Shear effects in aeroacoustic predictions

Journal of Sound and Vibration

Volumn 267, Issue 4, 2003, Pages 961-966

  Singer, B A ^a   Lockard, D P ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC WAVES; CODES (SYMBOLS); FINITE DIFFERENCE METHOD; RUNGE KUTTA METHODS; SHEAR FLOW;

SHEAR LAYER;

COMPUTATIONAL FLUID DYNAMICS;

EID: 0142247102     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0022-460X(03)00216-5     Document Type: Article

References (8)

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3. B.A. Singer, D.P. Lockard, K.S. Brentner, Computational aeroacoustic analysis of slat trailing-edge flow, American Institute of Aeronautics and Astronautics Journal 38 (9) (2000) 1558-1564.
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5. J.E. Ffowcs Williams, D.L. Hawkings, Sound generated by turbulence and surfaces in arbitrary motion, Philosophical Transactions of the Royal Society A264 (1151) (1969) 321-342.
6. M.J. Lighthill, On sound generated aerodynamically, II: turbulence as a source of sound, Proceedings of the Royal Society A222 (1954) 1-32.
7. K.S. Brentner, F. Farassat, An analytical comparison of the acoustic analogy and Kirchhoff formulation for moving surfaces, American Institute of Aeronautics and Astronautics Journal 36 (8) (1998) 1379-1386.
8. D.P. Lockard, An efficient, two-dimensional implementation of the Ffowcs Williams and Hawkings equation, Journal of Sound and Vibration 229 (4) (2000) 897.