Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 2. Installed Nozzles-Reference-Cited by-同舟云学术

Reducing Propulsion Airframe Aeroacoustic Interactions with Uniquely Tailored Chevrons: 2. Installed Nozzles

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2434

Reference10 articles.

1. Janardan,B.A.,Hoff,G.E.,Barter,J.W.,Martens,S.,Gliebe,P.R.,Mengle,V.andDalton,W.N."ASTCriticalPropulsion and n Internally MixedNozzles," AIAA Paper2005-2934.

2. A Contract NAS1-000

3. Noise Reduction Technologies for Future Commercial Subsonic Engines - Separate-Flow Exhaust System Noise Reduction Concept Evaluation," NASA/CR-2000-210039,Dec. 2000.

4. Mengle, V.G., Elkoby, R., Brusniak, L. and Thomas, R. "Reducing Propulsion Airframe Aeroacoustic Inte quely Tailored Chevrons. 1. IsolatedNozzles," AIAA PaperNo. 2006-2467.

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