Equivalence Between Schwarzschild and Wiener–Hopf Solutions for Flat Plate Trailing-Edge Scattering
Author:
Affiliation:
1. Peking University, 100871 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of 211 China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J063321
Reference29 articles.
1. Die Beugung und Polarisation des Lichts durch einen Spalt. I
2. LandahlM., Unsteady Transonic Flow, Pergamon Press, New York, 1961, pp. 76–80, Chap. 7.
3. High frequency thin-airfoil theory for subsonic flow
4. Back-scattering correction and further extensions of Amiet's trailing-edge noise model. Part 1: theory
5. Analytical model of the source and radiation of sound from the trailing edge of a swept airfoil
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