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Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 1. Isolated Nozzles

  • Published:2006-05-08 Issue: Volume: Page:
  • ISSN:
  • Container-title:12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference)
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Author:

Mengle Vinod1,Elkoby Ronen1,Brusniak Leon1,Thomas Russell2

Affiliation:

1. The Boeing Company

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference19 articles.

1. Mengle,V.G."RelativeClockingofEnhancedMixingDevicesforJetNoiseBenefit,"AIAAPaper2005-0996.

2. Mengle,V.G."JetNoiseCharacteristicsofChevronsinInternallyMixedNozzles,"AIAAPaper2005-2934.

3. Bhat,T.R.S."ExperimentalStudyofAcousticCharacteristicsofJetsfromDualFlowNozzles."AIAAPaper2001-2183.

4. Hunter. C., Thomas, R.H., Abdol-Hamid, K., Pao, S.P., Elmiligui, A.A. and Massey, S.J. "Computational Analysis of the Flow and Acoustic Effects ofJet-PylonInteraction " AIAA Paper2005-3083.

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