+06

579.3

0.85

W/UTOP

-0.2440

-0.0485

0.0749

-0.2122

-0.1967

-0.1580

-0.2536

-0,1516

-0.1662

-0.1023

815
TableK-2.Continued.

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:35:42.500 11:35:50.000 11:35:50.500 11:36:01.500 11:36:02.000

Y, in.

0.240

0.470

0.970

1.470

1.960

2.330

2.990

3.490

3.990

4.960

Camber 0/2

QINF = 301.3

MINF = 0.854

ALPT = 7.06

BETA -- -0.33

H = 31394.

TINF = -50.0

RNPU = 2.3E+06

PSUR -- 582.6

MTOP = 0.85

U/UTOP W/UTOP

0.6662 -0.2282

0.7678 -0.0596

0.8547 0.0625

0.9218 -0.1946

0.9727 -0.1962

0.9796 -0.1568

1.0098 -0.2433

1.0181 -0.1624

1.0072 -0.1511

1.0000 -0.0989

Camber 0/2

QINF -- 292.4

MINF = 0.844

ALPT = 7.92

BETA = 0.19

H= 31512.

TINF = -50.4

RNPU = 2.3E+06

PSUR -- 577.0

MTOP = 0.85

U/UTOP W/UTOP

0.6751 -0.2739

0.7656 -0.0528

0.8232 0.0499

0.8848 -0.2060

0.9326 -0.1872

0.9436 -0.1744

0.9814 -0.2566

1.0066 -0.1629

0.9959 -0.1733

1.0000 -0.1076

Camber 0/2

QINF = 292.6

MINF = 0.844

ALPT = 7.92

BETA = 0.02

H= 31513.

TINF = -50.1

RNPU = 2.3E+06

PSUR = 577.0

MTOP = 0.84

U/UTOP W/UTOP

0.6784 -0.2275

0.7676 -0.0416

0.8266 0.0402

0.8909 -0.2051

0.9420 -0.1763

0.9498 -0.1763

0.9897 -0.2501

1.0176 -0.1602

1.0165 -0.1644

1.0000 -0.1159

Camber 0/2

QINF = 310.2

MINF = 0.860

ALPT = 8.58

BETA = 0.66

H = 31038.

TINF -- -48.4

RNPU = 2.3E+06

PSUR = 588.2

MTOP = 0.85

U/UTOP W/UTOP

0.4083 0.0766

0.5344 0.1376

0.5783 0.0602

0.6256 -0.1574

0.6826 -0.0675

0.7664 -0.1890

0.8240 -0.2472

0.9079 -0.1234

0.9140 -0.1715

1.0000 -0.1115

Camber

QINF =

MINF =

ALPT ---

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP --

U/UTOP

0.3661

0.5246

0.5497

0.5662

0.5978

0.6658

0.7257

0.8407

0.8581

1.0000

0/2

311.6

0.861

8.67

0.74

31007.

-47.9

2.3E+06

577.3

0.79

W/UTOP

-0.0187

0.2020

0.0607

-0.1 647

-0.0453

-0.1788

-0.2286

-0.0903

-0.1636

-0.1156

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:36:24.500 11:37:37.000 11:37:38.000 11:37:38.500

Y, in.

0.240

0.470

0.970

1.470

1.960

2.330

2.990

3.490

3.990

4.960

Camber

QINF =

MINT=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.3513

0.6105

0.5711

0.5868

0.5835

0.6175

0.6721

0.8003

0.7342

1.0000

11:37:33.500

0/2 Camber

313.7 QINF =

0.860 MINF =

9.15 ALPT =

-0.15 BETA

30809. H =

-46.8 TINF =

2.4E+06 RNPU =

572.9 PSUR =

0.65 MTOP =

W/UTOP U/UTOP

-0.0177 0.6377

0.3724 0.7561

-0.1738 0.8615

-0.1880 0.9369

-0.0013 0.9873

-0.1305 0.9824

-0.2962 0.9935

-0.0134 1.0034

-0.1126 0.9833

-0.1211 1.0000

5/2

297.7

0.845

5.70

0.02

31162.

-49.2

2.3E+06

589.3

0.85

W/UTOP

-0.2081

-0.0207

0.0794

-0.1725

-0.1873

-0.1471

-0.2372

-0.1655

-0.1326

-0.0844

Camber 5/2

QINF -- 297.0

MINF = 0.844

ALPT -- 5.56

BETA = 0.02

H= 31172.

TINF -- -49.1

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.85

U/UTOP W/UTOP

0.6515 -0.1897

0.7709 -0.0315

0.8766 0.0902

0.9424 -0.1846

0.9983 -0.1817

0.9951 -0.1436

1.0052 -0.2326

1.0091 -0.1266

1.0040 -0.1525

1.0000 -0.0900

Camber 5/2

QINF = 297.3

MINF -- 0.844

ALPT = 5.53

BETA = 0.02

H = 31173.

TINF = -49.1

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.85

U/UTOP W/UTOP

0.6528 -0.2277

0.7656 -0.0335

0.8790 0.0893

0.9461 -0.1780

1.0036 -0.1926

0.9981 -0.1440

1.0083 -0.2338

1.0124 -0.1302

1.0078 -0.1337

1.00130 -0.0914

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6520

0.7698

0.8757

0.9463

1.0083

0.9948

1.0053

1.0096

1.0028

1.0000

5/2

297.3

0.844

5.53

-0.04

31173.

-49.1

2.3E+06

586.0

0.85

W/UTOP

-0.2127

-0.0314

0.0877

-0.1790

-0.1866

-0.1399

-0.2327

-0.1298

-0.1392

-0.0885

816
Table K-2. Continued.

FI 1 I/MAW BOUNDARY LAYER DATA. FLT 229

Time 11:37:55.000 11:37:55.500 11:38:10.500 11:38:11.000 11:38:12.000

Camber 5/2

QINF -- 296.6

MINF = 0.844

ALPT = 5.71

BETA = -0.01

H = 31194.

TINF -- -49.0

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.85

Y, in. U/LrrOP W/LrrOP

0.240 0.6574 -0.2398

0.470 0.7641 -0.0336

0.970 0.8710 0.0843

1.470 0.9416 -0.1843

1.960 0.9982 -0.1940

2.330 0.9963 -0.1401

2.990 1.0059 -0.2347

3.490 1.0109 -0.1300

3.990 1.0037 -0.1327

4.960 1.0000 -0.0907

Camber 5/2

QINF -- 296.6

MINF = 0.844

ALPT = 5.71

BETA = -0.01

H= 31194.

TINF = -49.0

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.85

U/UTOP W/UTOP

0.6586 -0.2017

0.7730 -0.0315

0.8725 0.0879

0.9428 -0.1845

0.9988 -0.1898

0.9957 -0.1462

1.0077 -0.2366

1.0040 -0.1376

1.0002 -0.1405

1.0000 -0.0947

Camber 5/2

QINF = 297.2

MINF = 0.845

ALPT = 5.91

BETA = -0.65

H = 31206.

TINF = -48.9

RNPU = 2.3E+06

PSUR = 580.4

MTOP = 0.85

U/UTOP W/UTOP

0.6638 -0.2312

0.7728 -0.0326

0.8706 0.0807

0.9321 -0.1983

1.0015 -0.1937

0.9986 -0.1344

1.0071 -0.2392

1.0122 -0.1178

1.0037 -0.1333

1.0000 -0.0901

Camber 5/2

QINF= 297.2

MINF = 0.845

ALPT = 5.91

BETA = -0.56

H = 31206.

TINF = -48.9

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.84

U/UTOP W/UTOP

0.6595 -0.2406

0.7588 -0.0360

0.8716 0.0701

0.9358 -0.1870

0.9960 -0.1956

0.9950 -0.1439

1.0100 -0.2342

1.0279 -0.1163

1.13011 -0.1303

1.0000 -0.0889

Camber

QINF =

MINF =

ALPT =

BETA --

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6547

0.7659

0.8653

0.9442

0.9919

0.9936

1.0094

1.0153

1.0022

1.0000

5/2

297.4

0.845

5.96

-0.53

31207.

-48.9

2.3E+06

584.9

0.85

W/UTOP

-0.2129

-0.0436

0.0788

-0.1736

-0.1946

-0.1473

-0.2410

-0.1085

-0.1303

-0.0909

F11 I/MAW BOUNDARY LAYER DATA. FLT 229

Time 11:38:13.500 11:38:17.500 11:38:18.000 11:38:19,000 11:38:22.500

Camber 5/2

QINF = 297.4

MINF = 0.845

ALPT = 6.11

BETA = -0.38

H = 31207.

TINF = -48.9

RNPU = 2.3E+06

PSUR= 584.9

MTOP = 0.85

Y,in. U/UTOP W/UTOP

0.240 0.6555 -0.2139

0.470 0.7733 -0.0411

0.970 0.8583 0.0735

1.470 0.9274 -0.1878

1.960 0.9840 -0.1920

2.330 0.9911 -0.1470

2.990 1.0084 -0.2348

3.490 1.0147 -0.1347

3.990 1.0031 -0.1431

4,960 1,0000 -0.0941

Camber 5/2

QINF = 299.3

MINF = 0.848

ALPT = 6.91

BETA = -0.44

H = 31221.

TINF = -48.6

RNPU = 2.3E+06

PSUR = 586,0

MTOP = 0.84

U/UTOP W/UTOP

0.6768 -0.2362

0.7688 -0.0437

0.8425 0.0690

0.9095 -0.1946

0.9669 -0.1901

0.9781 -0.1555

1.0101 -0.2444

1.0238 -0.1538

1.0182 -0.1577

1.0000 -0.1010

Camber 5/2

QINF = 299.9

MINF= 0.849

ALPT = 6.98

BETA = -0.38

H = 31223.

TINF = -48.7

RNPU = 2.3E+06

PSUR = 584.9

MTOP = 0.83

U/UTOP W/UTOP

0.6762 -0.2403

0.7684 -0.0567

0.8430 0.0699

0.9084 -0.2031

0.9693 -0.1916

0.9855 -0.1564

1.0175 -0.2462

1.0325 -0.1427

1.0408 -0.1522

1.0000 -0.1064

Camber 5/2

QINF = 300.1

MINF= 0.850

ALPT = 7.27

BETA = -0.44

H = 31234.

T1NF = -48.8

RNPU = 2.3E+06

PSUR = 586.0

MTOP = 0.84

U/UTOP W/UTOP

0.6651 -0.2389

0.7524 -0.0279

0.8206 00550

0.8831 -0.2087

0.9544 -0.1888

0.9687 -0.1625

1.0051 -0.2427

1.0275 -0.1497

1.0187 -0.1638

1.0000 -0.1040

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5908

0.6819

0.7405

0.8085

0.8773

0.9085

0.9633

0.9976

1.0044

1.0000

5/2

299.8

0.850

804

-0.36

31267.

-48.8

2.3E+06

588.2

0.85

W/UTOP

-0.2056

0.0128

0.0641

-0.1804

-0.1680

-0.1600

-0.2434

-0.1417

-0.1592

-0.1 047

817
Table K-2. Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:38:24.000 11:38:25.500 11:38:27.000 11:38:28.000 11:38:31.000

Camber 5/2

Q1NF = 299.4

MINF --- 0.850

ALPT = 8.04

BETA = -0.21

H = 31289.

TINF = -48.8

RNPU = 2.3E+06

PSUR = 589.3

MTOP = 0.85

Y, in. U/I.YrOP W/UTOP

0.240 0.5756 -0.2330

0.470 0.6659 0.0408

0,970 0.7301 0.0654

1.470 0.7954 -0.1855

1.960 0.8692 -0.1642

2.330 0.9034 -0.1569

2,990 0.9575 -0.2399

3,490 0.9962 -0.1977

3.990 0.9768 -0.1709

4.960 1.0000 -0.1067

Camber 5/2

QINF = 299.3

MINF = 0.850

ALPT = 8.01

BETA = -0.07

H= 31311.

TINF = -49.1

RNPU = 2.3E+06

PSUR = 587.1

MTOP = 0.85

U/UTOP W/UTOP

0.5972 -0.2075

0.6826 0.0134

0.7456 0.0645

0.8091 -0.1902

0.8797 -0.1683

0.9111 -0.1658

0.9669 -0.2485

1.0025 -0.1641

1.0000 -0.1697

1.0000 -0.1132

Camber 5/2

QINF = 298.6

MINF = 0.849

ALPT = 8.01

BETA = -0.10

H = 31333.

TINF = -49.4

RNPU = 2.3E+06

PSUR = 587.1

MTOP = 0.85

U/UTOP W/UTOP

0.5785 -0.1932

0.6799 0.0226

0.7264 0.0624

0.8003 -0.1918

0.8606 -0.1764

0.8989 -0.1632

0.9569 -0.2474

0.9919 -0.1622

0.9954 -0.1644

1.0000 -0.1095

Camber 5/2

QINF = 298.4

MINF -- 0.849

ALPT = 8.01

BETA = -0.12

H = 31343.

TINF = -49. I

RNPU = 2.3E+06

PSUR = 589.3

MTOP = 0.85

U/UTOP W/UTOP

0.5898 -0.2053

0.6773 0.0133

0.7412 0.0660

0.8273 -0.1771

0.8854 -0.1721

0.9099 -0.1574

0.9647 -0.2547

0.9991 -0.1566

1.0026 -0.1927

1.0000 -0.1115

Camber

QINF =

MINF =

ALPT =

BETA =

H=

T1NF =

RNPU --

PSUR =

MTOP --

U/UTOP

0.5513

0._85

0.7044

0.7850

0.8444

0.8859

0.9_9

0.9911

0.9_0

1.0000

5/2

299.2

0.851

8.20

-0.10

31367.

-49.3

2.3E+06

590.3

0.85

W/UTOP

-0.1991

0.0772

0.0568

-0.1704

-0.1574

-0.1630

-0.2454

-0.2070

-0.1705

-0.1107

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:38:31.500 11:38:32.000 11:38:32.500 11:38:33.000 11:38:34.000

Camber 5/2

QINF = 299.4

MINF = 0.851

ALPT = 8.38

BETA = -0.04

H = 31368.

TINF = -49.0

RNPU = 2.3E+06

PSUR = 586.0

MTOP = 0.86

Y, in. U/UTOP W/UTOP

0.240 0.4808 -0.4474

0.470 0.5760 0.1196

0.970 0.6282 0.0661

1.470 0.6850 -0.1471

1.960 0.7549 -0.1155

2.330 0.8156 -0.1656

2.990 0.8867 -0.2200

3.490 0.9500 -0.1485

3.990 0.9736 -0.1635

4.960 1.0000 -0.1127

Camber 5/2

QINF = 299.4

MINF = 0.851

ALPT = 8.78

BETA= 0.11

H = 31368.

TINF = -49.3

RNPU = 2.3E+06

PSUR = 577.2

MTOP = 0.81

U/UTOP W/UTOP

0.3431 -0.0502

0.5280 0.2625

0.5231 0.0355

0.5761 -0.1550

0.6228 -0.0656

0.6974 -0.1815

0.7610 -0.2121

0.8591 -0.1137

0.8901 -0.1625

1.0000 -0.1117

Camber 5/2

QINF = 299.2

MINI:: = 0.851

ALPT = 8.85

BETA = 0.05

H = 31367.

TINF = -49.3

RNPU = 2.3E+06

PSUR = 569.5

MTOP = 0.74

U/UTOP W/UTOP

0.3077 -0.0311

0.5410 0.3209

0.5336 0.0103

0.5554 -0.1535

0.5679 -0.0195

0.6256 -0.1362

0.6786 -0.2399

0.8185 -0.0836

0.7941 -0.1312

1.0000 -0.1017

Camber 5/2

Q1NF = 299.0

MINF = 0.851

ALPT = 8.90

BETA = 0.08

H = 31367.

TINF = -49.2

RNPU = 2.3E+06

PSUR = 564.0

MTOP = 0.67

U/UTOP W/UTOP

0.3120 -0.0246

0.5806 0.2754

0.5552 -0.0320

0.5872 -0.1799

0.5903 0.0030

0.6029 -0.1094

0.6752 -0.4431

0.8091 -0.0163

0.8167 -0.1024

1.0000 -0.1104

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.3846

0.6540

0.6218

0.6500

0.639O

0.6309

0.7294

0.8100

0.7910

1.0000

5/2

299.0

0.851

9.08

-0.10

31367.

-49.2

2.3E+06

551.9

0.62

W/UTOP

-0.0503

0.4442

-0.1475

-0.1814

-0.0030

-0.0746

-0.5914

-0.0002

-0.1029

-0.1083

818
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:31:28.000 12:31:28.500 12:31:37,000 12:31:42.000 12:31:44.500

Camber 0/2

QINF = 302.0

MINF = 0.902

ALPT = 5.70

BETA = -0.12

H = 33651.

TINF -- -59.4

RNPU = 2.3E+06

PSUR = 533.1

MTOP = 0.88

Y, im U/UTOP W/UTOP

0.240 0.5233 -0.4812

0.470 0.6441 0.0905

0,970 0.7806 0.1247

1.470 0.8911 -0.1729

1.960 1.0156 -0.1987

2.330 1.0002 -0.1450

2.990 1.0045 -0.2377

3.490 1.0187 -0.1216

3.990 1.0016 -0.1373

4.960 1.0000 -0.0831

Camber 0/2

QINF = 302.0

MINF = 0.902

ALPT = 5.70

BETA = 0.28

H = 33651.

TINF = -59.7

RNPU = 2.3E+06

PSUR = 533.1

MTOP = 0.88

U/UTOP W/UTOP

0.5231 -0.4810

0.6473 0.0685

0.7803 0.1247

0.8933 -0.1718

1.0120 -0.2038

1.0017 -0.1414

1.0057 -0.2425

1.0185 -0.1248

1.0062 -0.1338

1.0000 -0.0895

Camber 0/2

QINF = 3O 1.4

MINF= 0,899

ALPT = 5.70

BETA = 0.22

H = 33556.

TINF = -59.7

RNPU = 2.3E+06

PSUR = 535.4

MTOP = 0.88

U/UTOP W/UTOP

0.5376 -0.4093

0.6597 0.0975

0,7910 0.1224

0.9063 -0.1862

1.0252 -0.2027

1.0029 -0.1454

1.0064 -0.2400

1.0200 -0.1352

1.0022 -0.1423

1.0000 -0.0871

Camber 0/2

QINF = 301.7

MINF = 0.898

ALPT = 6.03

BETA = 0.11

H = 33500.

TINF = -59.6

RNPU = 2.3E+06

PSUR = 537.6

MTOP = 0.87

U/UTOP W/UTOP

0.5196 -0.5191

0.6354 0.0846

0.7587 0.1209

0.8750 -0.1791

1.0047 -0.1980

1.0019 -0.1492

1.0084 -0.2471

1.0209 -0.1303

1.0109 -0.1405

1.0003 -0.0943

Camber

QINF =

MINF =

ALPT =

BETA --

H=

TINF --

RNPU --

PSUR --

MTOP =

U/UTOP

0.5189

0.6358

0.7654

0.8746

1.0029

1,0011

1.0072

1.0179

1.0217

1.0000

0/2

301.4

0.897

6.11

-0.01

33465.

-59.4

2.3E+06

537.6

0.87

W/UTOP

-0.5184

0.1041

0.1186

-0.1695

-0.1968

-0.1575

-0.2472

-0.1350

-0.1299

-0.0917

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:31:58.000 12:31:59.000 12:32:01.000 12:32:01.500 12:32:03.000

Camber 0/2

QINF = 300.3

MINF = 0.895

ALPT = 6.70

BETA = -0.47

H = 33473.

T1NF = -59.2

RNPU = 2.3E+06

PSUR = 536.5

MTOP = 0.87

Y, in. U/UTOP W/UTOP

0.240 0.4559 0.1368

0.470 0.5963 0.1185

0.970 0.7197 0.1268

1.470 0.8211 -0.1628

1.960 0.9684 -0.1925

2.330 0.9967 -0.1475

2.990 1.0081 -0.2309

3.490 1.0235 -0.1219

3.990 1.0057 -0.1353

4.960 1.0000 -0.0862

Camber 0/2

QINF= 300.3

MINF = 0.895

ALPT = 7.27

BETA = -0.33

H = 33473.

T1NF = -59.2

RNPU = 2.3E+06

PSUR = 522.2

MTOP = 0.91

U/UTOP W/UTOP

0.3323 -0,0767

0.5305 0.2607

0.5674 0.1292

0.6101 -0.1433

0.7010 -0.1011

0.8273 -0.2473

0.9239 -0.2384

0.9958 -0.1017

0.9960 -0.1523

1.0000 -0.0893

Camber 0/2

QINF = 298.6

MINF = 0.893

ALPT = 7.60

BETA = -0.41

H = 33490.

TINF = -59.3

RNPU = 2.2E+06

PSUR = 500.3

MTOP = 0.72

U/UTOP W/UTOP

0.2940 -0.0395

0.6001 0.3587

0.5436 0.1488

0,5290 -0.2087

0.5335 0.0089

0.5006 -0.0521

0.5006 -0.2688

0.7247 0.0472

0.7001 -0.0833

1.0000 -0.0721

Camber 0/2

QINF = 297.9

MINF= 0.892

ALPT = 7.58

BETA = -0.53

H = 33499.

TINF = -59.5

RNPU = 2.2E+06

PSUR = 504.7

MTOP = 0.70

U/UTOP W/UTOP

0.3014 -0.0533

0.6203 0.4292

0.5353 0.1432

0.4977 -0.1963

0.4966 0.0388

0.4974 -0.0432

0.3389 0.1125

0.7314 0,0376

0.7031 -0.0552

1.0000 -0.0823

Camber

Q1NF =

MINF --

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.3063

0.5147

0.5275

0.5568

0.6457

0.7089

0.8374

0.9408

0.9820

1.0000

0/2

297.6

0.892

7.23

-0.15

33521.

-59.5

2.2E+06

522.3

0.90

W/UTOP

-0.0371

0.2664

0,1076

-0.1556

-0.0780

-0.0416

-0.2240

-0.1230

-0.1431

-0.0935

819
TableK-2.Continued.

FI 1 l/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:32:03.500 12:32:04.000 12:32:05.500 12:32:59.000 12:33:43.500

Camber 0/2

QINF = 297.9

MINF = 0,893

ALPT = 7.32

BETA = 0.05

H = 33522.

TINF = -59.6

RNPU = 2.2E+06

PSUR -- 520.1

MTOP = 0.90

Y,in. U/UTOP W/UTOP

0.240 0.2714 -0.0251

0.470 0.4902 0.2292

0.970 0.5124 0.1197

! .470 0.5299 -0.1571

1,960 0.6077 -0.0616

2.330 0.6779 -0.0805

2.990 0.8005 -0.2375

3.490 0.9120 -0.0956

3.990 0.9444 -0.1353

4.960 1.0000 -0.0983

Camber 0/2

QINF = 297.9

MINF -- 0.893

ALPT = 7.35

BETA= 0.31

H = 33522.

TINF = -59.2

RNPU = 2.2E+06

PSUR = 511.3

MTOP = 0.90

U/UTOP W/LrlrOP

0.2676 -0.0531

0.5203 0.3063

0.5141 0.1051

0.5139 -0,1289

0.5473 -0.0344

0.6243 -0.1189

0.7322 -0.2247

0.8765 -0.0612

0.9025 -0.1310

1.0000 -0.0972

Camber 0/2

QINF = 299.1

MINF = 0.895

ALPT = 7.58

BETA = 0.25

H = 33537.

TINF = -59.5

RNPU = 2.2E+06

PSUR -- 494.9

MTOP = 0.71

U/UTOP W/UTOP

0,2678 -0.0348

0.5925 0.3314

0.5351 0.1187

0.5378 -0.2231

0.5286 0.0305

0.5300 -0.0843

0.4123 0.3243

0.7345 0.0698

0.6764 -0.0480

1.0000 -0.0992

Camber 0/2

QINF = 324.0

MINF= 0.901

ALPT = 6.98

BETA = 0.05

H = 32125.

T1NF = -53.5

RNPU = 2.4E+06

PSUR = 550.2

MTOP = 0.86

U/UTOP W/UTOP

0.2255 -0.0374

0.5114 0.4416

0.4564 0.1461

0.4404 -0.1385

0.5111 -0.0122

0.5280 0.0153

0.6485 -0.1919

0.8218 -0.0729

0.9127 -0.1146

1.0000 -0.0729

Camber

QINF =

MINF =

ALPT =

BETA =

H--

TINF =

RNPU -

PSUR =

MTOP --

U/UTOP

0.2972

0.5012

0.5424

0.5573

0.6693

0.7856

0.9009

0.9782

0.9865

1.0000

5/2

299.9

0.896

6.45

0.05

33552.

-57.4

2.2E+06

530.0

0.90

W/UTOP

-0.0463

0.2900

0.1391

-0.1374

-0.0851

-0.1632

-0.2339

-0.1182

-0.1316

-0.0873

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:33:44.000 12:33:50.000 12:33:50,500 12:33:51.500 12:33:52.500

Camber 5/2

QINF = 299.9

MINF = 0.896

ALPT = 6.43

BETA -- -0.04

H = 33552.

TINF -- -57.4

RNPU = 2.2E+06

PSUR = 523.4

MTOP = 0.90

Y, in. U/UTOP W/LrrOP

0.240 0.2729 -0.0523

0.470 0.5119 0.4025

0.970 0.5029 0.1389

1.470 0.5060 -0.1220

1.960 0.5798 -0.0506

2.330 0.6849 -0.1668

2.990 0.7990 -0.2201

3.490 0.9156 -0.0831

3.990 0.9588 -0.0994

4.960 1.0000 -0.0878

Camber 5/2

QINF = 299.6

MINF = 0.897

ALPT = 5.83

BETA = -0.15

H = 33585.

TINF = -57.8

RNPU = 2.2E+06

PSUR = 542.0

MTOP = 0.87

U/UTOP W/UTOP

0.4418 -0.0652

0.5916 0.1882

0.6936 0.1358

0.7774 -0.1631

0.9286 -0.1712

0.9719 -0.1156

0.9960 -0.2364

1.0113 -0.1094

1.0020 -0.1244

1.0000 -0.0837

Camber 5/2

QINF = 299.6

MINF = 0.897

ALPT -- 5.83

BETA = -0.21

H = 33596.

TINF = -57.5

RNPU = 2.2E+06

PSUR = 539.9

MTOP = 0.87

U/UTOP W/UTOP

0.4686 -0.2029

0.6032 0.1402

0.7070 0.1328

0.7805 -0.1830

0.9369 -0.1674

0.9812 -0.1217

0.9956 -0.2338

1.0168 -0.1032

1.0058 -0.1249

1.0000 -0.0754

Camber 5/2

Q1NF = 300.2

MINF = 0.898

ALPT = 5.71

BETA = -0.04

H = 33598.

TINF -- -57.6

RNPU = 2.2E+06

PSUR = 541.0

MTOP = 0.87

U/UTOP W/UTOP

0.4726 0.3071

0.6249 0.1351

0.7173 0.1383

0.8207 -0.1466

0.9558 -0.1706

0.9880 -0.1194

1.0039 -0.2343

1.0198 -0,1114

1.0035 -0.1238

1.0000 -0.0779

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.4340

0.5850

0.6844

0.7664

0.9163

0.9693

0.9908

1.0054

1.0012

1.0000

5/2

300.6

0.899

5.83

-0.04

33611.

-57.7

2.2E+06

535.4

0.88

W/UTOP

-0.0321

0.2108

0.1367

-0.1645

-0.1644

-0.1337

-0.2312

-0.1043

-0.1210

-0.0752

820
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA. FLT 229

Time 12:33:53.000 12:33:58.000 12:34:06.000 12:34:07.000 12:34:07.500

Camber 5/2

QINF = 301.1

MINF = 0.899

ALPT = 5.79

BETA = -0.0 I

H = 33613.

TINF = -57.8

RNPU -- 2.2E+06

PSUR = 536.5

MTOP = 0.88

Y.in. U/LrroP W/UTOP

0.240 0.4340 -0.1826

0.470 0.5979 0.1416

0.970 0.6830 0.1379

1.470 0.7629 -0.1575

1.960 0.9121 -0.1575

2.330 0.9732 -0.1280

2.990 0.9909 -0.2297

3.490 1.0079 -0.1169

3.990 1.0006 -0.1243

4.960 1.0000 -0.0867

Camber 5/2

QINF = 302.1

MINF = 0.901

ALPT = 6.06

BETA = 0.02

H = 33628.

TINF = -57.7

RNPU = 2.2E+06

PSUR = 528.8

MTOP = 0.90

U/UTOP W/UTOP

0.2620 -0.0482

0.4906 0.3370

0.5149 0,1522

0.5197 -0.1302

0.6384 -0.0725

0.7345 -0.0790

0.8806 -0.2159

0.9736 -0.1052

0.9860 -0.1099

1.0000 -0.0813

Camber 5/2

QINF = 304.0

MINF = 0.904

ALPT = 6.38

BETA = -0.18

H = 33622.

TINF = -57.7

RNPU = 2.2E+06

PSUR = 511.3

MTOP = 0.83

U/UTOP W/UTOP

0.2202 -0.0278

0.5583 0.4866

0.4735 0.1586

0.4154 -0.2030

0.4434 0,0085

0.4287 -0.0251

0.5191 -0.2972

0.6971 0.0347

0.7589 -0.0774

1.0000 -0.0853

Camber 5/2

QINF = 304.0

MINF = 0.904

ALPT = 6.33

BETA = -0.07

H = 33622.

TINF = -58.1

RNPU = 2.3E+06

PSUR -- 510.2

MTOP = 0.86

U/UTOP W/UTOP

0.2392 -0.0335

0.5203 0.4226

0.4862 0.1613

0.4140 -0.2537

0.4450 0.0104

0.4310 0.0019

0.5301 -0.2735

0.7087 -0.0071

0.7769 -0.0838

1.0000 -0.0891

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.2210

0,4901

0.4585

0.4070

0.4460

0.4530

0.5578

0.7129

0.8103

1.0000

5/2

304.0

0.904

6.42

-0.36

33622.

-57.7

2.2E+06

513.5

0.88

W/UTOP

-0.0293

0.3125

0.1663

-0.1550

0.0083

-0.0112

-0.2245

-0.0097

-0.0967

-0,0760

FI 11/MAW BOUNDARY LAYER DATA. FLT 229

Time 12:34:12.500 12:34:13.500 12:34:22.000 12:34:22.500 12:34:23.000

Camber 5/2

QINF = 304.O

MINF = 0.904

ALPT = 6.33

BETA = -0.24

H = 33646.

TINF = -58.1

RNPU = 2.3E+06

PSUR = 510.2

MTOP = 0.84

Y, in. U/UTOP W/UTOP

0.240 0.2287 -0.0288

0.470 0.5018 0.3079

0.970 0.4717 0.1429

1.470 0.4339 -0.1621

1.960 0.4350 0.0106

2.330 0.4301 -0.0338

2.990 0.5306 -0.3317

3.490 0.6966 0.0057

3.990 0.7647 -0.0859

4.960 1.0000 -0.0932

Camber 5/2

QINF = 303.8

MINF= 0.904

ALPT = 6.32

BETA = 0.45

H = 33646.

TINF = -58.1

RNPU = 2.2E+06

PSUR = 513.5

MTOP = 0,88

U/UTOP W/UTOP

0.2182 -0.0333

0.4898 0.3280

0.4790 0.1572

0.4053 -0.1859

0.4534 0.0018

0.4609 -0.0042

0.5730 -0.2149

0.7397 -0.0720

0.8297 -0.0877

1.0000 -0.0888

Camber 5/2

QINF = 303.3

MINF = 0904

ALPT = 6.33

BETA = -0,62

H = 33667.

T1NF = -58.4

RNPU = 2.2E+06

PSUR = 510.1

MTOP = 0.92

U/UTOP W/UTOP

0.2696 -0.0338

0.5061 0.3728

0.5016 0.1486

0.4558 -0.1551

0.5158 -0.0242

0.6064 -0.1810

0.7202 -0.2074

0.8740 -0.0645

0.9096 -0.1112

1.0000 -0.0806

Camber 5/2

QINF= 303.3

MINF= 0.904

ALPT = 6.59

BETA = -0.47

H = 33656.

TINF = -58.3

RNPU = 2.2E+06

PSUR = 495.8

MTOP = 0.83

U/UTOP W/UTOP

0.3028 -0.0469

0.5341 0.3338

0.5329 0.1430

0.4716 -0.1761

0.4949 0.0128

0.5144 -02152

0.5819 -0.3286

0.7593 -0.0125

0.7443 -0.0700

1.0000 -0.0886

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.3132

0.6410

0.6227

0.5515

0.5130

05080

0.4457

0.7571

0.5680

1.0000

5/2

303.1

0,903

6.80

-0.38

33655.

-58.6

2.3E+06

492.5

0.66

W/UTOP

-0.0894

0.4209

0.1691

-0.2086

0.0440

-01964

0.1055

0.0548

-0.0379

-0.1101

821
TableK-2.Continued.

F111/MAW BOUNDARY LAYER DATA. FLT 229

Time 12:31:41.500 12:31:45.500 12:31:58.500 12:33:38.500 12:33:39.500

Camber 0/2

QINF = 301.7

MINF = 0.898

ALPT = 6.00

BETA = -0.04

H = 33500.

TINF = -59.2

RNPU = 2.3E+06

PSUR = 536.5

MTOP = 0.89

Y,in. u/15roP W/UTOP

0.240 0.5186 -0.3663

0.470 0.6399 0.0899

0.970 0.7646 0.1157

1.470 0.8747 -0.1777

1.960 0.9959 -0.1952

2,330 0.9893 -0.1473

2.990 0.9957 -0.2440

3,490 1.0082 -0.1319

3,990 0.9912 -0.1168

4.960 1.0000 -0.0852

Camber 0/2

QINF -- 301.2

MINF = 0.896

ALPT = 6.02

BETA = -0.27

H = 33464.

T1NF = -59.4

RNPU = 2.3E+06

PSUR = 541.0

MTOP = 0.87

U/LrroP W/UTOP

0.5298 -0.2810

0.6360 0.0938

0.7724 0.1118

0.8834 -0.1849

1.0092 -0.2028

0.9967 -0.1544

1.0060 -0.2419

1.0160 -0.1286

1.0055 -0. ! 443

1.0000 -0.1018

Camber 0/2

QINF = 300.3

MINF = 0.895

ALPT = 6.99

BETA = -0.12

H = 33473.

TINF = -59.2

RNPU = 2.3E+06

PSUR = 534.3

MTOP = 0.88

U/IYroP W/UTOP

0.4088 -0.2136

0.5800 0.1917

0.6641 0.1276

0.7560 -0.1641

0.8983 -0.1663

0.9709 -0.1481

0.9980 -0.2360

1.0258 -0.1110

1.0050 -0.1665

1.0000 -0.0915

Camber 5/2

QINF = 299.0

M1NF = 0.895

ALPT = 6.06

BETA = -0.10

H = 33572.

T1NF = -57.6

RNPU = 2.2E+06

PSUR = 535.4

MTOP = 0.88

U/UTOP W/UTOP

0.4027 -0.3261

0.5797 0.1491

0.6568 0.1339

0.7318 -0.1485

0.8720 -0.1525

0.9531 -0.1295

0.9907 -0.2295

1.0100 42.1127

0.9894 -0.1413

1.0000 -0.0884

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.4100

0.5697

0.6734

0.7537

0.8955

0.9571

0.9876

1.0126

1.0170

1.0000

5/2

299.2

0.896

5.98

-0.21

33572.

-57.7

2.2E+06

535.4

0.89

W/UTOP

-0.0498

0.2041

0.1371

-0.1547

-0.1619

-0.1325

-0.2417

-0.1136

-0.1162

-0.0881

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:33:49,500 12:34:02,000 12:34:15.500 12:34:23,500 12:31:46.000

Camber 5/2

QINF = 299.4

MINF = 0.896

ALPT = 6.00

BETA = -0.01

H = 33584.

TINF = -57.8

RNPU = 2.2E+06

PSUR = 542.0

MTOP = 0.87

Y, in. U/UTOP W/UTOP

0.240 0.3829 -0.1062

0.470 0.5496 0.2203

0.970 0.6354 0.1396

1.470 0.7226 -0.1425

1.960 0.8692 -0.1498

2,330 0.9435 -0.1162

2.990 0.9900 -0.2269

3.490 1.0098 -0.1092

3.990 1.0008 -0.1262

4.960 1.0000 -0.0831

Camber 5/2

QINF = 303.6

MINF = 0.903

ALPT = 6.02

BETA= 0.14

H = 33632.

TINF = -58.0

RNPU = 2.2E+06

PSUR = 522.2

MTOP = 0.92

U/UTOP W/UTOP

0.2477 -0.0382

0.4914 0.3096

0.5034 0.1498

0.4824 -0.1181

0.5756 -0.0494

0.6737 -0.1027

0.8128 -0.2085

0.9360 -0.0967

0.9808 -0.1184

1.0000 -0.0810

Camber 5/2

QINF = 303.5

MINF = 0.904

ALPT = 6.00

BETA -- -0.10

H = 33656.

TINF = -58.4

RNPU = 2.2E+06

PSUR = 525.5

MTOP = 0.91

U/UTOP W/UTOP

0.2610 -0.0461

0.4923 0.3417

0.5086 0.1503

0.5087 -0.1142

0.6147 -0.0553

0.7064 -0.0751

0.8520 -0.2225

0.9778 -0.0939

0.9875 -0.1241

1.0000 -0.0766

Camber 5/2

QINF = 302.9

MINF = 0.903

ALPT = 6.92

BETA = -0.44

H = 33643.

TINF = -58.2

RNPU = 2.2E+06

PSUR = 483.7

MTOP = 0.53

U/UTOP W/UTOP

0.4174 -0.0800

0.8184 0.4935

0.7722 0.2213

0.7178 -0.2943

0.6615 0.0557

0.5886 -0.1000

0.4934 -0.0122

0.8123 0.0889

0.4757 0.0302

1.0000 -0.1053

Camber

QINF =

MINF =

ALPT=

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.5708

0.6633

0.7833

0.8955

1.0067

0.9996

1.0049

1.0183

1.0099

1.0000

0/2

300.7

0.896

5.93

-0.10

33463.

-59.3

2.3E+06

535.4

0.88

W/UTOP

-0.5681

0.0725

0.1210

-0.1962

-0.2059

-0.1553

-0.2504

-0.1318

-0.1400

-0.1002

822
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:31:54.000 12:31:57,000 12:33:57.000 12:33:59.000 12:34:01.000

Camber 0/2

QINF = 300.8

MINF = 0,895

ALPT = 5.97

BETA = 0.11

H = 33451.

TINF = -59.3

RNPU = 2.3E+06

PSUR = 531.0

MTOP = 0.88

Y, in. U/UTOP W/UTOP

0.240 0.4385 0.3076

0.470 0.6586 0.0784

0.970 0.7670 0.1200

1,470 0.8828 -0.1821

1.960 1.0058 -0.1974

2.330 1.0037 -0.1519

2.990 1.0066 -0.2455

3.490 1.0277 -0.1222

3.990 1.0069 -0.1373

4.960 1.0000 -0.0913

Camber 0/2

QINF = 300.5

MINF = 0.896

ALPT = 6.02

BETA -- -0.65

H = 33473.

TINF = -59.3

RNPU = 2.3E+06

PSUR = 533.2

MTOP = 0.87

U/UTOP

0.5555

0.6768

0.7974

0.9029

1.0278

1.0049

1.0100

1.0293

1.0116

1.0000

W/UTOP

-0.3364

0.0825

0.1191

-0.1839

-0.2086

-0.1346

-0.2384

-0.0901

-0.1373

-0.0894

Camber 5/2

QINF = 3O2.1

MINF = 0,901

ALPT = 6.08

BETA = -0.07

H = 33628.

TINF = -57.7

RNPU = 2.2E+06

PSUR = 526.6

MTOP = 0.91

U/UTOP W/UTOP

0.2971 -0.0624

0.5138 0.2953

0.5639 0.1396

0.5690 -0.1111

0.6862 -0.0873

0.7987 -0.0947

0.9224 -0.2296

0,9886 -0.1159

0.9922 -0.1273

1.0000 -0.0843

Camber 5/2

QINF= 302.3

MINF = 0,902

ALPT = 5.97

BETA = -0.27

H = 33628.

TINF= -58.1

RNPU = 2.2E+06

PSUR = 533.3

MTOP = 0.90

U/UTOP W/UTOP

0.2633 -0.0597

0.4935 0.2945

0.5520 0.1520

0.5655 -0.1105

0.6921 -0.0919

0.8141 -0.0973

0.9333 -0.2256

0.9947 -0.1348

0.9946 -0.1214

1.0000 -0.0809

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.2819

0.5123

0.5476

0.5445

0.6557

0.7745

0.9050

0.9870

0.9946

1.00013

5/2

303.1

0.903

5.97

-0.10

33631.

-57.6

2.2E+06

527.7

0,90

W/UTOP

-0.0489

0.3450

0.1488

-0.1238

-0.0765

-0.1257

-0.2225

-0.1130

-0.1226

-0.0843

FI I I/MAW BOUNDARY LAYER DATA, FLT 229

Time 12:34:01.500 11:42:02.500 11:42:03.000 11:42:03.500 11:42:04.000

Camber 5/2

QINF = 303.4

MINF = 0,903

ALPT = 6.02

BETA = 0.08

H = 33632.

TINF= -58.0

RNPU = 2.2E+06

PSUR = 524.4

MTOP = 0.91

Y,in. U/UTOP W/UTOP

0,240 0.2819 -0.0421

0,470 0.4859 0.2708

0,970 0.5256 0.1549

1,470 0.5250 -0.1295

1.960 0.6415 -0.0711

2.330 0.7368 -0.1004

2.990 0.8760 -0.2166

3,490 0.9741 -0.1444

3.990 0.9896 -0.1247

4,960 1.0000 -0.0846

Camber 0/2

QINF = 301.6

MINF = 0.951

ALPT = 6.50

BETA = 0.22

H = 35906.

TINF = -67.1

RNPU = 2.2E+06

PSUR = 392.2

MTOP = 1.11

U/UTOP W/UTOP

0,2136 -0,04-40

0.4413 0.2084

0.4623 0.0068

0.4958 -0.0906

0.5953 -0.0354

0.7133 -0.0221

0.8518 -0.1869

0.9560 -0.0937

0.9925 -0.1377

1.0000 -0.0686

Camber 0/2

QINF= 301.4

MINF = 0.950

ALPT = 6.47

BETA = 0.34

H = 35905.

T1NF -- -67.4

RNPU = 2.2E+06

PSUR = 395.5

MTOP = 1.10

U/UTOP W/UTOP

0.1621 -0,0163

0.4217 0,2345

0.4042 0.0135

0.4628 -0,0861

0.5554 -0,0312

0.6758 -0.0186

0.8221 -0.1995

0.9415 -0.0908

0.9876 -0.1294

1.0000 -0.0612

Camber 0/2

QINF= 301,4

MINF = 0.950

ALPT = 6.36

BETA = O.37

H = 35905.

TINF = -67.1

RNPU = 2.2E+06

PSUR = 391.0

MTOP = 1.11

U/UTOP W/UTOP

0.2308 -0.0374

0.4562 0.3079

0.4466 0.1139

0.4777 -0.1025

0.5740 -0.0243

0.6870 -0.0161

0.8319 -0.1727

0.9444 -0.1003

0.9795 -0.1356

1.000(3 -0.0654

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.2233

0.4621

0.4929

0.5085

0.6062

0.7001

0.8390

0.9478

0.9904

1.0000

0/2

301.4

0,950

6.14

0.25

35905.

-67.4

2.2E+06

397.6

1.09

W/UTOP

-0.0295

0.2284

0.0637

-0.0916

-0.0475

-0.0104

-0.1890

-0.0839

-0.1325

-0.0677

823
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:42:04.500 11:42:05.000 11:42:05,500 11:42:06.500 11:42:07.000

Camber 0/2

QINF = 301,4

MINF = 0.950

ALPT = 6.10

BETA = 0.34

H = 35905.

TINF = -67.1

RNPU -- 2.2E+06

PSUR = 400.9

MTOP = 1.09

Y, in. U/UTOP W/UTOP

0.240 0.2048 -0.0147

0.470 0.4308 0.2730

0.970 0.4256 0.0870

1,470 0.4493 -0.1012

1.960 0.5320 -0.0247

2.330 0.6541 -0.0225

2,990 0.8079 -0.1801

3,490 0.9286 -0.0890

3.990 0.9641 -0.1494

4.960 1.0000 -0.0662

Camber 0/2

QINF = 301.4

MINF = 0,950

ALPT = 6.00

BETA = 0.22

H = 35917.

TINF = -67.4

RNPU = 2.2E+06

PSUR = 398.8

MTOP = 1.09

U/UTOP W/UTOP

0.2050 -0.0273

0.4487 0.3113

0.4149 0.0734

0.4366 -0.0998

0.5315 -0.0110

0,6391 -0.0204

0.7994 -0.1809

0.9395 -0.0796

0.9873 -0.1408

1.0000 -0.0630

Camber 0/2

QINF = 301.4

MINF = 0,950

ALPT = 5.98

BETA = 0.25

H -- 35917.

TINF = -67.1

RNPU = 2.2E+06

PSUR = 397.6

MTOP = 1.09

U/UTOP W/UTOP

0.2282 -0.0393

0.4409 0.2210

0.4077 0.1301

0.4292 -0.1452

0.5138 -0.0192

0.6390 -0.0214

0.8014 -0.1762

0.9399 -0.0836

0.9895 -0.1354

1.0000 -0.0649

Camber 0/2

QINF = 301.4

MINF = 0.950

ALPT = 6.10

BETA -- 0.22

H = 35917.

TINF = -67.1

RNPU -- 2.2E+06

PSUR = 398.8

MTOP = 1.10

U/UTOP W/UTOP

0.2311 -0.0398

0.4466 0.2701

0.4337 0.1083

0.4786 -0.1032

0.5708 -0.0249

0.6696 0.0063

0.8286 -0.1689

0.9397 -0.0884

0.9830 -0.1336

1.0000 -0.0622

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.2198

0.4452

0.4431

0.4815

0.5625

0.6669

0.8212

0.9437

0.9846

1.0000

0/2

301.4

0,950

6.07

0.28

35917.

-67.1

2.2E+06

399.8

1.10

W/UTOP

-0.0461

0.2248

0.0904

-0. i 076

-0.0254

-0.0098

-0.1871

-0.0772

-0.1328

-0.0671

FI 1 I/MAW BOUNDARY LAYER DATA, FIT 229

Time 11:42:15.500 11:42:16.500 11:42:28.000 11:42:28.500 11:42:29.000

Camber 0/2

QINF -- 300.4

MINF = 0.949

ALPT = 6.06

BETA = 0.22

H = 35911.

T1NF = -66.9

RNPU --- 2.2E+06

PSUR = 404.2

MTOP = 1.08

Y,in. U/UTOP W/UTOP

0,240 0.1516 -0.0168

0.470 0.4300 0.2692

0,970 0.3842 0.1217

1,470 0.3883 -0.1162

1.960 0.4449 -0.0002

2.330 0.5298 0.0112

2.990 0.6857 -0.1511

3,490 0.8713 -0.0502

3,990 0.9586 -0.1221

4,960 1.0000 -0.0509

Camber 0/2

QINF = 300.4

MINF = 0,949

ALPT = 6.10

BETA= 0.31

H = 35911.

TINF = -67.2

RNPU = 2.2E+06

PSUR = 400.9

MTOP = 1.08

U/UTOP W/UTOP

0.2046 -0.0208

0.4239 0.2531

0.3994 0.1265

0.3929 -0.1243

0.4646 0.0025

0.5406 0.0097

0.6940 -0.1669

0.8755 -0.0616

0.9558 -0.1304

1.0000 -0.0604

Camber 0/2

QINF = 301.0

MINF = 0.950

ALPT = 6.38

BETA = -0.15

H = 35915.

TINF = -67.3

RNPU -- 2.2E+06

PSUR = 400.9

MTOP = 1.09

U/UTOP W/UTOP

0.1483 -0.0187

0.4224 0.2416

0.3903 0.0845

0.4242 -0.0944

0.4507 0.0478

0.5544 -0.0004

0.7075 -0.1588

0.8789 -0.0991

0.9625 -0.1486

1.0000 -0.0615

Camber 0/2

QINF -- 301.0

MINF = 0,950

ALPT = 6.44

BETA = -0.12

H = 35915.

TINF = -67.0

RNPU = 2.2E+06

PSUR = 395.5

MTOP = 1.10

U/UTOP W/UTOP

0.2066 -0.0177

0.4413 0.2524

0.4377 0.0084

0.4369 -0.1334

0.4908 -0.0082

0.5716 -0.0013

0.7168 -0.1714

0.8751 -0.0643

0.9568 -0.1214

1.0000 -0.0564

Camber

QINF =

MINF --

ALPT --

BETA=

H=

TINF =

RNPU =

PSUR --

MTOP =

U/UTOP

0.2160

0.4459

0.4113

0.4393

0.4889

0.5648

0_7118

0.8772

0.9510

1.0000

0/2

301.0

0.950

6.61

-0.07

35915.

-67.0

2.2E+06

394.4

1.10

W/UTOP

-0.0218

0.2551

-0.0213

-0.1246

-0.0002

0.0001

-0.1640

-0.0564

-0.1266

-0.0558

824
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 11:42:29.500 11:42:31.000 11:42:31.500 l 1:42:32.000 11:42:32.500

Camber 0/2

QINF= 300.8

MINF = 0.949

ALPT = 6.56

BETA = -0.01

H = 35913.

T1NF = -67.0

RNPU = 2.2E+06

PSUR = 394.4

MTOP = 1.10

Y, in. U/UTOP W/UTOP

0,240 0.1683 -0.0142

0.470 0.4280 0.2365

0.970 0.3953 -0.0383

1.470 0.3945 -0.1341

1.960 0.4380 0.0042

2.330 0.5208 -0.0018

2,990 0.6665 -0.1533

3.490 0.8522 -0.0518

3.990 0.9414 -0.1235

4.960 1.0000 -0.0534

Camber 0/2

QINF= 300.6

MINF = 0.949

ALPT = 6,86

BETA = 0.05

H = 35901.

T1NF = -66.9

RNPU = 2.2E+06

PSUR = 386.7

MTOP = 1.11

U/UTOP W/LrrOP

0.2110 -0.0093

0.4364 0.2739

0.6037 0.2366

0.4177 -0.1311

0.4652 0.0086

0.5252 0.0133

0.6601 -0.1434

0.8372 -0.0394

0.9201 -0.1108

1.0000 -0.0552

Camber 0/2

QINF = 3OO.6

MINF = 0.949

ALPT = 6.95

BETA = 0.05

H = 35912.

TINF = -66.9

RNPU = 2.2E+06

PSUR = 387.8

MTOP = 1.11

U/UTOP W/UTOP

0.1763 -0.0326

0.4309 0.2704

0.3524 0.1687

0.3975 -0.1236

0.4334 0.0162

0.5021 0.0128

0.6497 -0.1541

0.8423 -0.0339

0.9322 -0.1205

1.0000 -0.0536

Camber 0/2

QINF = 3OO.6

MINF = 0.949

ALPT -- 7.08

BETA = 0.05

H = 35912.

TINF = -66.3

RNPU = 2.2E+06

PSUR = 384.6

MTOP = 1.11

U/UTOP W/UTOP

0.2601 -0.0242

0.4548 0.1970

0.3855 0.2214

0.4230 -0,1456

0.4810 0.0076

0.5316 0.0051

0.6736 -0.1456

0.8411 -0.0441

0.9319 -0.1220

1.0000 -0.0481

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.2047

0.4387

0.2860

0.4074

0.4419

0.5024

0.6312

0.8046

0.9119

1.0000

0/2

300.6

0.949

7.16

0.02

35912.

-66.9

2.2E+06

382.3

1.11

W/UTOP

-0.0115

0.2170

0.0957

-0.1254

0.0179

0.0067

-0.1422

-0.0336

-0.1182

-0.0571

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:04:24.500 14:04:25.000 14:04:26.000 14:04:27.000 14:04:36.500

Camber 0/2

QINF = 449.5

MINF = 0.802

ALPT = 3.95

BETA = 0.34

H = 19366.

T1NF = 2.7

RNPU = 3.1E+06

PSUR = 982.5

MTOP = 0.82

Y, in. U/UTOP W/UTOP

0.240 0.6248 -0.1802

0.470 0.7459 -0.0669

0,970 0.8967 0.1034

1.470 0.9782 -0.1523

1,960 1.0076 -0.1943

2,330 0.9814 -0.1264

2.990 0.9847 -0.1986

3.490 0.9947 -0.1233

3.990 0.9984 -0.1236

4.960 1.0000 -0.0765

Camber 0/2

QINF = 449.5

MINF = 0.802

ALPT = 4.01

BETA = 0.22

H = 19377.

TINF= 3.0

RNPU = 3.1E+06

PSUR = 982.5

MTOP = 0.82

U/UTOP W/UTOP

0.6235 -0.1798

0.7467 -0.0625

0.8909 0.1026

0.9748 -0.1521

1.0076 -0.1961

0.9794 -0.1262

0.9831 -0.2024

0.9913 -0.1242

0.9976 -0.1170

1.0000 -0.0776

Camber 0/2

QINF = 449.8

MINF = 0.802

ALPT = 4.04

BETA -- 0.25

H = 19378.

TINF= 2.7

RNPU = 3.1E+06

PSUR = 983.5

MTOP = 0.82

U/UTOP W/UTOP

0.6214 -0.1779

0.7483 -0.0612

0.8940 0.1014

0.9758 -0.1510

1.0043 -0.1899

0.9807 -0.1257

0.9821 -0.1961

0.9920 -0.11 64

0.9975 -0.1183

1.0000 -0.0806

Camber 0/2

QINF = 450.0

MINF = 0.803

ALPT = 4.01

BETA = 0.28

H = 19378.

TINF = 2.6

RNPU = 3.1E+06

PSUR = 980.3

MTOP = 0.82

U/UTOP W/UTOP

0.6249 -0.1802

0.7493 -0,0613

0.8935 0.1024

0.9722 -0.1556

1.0051 -0.1945

0.9792 -0.1277

0.9814 -0.1972

0.9919 -0.1195

0.9925 -0.1213

1.0000 -0.0778

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP --

U/UTOP

0.6200

0.7429

0.8925

0.9742

1.0052

0.9806

0.9831

0.9937

0.9862

1.0000

0/2

452.1

0.804

4.04

0.37

19347.

2.8

3. l E+06

982.5

0.82

W/'UTOP

-0.1860

-0.0695

0.1009

-0.1529

-0.1968

-0.1296

-0.2003

-0.1495

-0.1341

-0.0808

825
TableK-2.Continued.

F111/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:04:38,000 14:04:38.500 14:04:46.500 14:05:12,000 14:05:12.500

Camber 0/2

QINF = 451.8

MINF = 0.804

ALPT = 3.95

BETA = 0,31

H = 19358.

TINF= 2.8

RNPU = 3.1E+06

PSUR = 981.4

MTOP = 0.82

Y, in. U/UTOP W/UTOP

0,240 0.6244 43.1926

0,470 0.7485 43.0612

0,970 0.8942 0.1071

1.470 0.9759 43.1537

1,960 1.0061 43.1933

2,330 0.9808 43.1303

2,990 0.9831 43.1999

3,490 0.9908 43.1250

3,990 0.9966 -0.1290

4.960 1.0000 -0.0788

Camber 0/2

QINF = 452.0

MINF = 0,804

ALPT = 4.01

BETA = 0.34

H = 19358.

TINF = 2.8

RNPU = 3.1E+06

PSUR = 985.8

MTOP = 0.82

U/UTOP W/UTOP

0.6212 -0.1786

0.7453 -0.0609

0.8955 0.1015

0.9745 -0.1556

1.0060 -0.1932

0.9805 -0.1287

0.9834 -0.1971

0.9947 -0.1194

0.9944 -0.1027

1.0000 -0.0788

Camber 0/2

QINF = 451.7

MINF = 0.804

ALPT = 4.01

BETA = 0.31

H = 19369.

TINF = 2.1

RNPU = 3.1E+06

PSUR = 980.3

MTOP = 0.82

U/UTOP W/UTOP

0.6234 -0.1870

0.7447 -0.0567

0.8944 0.1025

0.9781 -0.1519

1.0071 -0.1930

0.9816 -0.1257

0.9837 -0.1960

0.9892 43.1275

0.9968 -0.1183

1.0000 -0.0773

Camber 0/2

QINF = 454.2

MINF = 0,805

ALPT = 4.94

BETA = 0.02

H = 19282.

TINF = 2.7

RNPU = 3.1E+06

PSUR = 982.4

MTOP = 0.83

U/UTOP W/UTOP

0.6135 -0.1990

0.7331 -0.0590

0.8776 0.0879

0.9690 -0.1633

1.0053 -0.1989

0.9769 -0.1373

0.9834 -0.2039

0.9870 -0.1325

0.9949 -0.1220

1.0000 -0.0797

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5992

0.7246

0.8698

0.9603

0.9983

0.9695

0.9757

0.9841

0.9879

1.0000

0/2

454.7

0,805

5.07

0.25

19283.

2.6

3.1E+06

983.5

0.83

W/UTOP

43.1725

43.0699

0.0835

-0.1640

-0.2009

-0.1403

-0.2075

-0.1388

-0.1302

-0.0823

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:05:13,000 14:05:16,000 14:05:16,500 14:05:18,000 14:05:21,000

Camber 0/2

QINF -- 454.7

MINF = 0.805

ALPT = 5.14

BETA = 0. I 1

H = 19283.

T1NF = 2.6

RNPU = 3.1E+06

PSUR = 983.5

MTOP = 0.83

Y,in. U/UTOP W/UTOP

0,240 0.6114 -0.1892

0.470 0.7267 -0.0708

0,970 0.8749 0.0809

1.470 0.9667 -0.1659

1,960 1.0070 43.2000

2,330 0.9790 -0.1406

2,990 0.9827 -0,2081

3,490 0.9905 -0.1397

3.990 0.9915 -0.1371

4,960 1.0000 -0.0850

Camber 0/2

QINF = 457.0

MINF = 0.807

ALPT = 6.04

BETA = 0.05

H = 19274,

TINF = 2.7

RNPU = 3. IE+06

PSUR = 981.3

MTOP = 0.83

U/UTOP W/UTOP

0.5971 -0.1838

0.7148 -0.0711

0.8549 0.0676

0.9512 -0.1784

0.9985 -0.2064

0.9729 43.1518

0.9770 -0.2136

0.9848 -0.1546

0.9883 -0.1456

1.0000 -0.0915

Camber 0/2

QINF = 457.3

MINF = 0,807

ALPT = 6.09

BETA = 0.05

H = 19275.

TINF = 2.7

RNPU -- 3.2E+06

PSUR = 981.3

MTOP = 0.83

U/UTOP W/UTOP

0.6092 -0.1992

0.7257 -0.0761

0.8569 0.0647

0.9541 -0.1788

1.0047 -0.2090

0.9804 -0.1560

0.9836 -0.2159

0,9928 -0.1647

0.9973 -0.1466

1.0000 -0.0960

Camber 0/2

QINF = 456.4

MINF = 0.807

ALPT = 6.20

BETA = -0.07

H = 19285.

TINF = 2.4

RNPU = 3.1E+06

PSUR -- 977.0

MTOP = 0.83

U/UTOP W/UTOP

0.6193 -0.2168

0.7317 -0.0628

0.8583 0.0639

0.9567 -0.1815

1.0070 -0.2034

0.9829 43.1558

0.9852 -0.2167

0.9914 -0.1590

0.9987 43.1479

1.0000 -0.0980

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.6345

0.7435

0.8514

0,9321

0.9932

0.9832

0.9897

0.9967

1.0029

1.0000

0/2

455.0

0,805

6.96

0.37

19272.

2.3

3.1E+06

978.0

0.82

W/UTOP

-0.2165

-0.0895

0.0504

-0.2006

-0.2132

-0.1691

-0.2342

-0.1762

-0.1603

-0.1089

826
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:05:21.500 14:05:22.000 14:05:22.500 14:05:23.000 14:05:26.500

Camber 0/2

QINF = 455.0

MINF = 0.805

ALPT = 7.02

BETA = 0.37

H = 19272.

TINF = 2.3

RNPU = 3.1E+06

PSUR = 979.1

MTOP = 0.82

Y, in. U/UTOP W/UTOP

0.240 0.6351 -0.2089

0.470 0.7431 -0.0976

0.970 0.8544 0.0457

1.470 0.9372 -0.1963

1.960 0.9920 -0.2051

2.330 0.9832 -0.1716

2.990 0.9882 -0.2306

3.490 0.995 l -0.1779

3.990 1.0026 -0.1598

4.960 1.0000 -0.1105

Camber 0/2

QINF = 455.1

MINF = 0.805

ALPT = 7.08

BETA = 0.34

H = 19261.

TINF = 2.3

RNPU = 3.1E+06

PSUR = 983.5

MTOP = 0.81

U/UTOP W/UTOP

0.6416 -0.1985

0.7479 -0.0935

O.8605 O.0472

0.9393 -0.1960

0.9953 -0.2136

0.9855 -0.1750

0.9913 -0.2299

0.9956 -0.1732

1.0018 -0.1649

1.0000 -0.1108

Camber 0/2

QINF = 454.8

MINF = 0.805

ALPT = 7.01

BETA = 0.17

H = 19249.

TINF = 2.0

RNPU = 3.1E+06

PSUR = 979.1

MTOP = 0.81

U/UTOP W/UTOP

0.6394 -0.2316

0.7481 -0.0915

0.8581 0.0485

0.9306 -0.2041

0.9872 -0.2181

0.9851 -0.1666

0.9925 -0.2377

0.9980 -0.1803

1.0003 -0.1702

1.0000 -0.1124

Camber 0/2

QINF = 454.5

MINF = 0.804

ALPT = 7.01

BETA = 0.25

H = 19249.

TINF = 2.0

RNPU = 3.1E+06

PSUR = 978.0

MTOP = 0.82

U/UTOP W/UTOP

0.6376 -0.1978

0.7424 -0.0941

0.8496 0.0477

0.9323 -0.2040

0.9880 -0.2189

0.9795 -0.1 646

0.9872 -0.2368

0.9918 -0.1708

0.9963 -0.1650

1.0000 -0.1055

Camber

QINF =

M1NF=

ALPT =

BETA --

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6693

0.7692

0.8504

0.9125

0.9623

0.9705

0.9926

0.9961

1.0039

1.0000

0/2

459.8

0.808

7.93

0.28

19177.

2.6

3.2E÷06

985.6

0.80

W/UTOP

-0.2130

-0.O893

0.0365

-0.2008

-0.2124

-0.1767

-0.2372

-0.1673

-0.1726

-0.1182

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:05:27.000 14:05:27.500 14:05:28.000 14:05:28.500 14:05:36.500

Camber 0/2

QINF = 460.1

MINF = 0.808

ALPT = 8.02

BETA = 0.22

H = 19166.

TI NF = 2.6

RNPU = 3.2E+06

PSUR = 988.9

MTOP = 0.79

Y,in. U/UTOP W/UTOP

0.240 0.6744 -0.2021

0.470 0.7736 -0.0956

0.970 0.8540 0.0316

1.470 0.9188 -0.2030

1.960 0.9642 -0.2100

2.330 0.9708 -0.1721

2.990 0.9966 -0.2417

3.490 1.0057 -0.1921

3.990 1.0073 -0.1 642

4.960 1.0000 -0.1191

Camber 0/2

QINF = 460.4

MINF = 0.808

ALPT = 7.97

BETA = 0.25

H = 19155.

TINF = 2.2

RNPU = 3.2E+06

PSUR = 988.9

MTOP = 0.80

U/UTOP W/UTOP

0.6682 -0.2139

0.7706 -0.0998

0_8505 0.0305

0.9136 -0.2038

0.9569 -0.2071

0.9639 -0.1776

0.9915 -0.2393

0.9983 -0.1904

0.9971 -0.1786

1.0000 -0.1167

Camber 0/2

QINF = 460.7

MINF -- 0.808

ALPT = 8.01

BETA = 0.25

H= 19144.

TINF = 2.2

RNPU = 3.2E+06

PSUR = 984.5

MTOP = 0.80

U/UTOP W/UTOP

0.6668 -0.2123

0.7764 -0.1053

0.8553 0.0352

0.9184 -0.2095

0.9546 -0.2007

0.9659 -0.1641

0.9907 -0.2434

1.0064 -0.1748

1.0033 -0.1678

1.0000 -0.1186

Camber 0/2

QINF = 461.3

MINF = 0.808

ALPT = 8.02

BETA = 0.34

H = 19122.

TINF = 2.5

RNPU = 3.2E+06

PSUR = 988.9

MTOP = 0.80

U/UTOP W/UTOP

0.6710 -0.2075

0.7712 -0.0869

0.8481 0.0334

0.9097 -0.1999

0.9542 -0.2098

0.9656 -0.1748

0.9929 -0.2406

1.0017 -0.1889

1.0078 -0.1715

1,0000 -0.1179

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6738

0.7617

0.8185

0.8708

0.9117

0.9225

0.9583

0.9877

1.0063

1.0000

0/2

472.3

0.813

8.52

0.19

18833.

3.9

3.2E+06

1007.4

0.80

W/UTOP

-0.2043

-0.1026

0.0267

-0.1924

-0.1962

-0.1729

-0.2339

-0.1866

-0.1692

-0A 160

827
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:05:37.000 14:05:37.500 14:05:38.000 14:05:38.500 14:05:39.000

Camber 0/2

QINF = 472.6

MINF= 0.813

ALPT = 8.52

BETA = 0.17

H = 18822.

TINF = 3.9

RNPU = 3.2E+06

PSUR = 1006.3

MTOP = 0.80

Y,in. U/UTOP W/UTOP

0.240 0.6696 -0.1987

0.470 0.7599 -0.0928

0.970 0.8247 0.0279

1.470 0.8780 -0.1912

1.960 0.9157 -0.1920

2.330 0.9217 -0.1755

2.990 0.9576 -0.2370

3.490 0.9883 -0.1940

3.990 1.0096 -0.1716

4.960 1.13000 -0.1149

Camber 0/2

QINF = 472.6

MINF = 0.813

ALPT = 8.48

BETA = 0.08

H= 18811.

TINF = 4.3

RNPU = 3.2E+06

PSUR -- 1005.2

MTOP = 0.80

U/UTOP W/UTOP

0.6842 -0.1918

0.7637 -0.0941

0.8213 0.0280

0.8795 -0.1929

0.9218 -0.1918

0.9256 -0.1714

0.9586 -0.2312

0.9842 -0.1778

1.0054 -0.1720

1.0000 -0.1175

Camber 0/2

QINF = 472.6

M1NF = 0.813

ALPT = 8.63

BETA -- 0.14

H= 18811.

TINF = 3.9

RNPU = 3.2E+06

PSUR = 1005.2

MTOP --- 0.80

U/UTOP W/UTOP

0.6714 -0.2107

0.7621 -0.0876

0.8196 0.0246

0.8710 -0.1942

0.9118 -0.1939

0.9199 -0.1689

0.9556 -0.2309

0.9825 -0.1607

1.0048 -0.1732

1.0000 -0.1160

Camber 0/2

QINF -- 472.6

MINF = 0.813

ALPT = 8.75

BETA = 0.22

H = 18800.

TINF = 4.0

RNPU = 3.2E+06

PSUR = 1008.5

MTOP = 0.80

U/UTOP W/UTOP

0.6629 -0.2122

0.7474 -0.0872

0.8021 0.0219

0.8561 -0.1867

0.8993 -0.1878

0.9094 -0.1673

0.9435 -0.2246

0.9769 -0.1798

1.0000 -0.1744

1.0000 -0.1227

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6586

0.7426

0.7921

0.8535

0.8934

0.8998

0.9342

0.9688

0.9934

1.0000

0/2

472.1

0.812

8.75

0.28

t 8799.

4.0

3.2E+06

1008.5

0.81

W/UTOP

-0.2108

-0.0882

0.0221

-0.1919

-0.1871

-0.1679

-0.2294

-0.1919

-0.1727

-0.1164

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:05:39.500 14:05:40.000 14:05:43.000 14:05:46.000 14:07:12.500

Camber 0/2

QINF = 471.8

MINF-- 0.812

ALPT = 8.93

BETA = 0.37

H -- 18799.

T1NF : 4.4

RNPU : 3.2E+06

PSUR = 1008.5

MTOP : 0.81

Y, in. U/UTOP W/UTOP

0.240 0.6413 -0.1939

0.470 0.7267 -0.0801

0.970 0.7761 0.0192

1.470 0.8364 -0.1924

1.960 0.8716 -0.1821

2.330 0.8855 -0.1699

2.990 0.9256 -0.2237

3.490 0.9643 -0.2017

3.990 0.9855 -0.1763

4.960 1.0000 -0.1190

Camber 0/2

QINF = 471.2

MINF = 0.811

ALPT = 9.14

BETA = 0.25

H = 18798.

TINF = 4.1

RNPU = 3.2E+06

PSUR = 1007.4

MTOP = 0.80

U/UTOP W/UTOP

0.6488 -0.1956

0.7315 -0.0814

0.7834 0.0162

0.8350 -0.1915

0.8705 -0.1803

0.8798 -0.1613

0.9177 -0.2251

0.9546 -0.1811

0.9783 -0.1671

1.0000 -0.1168

Camber 0/2

QINF = 462.4

MINF = 0.804

ALPT = 9.97

BETA = 0.I 1

H = 18810.

TINF = 4.4

RNPU = 3.2E+06

PSUR = 988.6

MTOP = 0.59

U/UTOP W/UTOP

0.4206 -0.3083

0.6506 0.3405

0.6776 -0.2548

0.6607 -0.0962

0.7293 -0.0419

0.7519 -0.0838

0.7820 -0.1285

0.8799 -0.0149

0.8851 -0.0954

1.0000 -0.0978

Camber 0/2

Q1NF = 454.6

MINF = 0.797

ALPT = 9.97

BETA = 0.05

H = 18790.

TINF = 4.4

RNPU = 3.2E+06

PSUR = 989.7

MTOP = 0.53

U/UTOP W/UTOP

0.3523 0.0088

0.7166 0.3182

0.7511 -0.2292

0.7575 -0.1070

0.8048 -0.0230

0.8043 -0.0260

0.8214 -0.2009

0.9138 -0.0221

0.8958 -0.1004

1.0000 -0.0880

Camber

QINF=

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6171

0.7368

0.8876

0.9702

1.0057

0.9801

0.9824

0.9904

0.9980

1.0000

5/2

451.2

0.801

4.18

0.28

19245.

2.8

3.1E+06

987.9

0.82

W/UTOP

-0.1814

-0.0543

0.0921

-0.1525

-0.1977

-0.1290

-0.1975

-0.1244

-0.1194

-0.0782

828
TableK-2.Continued.

F11 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:07:14,000 14:07:19.500 14:07:20.000 14:07:34.500 14:07:35.000

Camber 5/2

QINF = 450.1

MINF = 0.800

ALPT = 4.19

BETA = 0.34

H = 19243,

TINF = 3.2

RNPU = 3.1E+06

PSUR -- 992.2

MTOP = 0.81

Y,in. U/UTOP W/UTOP

0.240 0.6086 -0,1954

0.470 0.7346 -0.0592

0.970 0.8832 0.0906

1.470 0.9712 -0.1544

1.960 1.0069 -0.1989

2.330 0.9793 -0,1305

2,990 0.9827 -0,1992

3.490 0,9927 43.1234

3.990 0.9970 -0.1164

4.960 1.0000 -0.0786

Camber 5/2

QINF = 449.8

MINF = 0.800

ALPT = 4.19

BETA -- 0.19

H = 19254.

TINF = 2.9

RNPU = 3.1E+06

PSUR = 987,9

MTOP = 0.82

U/UTOP W/LrrOP

0.6205 43.1752

0.7387 -0.0638

0.8853 0.0912

0.9670 -0.1567

1.0063 -0.1924

0,9804 -0.1292

0.9831 -0.2001

0.9990 -0.1170

0.9981 °0.1192

1.00013 -0.0799

Camber 5/2

QINF = 450.3

MINF= 0,801

ALPT = 4.18

BETA = 0.43

H = 19255.

TINF = 2.9

RNPU = 3.1E+06

PSUR = 986.8

MTOP = 0.82

U/LrrOP W/UTOP

0.6203 43.1856

0.7434 -0.0640

0.8837 0.0896

0.9704 -0.1534

1.0020 43.1951

0.9786 -0.1297

0.9819 -0.1938

0.9907 -0.1289

0.9965 43.1237

1.0000 -0.0791

Camber 5/2

QINF = 452.3

MINF = 0.801

ALPT= 4.18

BETA = 0.28

H = 19145.

TINF = 3.2

RNPU = 3.1E+06

PSUR = 992.2

MTOP = 0.82

U/UTOP W/UTOP

0.6244 43.1755

0.7413 -0.0580

0.8832 0.0942

0.9733 43.1523

1.0027 -0.1959

0.9789 -0.1287

0.9832 43.2004

0.9922 -0.1253

0.9954 43.1229

1.0000 -0.0798

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP --

U/UTOP

0.6224

0.7366

0.8861

0.9664

1.0058

0,9783

0.9818

0.9917

0.9978

1.0000

5/2

452.3

0.801

4.19

0.34

19145.

3.2

3.1E+06

991.1

0.82

W/UTOP

-0.2035

-0.0635

0.0920

-0.1585

-0.1941

-0.1295

-0.1957

-0.1285

-0.1182

-0.0774

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:07:42.500 14:07:43.000 14:07:43.500 14:07:44.500 14:07:45.000

Camber 5/2

QINF = 454.2

MINF = 0.801

ALPT = 4.84

BETA = -0.85

H = 19069.

T1NF = 3.5

RNPU = 3.1E+06

PSUR = 993.3

MTOP = 0.82

Y, in. U/UTOP W/UTOP

0.240 0.5875 -0.1770

0,470 0.7168 -0.0526

0.970 0.8751 0.0876

1.470 0.9631 -0.1473

1.960 1.0019 -0.1859

2.330 0.9783 -0.1226

2.990 0.9812 -0.1895

3.490 0.9883 -0.0882

3.990 1.0041 -0.1060

4,960 1.0000 -0.0717

Camber 5/2

QINF = 454.1

M1NF = 0,801

ALPT = 5.00

BETA = -1.25

H = 19081.

TINF = 3.5

RNPU = 3.1E+06

PSUR = 993.3

MTOP = 0.82

U/UTOP W/UTOP

0.5911 -0.1590

0.7218 -0.0378

0.8760 0,0920

0.9600 -0.1407

0.9981 -0.1847

0.9763 -0.1113

0.9789 -0.1808

0.9876 -0.0982

0.9922 -0.1067

1.0000 43.0659

Camber 5/2

QINF = 454.4

MINF = 0.801

ALPT = 5.21

BETA = -1.31

H = 19081.

T1NF = 3,4

RNPU = 3.1E+06

PSUR = 994.4

MTOP = 0.82

U/UTOP W/UTOP

0.5989 -0.1569

0.7230 -0.0345

0.8697 0.0881

0.9606 -0.1349

1.0021 -0.1767

0.9792 -0,1123

0.9811 -0.1820

0.9895 -0.1048

0.9988 -0.1134

1.0000 -O.Ob40

Camber 5/2

QINF = 454.4

MINF = 0.801

ALPT = 5.83

BETA = -0.38

H = 19070.

T1NF= 3.5

RNPU = 3.1E+06

PSUR = 995.4

MTOP = 0.81

U/UTOP W/UTOP

0.6181 -0.1877

0.7390 -0.0655

0.8655 0.0712

0.9437 -0.1579

1.0021 -0.1979

0.9820 -0.1336

0.9806 -0.1990

0.9872 -0.1350

0.9993 -0.1250

1.0000 -0.0810

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6296

0.7466

0.8643

0.9327

1.0018

0.9811

0.9827

0.9937

0,9973

1.0000

5/2

454.4

0,801

6.11

0.08

19059.

3.5

3. l E+06

992,2

0.81

W/UTOP

-0.2011

-0.0821

0.0688

-0.1848

-0.2074

-0.1534

-0.2159

-0.1494

-0.1373

-0.0938

829
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:07:45.500 14:07:46.500 14:07:47,000 14:07:47.500 14:07:48.000

Camber 5/2

QINF = 453.9

MINF= 0.801

ALPT = 6.33

BETA = 0.43

H = 19058.

TINF = 3.2

RNPU = 3.1E+06

PSUR = 988.9

MTOP = 0.82

Yoin. U/UTOP W/UTOP

0,240 0.6436 -0.1993

0.470 0.7551 -0.0945

0,970 0.8643 0.0568

1.470 0.9423 -0.1843

1,960 0.9984 -0.2114

2,330 0.9822 -0.1604

2.990 0.9885 -0.2236

3.490 0.9936 -0.1614

3.990 1.0007 -0.1495

4.960 1.00_0 -0.1022

Camber 5/2

QINF = 453.1

MINF = 0.800

ALPT = 6.69

BETA = 0.48

H = 19046.

TINF = 3.3

RNPU = 3.1E+06

PSUR = 992.2

MTOP = 0.81

U/UTOP W/UTOP

0.6567 -0.2194

0.7543 -0.0976

0.8636 0.0486

0.9380 -0.1971

0,9921 -0.2169

0.9899 -0.1721

0.9943 -0.2327

1.0018 -0.1736

1.0155 -0.1567

1.0000 -0.1081

Camber 5/2

QINF = 452.2

MINF = 0,799

ALPT = 6.96

BETA = 0.40

H = 19045.

TINF = 3.8

RNPU = 3.1E+06

PSUR = 991.1

MTOP = 0.81

U/UTOP W/UTOP

0.6559 -0.2190

0.7589 -0.0998

0.8561 0.0481

0.9265 -0.2011

0.9772 -0.2138

0.9832 -0.1737

0.9902 -0.2317

0.9933 -0.1702

0.9990 -0.1567

1.0000 -0.1083

Camber 5/2

QINF = 451.4

MINF = 0,798

ALPT = 7.05

BETA = 0.25

H = 19044.

TINF = 3.2

RNPU = 3.1E+06

PSUR = 99 I. 1

MTOP = 0.81

U/UTOP W/UTOP

0.6492 -0.2118

0.7541 -0.0915

0.8475 0.0514

0,9163 -0.1890

0.9678 -0.2073

0.9762 -0.1722

0.9837 -0.2342

0.9904 -0.1973

0.9850 -0.1619

1.0000 -0.1014

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6561

0.7624

0.8568

0.9218

0.9814

0.9859

0.9933

1.0021

0.9964

1.0000

5/2

451.1

0.798

7.08

0.17

19043.

3.2

3AE+06

991.1

0.80

W/UTOP

-0.2137

-0.0875

0.0451

-0.2009

-0.2111

-0.1732

-0.2318

-0.2024

-0.1638

-0.1111

FI 11/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:07:50.500 14:07:51.000 14:07:51.500 14:07:52,000 14:07:52.500

Camber 5/2

QINF = 451.2

MINF = 0.798

ALPT = 7.60

BETA = 0.34

H = 19021.

TINF = 3.9

RNPU = 3.1E+06

PSUR = 990.0

MTOP = 0.80

Y, in. U/UTOP W/UTOP

0.240 0.6731 -0.2268

0.470 0.7751 -0.0989

0.970 0.8578 0.0406

1.470 0.9229 -0.1873

1,960 0.9700 -0.2093

2.330 0.9778 -0.1820

2,990 0.9950 -0.2357

3,490 0.9976 -0.1741

3,990 0.9977 -0.1661

4.960 1.0000 -0.1129

Camber 5/2

QINF = 451.5

MINF = 0.798

ALPT = 7.57

BETA = 0.31

H = 19010.

TINF = 3.3

RNPU = 3.1E+06

PSUR = 994.3

MTOP = 0.80

U/UTOP W/UTOP

0.6706 -0.2157

0.7674 -0.0986

0.8449 0.0392

0.9168 -0.1980

0.9684 -0.2084

0.9747 -0.1814

0.9963 -0.2372

0.9966 -0.1755

1.0005 -0.1532

1.0000 -0.1087

Camber 5/2

QINF = 451.8

MINF = 0,798

ALPT = 7.63

BETA = 0.31

H= 19011.

TINF = 3.6

RNPU = 3.1E+06

PSUR = 994.3

MTOP = 0.79

U/UTOP W/UTOP

0.6749 -0.2198

0.7713 -0.0886

0.8535 0.0441

0.9217 -0.1962

0.9720 -0.2116

0.9808 -0.1798

1.0017 -0.2430

1.0069 -0.1836

1.0163 -0.1592

1.0000 -0.1187

Camber 5/2

QINF = 452.1

MINF = 0,798

ALPT -- 7.92

BETA = 0.40

H = 19000.

T1NF = 3.5

RNPU = 3.1E+06

PSUR = 992.1

MTOP = 0.81

U/UTOP W/UTOP

0,6708 -0.2087

0.7634 -0.1050

0.8370 0.0251

0.8988 -0.1980

0.9442 -0.2097

0.9583 -0.1766

0.9878 -0.2444

0.9952 -0.1772

0.9995 -0.1694

1.0000 -0.1139

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6557

0.7576

0.8324

0.8989

0.9466

0.9609

0.9896

1.0012

1.0003

1.0000

5/2

452.1

0.798

8.00

0.31

19000.

3.2

3.1E+06

996.5

0.80

W/UTOP

-0.2139

-0.0933

0.0295

-0.1929

-0.2046

-0.1811

-0.2374

-0,1928

-0.1734

-0.1224

830
TableK-2.Continued.

Time 14:07:53.500

Camber 5/2

QINF = 452.4

MINF = 0.798

ALPT= 8.11

BETA = 0.02

H = 18989.

TINF = 3.5

RNPU= 3.1E+06

PSUR = 992.1

MTOP = 0.80

Y, in. U/UTOP W/UTOP

0.240 0.6646 -0.2136

0.470 0.7582 -0.0937

0.970 0.8308 0.0264

1.470 0.8938 -0.1971

1.960 0.9409 -0.1981

2.330 0.9523 -0.1737

2.990 0.9837 -0.2371

3.490 0.9995 -0.1856

3.990 0.9984 -0.1545

4.960 1.0000 -0.1142

FI I 1/MAW BOUNDARY LAYER DATA, FLT 229

14:07:54.000

Camber 5/2

QINF = 452.7

MINF= 0.798

ALPT= 8.11

BETA = 0.28

H = 18978.

TINF = 3.5

RNPU = 3.1E+06

PSUR = 995.4

MTOP = 0.80

U/UTOP W/UTOP

0.6669 -0.2106

0.7645 -0.0893

0.8364 0.0260

0.9008 -0.1920

0.9404 -0.2080

0.9550 -0.1731

0.9858 -0.2391

l.OOlO -0.1904

1.0009 -0.1678

1.000(3 -0.1156

14:07:57.500

Camber 5/2

QINF = 457.6

MINF -- 0.802

ALPT = 7.99

BETA = 0.45

H = 18917.

TINF = 3.4

RNPU = 3.2E+06

PS UR = 997.6

MTOP = 0.79

U/UTOP W/UTOP

0.6699 -0.2 190

0.7711 -0.0950

0.8484 0.0286

0.9095 -0.2042

0.9573 -0.2118

0.9702 -0.1789

1.0023 -0.2435

1.0136 -0.1672

1.0281 -0.1719

1.0000 -0.1248

14:07:58.000

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.6702

0.7672

0.8381

0.9015

0.9465

0.9613

0.9918

].0060

1.0026

1.0000

i

5/2

459.6

0.803

7.96

0.34

18908.

3.2

3.2E+06

997.6

0.80

W/UTOP

-0.2219

-0.0978

0.0318

-0.2005

-0.2073

-0.1747

-0.2376

-0.1871

-0.1703

-0.1184

14:07:58.500

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6729

0.7674

0.8394

0.9031

0.9492

0.9618

0.9923

1.0040

1.0019

1.0000

5/2

460.5

0.804

8.05

0.28

18898.

3.1

3.2E+06

998.7

0.80

W/UTOP

-0.2121

-0.0887

0.0294

-0.2002

-0.2088

-0.1772

-0.2372

-0.1904

-0.1768

-0.1162

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 229

Time 14:08:05.000 14:08:05.500 14:08:06.000 14:08:14.500

Camber 5/2

QINF = 475.2

MINF= 0.813

ALPT= 9.09

BETA = 0.28

H = 18691.

TINF= 3.9

RNPU = 3.2E+06

PSUR = 1018.2

MTOP = 0.81

Y, in. U/UTOP W/UTOP

0.240 0.6346 -0.1853

0.470 0.7155 -0.0760

0.970 0.7683 0.0180

1.470 0.8148 -0.1890

1.960 0.8602 -0.1794

2.330 0.8802 -0.1724

2.990 0.9258 -0.2336

3.490 0.9630 -0.1866

3.990 0.9877 -0.1667

4.960 1.0000 -0.1184

Camber 5/2

QINF = 475.8

MINF= 0.813

ALPT = 9. l 1

BETA = 0.25

H = 18680.

TINF= 4.2

RNPU = 3.2E+06

PSUR = 1019.3

MTOP = 0.81

U/UTOP W/UTOP

0.6289 -0.1836

0.7085 -0.0640

0.7572 0.0207

0.8124 -0.1844

0.8527 -0.1754

0.8705 -0.1642

0.9134 -0.2327

0.9494 -0.1505

0.9783 -0.1692

1.0000 -0.1140

Camber 5/2

QINF = 476.4

MINF= 0.814

ALPT = 9.08

BETA = 0.22

H = 18659.

TINF = 4.2

RNPU = 3.2E+06

PSUR = 1018.2

MTOP = 0.81

U/UTOP W/UTOP

0.6353 -0.1713

0.7117 -0.0576

0.7655 0.0176

0.8148 -0.1885

0.8592 -0.1779

0.8747 -0.1591

0.9176 -0.2275

0.9542 -0.1760

0.9807 -0.1703

1.0000 -0.1161

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5339

0.6721

0.7107

0.7276

0.7438

0.7741

0.8283

0.8724

0.9094

1.0000

5/2

467.1

0.802

9.99

0.05

18424.

5.1

3.2E+06

1011.5

0.71

W/UTOP

0.2149

0.1162

0.0045

-0.0989

-0.0936

-0.0949

-0.1904

-0.0621

-0.1136

-0.0988

831
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:53:04.500 08:53:06,000 08:53:06.500 08:53:09,000 08:53:09.500

Camber 0/2

QINF = 510.8

MINF = 0.780

ALPT = 2.82

BETA -- 0.72

H = 14914.

TINF = 13.0

RNPU = 3.5E+06

PSUR = 1188.3

MTOP = 0.79

Y,in. U/UTOP W/UTOP

0.240 0.6367 -0.1621

0.470 0.7657 -0.0524

0.970 0.9180 0.1269

1,470 0.9804 -0.1129

1.960 0.9989 -0.1870

2.330 0.9690 -0.1050

2.990 0.9738 -0.1753

3.490 0.9846 -0.0889

3.990 0.9948 -0.0935

4.960 1.0000 -0.0528

Camber 0/2

QINF = 505.0

MINF = 0.778

ALPT = 2.82

BETA = 0.45

H = 15042.

TINF = 11.9

RNPU = 3.5E+06

PSUR = I 181.8

MTOP -- 0.79

U/UTOP W/UTOP

0.6454 -0.1623

0.7684 -0.0411

0.9171 0.1254

0.9835 -0.1182

0.9984 -0.1850

0.9726 -0.1046

0.9760 -0.1726

0.9819 -0.0946

0.9998 -0.0954

1.0000 -0.0561

Camber 0/2

QINF -- 502.5

MINF = 0.777

ALPT = 2.82

BETA = 0.54

H = 15084.

TINF = l2.4

RNPU = 3.5E+06

PSUR = 1181.8

MTOP = 0.78

U/UTOP W/UTOP

0.6444 -0.1842

0.7711 -0.0521

0.9210 0.1242

0.9804 -0.1232

0.9989 -0.1867

0.9731 -0.1049

0.9782 -0.1742

0.9857 -0.0886

0.9994 -0.0970

1.0000 -0.0552

Camber 0/2

QINF = 498.0

MINF = 0.775

ALPT = 2.79

BETA -- 0.60

H = 15180.

TINF = 11.7

RNPU = 3.5E+06

PSUR = 1176.4

MTOP = 0.78

U/UTOP W/UTOP

0.6429 -0.1635

0.7722 -0.0483

0.9240 0.1252

0.9843 -0.1227

1.0056 -0.1871

0.9767 -0.1057

0.9811 -0.1750

0.9896 -0.0908

1.0025 -0.0957

1.00130 -0.0552

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR --

MTOP =

U/UTOP

0.6450

0.7732

0.9172

0.9762

1.0005

0.9727

0.9769

0.9852

0.9965

1.0000

0/2

498.6

0.775

2.85

0.60

15181.

11.9

3.5E+06

1176.4

0.79

W/UTOP

-0.1639

-0.0522

0.1215

-0.1264

-0.1861

-0.1051

-0.1783

-0.0966

-0.1017

-0.0575

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:53:15.500 08:53:16.000 08:53:17.000 08:54:44.500 08:54:46.000

Camber 0/2

QINF = 515.9

MINF = 0.785

ALPT = 3.97

BETA = 0.63

H = 14942.

TINF = 12.7

RNPU = 3.6E+06

PSUR = 1182.8

MTOP = 0.80

Y, in. U/UTOP W/UTOP

0.240 0.6275 -0.1931

0,470 0.7514 -0.0713

0.970 0.8982 0.1050

1.470 0.9727 -0. 1420

1.960 0.9945 -0.1939

2.330 0.9699 -0.1284

2.990 0.9753 -0.1926

3.490 0.9810 -0.1212

3.990 0.9977 -0.1157

4.960 1.0000 -0.0680

Camber 0/2

QINF = 518.4

MINF -- 0.786

ALPT = 4.06

BETA = 0.57

H = 14900.

TINF = 12.9

RNPU = 3.6E+06

PSUR = 1182.8

MTOP = 0.80

U/UTOP W/UTOP

0.6290 -0.2101

0.7517 -0.0783

0.8931 0.0972

0.9726 -0.1428

1.0001 -0.2009

0.9717 -0.1361

0.9802 -0.1900

0.9865 -0,1249

1.0019 -0.1169

1.0000 -0.0705

Camber 0/2

QINF = 523.9

MINF = 0.789

ALPT = 4,03

BETA = 0.63

H = 14827.

TINF = 12.9

RNPU = 3.6E+06

PSUR = 1193.6

MTOP = 0.80

U/UTOP W/UTOP

0.6244 -0.1613

0.7474 -0.0810

0.8950 0.1015

0.9752 -0.1354

0.9960 -0.1995

0.9728 -0.1272

0.9779 -0.1869

0.9810 -0.1272

0.9958 -0.1166

1.0000 -0.0754

Camber 0/3

QINF = 513.7

MINF = 0.783

ALPT = 4.20

BETA = 0.66

H = 14962.

TINF = 11.6

RNPU = 3.6E+06

PSUR = 1170.7

MTOP = 0.81

U/UTOP W/UTOP

0.5960 -0.2323

0.7191 -0.0830

0.8774 0.0861

0.9695 -0.1635

1.0004 -0.2083

0.9749 -0.1520

0.9796 -0.2036

0.9837 -0.1503

0.9988 -0.1374

1.0000 -0.0849

Camber

QINF --

MINF =

ALPT --

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5987

0.7216

0.8821

0.9730

1.0050

0,9788

0.9817

0.9864

1.0035

1.0000

0/3

513.4

0.783

4.20

0.66

14950.

11.6

3.6E+06

1169.6

0.81

W/UTOP

-0.2020

-0.0921

0.0834

-0.1698

-0.2091

-0.1472

-0.2081

-0.1467

-0.1387

-0.0884

832
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:54:47.500 08:54:48.500 08:54:54.500 08:54:55.000 08:54:55.500

Camber 0/3

QINF= 513.4

MINF = 0.783

ALPT = 4.19

BETA = 0.60

H = 14950.

TINF = 11.6

RNPU = 3.6E+06

PSUR = 1171.8

MTOP = 0.81

Y,in. U/UTOP W/UTOP

0.240 0.5987 -0.2477

0.470 0.7238 -0.0932

0.970 0.8839 0.0865

1.470 0.9703 -0.1622

1.960 1.0035 -0.2097

2.330 0.9767 -0.1502

2.990 0.9822 -0.2035

3.490 0.9875 -0.1495

3.990 1.0015 -0.1318

4.960 1.0000 -0.0849

Camber 0/3

QINF= 513.1

MINF = 0.783

ALPT -- 4.19

BETA = 0.54

H = 14950.

TINF = 11.6

RNPU = 3.6E+06

PSUR = 1172.9

MTOP = 0.80

U/UTOP W/UTOP

0.5961 -0.2324

0.7263 -0.0915

0.8849 0.0904

0.9737 -0.1642

1.0073 -0.2118

0.9802 -0.1500

0.9845 -0.2091

0.9880 -0.1509

1.0047 -0.1370

1.0000 -0.0850

Cam ber 1/4

QINF = 512.2

MINF = 0.782

ALPT = 5.80

BETA = 0.66

H = 14960.

TINF = 12.0

RNPU = 3.5E+06

PSUR = 1160.7

MTOP = 0.81

U/UTOP W/UTOP

0.5574 -0.2595

0.6824 -0.10t9

0.8382 0.0486

0.9538 -0.1965

1.001'6 -0.2272

0.9771 -0.1773

0.9834 -0.2267

0.9876 -0.1765

0.9987 -0.1643

1.0000 -0.1071

Camber 1/4

QINF= 510.7

MINF = 0.781

ALPT = 5.99

BETA = 0.60

H = 14970.

T1NF = 11.5

RNPU = 3.5E+06

PSUR = 1156.3

MTOP = 0.82

U/UTOP W/UTOP

0.5427 -0.2706

0.6635 -0.1072

0.8251 0.0413

0.9418 -0.2094

0.9982 -0.2325

0.9758 -0.1854

0.9824 -0.2364

0.9890 -0.1978

0.9998 -0.1832

1.0000 -0.1118

Camber

QINF =

MINF =

ALPT =

BETA=

H=

TINF =

RNPU =

PSUR =

MTOP --

U/UTOP

0.5384

0.6575

0.8223

0.9500

1.0010

0.9774

0.9839

0.9907

0.9990

1.0000

1/4

509.1

0.780

6.02

0.66

14991.

11.3

3.5E+06

1153.0

0.82

W/UTOP

-0.2912

-0.0964

0.0394

-0.2075

-0.2327

-0.1888

-0.2367

-0.2114

-0.1795

-0.1137

FI 11/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:54:56.000 08:54:57.000 08:54:57.500 08:54:58.000 08:55:05.500

Camber 1/4

QINF = 506.6

MINF = 0.779

ALPT = 6.21

BETA = 0.63

H = 15022.

TINF = 11.1

RNPU = 3.5E÷06

PSUR = 1151.9

MTOP = 0.81

Y,in. U/UTOP W/UTOP

0.240 0.5325 -0.3138

0.470 0.6468 -0.1034

0.970 0.8142 0.0323

1.470 0.9448 -0.2147

1.960 1.0020 -0.2374

2.330 0.9799 -0.1941

2.990 0.9865 -0.2415

3.490 0.9927 -0.2060

3.990 1.0013 -0.1843

4.960 1.0000 -0.1198

Camber 215/415

QINF = 500.1

MINF= 0.775

ALPT = 6.70

BETA = 0.45

H = 15082.

TINF = 11.0

RNPU = 3.5E+06

PSUR = 1142.0

MTOP = 0.82

U/UTOP W/UTOP

0.5191 -0.3122

0.6300 -0.0858

0.8015 0.0232

0.9386 -0.2200

0.9985 -0.2396

0.9806 -0.1957

0.9873 -0.2470

0.9918 -0.2135

0.9998 -0.1878

1.0000 -0.1236

Camber 2/5

QINF = 496.0

MINF = 0.772

ALPT = 6.70

BETA = 0.51

H = 15133.

TINF = 10.9

RNPU = 3.5E+06

PSUR = 1140.9

MTOP = 0.81

U/UTOP W/UTOP

0.5187 -0.3522

0.6228 -0.0880

0,7896 0.0172

0.9348 -0.2224

0.9983 -0.2389

0.9815 -0.1992

0.9888 -0.2503

0.9912 -0.2097

1.0024 -0A939

1.0000 -0.1276

Camber 2/5

QINF = 491.7

MINF= 0.770

ALPT = 6.59

BETA = 0.60

H = 15185.

TINF = 10.3

RNPU = 3.5E+06

PSUR = 1134.4

MTOP = 0.81

U/UTOP W/UTOP

0.5121 -0.3486

0.6208 -0.0980

0.7876 0.0197

0.9289 -0.2277

0.9962 -0.2334

0.9792 -0.2009

0.9863 -0.2523

0.9886 -0.2249

0.9976 -0.1985

1.0000 -0.1268

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6448

0.7785

0.9245

0.9821

1.0010

0.9745

0.9794

0.9860

0.9987

1.0000

0/2

444.3

0,747

2.63

0.69

16206.

6.4

3.3E+06

1128.8

0.76

W/UTOP

-0.1872

-0.0358

0.1213

-0.1356

-0.1855

-0.1085

-0.1860

-0.0928

-0.1085

-0_0606

833
TableK-2.Continued.

F111/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:55:06.500 08:55:07.500 08:55:09.500 08:55:12.000 08:55:13.500

Camber 0/2

QINF = 441.7

MINF = 0.746

ALPT = 2.62

BETA = 0.77

H = 16270.

T1NF = 6.5

RNPU = 3.3E+06

PSUR = 1123.4

MTOP = 0.76

Y, in. U/UTOP W/UTOP

0.240 0.6533 -0.1764

0.470 0.7829 -0.0440

0.970 0.9286 0.1213

1.470 0.9874 -0.1320

1,960 1.0053 -0.1845

2.330 0.9771 -0.1079

2.990 0.9818 -0.1844

3.490 0.9918 -0.0914

3,990 1.0003 -0.0981

4.960 1.0000 -0.0608

Camber 0/2

QINF = 439.9

MINF = 0.745

ALPT = 2.62

BETA = 0.74

H = 16313.

TINF = 6.7

RNPU = 3.2E+06

PSUR = 1123.4

MTOP = 0.75

U/UTOP W/UTOP

0.6413 -0.2004

0.7785 -0.0443

0.9222 0.1230

0.9884 -0.1322

1.0062 -0.1834

0.9764 -0.1086

0.9814 -0.1865

0.9916 -0.0991

1.0012 -0.0959

1.0000 -0.0621

Camber 0/2

QINF = 440.9

MINF = 0.746

ALPT= 3.10

BETA = 0.77

H = 16336.

TINF = 5.8

RNPU = 3.3E+06

PSUR = 1118.0

MTOP = 0.76

U/UTOP W/UTOP

0.6407 -0.1968

0.7703 -0.0488

0.9152 0.1124

0.9828 -0.1417

1.0009 -0.1865

0.9767 -0.1146

0.9779 -0.1878

0.9864 -0.1012

0.9985 -0.1072

1.0000 -0.0635

Camber 0/3/2/2

QINF = 447.9

MINF = 0.751

ALPT = 3.10

BETA = 0.80

H = 16266.

TINF = 6.2

RNPU = 3.3E+06

PSUR = 1120.1

MTOP = 0.76

U/UTOP W/UTOP

0.6284 -0.2102

0.7598 -0.0551

0.9125 0.1074

0.9820 -0.1548

1.0074 43.1941

0.9786 -0.1269

0.9829 -0.1928

0.9925 -0.1139

1.0019 -0.1103

1.0000 -0.0707

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6324

0.7645

0.9144

0.9837

1.0083

0.9763

0.9816

1.0000

1.0006

1.0000

0/2

454.7

0.755

3.10

0.77

16173.

6.4

3.3E+06

1124.5

0.77

W/UTOP

-0.1973

-0.0572

0.1118

-0.1455

-0.1908

-0.1232

-0.1883

-0.1047

-0.1127

-0.0675

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:55:26.500 08:55:27.000 08:55:27.500 08:55:34.000 08:55:42.000

Camber 1/4

Q1NF = 550.5

MINF = 0.804

ALPT = 6.29

BETA = 0.60

H = 14530.

TINF = 12.5

RNPU = 3.7E+06

PSUR = 1136.0

MTOP = 0.87

Y, in. U/UTOP W/UTOP

0.240 0.6318 -0.2947

0.470 0.7155 -0.1539

0.970 0.8202 0.0116

1.470 0.9243 -0.2183

1.960 0.9819 -0.2332

2.330 0.9760 -0.2023

2.990 0.9827 -0.2479

3.490 0.9890 -0.2437

3.990 1.0025 -0.2021

4.960 1.000(3 -0.1328

Camber 1151414

QINF = 552.2

MINF = 0.804

ALPT = 6.28

BETA = 0.66

H = 14487.

TINF = 12.8

RNPU = 3.7E+06

PSUR = 1132.6

MTOP = 0.88

uAYroP W/UTOP

0.6412 -0.3021

0.7199 -0.1548

0.8257 0.0149

0.9276 -0.2155

0.9806 -0.2350

0.9731 -0.2077

0.9820 -0.2483

0.9853 -0.2395

0.9989 -0.2072

1.0000 -0.1360

Camber 1151414

QINF = 553.6

MINT = 0.805

ALPT = 6.24

BETA = 0.72

H = 14433.

TINF = 13.1

RNPU = 3.7E+06

PSUR = 1128.2

MTOP = 0.88

U/UTOP W/UTOP

0.6503 -0.2840

0.7381 -0.1634

0.8285 0.0122

0.9221 -0.2159

0.9721 -0.2333

0.9690 -0.2060

0.9779 -0.2479

0.9838 -0.2337

0.9975 -0.2035

t.0000 -0.1376

Camber 1/4

QINF = 558.2

MINT = 0.805

ALPT = 6.21

BETA = 0.63

H = 14281.

TINT = 14.0

RNPU = 3.7E+06

PSUR = 1183.1

MTOP = 0.84

U/UTOP W/UTOP

0.5268 -0.3414

0.6331 -0.0892

0.8106 0.0367

0.9363 -0.2045

1.0007 -0.2369

0.9813 -0.1885

0.9872 -0.2343

0.9925 -0.2172

1.0051 -0.1745

1.0000 -0.1158

Camber

QINF =

MINF =

ALPT =

BETA=

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6410

0.7707

0.9194

0.9798

0.9991

0.9720

0.9774

0.9861

0.9979

1.0000

0/2

508.5

0.783

2.57

0.57

15214.

10.9

3.5E+06

1173.2

0.79

W/UTOP

-0.1844

-0.0516

0.1269

-0.1t86

-0.1879

-0.1074

-0.1744

-0.0910

-0.0998

-0.0585

834
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:55:43.000

Camber 0/2

QINF = 502.9

MINF= 0.780

ALPT = 2.59

BETA = 0.66

H = 15297.

TINF= 10.3

RNPU = 3.5E+06

PSUR = 1168.8

MTOP = 0.79

Y, in. U/UTOP W/UTOP

0.240 0.6461 -0.1693

0.470 0.7756 -0,0453

0.970 0.9224 0. ! 284

1.470 0.9804 -0.1241

1,960 1.0014 -0.1870

2.330 0.9740 -0.1078

2.990 0.9791 -0.1768

3.490 0.9858 -0.0917

3.990 0.9975 -0.0954

4.960 1.0000 -0.0569

08:55:44.000

Camber 0/2

QINF = 498,5

MINF= 0.778

ALPT = 2.59

BETA = 0.74

H= 15371.

TINF = 10.2

RNPU = 3.5E+06

PSUR = 1168.8

MTOP = 0.78

U/UTOP W/UTOP

0.6390 o0.1693

0.7756 -0.0519

0.9203 0.1269

0.9816 -0.1233

0,9988 -0.1821

0.9735 -0.1086

0.9780 -0.1826

0,9859 -0.0975

0.9990 -0.1010

1.0000 -0.0595

08:55:46.000

Camber 0/2

QINF = 494. l

MINF= 0.776

ALPT = 2.96

BETA = 0.69

H = 15433.

TINF= 10.2

RNPU = 3.5E+06

PSUR = 1162,3

MTOP = 0.79

U/UTOP W/UTOP

0.6372 -0,1895

0.7680 -0.0541

0.9116 0.1176

0.9781 -0.1351

0.9985 -0.1935

0.9727 -0,1188

0.9789 -0.1875

0.9863 -0.1042

0.9987 -0.1052

1.0000 -0.0622

08:55:46.500

Camber 0/2

QINF = 493.8

MINF = 0.775

ALPT = 3.02

BETA = 0.66

H = 15433.

TINF= 10.2

RNPU = 3.5E+06

PSUR = 1161.3

MTOP = 0.78

U/UTOP W/UTOP

0.6386 -0.1778

0.7623 -0.0588

0.9119 0.1189

0.9789 -0.1372

1.0016 -0.1934

0.9744 -0.1142

0.9796 -0.1885

0.9887 -0.1058

0.9980 -0.1083

1.0000 -0.0652

08:55:47.000

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6363

0.7631

0.9108

0.9813

1.0046

0.9754

0.9814

0.9843

1.0004

1.0000

0/2

494.1

0.776

3.01

0.74

15433,

10.2

3.5E+06

1159.1

0.79

W/UTOP

-0.1758

-0.0615

0.1157

-0.1393

-0.1919

-0,1189

-0.1851

-0.1184

-0.1133

-0.0648

F11 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:55:54.000 08:55:54.500 08:56:00.000 08:56:01,500 09:00:30.000

Camber 0/3

QINF = 523.9

MINF= 0.792

ALPT = 3.96

BETA = 0.66

H = 15051.

TINF = 11.4

RNPU = 3.6E+06

PSUR = 1171.9

MTOP = 0.81

Y.in. U/UTOP W/UTOP

0,240 0.6075 -0.2225

0.470 0.7305 -0.0842

0.970 0.8806 0.0936

1.470 0.9714 -0.1577

1.960 0.9990 -0,2085

2.330 0.9721 -0.1422

2.990 0.9781 -0.2010

3.490 0.9831 -0.1427

3.990 0.9986 -0.1283

4.960 1.0000 -0.0791

Camber 0/3

QINF = 526.7

MINF = 0.794

ALPT = 3.98

BETA = 0.66

H = 15009.

TINF = 11.8

RNPU = 3.6E+06

PSUR = 1171.9

MTOP = 0.8 l

U/UTOP W/UTOP

0.6017 -0.2234

0.7296 -0.0819

0.8797 0.0935

0.9715 -0.1566

1.0013 -0.2083

0.9739 -0.1437

0.9794 -0.1997

0,9847 -0.1456

0.9971 -0.1236

1.0000 -0.0820

Camber 0/3

QINF = 564.3

MINF= 0.813

ALPT = 4.00

BETA = 0.60

H = 14466.

TINF = 14.0

RNPU = 3,7E+06

PSUR = 1198.9

MTOP = 0.83

U/UTOP W,qJTOP

0.5980 -0.2206

0.7222 -0.0939

0.8817 0.1011

0.9703 -0.1577

0.9993 -0.2102

0.9728 -0.1444

0.9791 -0.1978

0.9862 -0.1443

1.0010 -0.1308

1.0000 -0.0809

Camber 0/3

QINF= 571.2

MINF= 0.815

ALPT = 3.97

BETA = 0.63

H = 14294.

TINF = 14.8

RNPU = 3.8E+06

PSUR = 1208.6

MTOP = 0.83

U/UTOP W/UTOP

0.5941 -0.2154

0.7238 -0.0942

0.8794 0.1000

0.9713 -0.1501

0.9996 -0.2105

0.9725 -0.1460

0.9790 -0.1976

0.9834 -0.1474

1.0017 -0.1227

1.0000 -0.0805

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5943

0.7264

0.8798

0.9709

1.0010

0.9765

0.9795

0.9862

1.0014

1.0000

0/3

512.6

0.783

4.01

0.66

15017.

11.9

3.5E+06

1170.7

0.80

W/UTOP

-0,2224

-0.0950

0.0900

-0.1621

-0.2076

-0.1486

-0.2058

-0.1420

-0.1389

-0.0829

835
TableK-2.Continued.

FL 11/MAW BOUNDARY LAYER DATA, FLT 230

Time 09:00:30.500 09:00:31.000 09:00:31.500 09:00:35.000 09:00:36.500

Camber 0/3

QINF = 514.5

MINF = 0.785

ALPT -- 4.02

BETA = 0.57

H -- 15019.

TINF = 12.0

RNPU -- 3.6E+06

PSUR = 1167.5

MTOP = 0.80

Y.in. U/UTOP W/UTOP

0.240 0.6024 -0.2441

0.470 0.7273 -0.0923

0.970 0.8870 0.0903

1.470 0.9777 -0.1622

1.960 1.0129 -0.2094

2.330 0.9830 -0.1480

2.990 0.9887 -0.1985

3.490 0.9921 -0.1529

3.990 1.0088 -0.1354

4.960 1.0000 -0.0834

Camber 0/3

QINF = 513.6

MINF = 0.784

ALPT = 3.98

BETA = 0.74

H = 15018.

TINF = 11.8

RNPU = 3.6E+06

PSUR = 1171.8

MTOP = 0.80

U/UTOP W/UTOP

0.5958 -0.2210

0.7206 -0.0950

0.8794 0.0895

0.9712 -0.1631

1.0029 -0.2101

0.9765 -0.1500

0.9830 -0.2061

0.9954 -0.1426

1.0051 -0.1348

1.0000 -0.0829

Camber 0/3

QINF = 513.0

MINF = 0.784

ALPT = 4.02

BETA = 0.45

H = 15017.

TINF = 11.9

RNPU = 3.5E+06

PSUR = 1171.8

MTOP = 0.81

U/UTOP W/UTOP

0.5920 -0.2449

0.7183 -0.0869

0.8735 0.0882

0.9698 -0.1617

0.9984 -0.2045

0.9739 -0.1475

0.9782 -0.1982

0.9831 -0.1502

0.9946 -0.1336

1.0000 -0.0813

Camber 0/3

QINF = 510.3

MINF = 0.781

ALP'/" = 4.17

BETA = 0.63

H = 15003.

TINF = 12.2

RNPU = 3.5E+06

PSUR = 1169.6

MTOP -- 0.81

U/UTOP W/UTOP

0.5886 -0.2348

0.7172 -0.0930

0.8716 0.0824

0.9669 -0.1700

1.0013 -0.2119

0.9764 -0.1521

0.9810 -0.2065

0.9882 -0.1536

0.9992 -0.1420

1.0000 -0.0888

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5896

0.7161

0.8776

0.9760

1.0042

0.9777

0.9843

0.9863

1.0013

1.0(KI0

0/3

512.1

0.783

4.18

0.63

15005.

12.0

3.5E+06

1166.4

0.81

W/UTOP

-0.2221

-0.0964

0.0821

-0.1665

-0.2088

-0.1506

-0.2060

-0.1562

-0.1394

-0.0869

FI 1 I/MAW BOUNDARY LAYER DATA. FIT 230

Time 09:00:45.500 09:00:46.000 09:00:46.500 09:00:56.000 09:00:56.500

Camber 3/6

QINF= 512.8

M1NF = 0.785

ALPT = 7.89

BETA = 0.34

H = 15084.

TINF = 11.7

RNPU = 3.5E+06

PSUR = 1064.7

MTOP = 0.86

Y.in. U/LrTOP W/LrI'OP

0.240 0.6824 -0.2553

0.470 0.7434 -0.1096

0.970 0.7722 -0.0506

1.470 0.8056 -0.1859

1.960 0.8093 -0.1543

2.330 0.8438 -0.2271

2.990 0.8824 -0.2208

3.490 0.9234 -0.1991

3.990 0.9607 -0.2096

4.960 1.0000 -0.1603

Camber 3/6

QINF= 510.1

MINF = 0.782

ALPT = 8.37

BETA = 0.34

H = 15081.

TINF = 11.7

RNPU = 3.5E+06

PSUR = 1056.9

MTOP = 0.85

U/UTOP W/UTOP

0.6954 -0.2323

0.7668 -0.1084

0.7729 -0.0728

0.7859 -0.1897

0.7455 -0.1407

0.7896 -0.2451

0.8337 -0.2372

0.8884 -0.1901

0.9391 -0.2146

1.0000 -0.1666

Camber 3/6

QINF = 506.4

MINF = 0.780

ALPT = 7.80

BETA = 0.43

H = 15088.

TINF = 11.7

RNPU = 3.5E+06

PSUR = 1047. I

MTOP = 0.82

U/LrFOP W/UTOP

0.6866 -0.2277

0.7568 -0.0945

0.7741 -0.0672

0.7777 -0.1890

0.7325 -0.1185

0.7642 -0.2249

0.8058 -0.2311

0.8673 -0.1577

0.9293 -0.2064

1.0000 -0.1740

Camber 3/6

QINF = 510.9

MINF = 0.783

ALPT= 8.11

BETA = 0.86

H = 15093.

TINF = 11.6

RNPU = 3.5E+06

PSUR = 1067.9

MTOP = 0.84

U/UTOP W/UTOP

0.6908 -0.2446

0.7584 -0.1244

0.7869 -0.0626

0.8070 -0.1964

0.7760 -0.1613

0.8224 -0.2815

0.8564 -0.2371

0.9068 -0.1813

0.9424 -0.2170

1.0000 -0.1694

Camber

QINF --

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6928

0.7520

0.7507

0.7524

0.7235

0.7593

0.7973

0.8620

0.9144

1.0000

3/6

508.8

0.782

8.22

0.74

15091.

11.8

3.5E+06

1049.2

0.83

W/UTOP

-0.2286

-0.0922

-0.1053

-0.1887

-0.1141

-0.2165

-0.2163

-0.1627

-0.2041

-0.1700

836
TableK-2.Continued.

F11 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 09:00:57.000 09:00:57.500 09:0l :04.500 09:01:05.000 09:01:08.500

Camber 3/6

QINF = 5O6. I

MINF = 0.780

ALPT = 8.46

BETA = 0.69

H = 15099.

T1NF = 11.7

RNPU = 3.5E+06

PSUR = 1063.4

MTOP = 0.79

Y.in. U/UTOP W/UTOP

0.240 0.6817 -0.2309

0.470 0.7309 -0.075 l

0.970 0.7202 -0.1418

1.470 0.7087 -0.1841

1.960 0.6636 -0.0842

2.330 0.7011 -0.1923

2.990 0.7457 -0.2259

3.490 0.8401 -0.1611

3.990 0.8911 -0.2201

4.960 1.0000 -0.1693

Camber 3/6

QINF= 502.8

MINF = 0.777

ALPT = 8.44

BETA = 0.60

H = 15096.

TINF = 11.7

RNPU = 3.5E+06

PSUR = 1046.8

MTOP = 0.81

U/UTOP W/LrrOP

0.6948 -0.2369

0.7528 -0.0845

0.7599 -0.1296

0.7461 -0.1819

0.6946 -0.0707

0.7079 -0.1624

0.7494 -0.2156

0.8208 -0.1389

0.8780 -0.1922

1.0000 -0.1661

Camber 1/4

QINF = 497.2

MINF = 0.775

ALPT = 5.77

BETA = 0.98

H = 15258.

TINF -- 10.9

RNPU -- 3.5E+06

PSUR = 1142.3

MTOP = 0.81

U/UTOP W/UTOP

0.5592 -0.2727

0.6779 -0.1066

0.8434 0.0459

0.9573 -0.2057

1.0024 -0.2326

0.9774 -0.1816

0.9855 -0.2330

0.9894 -0.2012

1.0003 -0.1740

1.00130 -0.1147

Camber 1/4

QINF = 498. I

MINF= 0.776

ALPT = 6.65

BETA = 0.83

H = 15259.

T1NF = 11.2

RNPU = 3.5E+O6

PSUR = 1143.3

MTOP = 0.81

U/U'FOP W/UTOP

0.5397 -0.3032

0.6561 -0.1198

0.8141 0.0228

0.9434 -0.2209

1.0006 -0.2414

0.9736 -0.1892

0.9853 -0.2467

0.9887 -0.2179

1.0012 -0.187]

1.0000 -0.1203

Camber

QINF =

MINF=

ALPT =

BETA=

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6985

0.7445

0.7_5

0.7514

0.6998

0.7357

0.7646

0.8373

0.8697

1.0000

4n

485.4

0.766

9.05

o.14

15245.

1o.8

3.4E+06

1051.4

0.77

WRYI'OP

-0.2170

-0.0729

-0.1766

-0.1913

-0.0713

-0.2121

-0.2128

-0.1479

-0.1876

-0.1662

F11 l/MAW BOUNDARY LAYER DATA. FLT 230

Time 09:01:09.000 09:01:19.000 09:01:19.500 09:01:20.000 09:01:20.500

Camber 4/7

QINF = 481.2

MINF= 0.763

ALPT = 9.10

BETA = 0.25

H = 15252.

TINF = 11.2

RNPU = 3.4E+06

PSUR = 1059.1

MTOP = 0.77

Y,in. U/UTOP W/UTOP

0.240 0.6941 -0.2308

0.470 0.7506 -0.0727

0.970 0.7666 -0.1469

1.470 0.7646 -0.1964

1.960 0.7312 -0.0869

2.330 0.7363 -0.1382

2.990 0.7637 -0.1964

3.490 0.8418 -0.1603

3.990 0.8903 -0.2018

4.960 1.0000 -0.1573

Camber 4/7

QINF = 454.0

MINF = 0.745

ALPT = 9.18

BETA = 0.63

H = 15536.

TINF = 9.7

RNPU = 3.3E+06

PSUR = 1066.0

MTOP = 0.79

U/UTOP W/UTOP

0.6606 -0.2682

0.7341 -0.1017

0.7892 -0.0938

0.8541 -0.2082

0.8478 -0.1868

0.8736 -0.2425

0.9064 -0.2464

0.9488 -0.2204

0.9771 -0.1992

1.0000 -0.1622

Camber 4/7

QINF = 450.3

MINF = 0.742

ALPT = 8.88

BETA = 0.74

H = 15543.

TINF = 9.7

RNPU = 3.3E+06

PSUR = 1050.6

MTOP = 0.78

U/UTOP W/UTOP

0.6967 -0.2532

0.7642 -0.0984

0,7887 -0.I175

0.7929 -0.2135

0.7644 -0.1348

0.7942 -0.2263

0.8272 -0.2410

0.8814 -0.1639

0.9174 -0.2118

1.000(I -0.1654

Camber 4/7

QINF = 447.4

MINF = 0.740

ALPT = 8.65

BETA = 0.83

H = 15551.

TINF = 9.7

RNPU = 3.3E+06

PSUR = 1038.5

MTOP = 0.80

U/UTOP W/UTOP

0.7059 -0.2402

0.7689 -0.1016

0.7953 -0.1038

0.8079 -0.2042

0.7741 -0.1396

0.7865 -0.1872

0.8316 -0.2460

0.8859 -0.1736

0.9356 -0.2153

1.0000 -0.1668

Camber

QINF =

M1NF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6773

0.7446

0.7850

0.8117

0.7913

0.8024

0.8487

0.9189

0.9519

1.0000

4/7

443.4

0.737

8.87

0.83

15558.

10. l

3.3E+06

1064.9

0.78

W/UTOP

-0.2503

-0.0983

-0.0970

-0.2105

-0.1429

-0.1562

-0.2382

-0.2336

-0.2266

-0.1687

837
TableK-2.Continued.

Time 09:01:21.000

Camber

QINF =

MINF =

ALPT =

BETA =

H--

T1NF =

RNPU =

PSUR =

MTOP =

Y,in. U/LrI'oP

0,240 0.6576

0,470 0.721 i

0,970 0.7763

1.470 0.8311

1.960 0.8402

2,330 0.8481

2,990 0.8903

3,490 0.9370

3,990 0.9758

4,960 1.0000

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 230

09:01:21.500

4/7 Camber

440.0 QINF =

0.734 MINF =

9.10 ALPT =

0.80 BETA =

15565, H =

9.7 TINF =

3.3E+06 RNPU =

1061.8 PSUR =

0.78 MTOP =

W/UTOP U/UTOP

-0.2703 0,6681

-0.0895 0.7348

-0.0988 0.7773

-0.2104 0.8193

-0.1441 0,803 I

-0.1570 0.8312

-0.2347 0.8674

-0.2092 0,9251

-0.2313 0.9500

4). 1690 1.0000

4/7

437.1

0.732

8.87

0.86

15584.

9.7

3.3E+06

1067.3

0.78

W/UTOP

-0.2729

-0.1102

-0.1003

-0.2127

-0.1424

-0.1847

-0.2432

-0.2112

-0.2292

-0.1692

09:01:24,000

Camber 1/4

QINF = 434.1

MINF = 0.731

ALP'r= 4.87

BETA = -1.51

H = 15682.

TINF = 9.8

RNPU = 3.2E+06

PSUR= 1132.8

MTOP = 0.75

U/UTOP W/UTOP

0.5657 -0.2369

0.7047 -0.0467

0.8703 0.0777

0.9716 -0.1510

1.0090 -0.1873

0.9790 -0.1222

0.9857 -0.1904

1.0018 -0.1056

1.0005 -0.1183

1.0000 -0.0670

09:01:25.000

Camber 1/4

QINF = 434.6

MINF = 0.731

ALPT = 5.02

BETA = -0.56

H = 15704.

TINF = 9.7

RNPU = 3.2E+06

PSUR = 1133.9

MTOP = 0.76

U/UTOP W/UTOP

0.5802 -0.2335

0.7197 -0.0682

0.8700 0.0715

0.9676 -0.1650

1.0064 -0.1954

0.9779 -0.1320

0.9835 -0.2000

0.9902 -0.1267

1.0037 -0.1303

1.0000 -0.0740

09:01:28,500

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6263

0.7580

0.9056

0.9865

1.0085

0.9818

0.9851

0.9936

1.0044

1.0000

0/3

433.2

0.732

3.09

0.80

15848.

9.2

3.2E+06

1134.1

0.75

W/UTOP

-0.2133

-0.0723

0.1008

-0.1557

-0.1941

-0.1329

-0.1971

-0.1215

-0.1211

-0.0754

F111/MAW BOUNDARY LAYER DATA, FLT 230

Time 09:01:29,000 09:01:29,500 09:01:35,500 09:01:36,500 09:01:37,500

Camber 0/3

QINF = 433.7

MINF = 0,733

ALPT = 3.01

BETA = 0.72

H = 15871.

TINF = 9.5

RNPU = 3.2E+06

PSUR = 1137.4

MTOP = 0.75

Y.in. U/LrrOP W/UTOP

0.240 0.6305 -0.2238

0.470 0.7602 -0.0626

0,970 0.9059 0.0999

1,470 0.9783 -0.1464

1,960 1.0005 -0.1942

2,330 0.9725 -0.1282

2,990 0.9781 -0.1930

3.490 0.9856 -0.1089

3.990 0.9966 -0.1138

4.960 1.0000 -0.0690

Camber 0/3

QINF = 436.9

MINF = 0.715

ALPT = 3.06

BETA -- 0.74

H = 14469.

TINF = 11.3

RNPU = 3.3E+06

PSUR = 1137.4

MTOP = 0.75

U/UTOP W/UTOP

0.6343 -0.1947

0.7677 -0.0582

0.9116 0.1034

0.9840 -0.1540

1.0045 -0.1924

0.9770 -0.1228

0.9820 -0.1924

0.9904 -0.1082

1.0062 -0.0970

1.0000 -0,0681

Camber 1/3

QINF = 449.3

MINF = 0,746

ALPT = 4.19

BETA = 0.63

H = 15865.

TINF = 8.5

RNPU = 3.3E+06

PSUR = 113t.8

MTOP = 0.77

U/UTOP W/UTOP

0.6040 -0.2130

0.7318 -0.0838

0.8863 0.0827

0.9788 -0.1705

1.0085 -0.1974

0.9801 -0.1485

0.9857 -0.2011

0.9940 -0.1391

1.0136 -0.1450

1.0000 -0.0871

Camber 1/3

QINF = 452.8

MINF = 0,749

ALPT = 4.23

BETA = 0.66

H = 15847.

TINF = 8.6

RNPU = 3.3E+06

PSUR = 1131.8

MTOP = 0.77

U/UTOP W/UTOP

0.6094 -0.2380

0.7401 -0.0806

0.8851 0.0806

0.9775 -0.1744

1.0096 -0.2055

0.9803 -0.1491

0.9866 -0.2073

0.9943 -0.1440

1.0038 -0.1513

1.0000 -0.0878

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5987

0.7254

0.8796

0.9803

1.0047

0.9778

0.9833

0.9903

1.0079

1.0000

1/3

456.3

0,751

4.24

0.63

15828.

8.9

3.3E+06

1131.8

0.77

W/UTOP

-0.2466

-0.0843

0.0789

-0.1754

-0.2102

-0.1507

-0.2085

-0.1517

-0.1453

-0.0873

838
TableK-2.Continued.

F11 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 09:01:39,000 09:01:39.500 09:01:41.500 09:04:26.500 09:04:27.000

Camber 1/3

QINF -- 463.8

MINF = 0,757

ALPT = 4.24

BETA = 0.63

H = 15803.

TINF = 8.8

RNPU = 3.3E+06

PSUR = 1131.8

MTOP = 0.78

Y, in. U/UTOP W/UTOP

0.240 0.5982 -0.2540

0,470 0.7256 -0.0828

0.970 0.8814 0.0799

1.470 0.9744 -0,1715

1.960 1.0063 -0.2040

2.330 0.9772 -0.1479

2.990 0.9840 -0.2100

3,490 0.9886 -0.1410

3.990 1.0001 -0.1361

4.960 1.0000 -0.0850

Camber 1/3

QINF = 465.3

MINF = 0,758

ALPT = 4.24

BETA = 0.57

H = 15793.

TINF = 8,7

RNPU = 3.4E+06

PSUR = 1131.8

MTOP = 0.78

U/UTOP W/UTOP

0.5997 -0.2354

0.7296 -0.0867

0,8796 0,0798

0.9738 -0.1728

1.0047 -0.2065

0.9765 -0.1462

0.9829 -0.2092

0.9896 -0.12 l 3

1.0001 -0.1381

1.0000 -0.0861

Camber 1/3

QINF = 472.7

MINF= 0.764

ALPT= 4.21

BETA = 1.29

H = 15757.

TINF = 8.7

RNPU = 3.4E+06

PSUR = 1132.9

MTOP = 0.79

U/UTOP W/UTOP

0.6070 -0.2254

0.7345 -0.0980

0.8798 0.0770

0.9772 -0.1791

1.0039 -0.2125

0.9793 -0.1549

0.9875 -0.2169

0.9956 -0.1826

1.0010 -0.1522

1,0000 -0.0949

Camber 1/4/3/3

QINF = 478.5

MINF = 0.767

ALPT = 4.97

BETA = 1.90

H = 1565 I.

TINF= 9.7

RNPU = 3.4E+06

PSUR = 1133.9

MTOP = 0,80

U/UTOP W/UTOP

0.5910 -0,2746

0,7079 -0.1208

0.8564 0.0549

0.9665 -0.2069

1.0018 -0.2292

0.9760 -0.1860

0.9838 -0.2371

0.9902 -0.2006

0.9988 -0.1731

1.0000 -0.1173

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5953

0.7123

0.8559

0.9683

1.0013

0.9768

0,9841

0.9907

0.9984

1.0000

1/4/3/3

477.8

0.766

4,94

1.53

15673.

10.0

3.4E+06

1133.9

0.80

W/UTOP

-0.2848

-0.1039

0.0579

-0.2024

-0.2225

-0.1822

-0.2323

-0.1943

-0.1737

-0,1144

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 09:04:27.500 09:04:35,000 09:04:35.500 09:04:36.000 09:07:50.000

Camber 1/4/3/3

QINF = 477,8

MINF = 0,767

ALPT = 5.00

BETA = 1,47

H = 15684,

TINF = 9.7

RNPU = 3.4E+06

PSUR = 1130.6

MTOP = 0.80

Win. U/UTOP W/UTOP

0,240 0.5727 -0.2684

0.470 0.6958 -0.1093

0.970 0,8456 0.0503

1,470 0.9527 -0.2050

1.960 0.9968 -0.2256

2,330 0.9709 -0.1773

2.990 0.9777 -0,2317

3.490 0.9829 -0.1874

3.990 0.9924 -0.1727

4.960 1.0000 -0.1090

Cam ber 1/4/5/5

QINF = 449.9

MINF = 0.747

ALPT = 4.91

BETA = 0.40

H = 15866.

TINF = 8.8

RNPU = 3.3E+06

PSUR= 1112.1

MTOP = O,79

U/UTOP W/UTOP

0.5353 -0,3008

0,6752 -0,0686

0.8528 0.0627

0.9659 -0.1948

1.0084 -0.2098

0.9792 -0.1607

0.9838 -0.2171

0.9950 -0.1598

1,0041 -0,1570

1.0000 -0.0986

Camber 1/4_/5

QINF = 450.4

MINF = 0.747

ALPT= 5.16

BETA = -0.65

H = 15878,

TINF = 8.7

RNPU = 3.3E+06

PSUR = 1120.8

MTOP = 0.78

U/UTOP W/UTOP

0.5256 -0.2530

0.6589 -0.0657

0.8394 0,0624

0.9639 -0.1770

1.0051 -0.2045

0.9783 -0.1546

0.9844 -0.2085

0.9932 -0.1506

1.0061 -0.1528

1,0000 -0.0893

Camber 1/4/5/5

QINF = 451.3

MINF = 0.748

ALPT = 4.96

BETA = -1.11

H = 15890.

TINF = 8.6

RNPU = 3.3E+06

PSUR = 1116.5

MTOP = 0.78

U/UTOP W/UTOP

0.5305 -0.2554

0.6697 -0.0538

0.8475 0.0682

0.9587 -0.1686

1.0042 -0.1968

0.9784 -0.1411

0.9834 -0,1945

0,9920 -0.1317

0.9995 -0.1350

1.0000 -0.0784

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5704

0.7020

0,8703

0.9661

1,0010

0,9756

0.9801

0.9808

0.9937

1.0000

0/3/4/4

519.0

0.788

4.12

0.08

15035.

10.5

3.6E+06

1165.3

0.81

W/UTOP

-0.2292

-0,0852

0.0896

-0.1599

-0.2070

-0.1436

-0.1962

-0.1521

-0.1278

-0.0811

839
TableK-2.Continued.

FI I 1/MAW BOUNDARY LAYER DATA, FLT 230

Time 09:07:50.500 09:07:51.000 09:07:56.500 09:07:57,000 09:08:17.500

Camber 0131414

QINF = 519.9

MINF = 0.789

ALPT = 4.13

BETA = -0.38

H = 15047.

TINF = 10.8

RNPU = 3.6E+06

PSUR = 1166.4

MTOP = 0.81

Y, in. U/UTOP W/UTOP

0.240 0.5705 -0.2130

0.470 0.7018 -0.0719

0,970 0.8708 0.0914

1.470 0.9661 -0.1503

1.960 1.0000 -0.2013

2.330 0.9735 -0.1347

2.990 0.9793 -0.1898

3.490 0.9833 -0.1343

3.990 0.9984 -0.1268

4.960 1.0000 -0.0739

Camber 0131414

QINF = 520.8

MINF = 0.790

ALPT = 4.22

BETA = -0.62

H = 15048.

TINF= 10.3

RNPU = 3.6E+06

PSUR = 1167.5

MTOP = 0.81

U/UTOP W/UTOP

0.5657 -0.2057

0.7035 -0.0705

0.8727 0.0932

0.9667 -0.1434

1.0000 -0.1998

0.9723 -0.1339

0.9779 -0.1900

0.9855 -0.1235

0.9988 -0.1233

1.0000 -0.0689

Camber 2/5/4/5

QINF = 523.9

MINF = 0.792

ALPT = 6.69

BETA = 0.45

H = 15029.

TINF -- 10.4

RNPU = 3.6E+06

PSUR = 1114.5

MTOP = 0.86

U/UTOP W/UTOP

0.6091 -0.3252

0.6862 -0.1412

0.8093 0.0028

0.9198 -0.2253

0.9793 -0.2317

0.9784 -0.2063

0.9864 -0.2490

0.9894 -0.2355

1.0019 -0.2066

1.00(_ -0.1356

Camber 2/5

QINF = 523.0

MINF = 0.791

ALPT = 6.75

BETA = 0.63

H = 15028.

TINF= 10.8

RNPU = 3.6E+06

PSUR = 1100.2

MTOP = 0.87

U/UTOP W/UTOP

0.6223 -0.3168

0.7081 -0.1449

0.8140 0.0032

0.9166 -0.2200

0.9781 -0.2182

0.9785 -0.2079

0.9874 -0.2436

0.9922 -0.2298

1.0004 -0.2047

1.0000 -0.1382

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP =

U/LrrOP

0.5781

0.7278

0.8694

0.9911

1.0271

0.9920

0.9977

1.0184

1.0010

1.0000

3/5/516

253.6

0.595

6.13

0.69

18739.

0.2

2.4E+06

991.9

0.63

W/UTOP

-0.4771

-0.0210

0.0313

-0.2196

-0.2012

-0.1905

-0.2561

-0.1472

-0.1836

-0.1232

F11 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 09:08:18.000 09:08:18.500 09:08:19.000 09:08:28.000 09:08:28.500

Camber 3/5

QINF = 247.2

MINF = 0.589

ALPT = 6.07

BETA = 0.43

H = 18898.

TINF = -0.6

RNPU = 2.4E+06

PSUR = 990.9

MTOP = 0.62

Y, in. U/LrI'OP W/UTOP

0.240 0.5669 -0.3570

0.470 0.6992 0.0012

0.970 0.8680 0.0335

1.470 0.9872 -0.2252

1.960 1.0218 -0.1986

2.330 0.9928 -0.1837

2.990 0.9954 -0.2645

3.490 1.0221 -0.1770

3.990 0.9948 -0.1812

4.960 1.0000 -0.1110

Camber 3/5

QINF = 240.9

MINF = 0.583

ALPT = 6.02

BETA = 0.22

H = 19058.

TINF = - 1.1

RNPU = 2.3E+06

PSUR = 984.4

MTOP = 0.61

U/UTOP W/UTOP

0.6063 -0.4600

0.7399 -0.0186

0.8823 0.0402

0.9976 -0.2302

1.0370 -0.1960

1.0000 -0.1709

1.0071 -0.2642

1.0313 -0.1143

1.0102 -0.1988

1.0000 -0.1097

Camber 3/5

QINF = 234.6

M1NF = 0.578

ALPT = 5.67

BETA = 0.22

H = 19218.

TINF = - 1.9

RNPU = 2.3E+06

PSUR = 982.2

MTOP = 0.60

U/UTOP W/UTOP

0.6189 -0.4531

0.7584 -0.0139

0.8952 0.0550

1.0001 -0.2048

1.0383 -0.1867

1.0031 -0.1561

1.0091 -0.2349

1.0333 -0.1013

1.0054 -0.1641

1.0000 -0.0979

Camber 2/4

QINF= 161.3

MINF = 0.500

ALPT = 5.12

BETA = 0.57

H = 21301.

T1NF= -10.8

RNPU = 1.9E+06

PSUR = 906.0

MTOP = 0.52

U/UTOP W/UTOP

0.7175 -0.5752

0.8226 0.0704

0.9624 0.0869

1.0499 -0.2300

1.0757 -0.1664

1.0194 -0.1397

1.0277 -0.2724

1.0626 -0.1048

1.0041 -0.1308

1,0000 -0.0888

Camber

QINF =

MINF =

ALPT =

BETA=

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.7200

0.8403

0.9680

1.0526

1.0795

1.0317

1.0398

1.0730

1.0119

1.0000

2/4

159.4

0,498

5.19

0.54

21366.

-11.0

1.9E+06

903.8

0.51

W/UTOP

-0.5593

0.0746

0.0849

-0.2512

-0.1669

-0.1397

-0.2673

-0.0416

-0,1391

-0.0945

840
TableK-2.Continued.

Time 09:08:29.000

Camber 2/4/4/5

QINF = 157.6

MINF = 0.496

ALPT = 5.17

BETA = 0.40

H = 21431.

T1NF= -11.1

RNPU = 1.8E+06

PSUR -- 899.4

MTOP = 0.51

Y,in. U/UTOP W/UTOP

0.240 0.5757 0.3162

0.470 0.8430 0.064.0

0.970 0.9834 0.0833

1.470 1.0571 -0.2756

1.960 1.0892 -0.1682

2.330 1.0343 -0.1211

2.990 1.0315 -0.2924

3.490 1.0627 -0.0541

3.990 1.0110 -0.1495

4.960 1 .IX)IX) -0.0897

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 230

09:08:29.500

Camber 2/4/4/5

QINF = 155.8

MINF = 0.494

ALPT = 5.14

BETA = 0.25

H = 21495.

TINF = -11.7

RNPU = 1.8E+06

PSUR = 896.1

MTOP = 0.51

U/LrrOP W/UTOP

0.7148 -0.5552

0.8376 0.1067

0.9698 0.0865

1.0458 -0.2334

1.0759 -0.1643

1.0320 -0.1270

1.0274 -0.2680

1.0594 -0.0456

1.0293 -0.1276

1.0000 -0.0967

09:08:30.000

Camber 2/4

QINF = 154.1

MINF = 0.492

ALPT = 5.18

BETA = 0.22

H = 21560.

TINF = -12.2

RNPU = 1.8E+06

PSUR = 898.3

MTOP = 0.51

U/UTOP W/UTOP

0.5236 0.4605

0.8137 0.0572

0.9590 0.0871

1.0333 -0.2418

1.0805 -0.1571

1.0122 -0.1340

1.0177 -0.2659

1.0394 -0.0224

0.9853 -0.1162

1.0000 -0.0702

09:08:34.000

Camber 2/5

QINF = 147.5

MINF = 0.484

ALPT = 5.54

BETA = 0.66

H = 21863.

T1NF = - 13.7

RNPU = 1.8E+06

PSUR = 881.9

MTOP = 0.50

U/UTOP W/UTOP

0.7714 0.4710

0.8459 0.0870

0.9649 0.0776

1.0697 -0.2346

1.0803 -0.1691

1.0379 -0.1337

1.0371 -0.2968

1.0726 -0.0600

1.0487 -0.1687

1.0000 -0.0942

09:08:34.500

Camber 2/5

QINF = 147.4

MINF= 0.484

ALPT = 5.53

BETA = 0.69

H = 21885.

TINF = -14.1

RNPU = 1.8E+06

PSUR = 880.8

MTOP = 0.51

U/UTOP W/UTOP

0.5100 0.4868

0.8306 0.0712

0.9643 0.0747

1.0471 -0.2634

1.0795 -0.1707

1.0373 -0.1357

1.0346 -0.3011

1.0626 -0.0802

0.9853 -0.1453

1.0000 -0.1005

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 09:08:35.000 09:08:35.500 09:11:18.000 09:11:18.500 09:11:19.000

Camber 2/5

QINF = 147.4

MINF = 0.484

ALPT = 5.49

BETA = 0.74

H = 21896.

TINF= -14.1

RNPU = 1.8E+06

PSUR = 880.8

MTOP = 0.51

Y,in. U/UTOP W/UTOP

0.240 0.7729 0.4719

0.470 0.8161 0.0777

0.970 0.9646 0.0776

1.470 1.0536 -0.2518

1.960 1.0795 -0.1707

2.330 1.0373 -0.1357

2.990 1.0367 -0.2973

3.490 1.0677 -0.0837

3.990 1.0001 -0.1521

4.960 1.0000 -0.1005

Camber 2/5

QINF = 147.5

MINF = 0.485

ALPT = 5.54

BETA = 0.83

H= 21919.

TINF= -13.8

RNPU = 1.8E+06

PSUR = 883.0

MTOP = 0.51

U/UTOP W/UTOP

0.6812 -0.5232

0.7993 0.0761

0.9471 0.0696

1.0415 -0.2506

1.0773 -0.1517

1.0202 -0.1334

1.0071 -0.2869

1.0503 -0.0772

0.9831 -0.1495

1.0000 -0.0844

Camber 2/5/5/- 1

QINF = 524.5

MINF= 0.791

ALPT = 7.33

BETA = 0.25

H = 14951.

TINF = 10.5

RNPU = 3.6E+06

PSUR = 1134.2

MTOP = 0.83

U/UTOP W/UTOP

0.7044 -0.3403

0.7812 -0.2461

0.7948 -0.0218

0.8673 -0.2642

0.8715 -0.2678

0.9024 -0.3426

0.9363 -0.3123

0.9670 -0.3477

0.9906 -0.3063

1.00130 -0.1951

Camber 2/5/5/- 1

QINF = 523.2

MINF = 0.790

ALPT = 7.01

BETA = 0.31

H = 14961.

TINF = 10.6

RNPU = 3.6E+06

PSUR = 1133.1

MTOP = 0.83

U/UTOP W/UTOP

0.7049 -0.3218

0.7816 -0.2415

0.7854 -0.0164

0.8389 -0.2663

0.8459 -0.2523

0.8738 -0.2941

0.9176 -0.3045

0.9612 -0.3247

0.9849 -0.3075

1.0000 -0.1976

Camber

QINF =

MINF=

ALPT

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.7072

0.7849

0.7_7

0.8527

0.8620

0.8784

0.9201

0.9640

0.9_5

1.0000

2/5/5/- 1

521.0

0.789

7.14

0.48

14970.

10.5

3.6E+06

1133.1

0.83

W/UTOP

-0.3380

-0.2388

-0.0162

-0.2668

-0.2584

-0.2935

-0.3139

-0.3670

-0.3067

-0.2029

841
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 09:11:19.500 08:46:19.000 08:46:20.500 08:46:25.500 08:46:26.500

Camber 21515/-1

QINF = 518.6

MINF = 0.787

ALPT = 7.32

BETA = 0.40

H = 14978.

TINF = 10.4

RNPU = 3.6E+06

PSUR = 1127.7

MTOP = 0.83

Y.in. U/UTOP W/UTOP

0.240 0.7032 -0.3293

0.470 0.7791 -0.2373

0.970 0.7907 -0.0239

1.470 0.8458 -0.2682

1.960 0.8478 -0.2629

2.330 0.8781 -0.2906

2.990 0.9212 -0.3119

3.490 0.9655 -0.3274

3.990 0.9955 -0.3086

4.960 1.0000 -0.1968

Camber 0/2

QINF = 596.6

MINF = 0.796

ALPT = 3.98

BETA = 0.51

H = 12014.

TINF = 21.5

RNPU = 4.0E+06

PSUR = 1329.8

MTOP = 0.81

U/UTOP W/UTOP

0.6155 -0.1817

0.7445 -0.0809

0.8874 0.1013

0.9683 -0.1418

0.9951 -0.2034

0.9695 -0.1348

0.9738 -0.1880

0.9805 -0.1494

0.9973 -0.1191

1.0000 -0.0723

Camber 0/2

QINF = 592.6

MINF = 0.793

ALPT -- 4.02

BETA = 0.60

H = 12022.

TINF -- 21.8

RNPU _- 3.9E+06

PSUR = 1328.7

MTOP = 0.81

U/UTOP W/UTOP

0.6180 -0.1841

0.7425 -0.0936

0.8870 0.0963

0.9661 -0.1469

0.9948 -0.2047

0.9666 -0.1406

0.9743 -0.1864

0.9808 -0.1 448

0.9890 -0.1169

1.0000 -0.0771

Camber 0/2

QINF = 588.8

MINF = 0.791

ALPT = 4.06

BETA = 0.43

H = 12052.

TINF = 21.7

RNPU = 3.9E+06

PSUR -- 1324.4

MTOP = 0.81

U/UTOP W/UTOP

0.6230 -0.1891

0.7491 -0.0882

0.8908 0.0979

0.9682 -0.1452

0.9963 -0.2025

0.9704 -0.1371

0.9755 -0.1888

0.9817 -0.1342

0.9988 -0.1206

1.0000 -0.0739

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6247

0.7453

0.8882

0.9692

0.9964

0.9702

0.9752

0.9807

1.0041

1.0000

0/2

588.2

0.791

4.05

0.48

12051.

22.1

3.9E+06

1324.4

0.81

W/UTOP

-0.1998

-0.0909

0.0990

-0.1444

-0.2033

-0.1351

-0.1901

-0.1372

-0.1198

-0.0739

F11 I/MAW BOUNDARY LAYER DATA. FLT 230

Time 08:46:27.500 08:46:44.500 08:46:45.000 08:46:46.500 08:46:48.000

Camber 0/2

QINF = 587.2

MINF = 0.790

ALPT = 4.01

BETA = 0.60

H = 12061.

TINF = 22.6

RNPU = 3.9E+06

PSUR = 1323.3

MTOP = 0.81

Y.in. U/UTOP W/UTOP

0.240 0.6274 -0.2106

0.470 0.7507 -0.0884

0.970 0.8894 0.0974

1.470 0.9686 -0.1452

1.960 0.9959 -0.2046

2.330 0.9706 -0.1379

2.990 0.9759 -0.1893

3.490 0.9828 -0.1287

3.990 0.9960 -0.1198

4.960 1.0000 -0.0759

Camber 5/6

QINF = 608.5

MINF = 0.806

ALPT = 3.52

BETA = 0.28

H = 12149.

TINF = 23.2

RNPU = 4.0E+06

PSUR = 1216.7

MTOP = 0.89

U/UTOP W/UTOP

0.6562 -0.2143

0.7432 -0.1027

0.8126 0.0572

0.8633 -0.1552

0.9067 -0.1684

0.9088 -0.1607

0.9305 -0.2081

0.9498 -0.1704

0.9805 -0.1779

1.0000 -0.1186

Camber 5/6

QINF = 609.5

MINF = 0.807

ALPT = 3.52

BETA = 0.31

H = 12150.

TINF = 23.1

RNPU = 4.0E+06

PSUR = 1206.8

MTOP = 0.90

U/UTOP W/UTOP

0.6661 -0.2092

0.7548 -0.1053

0.8273 0.0611

0.8860 -0.1525

0.9236 -0.1892

0.9175 -0.1469

0.9404 -0.2102

0.9629 -0.1932

0.9874 -0.1696

1.0000 -0.1161

Camber 5/6

QINF = 608.2

MINF -- 0.806

ALPT = 3.53

BETA = 0.22

H = 12148.

TINF= 23.2

RNPU = 4.0E+06

PSUR = 1200.2

MTOP = 0.91

U/UTOP W/UTOP

0.6823 -0.2210

0.7648 -0.1103

0.8290 0.0584

0.8804 -0.1477

0.9144 -0.1767

0.9094 -0.1577

0.9295 -0.2064

0.9487 -0.1923

0.9812 -0.1734

1.0000 -0.1175

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6735

0.7571

0.8293

0.8918

0.9328

0.9170

0.9371

0.9529

0.9844

1.0000

5/6

606.2

0.804

3.53

0.40

12146.

23.4

4.0E+06

1209.0

0.90

W/UTOP

-0.2167

-0.1131

0.0599

-0.1614

-0.1911

-0.1430

-0.2091

-0.1992

-0.1740

-0.1191

842
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:46:49.500 08:46:55.000 08:47:24,000 08:47:32.500 08:48:03.500

Camber 5/6

QINF = 605.2

MINF -- 0.804

ALPT = 3.53

BETA = 0.34

H = 12145.

TINF = 23.1

RNPU = 4.0E+06

PSUR = 1212.3

MTOP = 0.90

Y,in. U/Lrl'OP W/UTOP

0,240 0.6754 -0.2286

0,470 0.7574 -0.1173

0.970 0.8226 0.0539

1.470 0.8766 -0.1626

1.960 0.9102 -0.1844

2.330 0.9067 -0.1641

2.990 0.9292 -0.2115

3.490 0.9505 -0.1905

3.990 0.9833 -0.1766

4.960 1.0000 -0.1200

Camber 5/6

QINF = 602.8

MINF = 0.802

ALPT = 3.53

BETA = 0.40

H = 12154,

TINF = 23.3

RNPU = 3.9E+06

PSUR = 1201.3

MTOP = 0.90

U/UTOP W/UTOP

0.6681 -0.2244

0.7523 -0.1139

0.8209 0.0557

0.8796 -0.1599

0.9162 -0.1844

0.9122 -0.1570

0.9343 -0.2133

0.9577 -0.1841

0.9814 -0.1781

1.0000 -0.1208

Camber 0/2

QINF = 604.6

MINF = 0.805

ALPT = 4.02

BETA = 0.63

H = 12123,

TINF = 21.2

RNPU = 4.0E+06

PSUR = 1323.4

MTOP = 0.82

U/UTOP W/UTOP

0.6202 -0.1848

0.7452 -0.0815

0.8919 0.1050

0.9729 -0.1312

0.9945 -0.2025

0.9685 -0.1330

0.9743 -0.1865

0.9803 -0.1321

0.9981 -0.1189

1.0000 -0.0711

Camber 0/2

QINF = 601.7

MINF= 0,800

ALPT = 4.03

BETA = 0.74

H = 12064.

TINF = 20.2

RNPU = 4.0E+06

PSUR = 1326.6

MTOP = 0.81

U/UTOP W/UTOP

0.6282 -0.1871

0.7490 -0.0896

0.8917 0.1016

0.9658 -0.1468

0.9950 -0.2039

0.9698 -0.1353

0.9749 -0.1910

0.9816 -0.1326

0.9965 -0.1211

1.0000 -0.0738

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6223

0.7441

0.8921

0.9644

0.9948

0.9714

0.9765

0.9789

09993

1.0000

0/2

600.9

0,799

4.02

0.66

12019.

20.7

4.0E+06

1326.6

0.81

W/UTOP

-0.1773

-0.0826

0.1064

-0.1498

-0.2063

-0.1317

-0.1889

-0.1346

-0.1141

-0.0721

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:48:18.000 08:48:18.500 08:48:19,000 08:48:20.000 08:48:27.500

Camber 0/2

QINF = 600.1

MINF = 0.795

ALPT = 5.25

BETA = 1.15

H = 11828.

T1NF = 21.5

RNPU = 4.0E+06

PSUR = 1332.8

MTOP = 0.81

Y, in. U/UTOP W/UTOP

0.240 0.6233 -0.2057

0,470 0.7385 -0.1021

0,970 0.8727 0.0786

1.470 0.9642 -0.1695

1.960 0.9959 -0.2199

2.330 0.9708 -0.1579

2.990 0.9767 -0.2088

3,490 0.9800 -0.1649

3,990 1.0010 -0.1407

4.960 1.0000 -0.0886

Camber _2

QINF= 599.9

MINF = 0,795

ALPT= 4.92

BETA = 0.98

H = 11816.

TINF = 21.6

RNPU = 4.0E+06

PSUR = 1333.9

MTOP = 0.81

U/UTOP W/UTOP

0.6300 -0.2100

0.7451 -0.1049

0.8799 0.0808

0.9665 -0.1630

0.9979 -0.2173

0.9722 -0.1590

0.9789 -0.2071

0.9824 -0.1644

1.0010 -0.1388

1.0000 -0.0895

Camber 0/2

QINF = 599.2

MINF = 0.795

ALPT= 4.84

BETA = 1.01

H = 11816.

TINF = 21.6

RNPU = 4.0E+06

PSUR= 1333.9

MTOP = 0.81

U/UTOP W/UTOP

0.6253 -0.2230

0.7417 -0.1001

0.8759 0.0820

0.9666 -0.1581

0.9960 -0.2146

0.9705 -0.1555

0.9767 -0.2023

0.9804 -0.1575

0.9994 -0.1378

1.0000 -0.0889

Camber 0/2

QINF = 596.9

MINF = 0,793

ALPT = 5.06

BETA = 0.83

H= 11814.

TINF= 21.5

RNPU = 4.0E+06

PSUR = 1332.8

MTOP = 0.81

U/UTOP W/UTOP

0.6257 -0.2065

0.7409 -0.0976

0.8741 0.0764

0.9625 -0.1630

0.9977 -0.2153

0.9718 -0.1552

0.9777 -0.2032

0.9772 -0.1696

1.0004 -0.1371

1.0000 -0.0887

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF=

RNPU =

PSUR =

MTOP =

U/UTOP

0.6141

0.7276

0.8661

0.9563

0.9972

0.9697

0.9756

0.9818

1.0000

1.0000

0/2

573.1

0.783

5.89

0.80

12171.

20.9

3.9E+06

1310.3

0.81

W/UTOP

-0.2199

-0,0961

0.0697

-0,1704

-0.2138

-0.1692

-0.2137

-0.1584

-0.1400

-0.0913

843
Table K-2. Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 230

Time 08:48:28.000 08:48:28,500 08:48:29.000

Camber 0/2

QINF = 570.6

MINF = 0.782

ALPT = 5.98

BETA = 0.95

H = 12213.

TINF = 21.0

RNPU = 3.9E+06

PSUR = 1309.2

MTOP = 0.81

Y, in. U/IYroP W/UTOP

0.240 0.6131 -0.2260

0.470 0.7277 -0.1016

0.970 0.8514 0.0604

1.470 0.9503 -0.1670

1,960 0.9887 -0.2182

2,330 0.9649 -0.1655

2.990 0.9713 -0.2114

3.490 0.9770 -0.1592

3.990 0.9949 -0.1439

4.960 1.0000 -0.0922

Camber 0/2

QINF = 568.2

MINF = 0.781

ALPT = 5.96

BETA = 0.92

H = 12267.

TINF = 20.8

RNPU = 3.9E+06

PSUR = 1309.2

MTOP = 0.80

U/UTOP W/UTOP

0.6157 -0.2223

0.7295 -0.1007

0.8591 0.0646

0.9588 -0.1698

0.9963 -0.2168

0.9711 -0.1669

0.9778 -0.2147

0.9836 -0.1689

0.9992 -0.1447

1.0000 -0.0958

Camber 0/2

QINF = 565.2

MINF = 0.779

ALPT -- 5.86

BETA = 0.74

H = 12320.

TINF = 20.6

RNPU = 3,8E+06

PSUR = 1309.2

MTOP = 0.80

U/UTOP W/UTOP

0.6170 -0.2207

0.7365 -0.0966

0.8630 0.0673

0.9590 -0.1709

0.9990 -0.2167

0.9721 -0.1679

0.9784 -0.2122

0.9833 -0.1450

1.0012 -0.1472

1.0000 -0.0933

FI 1 I/MAW BOUNDARY LAYER DATA, FIT 231

Time 13:03:14.500 13:03:30.000 13:03:31.500 13:03:32.500 13:03:42.000

Camber 0/2

QINF = 601.0

MINF = 0.799

ALPT = 4.01

BETA = 0.48

H = 11996.

TINF = 22.1

RNPU = 4.0E+06

PSUR = 1326.6

MTOP = 0.82

Y,in. U/UTOP WAJTOP

0.240 0.6338 -0.1589

0.470 0.7337 -0.1305

0,970 0.8914 0.0875

1.470 0.9904 -0.1294

1.960 1.0116 -0.1892

2.330 1.0022 -0.1122

2.990 1.0100 -0.1798

3.490 0.9984 -0.1187

3.990 0.9942 -0.1118

4.960 1.0000 -0.0948

Camber 0/2

QINF = 595.6

MINF = 0.795

ALPT = 4.01

BETA = 0.48

H = 12002.

TINF = 22.6

RNPU = 3.9E+06

PSUR = 1329.8

MTOP = 0.81

U/UTOP W/UTOP

0.6337 -0.1659

0.7360 -0.1412

0.8932 0.0882

0.9886 -0.1365

1.0112 -0,1878

1.0024 -0.1081

1.0103 -0.1817

0.9989 -0.1263

0.9992 -0.1086

1.0000 -0.0978

Camber 0/2

QINF = 593.3

MINF = 0.794

ALPT = 4.02

BETA = 0.40

H = 12000.

TINF = 22,5

RNPU = 3.9E+06

PSUR = 1329.8

MTOP = 0.81

U/UTOP W/UTOP

0.6306 -0.1703

0.7370 -0.1332

0.8910 0.0876

0.9878 -0.1375

1.0120 -0.1923

1.0033 -0.1099

1.0110 -0.1804

0.9967 -0.1235

0.9977 -0.1047

1.0000 -0.0956

Camber 0/2

QINF = 593.0

MINF = 0.793

ALP'r= 4.02

BETA = 0.40

H= 12000.

TINF = 22.2

RNPU = 3.9E+06

PSUR = 1327.6

MTOP = 0.81

U/UTOP W/UTOP

0.6322 -0.1595

0.7359 -0.1317

0.8918 0.0872

0.9872 -0.1348

1.0107 -0.1852

0.9997 -0.1084

1.0076 -0.1806

0.9965 -0.1263

0.9960 -0.1069

1.0000 -0.0924

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP --

U/UTOP

0.6394

0.7430

0.9104

0.9906

1.0117

0.9996

1.0060

0.9944

0.9948

1.0000

0/2

597.7

0.796

3.04

0.48

11982.

21.4

4.0E+06

1337.5

0.81

W/UTOP

-0.1492

-0.1109

0.1086

-0.1208

-0.1801

-0.0956

-0.1670

-0.1055

-0.0885

-0.0823

844
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 231

Time 13:03:43.000 13:03:47.000 13:03:47.500 13:03:49.500 13:03:50,000

Camber 0/2

QINF = 597.1

MINF = 0.795

ALPT = 3.02

BETA = 0.48

H -- 11959.

TINF = 21.9

RNPU = 4.0E+06

PSUR -- 1336.4

MTOP = 0.81

Y, in. U/LrrOP W/UTOP

0.240 0.6453 -0.1508

0.470 0.7510 -0.1175

0.970 0.9114 0.1083

1.470 0.9969 -0.1125

1.960 1.0108 -0.1808

2.330 0.9994 -0.0935

2.990 1.0063 -0.1650

3.490 0.9931 -0.1039

3.990 0.9973 -0.0895

4.960 1.0000 -0.0776

Camber 0/2

QINF = 616.0

MINF = 0.804

ALPT = 3.06

BETA = 0.31

H = 11686.

TINF = 24.2

RNPU = 4.0E+06

PSUR = 1354.7

MTOP = 0.82

U/UTOP W/UTOP

0.6375 -0.1392

0.7449 -0.1063

0.9080 0.1089

0.9893 -0.1168

1.0080 -0.1831

0.9966 -0.0917

0.9918 -0.1759

0.9928 -0.1063

0.9940 -0.0887

1.0000 -0.0763

Camber 0/2

QINF = 619.2

MINF = 0.805

ALPT = 3.07

BETA = 0.37

H = 11633.

TINF = 24.0

RNPU = 4.0E+06

PSUR = 1357.8

MTOP = 0.81

U/UTOP W/UTOP

0.6428 -0.1486

0.7513 -0.1112

0.9078 0.1109

0.9924 -0A178

1.0124 -0.1814

1.0007 -0.0913

0.9916 -0.1774

0.9957 -0.1065

0.9998 -0.0873

1.0000 -0.0799

Camber 0/2

QINF = 639.9

MINF = 0.814

ALPT = 5.95

BETA = 0.51

H = 11384.

TINF = 24.8

RNPU = 4.1E+06

PSUR = 1356.4

MTOP = 0.83

U/UTOP W/UTOP

0.6073 -0.1741

0.7056 -0.1663

0.8554 0.0501

0.9691 -0.1648

1.0109 -0.2080

0.9919 -0.1375

0.9804 -0.2345

0.9969 -0.1571

0.9975 -0.1404

1.0000 -0.1179

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6156

0.7084

0.8435

0.9508

1.0038

0.9973

0.9810

0.9967

0.9966

1.0000

0/2

641.8

0.815

6.40

0.40

11330.

25.1

4.1E+06

1357.3

0.83

W/UTOP

-0.1810

-0.1621

0.0488

-0.1707

-0.2107

-0.1427

-0.2382

-0.1670

-0.1495

-0.1275

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 231

Time 13:03:50.500 13:03:51.000 13:03:51.500 13:03:52.000 13:03:52.500

Camber 0/2

QINF= 642.7

MINF= 0.814

ALPT = 6.86

BETA = 0.40

H = 11286.

TINF = 25.8

RNPU = 4.1E+06

PSUR = 1357.2

MTOP = 0.83

Y,in. U/LrFOP W/UTOP

0.240 0.6358 -0.1802

0.470 0.7245 -0.1627

0.970 0.8323 0.0312

1.470 0.9380 -0.1760

1.960 0.9964 -0.2129

2.330 1.0002 -0.1464

2.990 0.9866 -0.2382

3.490 0.9968 -0.1928

3.990 0.9952 -0.1566

4.960 1.0000 -0.1336

Camber 0/2

QINF= 641.4

MINF= 0.813

ALPT = 7.20

BETA = 0.51

H = 11251.

TINF = 26.0

RNPU = 4.1E+06

PSUR = 1360.4

MTOP = 0.82

U/UTOP W/UTOP

0.6518 -0.1865

0.7306 -0.1690

0.8325 0.0291

0.9288 -0.1755

0.9879 -0.2155

1.0005 -0.1530

0.9917 -0.2382

1.0010 -0.1798

0.9987 -0.1558

1.0000 -0.1399

Camber 0/2

QINF = 639.1

MINF = 0.811

ALPT = 7.43

BETA = 0.60

H = 11227.

TINF = 26.3

RNPU = 4.1E+06

PSUR = 1363.5

MTOP = 0.82

U/UTOP W/UTOP

0.6429 -0.1828

0.7272 -0.1627

0.8239 0.0228

0.9149 -0.1758

0.9686 -0.2126

0.9897 -0,1561

1.0055 -0.2148

0.9928 -0.1819

0.9924 -0.1612

1.000t3 -0.1365

Camber 0/2

QINF = 634.6

MINF = O.808

ALPT = 7.69

BETA = 0.57

H = 11223.

TINF = 26.0

RNPU = 4. IE+06

PSUR = 1363.4

MTOP = 0.81

U/UTOP W/UTOP

0.6665 -0.1975

0.7413 -0.1542

0.8213 0.0183

0.9067 -0.1779

0.9584 -0.2119

0.9867 -0.1593

1.0062 -0.2203

0.9941 -0.1902

0.9948 -0.1648

1.00t30 -0.1437

Camber

QINF =

MINF=

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6743

0.7513

0.8265

0.9049

0.9512

0.9817

1.0087

0.9978

0.9903

1.0000

O/2

628.4

0.805

8.08

0.66

I 1239,

26.5

4.1E+06

1359.0

0.80

W/UTOP

-0.1916

-0.1698

0.0118

-0.1857

-0.2111

-0.1646

-0.2199

-0.1874

-0.1698

-0.1446

845
TableK-2.Continued.

FI 11/MAW BOUNDARY LAYER DATA, FLT 231

Time 13:03:54.000 13:03:54,500 13:03:55.000 13:05:56.500 13:06:08.500

Camber 0/2

QINF = 605.2

MINF = 0.792

ALPT = 8.66

BETA = 0.51

H = 11374.

TINF = 26.2

RNPU = 4.0E+06

PSUR = 1346.9

MTOP = 0.78

Y,in. U/UTOP W/U'TOP

0,240 0.6785 -0.1847

0,470 0.7496 -0.1550

0.970 0.8096 0.0022

1.470 0.8832 -0.1739

1.960 0.9235 -0.1938

2.330 0.9503 -0.1581

2.990 0.9877 -0.2149

3.490 0.9935 -0.1890

3.990 0.9967 -0.1644

4.960 1.0000 .0.1407

Camber 0/2

Q1NF = 5%.6

MINF -- 0.787

ALPT = 8.59

BETA = 0.60

H = 11455.

TINF = 26.1

RNPU = 4.0E+06

PSUR = 1343.8

MTOP = 0.78

U/UTOP W/UTOP

0.6798 -0.1794

0.7455 -0.1659

0.8106 0.0005

0.8887 -0.1689

0.9240 -0.2019

0.9517 -0.1561

0.9879 -0.2139

0.9957 -0.1904

1.0012 -0.1623

1.0000 -0.1447

Camber 0/2

QINF = 587.0

MINF = 0.782

ALPT = 8.75

BETA = 0.51

H = 11547.

TINF = 25.7

RNPU = 3.9E+06

PSUR = 1337.3

MTOP = 0.77

U/UTOP W/UTOP

0.6755 -0.1845

0.7436 -0.1495

0.8090 -0.0027

0.8800 -0.1760

0.9213 -0.1997

0.9478 .0.1569

0.9848 -0.2128

0.9907 -0.1886

0.9996 -0.1631

1.0000 -0.1423

Camber 0/3

QINF = 599.7

MINF = 0.801

ALPT = 3.98

BETA = 0.37

H = 12185.

TINF= 22.2

RNPU = 3.9E+06

PSUR = 1312.5

MTOP = 0.82

U/UTOP W/UTOP

0.6020 -0.1722

0.7117 -0.1449

0.8797 0.0842

0.9869 -0.1527

1.0133 -0.1963

1.0032 -0.1188

1.0100 -0.1837

0.9971 -0.1358

1.0012 -0.1166

1.0000 -0.1035

Camber

Q1NF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU --

PSUR =

MTOP --

U/UTOP

0.6064

0.7099

0.8758

0.9852

1.0116

0.9977

1.0056

0.9968

0.9973

1.0000

0/3

604.7

0,804

3.98

0.34

12179.

21.7

4.0E+06

1314.7

0.82

W/UTOP

-0.1641

-0.1418

0,0811

-0.1490

-0.1944

-0.1192

-0.1888

-0.1345

-0.1174

-0.1018

F11 I/MAW BOUNDARY LAYER DATA, FLT 231

Time 13:06:22.000 13:06:58.000 13:06:59.500 13:07:01,000 13:07:02.500

Camber 0/3

QINF = 600.1

MINF = 0.801

ALPT = 3.98

BETA = 0.45

H = 12174.

TINF = 22.2

RNPU = 4.0E+06

PSUR = 1313.6

MTOP = 0.82

Y, in. U/UTOP W/UTOP

0,240 0.5995 -0.1715

0.470 0.7049 -0.1426

0.970 0.8797 0.0810

1.470 0.9852 -0.1473

1.960 1.0131 -0.1956

2.330 0.9985 -0.1164

2,990 1.0093 -0.1879

3,490 0.9958 .0.1347

3,990 0.9999 -0.1124

4.960 1.0000 -0.1037

Camber 0/2

QINF = 598.8

MINF = 0.800

ALPT = 3.01

BETA = 0.40

H = 12173.

TINF = 22.0

RNPU = 3.9E+06

PSUR = 1325.6

MTOP = 0.81

U/UTOP W/UTOP

0.6367 .0.1517

0.7414 -0.1161

0.9099 0.1062

0.9952 -0.1222

1.0144 -0.1828

1.0025 -0.0962

1.0095 -0.1674

0.9947 -0.1087

1.0002 -0.0935

1.0000 -0.0818

Camber 0/2

QINF = 602.6

MINF = 0.801

ALPT = 3.03

BETA = 0.45

H= 12110.

TINF = 22.4

RNPU = 4.0E+06

PSUR = 1328.9

MTOP = 0.81

U/UTOP W/UTOP

0.6378 .0.1500

0.7465 .0.1127

0.9124 0.1069

0.9912 -0.1224

1.0122 .0.1852

0.9999 -0.0956

1.0064 -0.1690

0.9%2 .0.1044

0.9942 -0.0933

1.0000 -0.0792

Camber 0/2

QINF = 613.2

MINF = 0.807

ALPT = 3.03

BETA = 0.57

H = 12030.

TINF = 23.0

RNPU = 4.0E+06

PSUR = 1335.4

MTOP = 0.81

U/UTOP W/UTOP

0.6394 -0.1552

0.7477 -0.1104

0.9148 0.1091

0.9983 -0.1240

1.0203 -0.1852

1.0070 -0.0953

1.0035 -0.1798

1.0040 -0.1234

0.9965 -0.0960

1.0000 .0.0858

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.6329

0.7331

0.9002

0.9901

1.0119

1.0004

0.9878

0.9975

0.9971

1.0000

0/2

624.8

0.813

3.46

0.45

11907.

23.3

4.0E+06

1339.7

0.82

W/UTOP

-0.1482

-0.1174

0.1048

-0.1273

-0.1859

-0.0968

-0.1928

-0.1128

-0.0989

-0.0840

846
TableK-2.Continued.

FI 1 I/MAW BOUNDARY LAYER DATA, FLT 231

Time 13:07:03.000 13:07:04.000 13:07:04.500 13:07:06.000 13:07:06.500

Camber 0/2

QINF = 628.7

M1NF = 0.815

ALPT = 3.95

BETA = 0.40

H = I 1855.

TINF = 23.0

RNPU = 4.1E+06

PSUR = 1337.3

MTOP = 0.83

Y, in. U/LrrOP W/LrTOP

0.240 0.6271 43.1549

0.470 0.7304 -0.1400

0.970 0.8914 0.0910

1.470 0.9938 -0.1364

1.960 1.0143 -0.1912

2.330 0.9979 43.1086

2.990 0.9852 -0.2033

3,490 0.9956 43.1154

3.990 0.9993 -0.1056

4.960 1.0000 43.0944

Camber 0/3

QINF = 635.2

MINF = 0.817

ALPT = 5.04

BETA = 0.37

H = 11749.

TINF = 23.4

RNPU = 4.1E+06

PSUR = 1334.9

MTOP = 0.84

U/UTOP W/UTOP

0.5823 -0.1753

0.6861 -0.1616

0.8525 0.0628

0.9770 -0.1651

1.0134 -0.2072

0.9926 -0.1382

0.9824 -0.2293

0.9985 -0.1553

0.9988 -0.1374

1.0000 -0.1175

Camber 0/3

QINF = 637.1

MINF= 0.818

ALPT = 5.50

BETA = 0.48

H = 11706.

TINF = 23.6

RNPU = 4.1E+06

PSUR = 1331.5

MTOP = 0.84

U/UTOP W/UTOP

0.5543 -0.1879

0.6546 -0.1779

0.8280 0.0481

0.9687 -0.1795

1.0165 -0.2149

1.0029 -0.1436

0.9877 -0.2442

0.9999 -0.1731

0.9980 -0.1566

1.0000 -0.1276

Camber 1/4

QINF = 634.7

MINF= 0,815

ALPT = 6.39

BETA = 0.37

H= 11614.

TINF = 24.4

RNPU = 4.1E+06

PSUR = 1268.5

MTOP -- 0.89

U/UTOP W/UTOP

0.6360 43.2423

0.7081 -0.2109

0.8135 0.0043

0.9247 -0.1993

0.9801 -0.2223

0.9941 -0.1710

0.9896 -0.2585

0.9969 -0.2199

0.9986 -0.1957

1.0000 -0.1611

Camber

QINF =

MINF=

ALPT =

BETA --

H=

TINF =

RNPU --

PSUR =

MTOP =

U/UTOP

0.6784

0.7454

0.8230

0.9101

0,9581

0.9767

0.9989

0.9911

0.9927

1.0000

1/4

632.0

0.813

6.62

0.34

11600.

24.0

4.1E+06

1240.8

0.91

W/UTOP

-0.2457

43.2138

43.0111

-0.1997

43.2121

-0A893

-0.2333

-0.2277

-0.2079

-0.1726

FI 11/MAW BOUNDARY LAYER DATA, FLT 231

Time 13:07:09.000 13:07:09.500 13:07:10,500 13:07:11.500 13:08:43.500

Camber 2/5

QINF = 608.7

MINF= 0,800

ALPT = 7.01

BETA = 0.37

H = 11769.

TINF = 23.6

RNPU = 4.0E+06

PSUR = 1207.8

MTOP = 0.91

Y, in. U/UTOP W/UTOP

0,240 0.6956 -0.2340

0.470 0.7547 -0.2021

0,970 0.8000 -0.0350

1.470 0.8708 43.1953

1,960 0.9006 -0.2103

2.330 0.9338 -0.1818

2.990 0.9599 -0.2319

3.490 0.9650 -0.2407

3.990 0.9829 -0.2207

4,960 1.0000 -0.1859

Camber 2/5

QINF = 600.8

MINF = 0.796

ALPT = 7.04

BETA = 0.40

H = 11839.

TINF = 23.5

RNPU = 4.0E+06

PSUR = 1188.2

MTOP = 0,91

U/UTOP W/UTOP

0.7050 -0.2282

0.7609 -0.1988

0.7925 -0.0405

0.8527 -0.1838

0.8745 -0.2013

0.9142 -0.1957

0.9469 -0.2170

0.9570 -0.2289

0.9799 -0.2001

1.0000 -0.1810

Camber 2/5

QINF = 581.0

M1NF = 0.786

ALPT = 6.92

BETA = 0.37

H = 12022.

TINF = 22.5

RNPU = 3.9E+06

PSUR = 1203.8

MTOP = 0.89

U/UTOP W/UTOP

0.7007 -0.2442

0.7632 -0.2163

0.8110 -0.0372

0.8907 -0.2085

0.9171 -0,2251

0.9453 -0.1817

0.9695 -0.2313

0.9722 -0,2536

0.9828 -0.2302

1.0000 43.1860

Camber 2/5

QINF = 557.5

MINF = 0.773

ALPT = 5.05

BETA = 0.34

H = 12268.

T1NF= 22.1

RNPU = 3.8E+06

PSUR = 1273.8

MTOP = 0.82

U/UTOP W/UTOP

0.5069 -0,2126

0.6155 -0.2051

0.7996 0.0294

0.9592 -0.1943

1.0090 -0.2205

0.9994 -0.1549

1.0083 -0.2198

0.9960 43.2031

0.9954 -0.1749

1.0000 -0.1509

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5944

0.7010

0.8793

0.9833

1.0098

0.9986

1.0018

0.9942

0.9957

1.0000

0/3

609.1

0.805

3.91

0.02

12071.

21.9

4.0E+06

1315.8

0.83

W/UTOP

-0.1617

-0.1414

0.0874

-0.1421

-0.1899

-0.1090

-0.1829

-0.1235

-0.1116

-0.0912

847
TableK-2.Concluded.

F11 I/MAW BOUNDARY LAYER DATA, FLT 231

Time 13:08:44.000 13:08:44.500 13:08:45.000 13:08:47.000 13:08:47.500

Camber 0/3

QINF = 609.4

MINF = 0.805

ALPT = 3.99

BETA = -0.01

H = 12060.

TINF = 21.9

RNPU = 4.0E+06

PSUR = 1318.9

MTOP = 0.83

Y, in. U/UTOP W/UTOP

0.240 0.5951 -0.1660

0.470 0.7021 -0.1347

0.970 0.8766 0.0858

1.470 0.9860 -0.1407

1.960 1.0123 -0.1924

2.330 0.9995 -0.1111

2.990 1.0022 -0.1884

3.490 0.9963 -0.1269

3.990 0.9987 -0.1092

4.960 1.0000 -0.0955

Camber 0/3

QINF= 610.1

MINF = 0.806

ALPT = 3.95

BETA = -0.04

H= 12061.

T1NF = 21.8

RNPU = 4.0E+06

PSUR = 1318.9

MTOP = 0.83

U/UTOP W/UTOP

0.5942 -0.1699

0.7037 -0.1438

0.8769 0.0850

0.9847 -0.1427

1.0126 -0.1926

1.0010 -0.1108

1.0027 -0.1888

0.9976 -0.1245

1.0004 -0.1086

1.0000 -0.0991

Camber 0/3

QINF = 610.8

MINF = 0.806

ALPT = 4.07

BETA = -0.04

H = 12050.

TINF -- 21.8

RNPU : 4.0E+06

PSUR = 1317.8

MTOP = 0.83

U/UTOP W/UTOP

0.5862 -0.1561

0.6990 -0.1414

0.8755 0.0824

0.9866 -0.1441

1.0123 -0.1927

1.0010 -0.1124

1.0015 -0.1889

0.9946 -0.1292

0.9969 -0.1134

1.0000 -0.0965

Camber 0/3

QINF = 613.3

MINF = 0.807

ALPT = 4.66

BETA = -0.04

H = 12019.

TINF = 21.7

RNPU = 4.0E+06

PSUR = 1312.3

MTOP = 0.83

U/UTOP W/UTOP

0.5657 -0.1758

0.6719 -0.1589

0.8506 0.0647

0.9787 -0.1638

1.0148 -0.2049

1.0034 -0.1307

1.0047 -0.2054

0.9986 -0.1555

0.9990 -0.1336

1.0000 -0.1157

Camber

QINF =

MINF =

ALPT =

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5637

0.6706

0.8492

0.9777

1.0146

1.0029

1.0047

0.9986

0.9978

1.0000

0/3

613.3

0.807

4.85

-0.10

12008.

22.0

4.0E+06

1310.0

0.83

W/UTOP

-0.1765

-0.1675

0.0612

-0.1636

-0.2046

-0.1326

-0.2062

-0.1568

-0.1353

-0.1170

F11 I/MAW BOUNDARY LAYER DATA, FLT 231

Time 13:08:48.000 13:08:49.500 13:08:50.500 13:09:02.000 t 3:09:02.500

Camber 0/3

QINF = 613.0

MINF = 0.807

ALPT = 5.16

BETA = 0.05

H = 11996.

TINF = 22.1

RNPU = 4.0E+06

PSUR = 1312.1

MTOP = 0.84

Y, in. U/UTOP W/UTOP

0.240 0.5570 -0.1772

0.470 0.6582 -0.1711

0.970 0.8387 0.0525

1.470 0.9707 -0.1698

1.960 1.0118 -0.2107

2.330 0.9989 -0.1383

2.990 1.0018 -0.2072

3.490 0.9957 -0.1722

3.990 0.9924 -0.1457

4.960 1.0000 -0.1141

Camber 1/4

QINF = 611.4

MINI: = 0.805

ALPT = 5.86

BETA -- -0.07

H = 1 t961.

TINF = 22.3

RNPU = 4.0E+06

PSUR = 1237.1

MTOP -- 0.90

U/UTOP W/UTOP

0.6379 -0.2534

0.7074 -0.2129

0.8214 0.0133

0.9424 -0.1917

0.9966 -0.2159

0.9964 -0.1591

1.0068 -0.2218

0.9973 -0.2090

0.9985 -0.1771

1.0000 -0.1514

Camber 1/4

QINF = 610.5

MINF = 0.804

ALPT = 6.04

BETA = -0.24

H = 11949.

TINF = 22.7

RNPU = 4.0E+06

PSUR = 1248.1

MTOP = 0.89

U/UTOP W/UTOP

0.6201 -0.2398

0.6840 -0.2071

0.8062 0.0073

0.9336 -0.1885

0.9902 -0.2198

0.9898 -0.1585

1.0017 -0.2230

0.9916 -0.2060

0.9951 -0.1721

1.0000 -0.1495

Camber 1/4

QINF = 628.9

MINF= 0.801

ALPT = 5.09

BETA = 0.60

H = 10960.

TINF = 25.0

RNPU = 4.1E+06

PSUR = 1362.0

MTOP = 0.83

U/UTOP W/UTOP

0.5455 -0.1963

0.6542 -0.1881

0.8318 0.0454

0.9726 -0.1837

1.0150 -0.2166

1.0021 -0.1487

0.9992 -0.2282

0.9995 -0.1779

0.9983 -0.1580

1.0000 -0.1332

Camber

QINF =

MINF =

ALP'I" --

BETA =

H=

TINF =

RNPU =

PSUR =

MTOP =

U/UTOP

0.5500

0.6546

0.8374

0.9761

1.0146

1.0016

0.9978

0.9975

0.9974

1.0000

1/4

629.4

0.800

4.77

0.37

10927.

25.0

4.1E+06

1365.3

0.83

W/UTOP

-0.1833

-0.1795

0.0536

-0.1770

-0.2141

-0.1442

-0.2212

-0.1700

-0.1513

-0.1277

848
REFERENCES

I Painter, Weneth D. and Lawrence J. Caw, Design and Physical Characteristics of the Transonic Aircraft

Technology (TACT) Research Aircraft, NASA-TM-56048, Jan. 1979.

2 Symposium on Transonic Aircraft Technology (TACT). AFFDL-TR-78-100, Aug. 1978.

3Supercritical Wing Technology: A Progress Report on Flight Evaluations, NASA-SP-301, Feb. 1972.

4 Ayers, Theodore G. and James B. Hallissy, Historical Background and Design Evolution of the Transonic

Aircraft Technology Supercritical Wing, NASA-TM-81365, Aug. 1981.

5Compiled by Powers, Sheryll Goecke, Advanced Fighter Technology Integration F-111 Mission Adaptive

Wing, NASA-CP-3055, 1990.

6 Gould, D. K., Boeing Pre-Design of AFTI-I11 Mission Adaptive Wing, Volume H - Aerodynamic Trade

Studies, Theoretical Calculations and Wind Tunnel Tests, AFFDL-TR-73, June 1978.

7 Nelson, D. W. and G. R. Letsinger, "AFTI-F-111 Mission Adaptive Wing Wind Tunnel Analysis Report,"

AEDC PWT-16T, test no. 550, Boeing D365-10058-I, rev. A, Apr. 1981.

8 Hall, Joseph M., "AFTUF- 111 Flight Control System," AFWAL-TR-87-3012, 1987.

9 Steers, Louis L. and Paul R. Bussing, Flight Demonstration and Research of the Smooth Variable-Camber

Wing, Advanced Fighter Technology Integration F-111 Mission Adaptive Wing, NASA-CP-3055, 1990.

10 Bonnema, Kenneth L. and William A. Lokos, "AFTI/F-111 Mission Adaptive Wing Flight Test

Instrumentation Overview," paper no. 89-0084, 35th International Instrumentation Symposium, Orlando, Florida,

May 1989.

11 Webb, Lannie D., William E. McCain, and Lucinda A. Rose, Measured and Predicted Pressure

Distributions on the AFTI/F-111 Mission Adaptive Wing, NASA-TM-100443, Nov. 1988.

12Powers, Sheryll Goecke, Lannie D. Webb, Edward L. Friend, and William A. Lokos, Flight Test Results

From a Supercritical Mission Adaptive Wing With Smooth Variable Camber, NASA-TM-4415, Nov. 1992.

13Friend, Edward L., "Flight Buffet Characteristics of a Smooth Variable-Camber Mission Adaptive Wing for

Selected Wing Flap Deflections," The Advanced Fighter Technology Integration AFTI/F-I11 Airplane, NASATM-4455, Feb. 1993.

14Wong, Kent J., AFTI/F-111 Mission Adaptive Wing Lift and Drag Results, Air Force Flight Test Center,

Edwards AFB, California, AFFFC TR-87-02, Apr. 1987.

15Phillips, Paul W. and Stephen B. Smith, AFTI/F-111 Mission Adaptive Wing (MAW) Automatic Flight

Control System Modes Lift and Drag Characteristics, AFFTC-TR-89-03, May 1989.

16 McCain, William E., "Comparison of Two Predication Methods with Flight-Measured Wing Surface

Pressure Distributions from the Mission Adaptive Wing," Advanced Fighter Technology Integration F-111 Mission

Adaptive Wing, NASA-CP-3055, 1990.

17Fehl, John E., AFTI/F-111 Mission Adaptive Wing 1/12 Scale Wind Tunnel Model Inspection, AFWALTM-80-114-FIMS, Dec. 1980.

18Gould, Douglas K., AFTI/F-111 Mission Adaptive Wing, Advanced Fighter Technology Integration F-111

Mission Adaptive Wing, NASA-CP-3055, 1990.

19Bussing, P. R., AFTI F-111 Final Instrumentation Report, Boeing Document no. D365-10016-2, 1984.

20 Dudzinski, Thomas J. and Lloyd N. Krause, Flow-Direction Measurement with Fixed-Position Probes,

NASA-TM-X- 1904, Oct. 1969.

849
21DeAngelis,V. Michael,In-Flight Deflection Measurement of the HiMAT Aeroelastically Tailored Wing,

AIAA-81-2450, Nov. 1981.

22Lokos, William A., Predicted and Measured In-Flight Wing Deflections of a Forward-Swept-Wing Aircraft,

NASA-TM-4245, 1990.

23DeAngelis, V. Michael, and Robert Fodale, "Electro-Optical Flight Deflection Measurement System" SFTE

18th Annual Symposium Proceedings, SFTE Technical Paper 22, Sept. 1987.

24Webb, Lannie D. and Harold P. Washington, Flight Calibration of Compensated and Uncompensated

Pitot-Static Airspeed Probes and Application of the Probes to Supersonic Cruise Vehicles, NASA-TN-D-6827,

May 1972.

25 Sakamoto, Glenn M., Aerodynamic Characteristics a Vane Flow Angularity Sensor System Capable of

Measuring Flight Path Accelerations for the Mach Number Range From 0.40 to 2.54, NASA-TN-D-8242, 1972.

26Beers, Yardley, Introduction to the Theory of Error, Addison-Wesley Publishing Co., Inc., 1957.

27Webb, Lannie D., Sheryll Goecke Powers, and Lucinda A. Rose, Selected Local Flow-Field Measurements

on the Advanced Fighter Technology Integration (AFT1)/F-111 Aircraft Mission Adaptive Wing, NASA-TM-4405,

1992. (Also published in, Advanced Fighter Technology Integration F-111 Mission Adaptive Wing,

NASA-CP-3055, 1990.)

28Montoya, Lawrence C. and Richard D. Banner, F-8 Supercritical Wing Flight Pressure, Boundary-layer,

and Wake Measurements and Comparisons With Wind Tunnel Data, NASA-TM-X-3544, 1977.

29Friend, Edward L. and Jeffrey M. Thompson, Buffet Characteristics of the Advanced Fighter Technology

Integration AFTI/F-111 Airplane with the Mission Adaptive Wing, NASA-CP-3055, 1990.

30Smith, Stephen B. and Kent Wong, "Lift and Drag Characteristics of the AFrI/F- 111 in the Manual Mode,"

Advanced Fighter Technology Integration AFTI/F-111 Airplane with the Mission Adaptive Wing, NASACP-3055, 1990.

31Phillips, Paul W. "Lift and Drag Characteristics of the AFrI/F-111 With the MAW Automatic Control

Modes," Advanced Fighter Technology Integration AFTI/F-111 Airplane with the Mission Adaptive Wing, NASACP-3055, 1990.

3zNelson, David W., AFTI/F-111 Aerodynamics Final Report, D365-10110-1, Boeing, Feb. 1987.

85O

REPORT DOCUMENTATION PAGE Fo,r_ Approved

OMB No. 0704-0188

Public reporting burOen for th*s collection oI informatH3¢3 is est=mateO to average I hour per response, incluO=ng the t_me for reviewing instruCtiOns, searching exlshng Oats sources, gathering anO

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including suggestions for recluclng this burOen, 1o Washington Headquarters Services, Directorate for Inforrnstio¢l ODeratlons =,nO Reports, 1215 Jefferson Davis Highway, $ufte 1204, Arhnglon,

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1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3. REPORT'TYPE AND DATES COVERED

June 1997 Technical Memorandum

4.TITLE AND SUBTITLE S. FUNDING NUMBERS

Flight Wing Surface Pressure and Boundary-Layer Data Report from the

F-111 Smooth Variable-Camber Supercritical Mission Adaptive Wing

6. AUTHOR(S)

Sheryll Goecke Powers and Lannie D. Webb

7. PERFORMINGORGANIZATIONNAME(S)ANDADDRESS(ES)

NASA Dryden Flight Research Center

P.O. Box 273

Edwards, California 93523-0273

9. SPONSOFIINGtMONOTORING AGENCY NAME(S) AND ADDRESS(F.S)

National Aeronautics and Space Administration

Washington, DC 20546-0001

11. SUPPLEMENTARY NOI_P._

WU 953-36-00

8. PERFORMING ORGANIZATION

REPORT NUMBER

H-2102

10. SPONSORING/MONITORING

AGENCY REPORT NUMBER

NASA TM-4789

12L _k_imiUTION/AVAILABILII_ STATEMENT

Unclassified--Unlimited

Subject Category 02

121. DISTRIBUTION COOE

13. AB=*iMACT (Maximum 200 words)

Flight tests were conducted using the advanced fighter technology integration F- 111 (AFTI/F- 111) aircraft modified with

a variable-sweep supercridcal mission adaptive wing (MAW). The MAW leading- and trailing-edge variable-camber

surfaces were deflected in flight to provide a near-ideal wing camber shape for the flight condition. The MAW features

smooth, flexible upper surfaces and fully enclosed lower surfaces, which distinguishes it from conventional flaps that have

discontinuous surfaces and exposed or semi-exposed mechanisms. Upper and lower surface wing pressure distributions

were measured along four streamwise rows on the right wing for cruise, maneuvering, and landing configurations.

Boundary-layer measurements were obtained near the trailing edge for one of the rows. Cruise and maneuvering wing

leading-edge sweeps were 26 ° for Mach numbers less than 1 and 45 ° or 58 ° for Math numbers greater than 1. The landing

wing sweep was 9° or 16°. Mach numbers ranged from 0.27 to 1.41, angles of attack from 2° to 13°, and Reynolds number

per unit foot from 1.4 x 106 to 6.5 x 106. Leading-edge cambers ranged from 0° to 20 ° down, and trailing-edge cambers

ranged from 1° up to 19° down. Wing deflection data for a Mach number of 0.85 are shown for three cambers. Wing

pressure and boundary-layer data are given. Selected data comparisons are shown. Measured wing coordinates are given

for three streamwise semispan locations for cruise camber and one spanwise location for maneuver camber.

14. SUBJECTTERMS

Boundary layers, Pressure distributions, Smooth variable camber,

Supercritical wing

17. SECURITY CLASSIFICATION 118. SECURITY CLASSIFICATION 19. SECURFrY CLASSIFICATION

OF REPORT OF THIS PAGE OF ABSTRACT

Unclassified Unclassified Unclassified

NSN 7540-01-280-5500 AvatlaD/e from the NASA Center for AeroSpace Information, 800 Elkrt<lge Landing Road,

Linthicum Heights, MD 21090; (301)621-0390

15. NUMBER OF PAGES

862

!16. PRICE CODE

A99

20. LIMITATION OF ABSTRACT

Unlimited

Standard Form 298 (Rev. 2-89)

Prmrcnbed by ANSI Std Z39- t 8

298.102