Trailing edge noise at low Mach numbers, Part 2: Attached and separated edge flows

Journal of Sound and Vibration

Volumn 234, Issue 5, 2000, Pages 761-775

  Howe, M S ^a  

^a Boston University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; APPROXIMATION THEORY; BOUNDARY LAYER FLOW; SPECTRUM ANALYSIS; TURBULENT FLOW;

MACH NUMBER; TRAILING EDGE NOISE;

ACOUSTIC NOISE;

EID: 0034226025     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1999.2861     Document Type: Article

References (10)

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3. BLAKE W. K. Excitation of plates and hydrofoils by tailing edge flows. Sevik M. M. Proceedings of the International Symposium on Turbulence Induced Vibrations and Noise of Structures. 1983;45-65 American Society of Mechanical Engineers, New York.
4. J. GERSHFELD, W. K. BLAKE, C. W. KNISELY, 1988, American Institute of Aeronautics and Astronautics Paper 88-3826-CP, Trailing edge flow and aerodynamic sound.
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10. CORCOS G. M. The structure of the turbulent pressure field in boundary layer flows. Journal of Fluid Mechanics. 18:1964;353-378.