Time accurate numerical study of turbulent supersonic jets

Journal of Sound and Vibration

Volumn 270, Issue 1-2, 2004, Pages 297-321

  Rona, A ^a   Zhang, X ^b  

^a UNIVERSITY OF LEICESTER   (United Kingdom)

^b UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ENTHALPY; HEAT FLUX; JETS; KINETIC ENERGY; NOZZLES; PRANDTL NUMBER; REYNOLDS NUMBER; SPECIFIC HEAT; STEADY FLOW; TURBULENT FLOW; VISCOSITY;

SHOCK EXPANSION SYSTEMS; STROUHAL NUMBER;

SUPERSONIC FLOW;

EID: 0942279341     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0022-460X(03)00537-6     Document Type: Article

References (34)

1. Y. Nakamura, T. Oishi, J. Julliard, A. Dravet, Mixer-ejector noise characteristics with aerodynamic performances, AIAA Paper 98-2325, Fourth CEAS/AIAA Aeroacoustics Conference, Toulouse, France, 1998.
2. J. Seiner, D. McLaughlin, C. Liu, Supersonic jet noise generated by large-scale instabilities, Technical Paper 2072, NASA, September 1982.
3. T. Norum, J. Seiner, Measurements of mean static pressure and far-field acoustics of shock-containing supersonic jets, Technical Memorandum 84521, NASA, 1982.
4. A. Powell, On the mechanism of chocked jet noise, Proceedings of the Royal Society of London 66 (408B) (1953) 1039-1056.
5. J. Seiner, T. Norum, Aerodynamic aspects of shock containing jet plumes, AIAA Paper 80-0965, Sixth AIAA Aeroacoustics Conference, Hartford, CT, USA, June 1980.
6. J. Seiner, Advances in high speed jet aeroacoustics, AIAA Paper 84-2275, October 1984.
7. G. Raman, Advances in understanding jet screech, AIAA Paper 98-0279, 36th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, USA, January 1998.
8. G. Raman, Advances in understanding supersonic jet screech: review and perspective, Progress in Aerospace Sciences 34 (1-2) (1998) 45-106.
9. R. Westley, J. Woolley, Flow and sound visualization of an axisymmetric chocked jet (24 in schlieren), Film 20, National Research Council of Canada, National Aeronautical Establishment, YC. NRC, ME, May 1969.
10. J. Panda, An experimental investigation of screech noise generation, AIAA Paper 96-1718, Second AIAA/CEAS Aeroacoustics Conference, State College, PA, USA, May 1996.
11. J. Panda, Shock oscillation in underexpanded screeching jets, Journal of Fluid Mechanics 963 (1998) 173-198.
12. D. Pack, On the formation of shock waves in supersonic jets (two-dimensional flow), The Quarterly Journal of Mechanics and Applied Mathematics 1 (1948) 451-469.
13. J. Hay, E. Rose, In-flight shock cell noise, Journal of Sound and Vibration 11 (4) (1970) 411-420.
14. C. Tam, F. Hu, On the three families of instability waves of high-speed jets, Journal of Fluid Mechanics 201 (1989) 447-483.
15. G. Lilley, X. Zhang, A. Rona, Progress in computational aeroacoustics in predicting the noise radiated from turbulent flows, International Journal of Acoustics and Vibration 2 (1) (1997) 3-10.
16. D. Wilcox, Turbulence Modeling for CFD, Griffin Printing, Glendale, CA, USA, 1993.
17. G. Lilley, On the noise from air jets, Report 20376, Aeronautical Research Council, UK, September 1958.
18. F. Menter, Improved two-equation k-ω turbulence models for aerodynamic flows, Technical Memorandum 103975, NASA, 1992.
19. X. Zhang, J. Edwards, A computational analysis of supersonic jet instability wave interaction, AIAA Paper 94-2194, 25th AIAA Fluid Dynamics Conference, Colorado Springs, CO, USA, June 1994.
20. P. Roe, Approximate Riemman solvers, parameter vectors and difference schemes, Journal of Computational Physics 43 (2) (1981) 357-372.
21. P. Roe, Characteristics-based schemes for the Euler equations, Annual Review of Fluid Mechanics 18 (1986) 337-365.
22. J. Quirk, An Adaptive Grid Algorithm for Computational Shock Hydrodynamics, Ph.D. Thesis, Cranfield Institute of Technology, Cranfield, UK, January 1991.
23. M. Manna, A Three Dimensional High Resolution Compressible Flow Solver, Ph.D. Thesis, Université Catholique de Louvain, Belgium, October 1992.
24. A. Rona, Aerodynamic and Aeroacoustic Estimations of Oscillatory Supersonic Flows, Ph.D. Thesis, University of Southampton, Southampton, UK, June 1997.
25. C. Tam, Jet noise generated by large-scale coherent motion, in: H. Hubbard (Ed.), Aeroacoustics of Flight Vehicles: Theory and Practice, Reference Publication 1258, Vol. 1, NASA, Acoustical Society of America, Woodbury, NY, 1995, pp. 311-390.
26. M. Harper-Bourne, M. Fisher, The noise from shock waves in supersonic jets, in: Noise Mechanisms, AGARD Conference Proceedings 131, Brussels, Belgium, Advisory Group for Aeronautical Research and Development, 1973, pp. 11-1-11-13.
27. T. Colonuis, S. Lele, P. Moin, Sound generation in a mixing layer, Journal Fluid Mechanics 330 (1997) 375-409.
28. J. Seiner, M. Ponton, Aeroacoustic data for high Reynolds number supersonic axisymmetric jets, Technical Memorandum 86296, NASA, January 1985.
29. J. Seiner, J. Manning, M. Ponton, The preferred spatial mode of instability for a Mach 2 jet, AIAA Paper 86-1942, July 1986.
30. M. Gharib, A. Roshko, The effect of flow oscillations on cavity drag, Journal of Fluid Mechanics 177 (1987) 44-50.
31. H. Shen, C. Tam, Numerical simulation of the generation of axisymmetric mode jet screech tones, AIAA Paper 98-0283, 36th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, USA, January 1998.
32. T. Manning, S. Lele, Numerical simulations of shock-vortex interactions in supersonic jet screech, AIAA Paper 98-0282, 36th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, USA, January 1998.
33. A. Michalke, Survey on jet instability theory, Progress in Aerospace Sciences 21 (1984) 159-199.
34. B. Mitchell, S. Lele, P. Moin, Direct computation of sound generated by subsonic and supersonic axisymmetric jets, Report TF-66, Thermosciences Division, Department of Mechanical Engineering, Stanford University, CA, USA, November 1995.