Computation of Trailing-Edge Noise Due to Turbulent Flow over an Airfoil
Author:
Affiliation:
1. Stanford University, Stanford, California 94305-4040
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1582
Reference33 articles.
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2. On sound generated aerodynamically I. General theory
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4. Sound generation by turbulence and surfaces in arbitrary motion
5. Analytical Comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces
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