An experimental study of the oscillatory flow structure of tone-producing supersonic impinging jets

Journal of Fluid Mechanics

Volumn 542, Issue , 2005, Pages 115-137

  Henderson, Brenda ^a   Bridges, James ^b   Wernet, Mark ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC VARIABLES MEASUREMENT; ACOUSTIC WAVES; FLOW MEASUREMENT; JETS; NOZZLES; OSCILLATIONS; PHOTOGRAPHY; SHOCK WAVES;

DIGITAL PARTICLE IMAGE VELOCIMETRY; OSCILLATORY FLOW; SHADOWGRAPH PHOTOGRAPHY; SUPERSONIC IMPINGING JET;

SUPERSONIC FLOW;

JET IMPINGEMENT; OSCILLATING FLOW; PARTICLE IMAGE VELOCIMETER;

EID: 27844452018     PISSN: 00221120     EISSN: 14697645     Source Type: Journal    
DOI: 10.1017/S0022112005006385     Document Type: Article

References (33)

1. Alvi, F. S. & Iyer, K. G. 1999 Mean and unsteady flowfield properties of supersonic impinging jets with lift plates. AIAA 99-1829.
2. Alvi, F. S., Ladd, J. A. & Bower, W. W. 2002 Experimental and computational investigation of supersonic impinging jets. AIAA J. 40, 599-609.
3. Arunajatesan, S. & Sinha, N. 2002 Large eddy simulations of supersonic impinging jet flow fields. AIAA 2002-4287.
4. Carling, J. C. & Hunt, B. L. 1974 The near wall jet of a normally impinging, uniform, axisymmetric, supersonic jet. J. Fluid Mech. 66, 159-176.
5. Donaldson, C. duP. & Snedeker, R. S. 1971 A study of free jet impingement. Part 1. Mean properties of free and impinging jets. J. Fluid Mech. 45, 281-319.
6. Elevarasan, R., Krothapalli, A., Venkatakrishnan, L. & Lourenco, L. 2002 Suppression of self-sustained oscillations in a supersonic impinging jet. AIAA J. 39, 2366-2373.
7. Elavarasan, R., Lourenco, L., Venkatakrishnan, L. & Krothapalli, A. 1999 Application of PIV to large scale STOVL supersonic jet facility. AIAA Paper A99-16176.
8. Ginzburg, I. P., Semiletenko, B. G., Terpigor'ev, V. S. & Uskov, V. N. 1970 Some singularities of supersonic jet interaction with a plane obstacle. Inzhenerno-Fizicheskii Z. 19, 412-417. (Eng. trans. J. Engng Phys. 19, 1081-1084 (1973)).
9. Ginzburg, I. P., Semiletenko, V. N. & Uskov, V. N. 1975 Experimental study of underexpanded jets impinging normally on a plane baffle. Fluid Mech. Sov. Res. 4, 93-105.
10. Glaznev, V. N. 1977 Sound field of an underexpanded supersonic jet impinging on a barrier. Sov. Phys. Acoust. 23, 142-145.
11. Gummer, J. H. & Hunt, B. L. 1974 The impingement of non-uniform, axisymmetric supersonic jets on a perpendicular flat plate. Israel J. Technol. 12, 221-235.
12. Henderson, B. 1993 Sound source mechanisms of the axisymmetric supersonic impinging jet. PhD thesis, University of Houston.
13. Henderson, B. 2002 The connection between sound production and jet structure of the supersonic impinging jet. J. Acoust. Soc. Am. 111, 735-747.
14. Henderson, B., Bridges, J. & Wernet, M. 2002 An investigation of the flow structure of tone producing supersonic impinging jets. 8th AIAA/ CEAS Aeroacoustics Conf. Breckenridge, Co. AIAA Paper 2002-2529.
15. Henderson, B. & Powell, A. 1993 Experiments concerning tones produced by an axisymmetric choked jet impinging on a flat plate. J. Sound Vib. 168, 307-326.
16. Henderson, B. & Powell, A. 1996 Sound-producing mechanisms of the axisymmetric choked jet impinging on small plates: The production of primary tones. J. Acoust. Soc. Am. 99, 153-162.
17. Henderson, B. & Powell, A. 1997 The use of an array to explain the sound characteristics of secondary small plate tones produced by the impingement of an axisymmetric choked jet. J. Acoust. Soc. Am. 102, 1454-1462.
18. Iwamoto, J. & Deckker, B. E. L. 1981 Development of flow field when a symmetrical underexpanded sonic jet impinges on a flat plate. J. Fluid Mech. 113, 299-313.
19. Kalghatgi, G. T. & Hunt, B. L. 1976 The occurrence of stagnation bubbles in supersonic jet impingement flows. Aero. Q. 27, 169-185.
20. Krothapalli, A., Rajkuperan, E., Alvi, F. & Lourenco, L. 1999 Flow field noise characteristics of a supersonic impinging jet. J. Fluid Mech. 392, 155-181.
21. Kuo, C. & Dowling, A. P. 1996 Oscillations of a moderately underexpanded choked jet impinging upon a flat plate. J. Fluid Mech. 315, 267-291.
22. Melling, A. 1997 Tracer particles and seeding for particle image velocimetry. Meas. Sci. Technol. 8, 1406-1416.
23. Morch, K. A. 1964 A theory for the mode of operation of the Hartmann air jet generator. J. Fluid Mech. 20, 141-159.
24. Morch, K. A. 1973 On the impingement of a composite jet. The Technical University of Denmark Rep. 47.
25. Nakatogawa, T., Hirata, M. & Kukita, Y. 1971 Disintegration of a supersonic jet impinging normally on a flat plate. J. Spacecraft 8, 410-411.
26. Powell, A. 1953 On edge tones and associated phenomena. Acustica 3, 233-243.
27. Powell, A. 1958 One-dimensional treatment of weak disturbances of a shock wave. Fluid Motion Sub-committee, Aeronautical Research Council (UK).
28. Powell, A. 1988 The sound-producing oscillations of round underexpanded jet impinging on normal plates. J. Acoust. Soc. Am. 83, 515-533.
29. Prandtl, L. 1904 Uber die stationarem wellen in einem gasstrahle. Phys. Z. 5, 599-601.
30. Ribner, H. S. 1953 Convection of a pattern of vorticity through a shock wave. NACA TN 2864.
31. Ribner, H. S. & Moore, F. K. 1953 Unsteady interaction of disturbances with a shock wave, with applications to turbulence and noise. Presented at the Heat Transfer and Fluid Mechanics Institute, Palo Alto, CA.
32. Semiletenko, B. G., Sobkolov, B. N. & Uskov, V. N. 1974 Features of unstable interaction between a supersonic jet and infinite baffle. Fluid Mech. Sov. Res. 3, 90-95.
33. Wernet, M. P. 1999 Fuzzy logic digital PIV processing software. 18th Intl Congress on Instrumentation for Aerospace Simulation Facilities (ICIASF) Conf. Toulouse, France.