Near-field fluctuations and far-field noise of a three-element airfoil system by a discrete vortex method

DOI10.1016/j.amc.2010.01.129zbMath1303.76080OpenAlexW2124099761MaRDI QIDQ972150

B. E. Eshmatov

Publication date: 25 May 2010

Published in: Applied Mathematics and Computation (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.amc.2010.01.129

zbMATH Keywords

vortex methodaeroacousticsairframe noisehigh-lift system

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25)

Cites Work

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• Kutta condition for sharp edge flows
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• Application of the Ffowcs Williams/Hawkings equation to two-dimensional problems
• An Introduction to Fluid Dynamics
• Theory of Vortex Sound
• Sound generation by turbulence and surfaces in arbitrary motion
• Radiation from vortex filament motion near a half plane
• An inviscid model of two-dimensional vortex shedding
• On sound generated aerodynamically I. General theory
• On sound generated aerodynamically II. Turbulence as a source of sound

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