The effect of boundary layer type on trailing edge noise from sharp-edged flat plates at low-to-moderate Reynolds number-Reference-Cited by-同舟云学术

The effect of boundary layer type on trailing edge noise from sharp-edged flat plates at low-to-moderate Reynolds number

Published:2012-08 Issue:17 Volume:331 Page:3976-3988
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Moreau Danielle J.,Brooks Laura A.,Doolan Con J.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference38 articles.

1. Frontiers in Experimental Fluid Mechanics: The Aeroacoustics of Trailing Edges;Blake,1989

2. Trailing edge noise prediction from measured surface pressures;Brooks;Journal of Sound and Vibration,1981

3. R. Schlinker, R. Amiet, Helicopter Rotor Trailing Edge Noise, NASA Contractor Report No. 3470, NASA, 1981.

4. W. Blake, A Statistical Description of Pressure and Velocity Fields at the Trailing Edges of a Flat Strut, Technical Report 4241, David W. Taylor Naval Ship Research and Development Center, Bethesda, MD, 1975.

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