Experimental investigation of fluid dynamic instability in a transonic cavity flow

Experimental Thermal and Fluid Science

Volumn 31, Issue 4, 2007, Pages 333-347

  Hirahara, Hiroyuki ^a   Kawahashi, Masaaki ^a   Khan, Maksud Uddin ^b   Hourigan, Kerry ^c  

^a SAITAMA UNIVERSITY   (Japan)

^b UNIVERSITY OF TOYAMA   (Japan)

^c MONASH UNIVERSITY   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; RESONANCE; VELOCITY MEASUREMENT; VORTEX FLOW;

CAVITY FLOW; PARTICLE IMAGE VELOCIMETRY (PIV); ROSSITER CONSTANTS; VORTICITY DISTRIBUTION;

TRANSONIC FLOW;

BOUNDARY LAYERS; RESONANCE; TRANSONIC FLOW; VELOCITY MEASUREMENT; VORTEX FLOW;

EID: 33845877744     PISSN: 08941777     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.expthermflusci.2006.05.007     Document Type: Article

References (22)

1. T.B. Owen, Techniques of pressure-fluctuation measurements employed in the RAE low-speed wind tunnels, AGRAD Report 172, 1958.
2. D.A. Norton, Investigation of B47 Bomb Bay Buffet, Boeing Airplane Co. Document No. D12675, 1952.
3. K. Krishnamurty, Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces, NACA Technical Note, 1955, p. 3487.
4. H.E. Plumblee, J.S. Gibson, L.W. Lassiter, A theoretical and experimental investigation of the acoustic response of cavities in an aerodynamic flow, WRDD-TR-61-75, 1962.
5. J.E. Rossiter, Wind-tunnel experiment on the flow over rectangular cavities at subsonic and transonic speeds, Royal Aircraft Establishment ARC R&M, No. 3438, 1964.
6. Heller H.H., Holmes D.G., and Covert E.E. Flow-induced pressure oscillations in shallow cavities. J. Sound Vib. 18 4 (1971) 545-553
7. H.H. Heller, D.B. Bliss, The physical mechanism and flow-induced pressure fluctuations in cavities and concept for their suppression, AIAA Paper, 75-491, 1975.
8. Rockwell D. Prediction of oscillation frequencies for unstable flow past cavities. ASME J. Fluid Eng. 99 (1977) 294-300
9. Rockwell D., and Naudascher E. Review of self-sustaining oscillations of flow past cavities. Trans. ASME, J. Fluids Eng. 100 (1978) 152-165
10. Tam C.K.W. The acoustic mode of a two-dimensional rectangular cavity. J. Sound Vib. 49 (1976) 353-364
11. Tam C.K.W., and Block P.J.W. On the tones and pressure oscillation induced by flow over rectangular cavities. J. Fluid Mech. 89 2 (1978) 373-399
12. Zhang X., and Edwards J.A. Computational analysis of unsteady supersonic cavity flows driven by thick shear layers. Aeronaut. J. 92 919 (1988) 365-374
13. Sakamoto K., Fujii K., Tamura Y., and Matsunaga K. Numerical analysis of a three-dimensional cavity flow field in a supersonic duct. JSME J. B 63 606 (1997) (in Japanese)
14. M.B. Tracy, E.B. Plentovich, J. Chu, Measurements of fluctuating pressure in a rectangular cavity in transonic flow at high Reynolds numbers, NASA TM-4363, 1992.
15. Y. Takakura, F. Higashino, T. Yoshizawa, S. Ogawa, Numerical study on unsteady supersonic cavity flows, in: 27th AIAA Fluid Dynamics Conference, New Orleans, LA, 1996, AIAA 96-2092.
16. Y. Takakura, F. Higashino, T. Yoshizawa, M. Yoshida, S. Ogawa, Parallel computations of unsteady supersonic cavity flows, in: A. Ecer, J. Periaux, N. Satofuka, S. Taylor (Eds.), Parallel Computational Fluid Dynamics (Implementations and Results Using Parallel Computers), 1995, pp. 59-66.
17. G. Raman, E. Envia, T.J. Bencic, Tone noise and nearfield pressure produced by jet-cavity interaction, NASA-TM-20836, 1988.
18. Rowley C.W., Colonius T., and Basu A.J. On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities. J. Fluid Mech. 455 Mar (2002) 315-346
19. Hourigan K., Welsh M.C., Thompson M.C., and Stokes A.N. Aerodynamic sources of acoustic resonance in a duct with baffles. J. Fluids Struct. 4 345 (1990) 70
20. Khan M.U., Hirahara H., and Kawahashi M. Vortex shedding and wave propagation in transonic two-dimensional cavity flows. J. Visualization 3 4 (2001) 331-339
21. Lighthill S.J. On sound generated aerodynamically: I general theory. Proc. Roy. Soc. London A211 (1952) 564
22. Curle N. The influence of solid boundaries upon aerodynamic sound. Proc. Roy. Soc. London A231 (1955) 505