Measurements of 26%-Scale 777 Airframe Noise in the NASA Ames 40- by 80 Foot Wind Tunnel-Reference-Cited by-同舟云学术

Measurements of 26%-Scale 777 Airframe Noise in the NASA Ames 40- by 80 Foot Wind Tunnel

Published:2005-05-23 Issue: Volume: Page:
ISSN:
Container-title:11th AIAA/CEAS Aeroacoustics Conference
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Author:

Horne William¹,James Kevin¹,Arledge Thomas¹,Soderman Paul¹,Burnside Nathan²,Jaeger Steven³

Affiliation:

1. NASA Ames Research Center

2. AerospaceComputing, Inc

3. Colin Gordon and Assoc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2810

Reference17 articles.

1. Horne, W.C., Burnside, N.J., Soderman, P.T., Jaeger, S.M., Reinero, B.R., James, K.D., and Arledge, T.K. "Aeroacoustic Study of a 26%-scale Semispan Model of a Boeing 777 Wing in the NASA Ames 40- by 80-Foot Wind Tunnel, NASA/TP-2004-212802, Oct. 2004.

2. Microphone Array Assessment of an Isolated, 26%-scale, High-fidelity Landing Gear

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