Unstructured adaptive mesh computations of rotorcraft high-speed impulsive noise
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
2. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46787
Reference14 articles.
1. Sound generation by turbulence and surfaces in arbitrary motion
2. "Goldstein. M. E. Aeroacoustics, McGraw-Hill, New York, 1976, pp.346-357.
3. Geometrical acoustics and transonic helicopter sound
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