Numerical simulation of aerodynamic sound radiation from two-dimensional wing
Author:
Affiliation:
1. Mitsubishi Electric Corp., Amagasaki, Japan
2. Tokyo, University, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-2672
Reference4 articles.
1. x 2-40-
2. z/a(x 10-1) Fig.9 Surface dipole strength distribution on airfoil.
3. Surface dipole strength by cross‐correlation method
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1. An Overset Finite-Element Large-Eddy Simulation Method With Applications to Turbomachinery and Aeroacoustics;Journal of Applied Mechanics;2003-01-01
2. Turbulence simulation in the Japanese automotive industry;Engineering Turbulence Modelling and Experiments;1996
3. Numerical prediction of aerodynamic noise radiated from low Mach number turbulent wake;31st Aerospace Sciences Meeting;1993-01-11
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