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Characteristics of the Shock Noise Component of Jet Noise

  • Published:2008-05-05 Issue: Volume: Page:
  • ISSN:
  • Container-title:14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference)
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Author:

Viswanathan Krishna1,Alkislar Mehmet1,Czech Michael1

Affiliation:

1. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Reference25 articles.

1. An experimental study of jet noise part II: Shock associated noise

2. 3Seiner,J.M.,andNorum,T.D."ExperimentsonShockAssociatedNoiseofSupersonicJets,"AIAApaper79-1526,1979.

3. 4Seiner,J.M.,andNorum,T.D."AerodynamicAspectsofShockContainingJetPlumes,"AIAApaper80-0965,1980.

4. 5Norum, T. D., and Seiner, J.M."Measurements ofStaticPressureand Far FieldAcoustics ofShock-containingSupersonic Jets,"NASATM 84521,1982.

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1. Noisy Flow Structures in a Heated and Unheated Jet Produced by a Three-Stream Rectangular Nozzle with an Aft Deck;54th AIAA Aerospace Sciences Meeting;2016-01-02

2. Numerical Study of Noise Characteristics in Overexpanded Jet Flows;53rd AIAA Aerospace Sciences Meeting;2015-01-03

3. Numerical Study of Noise Sources Characteristics in An Underexpanded Jet Flow;20th AIAA/CEAS Aeroacoustics Conference;2014-06-13

4. Computational Study of Shock-Associated Noise Characteristics Using LES;19th AIAA/CEAS Aeroacoustics Conference;2013-05-24

5. PIV Measurements of Supersonic Internally-Mixed Dual-Stream Jets;17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference);2011-06-05
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