**Upender K. Kaul**

**904 Boar Circle, Fremont, CA 94539**

**(510) 490-4506**

**EDUCATION**

**University of California at Berkeley, Berkeley, California**

**Ph.D., Mech. Engineering (Fluid Dynamics & Heat Transfer); 1982**

Subjects: Fluid Dynamics, Computational Fluid Dynamics, Heat Transfer,

Continuum Mechanics, Advanced Applied Mathematics, Numerical Methods &

Analysis, Finite Difference, Finite Volume, Finite Element and Spectral

Methods in Engineering

**University of Tennessee Space Institute, Tullahoma, Tennessee**

**M.S., Mech. Engineering (Fluid Dynamics & Heat Transfer), 1975**

Subjects: Fluid Dynamics, Turbulence, Aerodynamics, Propulsion,

Thermodynamics, Radiation & Convection Heat Transfer, Applied
Mathematics,

Numerical Methods for Ordinary & Partial Differential Equations

**Punjab University, Chandigarh, India**

**B.S., Aeronautical Engineering; 1970**

Subjects: Fluid Dynamics, Aerodynamics, Jet & Rocket Propulsion,
Aircraft

Materials, Aircraft Structures, Thermodynamics, Engineering Mathematics,

Machine Design, Labs: Wind Tunnel, Mechanical Engineering, Materials and

Electrical Engineering

**J & K University, Kashmir, India**

**B.Sc.,** Physics: Mechanics, Acoustics, Thermodynamics & Heat
Transfer, Optics,

Electricity, Magnetism; Mathematics, Chemistry, English

**SUMMARY OF TECHNICAL EXPERIENCE**

**Development of new Mathematical Algorithms for use in Computational
Structural Dynamics simulation of engineering and natural systems.**

**First Principles Prediction of Time-Series Vibrations Data typical of
Rotating Systems such as Helicopter Transmission Components; Statistical
Data Analysis and Data Modeling .**

**Design, Development and Application of graphics and animation software
for**

**Scientific Visualization and for animating Virtual Reality
Environments using**

**object-oriented software technology.**

**Applications/Development of Numerical Schemes and Computer Codes**
**for**

**Computational Fluid Dynamics (CFD) and Computational Heat Transfer
Analysis and Design of Aircraft Configurations (External Flow) and
Rocket Engine**

**Components & Wind Tunnels (Internal Flow) in all flow regimes -**
**Potential,**

**Euler, Laminar and Turbulent Flows.**

Applications Include: **Cobra Helicopter Vibrations, OH58 Helicopter
Vibrations**, **Space Shuttle Main Engine Re-Design Problems, National
Aerospace Plane**

**External Flow Turbulence/Transition Modeling, NASA Ames 80x120 Full
Scale Wind Tunnel Inlet/Test Section Redesign, X-24C Hypersonic Research
Aircraft External Flow Simulations and Analysis**, Simulation of Mixing
Layers in Dump Combustors, Internal Air Cooling of Rotating Turbine
Blades

**Three-Dimensional Numerical Grid Generation Geometry Definition**

of Aircraft and Other Configurations on Workstations

**PROJECT EXPERIENCE**

**NASA Ames Research Center Dates Employed: 2/01 - Present**

Mail Stop 269-2, NASA Ames Research Center

Moffett Field, CA 94035-1000

**Computer Scientist**

Worked in various capacities on **the Intelligent Health and Systems
Monitoring**

**(IHASM)** project.

Finalized a plan to do the first principles finite-difference modeling
of helicopter transmission components. Work is well under way. Developed
a fully automated procedure to generate a three-dimensional elliptic
grid for the 19-tooth spiral-bevel pinion gear and a shaft (**OH58
helicopter transmission pinion**). Paper presented at 2001 SIAM Meeting
and a U.S. patent has been filed for the new algorithm. Another paper
has been published in J. Computational Physics in 2003. Two other
journal papers are in preparation. Developed a new OpenGL based graphics
animator to create animations to demonstrate the pinion gear in mesh,
the evolution of the elliptic grid from a given initial state to a final
desired state and the evolution of dynamic stresses over gear geometries
in time.

Created simplified physical models (lumped parameter systems) of simple
gears and generated vibrations data. In collaboration with IHASM team
members, analyzed these data and presented two papers in 2001 IEEE
Aerospace conference.

Wrote **Matlab** routines to reduce large helicopter transmission
vibrations data to intermediate matrix forms suitable for statistical
data analyses..

**Computer Sciences Corporation Dates Employed: 3/99 - 2/01**

Mail Stop 269-2, NASA Ames Research Center

Moffett Field, CA 94035-1000

**Computer Scientist**

Worked in various capacities on **the Intelligent Health and Systems
Monitoring**

**(IHASM)** project.

Developed a plan and a proposal to do the first principles
finite-difference and

finite-element modeling of helicopter transmission components.Work is
well under

way - developed a three-dimensional grid for the 19-tooth gear and a
shaft (**OH58 helicopter transmission pinion**) using an elliptic grid
generation technique.

Working in collaboration with IHASM team members on simplified physical

modeling of gears typical of a helicopter transmission.

Maintained and wrote drivers for reducing large amounts of field data in
two-tier

matrix forms using **Matlab.** Wrote Matlab routines to process the data
for statistical

analysis. Wrote a Matlab **Graphical User Interface (GUI**) for one such
driver.

**Caelum Research Corporation Dates Employed: 11/98 - 3/99**

Mail Stop 269-2 NASA Ames Research Center

Moffett Field, CA 94035-1000

U.S.A.

**Computer Scientist**

Worked on the **IHASM** and **EPMS** data understanding and analysis
projects.

Used **Matlab** to reduce large amounts of **Cobra helicopter flight
data** for statistical

analysis under the IHASM project.

Developed a **C++** program to generate hypothetical data in the exact
format as that

used by Alaska Airlines. Data generated thus are being used to refine
data analysis

models. Used **Java (Visual J++)** to read **C++** **COM objects** for
data extraction,

analyses and modeling.

Designed, developed and implemented a **Virtual Reality
Environment(VRE**) using **Java/Java 3D** for a multi-agent model. This
graphics and animation environment graphically displays various agents
and their surroundings and animates them

according to a rule-based system. This work is being extended to execute
a real-time animation of the multi-agent model. System specifications
and design done using

**Use Case Modeling** and **Unified Modeling Language (UML**)
respectively.

**MCAT, Inc. Dates Employed: 03/97-10/98**

Mail Stop 227-2

NASA Ames Research Center

Moffett Field, CA 94035-1000

U.S.A.

**Senior Research Scientist**

Independently designed, developed and implemented **C/C++/OpenGL/Xlib**
based

graphics software for the **NASA scientific visualization package,
PLOT3D**, towards automation of the Computational Fluid Dynamics (CFD)
processes at NASA Ames Research Center. The PLOT3D package, a NASA award
winning software system, is being used nationally all over the aerospace
industry. The graphics system integrates the geometric objects as well
as function surfaces from the CFD platform into the graphics platform.

**PROJECT EXPERIENCE Dates Employed: 8/90 - 3/97**

**Flow Modeling & Simulation, Fremont, California**

**Self-Employed**

**Independent Consulting and CFD Contract Work** with the Federal
Government.

Proposed Projects to the Government/Commercial Sector including
Automobile

Industry.

**Developed and applied a fully implicit CFD and Heat Transfer Analysis
Code** in generalized curvilinear coordinates and a **fully implicit
Transport Equation**

**Solver (k-epsilon turbulence solver)** in generalized curvilinear
coordinates for

turbine-blade cooling flow problems.

**Under contract from the U.S. Navy, developed a computational
analysis**

**methodology** to be used as a part of an overall methodology in
predicting the

performance characteristics of jet engine turbine blades, in particular,
the heat

transfer characteristics of turbulent flow within the internal passages
of blades under rotation.

**Developed computer models** to study the flow inside and through
three-dimensional geometries such as curved ducts, ducts with sudden
expansion (to simulate

combustors), ducts with pin fins (to simulate heat exchange mechanism),
etc., to

predict the corresponding pressure losses, frictional losses and heat
transfer.

**Turbopropulsion Laboratory Dates Employed: 5/92 - 9/94**

**Naval Postgraduate School, Monterey, CA**

**Sr. Research Associate, Nat\'l Research Council**

**Demonstrated a Computational Design Capability by Simulating Three**

**Dimensional Viscous Flow with Heat Transfer in the Internal**

**Passages of Rotating Turbine Blades.**

**Sterling Federal Systems Dates Employed: 10/82 - 2/90**

**Mountain View, California**

**Research Scientist**

Worked on numerous **NASA projects** such as the **Space Shuttle Main**

**Engine**, **NASA Ames National Full-Scale Aerodynamics Complex
(NFAC)** and

the **National Aerospace Plane** (**NASP**). Also developed computer
graphics and

computer animation for some of these projects as well as geometry and
grid

definition of aerospace and mechanical systems.

As a member of R & D team at NASA Ames, developed a computational
analysis

and design methodology to predict the pressure losses and viscous
frictional forces

in various fluid passages of the Space Shuttle Main Engine. **This
methodology has successfully been applied at Rockwell Corporation and
NASA in the main**

**engine redesign of the newest Space Shuttle.**

Independently, modified and applied a previously established Finite
Volume

computer code to predict the pressure losses in the test section of
NASA\'s largest

wind tunnel at NASA Ames. **This study, in conjunction with other
studies, was**

**used to redesign the inlet and the test section of this wind tunnel.**

Independently, developed a computer model for transition of laminar flow
to

turbulent flow which is being used at NASA Ames in predicting the
pressure and

viscous forces as well as heat transfer over the body of the proposed
**National**

**Aerospace Plane.**

**SAI, San Rafael, California Dates Employed:** **7/79 - 8/80**

**Senior Scientist**

Worked on **EPA project** on **computer modeling and simulation of air
pollution**

**diffusion and transport with photochemical smog and acid rain
chemistry.**

**JOB-RELATED TRAINING COURSES**

Graduated from an intensive six-week course on **semiconductor
technology** offered

by **SEMI** in Mountain View in 1996.

Overall basic knowledge of semiconductor technology such as wafer
fabrication and

manufacturing, **IC layout**, **CMOS IC Design** concepts, (**Control
Systems - PID and**

**Fuzzy Logic), SPICE simulation.**

**JOB-RELATED SKILLS**

**Computer systems used**

PC, SGI Workstation, DEC Alpha Workstation, SUN Workstation, Cray

**Computer languages used**

**C, C++, Java, Swing, Visual Basic, Fortran; Unified Modeling Language
(UML).**

**Other software used**

**IRIS GL, OpenGL/GLUT, Xlib, Java 3D, MS Visual Studio, SQL/MS Access
Database, MATLAB.**

**Operating Systems used**

**UNIX, Linux, Windows NT/95, VMS, UNICOS**

**AWARDS, PATENTS, HONORS, AFFILIATIONS & OTHER ACTIVITIES**

\> University of California at Berkeley **Chancellor\'s Patent Fund**

**Award** for Doctoral Dissertation, 1980

\> **AIAA Joint Group Award** (Fluid Dynamics Division) for the

Aerospace Images Art Exhibition and Competition

**\> NASA Group Achievement Award** for the National Aerospace Plane

Project, 1990

\> Three 1991 **NASA Tech Brief Awards** for three papers signifying

technology transfer to industry and government. Tech Briefs

published in the **NASA Tech Brief Journals in 1991**

\> **National Research Council Senior Research Associateship**

\> Listed in **Who\'s Who in Science and Engineering**, 2000-2001,

**Marquis 5th Edition**.

**\> U.S. Patent** for **Enhanced Elliptic Grid Generation** filed with
the U.S. patent office on Nov. 11, 2003

\> 2004 **NASA Tech Brief Award**

**\> Reviewed many articles of peers submitted for journal
publication**.

\> **Taught a short course on Finite Element Method at NASA Ames in
1984**

**to Sterling Software and other team members**

\> Senior Member, AIAA

**PUBLICATIONS**

**Journal Articles**

**\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\--**

Kaul, U. K., "New Boundary Constraints for Elliptic Systems Used in Grid
Generation Problems," **Journal of Computational Physics**, vol 189/2,
pp 476-492,, 2003

Kaul, U. K. and Shreeve, R. P., \"A Fully Viscous Navier-Stokes

Formulation in Generalized Curvilinear Coordinates for Prediction of

Internal Turbine Blade-Cooling Flows,\" **AIAA Journal**

**of Thermophysics and Heat Transfer**, Vol. 10, No. 4,
October-December, 1996

Kaul, U. K., \"A Fully Implicit Numerical Scheme for the Solution of

Transport Equations in Fluid Dynamics,\" Paper accepted for publication

in **J. Computational Physics**

Kaul, U. K., \"Do Large Structures Control Their Own Growth in a Mixing

Layer? An Assessment,\" **J. Fluid Mech**., Vol.190, May 1988

Kaul, U. K. (with S. Rogers and D. Kwak), \"On the Accuracy of the

Pseudocompressibility Method in Solving the Incompressible Navier -

Stokes Equations,\" **Int. J. Applied Math. Modelling**, 1987, Vol. 11

Kaul, U. K., \"A Relaxation Technique for the Parabolized Navier-Stokes

(PNS) Equations,\" **Comm. App. Numerical Methods**, 1986, Vol.2

Kaul, U. K., \"A Wind-Tunnel Inlet Flow Simulation,\" **J. Aircraft**,
Vol.

22, pp 927, October 1985

Kaul, U.K. and Kwak, D., \"Computation of Internal Turbulent Flow with

a Large Separated Flow Region,\" **Int. J. Numerical Methods in
Fluids**,

# Vol. 6, December 1986

Kaul, U. K. and Chaussee, D. S., \"A Comparative Study of the

Parabolized Navier-Stokes (PNS) Code Using Various Grid Generation

Techniques**,\" J. Computers and Fluids**, Vol. 13, No. 4, 1985

# SIAM Conference 

\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\--

Kaul, U. K. and Huff, E. M., "Automated gear teeth grid generation via
solution of elliptic pdes," SIAM Conference on Geometric Design and
Computing, Sacramento, CA., Nov. 5-8, 2001

# IEEE Conference Proceedings

\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\--

Hambaba, A., Huff, E. M.. and Kaul, U. K., "Detection and Diagnosis of
Changes in the Time-Scale Eigenstructure for Vibrating Systems," Proc.
2001 IEEE Aerospace Conference Proceedings, Big Sky, MT, March 10-17,
2001, ISBN: 0-7803-6599-2, Product No.: TH8542-TBR

Hambaba, A., Huff, E. M.. and Kaul, U. K., "Time-Scale Local Approach
for Vibration Monitoring," Proc. 2001 IEEE Aerospace Conference
Proceedings, Big Sky, MT, March 10-17, 2001, ISBN: 0-7803-6599-2,
Product No.: TH8542-TBR

**International and National Conference/Congress Proceedings**

\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\--

Kaul, U. K., \"A Fully Implicit Numerical Scheme for the Solution of

Transport Equations in Fluid Dynamics,\" Proc. 7th Int. Conf. Num.

Methods Laminar and Turbulent Flow, Stanford University, CA,

July 15-19, 1991

Kaul, U. K., \"Prediction of Transitional (Laminar-Turbulent)

Hypersonic Flows Using the Parabolized Navier-Stokes Equations,\" Paper

No. 24, Proc. Royal Aeronautical Society Conf., Int. Conf. Hypersonic

Aerodynamics, September 1989, Univ. of Manchester, U.K.

Kaul, U. K., \"On Some Aspects of Wave Interactions in Mixing layers,\"

Proc. First Woodward Conference on Wave Phenomena, June 1988, San Jose

State Univ.; Wave Phenomena, 1989, Springer-Verlag

Kaul, U. K., \"A Numerical Method to Assess the Feedback in a Free

Shear Layer,\" Proc. 10th Int. Conf Num. Methods Fluid Dynamics,

June 1986, China; Lecture Notes in Physics,No.264, Springer-Verlag

Kaul, U. K. (with D. Kwak, et al), \"A Numerical Study of

Incompressible Juncture Flows,\" Proc. 10th Int. Conf Num. Methods

Fluid Dynamics, June 1986, China; Lecture Notes in Physics, No.

264, Springer-Verlag

Kaul, U.K.,\"A Computational Study of the Subharmonic Instability in

Mixing Layers,\" Proc. 10th U.S. Congress App. Mechanics, June 1986,

Univ. Texas at Austin, Austin, Texas, pp 545, Published by ASME

**AIAA and ASME Conference Papers**

**\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\--**

Kaul, U. K. and Shreeve, R. P., \"A Fully Viscous Navier-Stokes

Formulation in Generalized Curvilinear Coordinates for Prediction

of Internal Turbine Blade-Cooling Flows,\" AIAA Paper 93-2579, 29th

AIAA/SAE/ASME/ASEE Joint Propulsion Conf, Monterey, California,

June 28-30, 1993

Kaul, U. K. and Shreeve, R. P., \"On a Fully Viscous Navier-Stokes

Formulation for Approximate Factorization Schemes,\" AIAA Paper -

Open Forum Session, AIAA 11th Comp. Fluid Dynamics Conference,

Orlando, Florida; July 6-9, 1993

Kaul, U. K., \"Laminar-Turbulent Transition Calculations of Heat

Transfer at Hypersonic Mach Numbers Over Sharp Cones,\"

Proceedings of the ASME Heat Transfer Division, ASME Winter

Annual Meeting, 1988, Chicago, Ill, Collected Works in Heat

Transfer, HTD-Vol.104, vol. 2, Published by the ASME, Ed. K. T. Yang

Kaul, U. K. (with S. Rogers and D. Kwak), \"A Numerical Study of

Three-Dimensional Vortical Flows Around Multiple Posts and its

Applications to the Space Shuttle Main Engine,\" AIAA Paper 86-0353,

AIAA 24th Aerospace Sciences Meeting, January 1986, Reno, Nevada

Kaul, U. K. (with D. Kwak et al), \"On the Grid-Induced Error in

Numerical Simulation of Viscous Incompressible Flows,\" Open Forum

Paper AIAA 86-0594, AIAA 24th Aerospace Sciences Meeting, Reno,

Nevada, January 1986

Kaul, U.K. and Kwak, D., \"Computations of Internal Turbulent Flow

with Large Separated Flow Regions,\" AIAA Paper 85-1687, AIAA 18th

Fluid Dynamics, PlasmaDynamics and Laser Conference, July 1985,

Cincinnati, Ohio

Kaul, U. K., \"A Global Iteration Scheme for the Parabolized Navier-

Stokes (PNS) Equations,\" Open Forum Paper AIAA 85-1535, AIAA 7th

Computational Fluid Dynamics Conference, July 1985, Cincinnati, OH

Kaul, U. K. (with S. Rogers and D. Kwak), \"On the Accuracy of the

Pseudocompressibility Method in Solving the Incompressible Navier-

Stokes Equations,\" AIAA Paper 85-1689, AIAA 18th Fluid Dynamics,

Plasmadynamics and Laser Conference, July 1985, Cincinnati, Ohio

Kaul, U. K., Kwak, D. and Wagner, C., \"A Computational Study of

Saddle Point Separation and Horseshoe Vortex System,\" AIAA Paper

85-0182, AIAA 23rd Aerospace Sciences Meeting, Jan. 1985, Reno, NV

Kaul, U. K., Ross, J. C. and Jacocks, J. L., \"A Numerical

Simulation of the NFAC (National Full-Scale Aerodynamic Complex)

Open-Return Wind Tunnel Inlet Flow,\" AIAA Paper 85-0437, AIAA 23rd

Aerospace Sciences Meeting, January 1985, Reno, Nevada

Kaul, U. K. and Chaussee, D. S., \"A Comparative Study of the

Parabolized Navier-Stokes (PNS) Code Using Various Grid Generation

Techniques,\" AIAA Paper 84-0459, AIAA 22nd Aerospace Sciences

Meeting, January 1984, Reno, Nevada

**Symposia and Other Conference Abstracts**

**\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\--**

Kaul, U. K. (with J. Flores, et al), \"CNS Code Enhancements (U),\"

Paper No. 15, 6th National Aerospace Plane Technology Symposium,

April 24-28, 1989, Monterey, California

Kaul, U. K. (with S. Lawrence and J. Tannehill), \"UPS Code

Enhancements,\" Paper No. 16, 6th National Aerospace Plane

Technology Symposium, April 24-28, 1989, Monterey, California

Kaul, U. K., \"Planetary Boundary Layer Flow Over a Building,\" Bull.

American Met. Soc., Vol. 61 (11), 1980

Kaul, U. K. et al, \"Development and Application of a Mesoscale Air

Quality Model,\" Bull. American Met. Soc., Vol. 61 (11), 1980

**Technical Reports**

**\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\--**

Kaul, U. K. and Huff, E. M., "Elliptic grid generation of spiral-bevel
pinion gear typical of OH-58 helicopter transmission, NASA
TM-2002-210932, February 2002

Kaul, U. K. (with J. Chou and S. Nash), "Automated Analysis Methods,"

MCAT, Inc. Technical Report to NASA Ames Research Center under

Contract No. NAS2-14109, October 1998

Kaul, U. K. (with J. Chou and S. Nash), "Automated Analysis Methods,"

MCAT, Inc. Technical Report to NASA Ames Research Center under

Contract No. NAS2-14109, October 1997

Kaul, U. K., \"Turbulent Flow in a 180-degree Bend: Modeling and

Computations,\" NASA CR-4141, June 1988

Kaul, U. K. (with D. Kwak et al), \"A Numerical Study of

Incompressible Juncture Flows,\" NASA TM-88319, August 1986

Kaul, U. K. (with J. Champney et al), \"Incompressible Viscous Flow

Simulations of the NFAC Wind Tunnel,\" Final Report ATM-FR-25-012

under Contract NAS2-12187 to NASA Ames Research Center, June 1986

Kaul, U. K.,\"An Implicit Finite Difference Code for a Two-Equation

Turbulence Model for 3-D Flows,\" NASA TM-85241, June 1985

Kaul, U. K. and Chaussee, D. S., \"AFWAL Parabolized Navier-Stokes

Code: 1983 AFWAL/NASA Merged Baseline Version,\" AF Wright

Aeronautical Laboratories Report, AFWAL-TR-83-3118, Wright-

Patterson Air Force Base, Ohio, May 1984

Kaul, U. K. et al, \"Development and Evaluation of a Mesoscale

Photochemical Air Quality Simulation Model,\" December 1979, SAI

Report No. EI79-160 to US EPA

Kaul, U. K. and Frost, W., \"Turbulent Atmospheric Flow

Over a Backward-Facing Step,\" NASA CR-2749, October 1976

**Some Workshop Reports**

**\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\-\--**

Kaul, U. K., 180 degree Bend: Turbulence Modeling and Simulation,\"

Workshop Notes, Fifth Space Shuttle Main Engine CFD Workshop, NASA

Marshall Space Flight Center; April 1987

Kaul, U. K., \"Turbulence Modeling via a Deterministic Route,\"

Workshop Notes, Fourth Space Shuttle Main Engine CFD Workshop, NASA

Marshall Space Flight Center; April 1986

Kaul, U. K. and Kwak, D., \"A Low Reynolds Number Two-Equation

Tubulence Model and Some Applications,\" Third Space Shuttle Main Engine

CFD Workshop, NASA Marshall Space Flight Center, 1985

Kaul, U. K. and Chaussee, D. S., \"Computations With the AFWAL/NASA

Merged PNS Code,\" 1984 Parabolized Navier-Stokes Code Workshop, AFWAL

Flight Dynamics Laboratory, Dayton, Ohio; September 1984

Kaul, U. K., \"Upgrading the AFWAL PNS Code,\" Workshop Notes, 1983

Parabolized Navier-Stokes Code Workshop, AFWAL Flight Dynamics

Laboratory, Dayton, Ohio; May 1983