Design and analysis of a supersonic jet noise reduction concept

Anthony R. Pilony, Ussell W. Powers, Dennis K. McLaughlin, Philip J. Morris

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The design and analysis of a simple jet noise reduction concept is discussed. The concept is intended for use on the type of supersonic exhaust nozzles typically employed on tactical aircraft. The concept addresses both broadband shock associated noise (BBSAN), and turbulent mixing noise. BBSAN is addressed through a reduction in the effective exhaust area, which reduces the strength of the shock cell structure in the jet. Turbulent mixing noise is reduced by enhancement of mixing in the jet shear layer, which creates a shorter region of strongly turbulent ow, and breaks up the large scale turbulent structures. This paper describes an active control device that de ects a fraction of the adjustable seals in the divergent section of the engine exhaust nozzle. After takeoff, the de ected seals would be returned to their unde ected position. Very favorable jet noise reductions are demonstrated at multiple observer angles for nominal takeoff conditions.

Original languageEnglish (US)
Title of host publication52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624102561
StatePublished - Jan 1 2014
Event52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014 - National Harbor, MD, United States
Duration: Jan 13 2014Jan 17 2014

Publication series

Name52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014

Other

Other52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
CountryUnited States
CityNational Harbor, MD
Period1/13/141/17/14

Fingerprint

jet aircraft noise
Noise abatement
noise reduction
exhaust nozzles
takeoff
turbulent mixing
shock
Takeoff
Seals
Nozzles
broadband
active control
Exhaust systems (engine)
control equipment
shear layers
aircraft
engines
engine
Aircraft
analysis

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Pilony, A. R., Powers, U. W., McLaughlin, D. K., & Morris, P. J. (2014). Design and analysis of a supersonic jet noise reduction concept. In 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014 (52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014). American Institute of Aeronautics and Astronautics Inc..
Pilony, Anthony R. ; Powers, Ussell W. ; McLaughlin, Dennis K. ; Morris, Philip J. / Design and analysis of a supersonic jet noise reduction concept. 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc., 2014. (52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014).
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abstract = "The design and analysis of a simple jet noise reduction concept is discussed. The concept is intended for use on the type of supersonic exhaust nozzles typically employed on tactical aircraft. The concept addresses both broadband shock associated noise (BBSAN), and turbulent mixing noise. BBSAN is addressed through a reduction in the effective exhaust area, which reduces the strength of the shock cell structure in the jet. Turbulent mixing noise is reduced by enhancement of mixing in the jet shear layer, which creates a shorter region of strongly turbulent ow, and breaks up the large scale turbulent structures. This paper describes an active control device that de ects a fraction of the adjustable seals in the divergent section of the engine exhaust nozzle. After takeoff, the de ected seals would be returned to their unde ected position. Very favorable jet noise reductions are demonstrated at multiple observer angles for nominal takeoff conditions.",
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Pilony, AR, Powers, UW, McLaughlin, DK & Morris, PJ 2014, Design and analysis of a supersonic jet noise reduction concept. in 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, American Institute of Aeronautics and Astronautics Inc., 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014, National Harbor, MD, United States, 1/13/14.

Design and analysis of a supersonic jet noise reduction concept. / Pilony, Anthony R.; Powers, Ussell W.; McLaughlin, Dennis K.; Morris, Philip J.

52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc., 2014. (52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Pilony AR, Powers UW, McLaughlin DK, Morris PJ. Design and analysis of a supersonic jet noise reduction concept. In 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc. 2014. (52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014).