Flight Test Results for Uniquely Tailored Propulsion-Airframe Aeroacoustic Chevrons: Community Noise-Reference-Cited by-同舟云学术

Flight Test Results for Uniquely Tailored Propulsion-Airframe Aeroacoustic Chevrons: Community Noise

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

Author:

Nesbitt Eric¹,Mengle Vinod¹,Czech Michael¹,Callender Bryan²,Thomas Russ³

Affiliation:

1. The Boeing Company

2. GE Transportation

3. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2438

Reference17 articles.

1. Figure28. Band LimitedAftArc Power Level-All Configurations compared

2. 2Janardan, B.A., Hoff, G.E., Barter, J.W., Martens, S., Gliebe, P.R., Mengle, V. and Dalton, W.N. "AST Critical Propulsion and Noise Reduction Technologies for Future Commercial Subsonic Engines, Separate-Flow Exhaust System Noise Reduction ConceptEvaluation."NASA CR-2000-210039,December, 2000.

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