An investigation of airfoil tonal noise at different Reynolds numbers and angles of attack-Reference-Cited by-同舟云学术

An investigation of airfoil tonal noise at different Reynolds numbers and angles of attack

Published:2013-01 Issue:1 Volume:74 Page:38-48
ISSN:0003-682X
Container-title:Applied Acoustics
language:en
Short-container-title:Applied Acoustics

Author:

Chong T.P.,Joseph P.F.,Kingan M.J.

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference23 articles.

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2. Unsteady flow computations of a slat with a blunt trailing edge;Khorrami;AIAA J.,2000

3. Computational aeroacoustic simulations of leading-edge slat flow;Takeda;JSV,2004

4. The radiation of sound from an airfoil immersed in a laminar flow;Clark;J. Eng. Power – Trans. ASME,1971

5. Hersh AS, Hayden RE. Aerodynamic sound radiation from lifting surfaces with and without leading-edge serrations. NASA contract, report no. 114370; 1971.

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