NASA/CP--2000-210524

Separate Flow Nozzle Test Status Meeting

December 2000
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NASA/CP--2000-210524

Separate Flow Nozzle Test Status Meeting

Proceedings of a conference held at and sponsored by

NASA Glenn Research Center

Cleveland, Ohio

September 9-10, 1997

National Aeronautics and

Space Administration

Glenn Research Center

December 2000
I Note

that at the time of research, the NASA Lewis Research Center

was undergoing a name change to the

NASA John H. Glenn Research Center at Lewis Field.

Both names may appear in this report.

Available from

NASA Center for Aerospace Information

7121 Standard Drive

Hanover, MD 21076

Price Code: A16

Available electronically at http: //gltrs.grc.nasa.gov/GLTRS
PREFACE

In 1995, NASA GRC initiated efforts to meet the US industry's rising need to develop jet noise technology for separate flow nozzle exhaust systems. Such technology would be applicable to long-range aircraft

using medium to high by-pass ratio engines. With support from the Advanced Subsonic Technology Noise

Reduction program, these efforts resulted in the formulation of an experimental study, the Separate Flow

Nozzle Test (SFNT). SFNT's objectives were to develop a data base on various by-pass ratio nozzles,

screen quietest configurations and acquire pertinent data for predicting the plume behavior and ultimately

its corresponding jet noise. The SFNT was a team effort between NASA GRC's various divisions, NASA

Langley, General Electric, Pratt&Whitney, United Technologies Research Corporation, Allison Engine

Company, Boeing, ASE FluiDyne, MicroCraft, Eagle Aeronautics and Combustion Research and Flow

Technology Incorporated.

SFNT found several exhaust systems providing over 2.5 EPNdB reduction at take-off with less than 0.5%

thrust loss at cruise with simulated flight speed of 0.8 Mach. Please see the following SFNT related

reports: Saiyed, et al. (NASA/TM_000-209948), Saiyed, et al. (NASA/C_2000-210524),

Low, et al. (NASA/CRY000-210040), Janardan et al. (NASA/CR 2000-210039), Bobbitt, et al.

(NASA/CR 201-210706) and Kenzakowski et al. (NASA/C_2001-210611.).

I wish to thank the entire SFNT team of nearly 50 scientists, engineers, technicians and programmers

involved in this project. SFNT would have fallen well short of its goals without their untiring support,

dedication to developing the jet noise technology.

Naseem Saiyed

SFNT Research Engineer

NASA/C_2000-210524 iii
TABLE OF CONTENTS

Advanced Subsonic Technology Separate Flow Nozzle Tests for Engine Noise Reduction Sub-Element

Naseem H. Saiyed, NASA Glenn Research Center ....................................................................................... 1

Advanced Subsonic Technology Noise Reduction Element Separate Flow Nozzle Tests for

Engine Noise Reduclion Sub-Element

Naseem H. Saiyed, NASA Glenn Research Center ..................................................................................... 41

Separate Flow Nozzle Jet Noise Test Stares Meeting at NASA Lewis Research Center

J. Low, T. Barber, and S. Bhat ................................................................................................................... 117

CH) Analysis for Selected Nozzles

Thomas J. Barber, United Technologies Research Center ................................................................... 132

Phased An'ay Measurements for the Separate Flow Jet Noise Test at Glenn

Srini Bhat and John Premo, Boeing Commercial Airplane Group ...................................................... 159

Discussion of Measured Acoustic and Related Aero Data

Thomas J. Barber, United Technologies Research Center ................................................................... 176

Critical Propulsion and Noise Reduction Technologies for Future Commercial Subsonic Engines

B.A. Janardan, G.E. Hoff, J.W. Barter, J.F. Bransch, P.R. Gliebe, R.S. Coffin,

S. Martens, and B.R. Delaney, GE Aircraft Engines; W.N. Dalton, V.G. Mengle, B.R. Vittal,

V.D. Baker, and F. Smith, Allison Engine Company ................................................................................... 181

SFNT97 Flow Field Measurements .................................................................................................................... 255

LaRC Separate Flow Testing Stares

Jack Seiner, Jet Noise Laboratory, NASA Langley Research Center ........................................................ 337

Installed Jet Noise

Thonse R.S. (Srini Bhat), NASA Glenn Research Center ......................................................................... 345

List of Attendees ................................................................................................................................................. 363

NASA/C_2000-210524 iv
A__genda

LeRC

LeRC

LeRC

PW

GE

LeRC

LeRC

LaRC

Boeing

All

Separate Flow Test Status Meeting

September 10, 1997

NASA Lewis Bldg 86 Rm 100

Welcome

Discussion of configurations, concepts tested, measurements,

quality of data, schedule

Results overview (EPNL Summary)

Break

PW noise reduction concept results

Phased array results

Lunch

GE noise reduction concept results

Diagnostic Measurements

Break

Outstanding issues and schedule

LaRC Separate Flow Testing Status

Installed Jet Test Results

Open Discussion

Adjourn

9:00

9:15

9:45

10:15

10:30

12:00

1:00

2:30

3:00

3:15

3:30

4:00

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Table 6. _PL $epa_ Row Nozzle IR Camera Test Summary.

Configuration Oate Mach No. _leJPower Co_pondIng IR #-

Setting Escort Rdg.

? ? ? ? ? 1

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NASA/CP--2000-210524 68
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Table 6. AAPL S_arate Flow Nozzle !R Camera Test Summary (Concluded).

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Yunis

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Dennis

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Eugene

Naseem

James Bridges

Valerie Lyons

Company Telephone

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216-433-3951

216-433-6736

216-433-2693

NASA Lewis

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Jeffery Miles NASA Lewis 216-433-5909

James Scott

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M_vin

Goodrich

Blaha

Hughes

McNelis

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Hugh Kao

Nicholas Georgiadis

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NASA Lewis 216-433-2597

NASA Lewis 216-433-8395

NASA Lewis 216-433-8880

NASA Lewis 216-433-5825

NASA Lewis 216-433-5866

NASA Lewis 216-433-3958

NASA Lewis 216-433-8716

NASA Lewis

NASA Lewis

NASA Lewis

NASA Lewis

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NASA Lewis

ICOMP 216-962-3146

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NASA/CP 2000-210524 363
Jet Noise Analysis and Separate Flow Nozzle Test Workshops

Sept. 9-10, 1997

Title

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FirstName LastName

Dale Ashby

Phillip Gliebe GE Aircraft Engines

Bangalore Janardan GE Aircraft Engines

R.K. Majjigi GE Aircraft Engines

Steve Martens GE Aircraft Engines

Ramani Mani GE CR&D

Brian Mitchell GE CR&D

Sayed Saddoughi GE CR&D

Donald Weir AlliedSignal Engines

Douglas Mathews Pratt & Whitney

John Low Pratt & Whitney

Barry Wagner

Company Telephone Here

9/9

NASA Ames

Pratt & Whitney

513-243-2865 X X

513-243-3393 X X

513-552-4308 X X

513-552-2768 X X

518-387-6341 X X

518-387-7845 X X

518-387-6878 X

602-231-1214 X X

860-565-2664 X

860-565-4279 X X

860-565-3888 X

Alfred Stern Pratt & Whitney

Robert Manzi Pratt & Whitney

Thomas

860-565-2566 X

Barber UTRC 860-610-7619

John Simonich UTRC 860-610-787 l

William Dalton Allison Engine Co. 317-230-2430

Vinod Mengle Allison Engine Co. 317-230-2400

David Reed Boeing Commercial

John Premo Boeing Commercial

Mahendra Joshi Boeing - Long Beach

Belur Shivashankara The Boeing Company

Srini Bhat The Boeing Company

Krishna Viswanathan The Boeing Company

Philip Morris Penn State University

Anthony Pilon Penn State University

562-593-8583

425-234-955l

425-234-9550

425-965-1186

814-863-0157

814-865-1966

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NASA/C_2000-210524 364
Form Approved REPORT DOCUMENTATION PAGE

OMB No. 0704-0188

Publicreportingburdenfor this collectionof informationis estimatedto average1 hourperresponse,includingthe timefor reviewinginstructions,searchingexistingdata sources,

gatheringand maintainingthe data needed,and completingandreviewingthe collectionof information.Sendcommentsregardingthis burdenestimateor anyother aspectof this

collectionof information,includingsuggestionsfor reducingthis burden,to WashingtonHeadquartersServices,Directoratefor InformationOperationsand Reports,1215Jefferson

DavisHighway,Suite1204,Arlington,VA 22202-4302,and to the Officeof Managementand Budget,PaperworkReductionProject(0704-0188),Washington,DC 20503.

1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE

December 2000

4. TITLE AND SUBTITLE

Separate Flow Nozzle Test Status Meeting

6. AUTHOR(S)

N. Saiyed, editor

7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES)

National Aeronautics and Space Administration

John H. Glenn Research Center at Lewis Field

Cleveland, Ohio 44135 3191

9. SPONSORINGIMONITORING AGENCY NAME(S) AND ADDRESS(ES)

National Aeronautics and Space Administration

Washington, DC 20546 0001

3. REPORT TYPE AND DATES COVERED

Conference Publication

5. FUNDING NUMBERS

WU 522 81 11 00

8. PERFORMING ORGANIZATION

REPORT NUMBER

E 12499

10. SPONSORING/MONITORING

AGENCY REPORT NUMBER

NASA CP 2000-210524

11. SUPPLEMENTARY NOTES

Proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio,

September 9 10, 1997. Responsible person, N. Saiyed, organization code 5940, 216-433 6736.

12a. DISTRI B UTIO N/AVAI LAB I LITY STATEMENT

Unclassified - Unlimited

Subject Category: 71 Distribution: Nonstandard

Available electronically at http://gltrs._c.nasa.gov/GLTRS

This publication is available from the NASA Center for AeroSpace Information, 301_21_)390.

12b. DISTRIBUTION CODE

13. ABSTRACT (Maximum 200 words)

NASA Glenn, in partnership with US industry, completed an exhaustive experimental study on jet noise reduction from

separate flow nozzle exhaust systems. The study developed a data base on various bypass ratio nozzles, screened quietest

configurations and acquired pertinent data for predicting the plume behavior and ultimately its corresponding jet noise.

Several exhaust system configurations provided over 2.5 EPNdB jet noise reduction at take-off power. These data were

disseminated to US aerospace industry in a conference hosted by NASA GRC whose proceedings are shown in this

report.

14. SUBJECT TERMS

Engine noise; Acoustic nozzles; Aeroacoustics; Aircraft; Noise;

Exhaust noise; Noise suppressor; Sonic nozzles

17. SECURITY CLASSIFICATION 18. SECURITY CLASSIFICATION 19. SECURITY CLASSIFICATION

OF REPORT OF THIS PAGE OF ABSTRACT

Unclassified Unclassified Unclassified

NSN 7540-01-280-5500

15. NUMBER OF PAGES

372

16. PRICE CODE

A16

20. LIMITATION OF ABSTRACT

Standard Form 298 (Rev. 2-89)

Prescribed by ANSI Std. Z39-18

298-102