Curle's theory and implications for dense acoustically compact objects in turbulent flows

9th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2003, Pages

  Leclercq, Damien J J ^a   Symes, Mark K ^a  

^a UNIVERSITY OF ADELAIDE   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS;

COMPACT OBJECTS; EXPERIMENTAL SET UP; FLOW SURFACES; GENERALISATION; NOISE GENERATION MECHANISMS; RELATIVE MOTION; RIGID BODY; WILLIAMS;

ACOUSTIC NOISE;

EID: 85087189322     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3231     Document Type: Conference Paper

References (11)

1. N. CURLE 1955. Proceedings of the Royal Society, Series A 231, 505-514. The influence of solid boundaries upon aerodynamic sound.
2. H.H. HELLER AND S.E. WINDNALL 1970. Journal of the Acoustical Society of America 47,3(2) 924-936. Sound Radiation from Rigid Flow Spoilers Correlated with Fluctuating Forces
3. P.J.F. CLARK AND H.S. RIBNER 1970. Journal of the Acoustical Society of America 46,3(2) 802-805. Direct Correlation of Fluctuating Lift with Radiated Sound for an Airfoil in Turbulent Flow.
4. P. LEEHEY AND C.E. HANSON 1971. Journal of Sound and Vibration 13, 465-483. Aeolian tones associated with resonant vibration.
5. B.T. MARTIN AND D.A. BIES 1992. Journal of Sound and Vibration 155(2), 317-324. On Aerodynamic Noise Generation from Vortex Shedding in Rotating Blades.
6. D.A. BIES, J.M. PICKLES, AND D.J.J. LECLERCQ.1997. Journal of Sound and Vibration 204(4), 631-634. Aerodynamic Noise Generation by a Stationary Body in a Turbulent Air Stream.
7. P.M. MORSE 1948. Vibration and Sound. New York: Mc Graw-Hill; second edition.
8. D.J.J. LECLERCQ 2002. Journal of Sound and Vibration 260(1), 183-190. Comments on Aerodynamic noise generation by a stationary body in a turbulent air stream
9. th AIAA/CEAS Aeroacoustics Conference, Breckenridge (USA). AIAA-2002-2577 "Dense compact rigid object in a turbulent flow: application of Curle's theory"
10. D.P. LOCKARD 2000. Journal of Sound and Vibration 229(4), 987-911. An efficient, two-dimensional implementation of the Ffowcs Williams and Hawkings equation.
11. M. ROGER 1996. Applied Aero-acoustics: prediction methods. Lecture Series 1996-04. February 26 - March 1, 1996. Fundamentals of Aero-acoustics Part I. Von Karman Institute for Fluid Dynamics