Computational aeroacoustic analysis of slat trailing-edge flow
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. High Technology Corp., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1802
Reference20 articles.
1. Airframe noise characteristics of a 1/11 scale Airbus model
2. Airframe noise characteristics of a 4.7 percent scale DC-10 model
3. Airframe noise studies on wings with deployed high-lift devices
4. Macaraeg, M. G. "Fundamental Investigations of Airframe Noise,`, AIAA Paper No. 98-2224, June 1998.
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