Numerical simulation of the generation mechanism of axisymmetric supersonic jet screech tones

Physics of Fluids

Volumn 17, Issue 8, 2005, Pages 1-8

  Li, X D ^a   Gao, J H ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FLOW OF FLUIDS; INTEGRAL EQUATIONS; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; NOZZLES; RUNGE KUTTA METHODS; TURBULENCE;

SUPERSONIC JET SCREECH TONES; TURBULENCE MODEL;

JETS;

ACOUSTICS;

EID: 24144453171     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.2033909     Document Type: Article

References (28)

1. A. Powell, "On the noise emanating from a two-dimensional jet above the critical pressure," Aeronaut. Q. 4, 103 (1953). AEQUAY 0001-9259
2. H. Shen and C. K. W. Tam, "Numerical simulation of the generation of axisymmetric mode jet screech tones," AIAA J. 36, 1801 (1998). AIAJAH 0001-1452
3. A. T. Thies and C. K. W. Tam, "Computational of turbulent axisymmetric and nonaxisymmetric jet flows using the k-ε model," AIAA J. 34, 309 (1996). AIAJAH 0001-1452
4. M. K. Ponton and J. M. Seiner, "The effects of nozzle exit lip thickness on plume resonance," J. Sound Vib. 154, 531 (1992). JSVIAG 0022-460X 10.1016/0022-460X(92)90784-U
5. T. A. Manning and S. K. Lele, "Numerical simulation of shock-vortex interactions in supersonic jet screech," AIAA Paper No. 1998-0282 (1998).
6. C. Y. Loh, L. S. Hultgren, and P. C. E. Jorgenson, "Near field screech noise computation for an underexpanded supersonic jet by the CE/ SE method," AIAA Paper No. 2001-2252 (2001).
7. P. C. E. Jorgenson and C. Y. Loh, "Computing axisymmetric jet screech tones using unstructured grids," AIAA Paper No. 2002-3889 (2002).
8. B. Imamoglu and P. Balakumar, "Computation of shock induced noise in imperfectly expanded supersonic jets," AIAA Paper No. 2002-2527 (2002).
9. C. K. M. Tam, "Excitation of instability waves by sound-A physical interpretation," J. Sound Vib. 105, 169 (1986). JSVIAG 0022-460X 10.1016/0022-460X(86)90228-2
10. R. Westley and J. H. Woolley, "An investigation of the near noise fields of a choked axisymmetric jet," in Aerodynamic Noise, Proceedings of AFOSR-V. T. A. S. Symposium, Toronto, Canada, 20-21 May 1968, edited by H. B. Ribner, pp. 147-167.
11. M. Suda, T. A. Manning, and S. Kaji, "Transition of oscillation modes of rectangular supersonic jet in screech," AIAA Paper No. 1993-4323 (1993).
12. J. Panda, "Shock oscillation in underexpanded screeching jets," J. Fluid Mech. 363, 173 (1998). JFLSA7 0022-1120 10.1017/ S0022112098008842
13. A. Dillmann, "Linear potential theory of steady internal supersonic flow with quasi-cylindrical geometry. Part 2. Free jet flow," J. Fluid Mech. 286, 327 (1995). JFLSA7 0022-1120
14. G. Turpin and J. Troyes, "Validation of a two-equation turbulence model for axisymmetric reacting and non-reaction flows," AIAA Paper No. 2000-3463 (2000).
15. T. H. Shih, L. A. Povinelli, and N. S. Liu, "Application of generalized wall function for complex turbulent flows," J. Turbul. 4, 015 (2003). ZZZZZZ 1468-5248
16. T. H. Shih, L. A. Povinelli, N. S. Liu, M. G. Potapczuk, and J. L. Lumley, "Turbulent surface flow and wall function," AIAA Paper No. 1999-2392 (1999).
17. T. D. Norum and M. C. Brown, "Simulated high-speed flight effects on supersonic jet noise," AIAA Paper No. 1993-4388 (1993).
18. C. K. W. Tam and J. C. Webb, "Dispersion-relation-preserving finite difference schemes for computational acoustics," J. Comput. Phys. 107, 262 (1993). JCTPAH 0021-9991 10.1006/jcph.1993.1142
19. F. Q. Hu, M. Y. Hussaini, and J. L. Manthey, "Low-dissipation and low-dispersion Runge-Kutta schemes for computational acoustics," J. Comput. Phys. 124, 177 (1996). JCTPAH 0021-9991 10.1006/jcph.1996.0052
20. D. Stanescu and W. G. Habashi, "2N-storage low-dissipation and low-dispersion Runge-Kutta schemes for computational aeroacoustics," J. Comput. Phys. 143, 674 (1998). JCTPAH0021-9991 10.1006/jcph.1998.5986
21. C. K. W. Tam, J. C. Webb, and T. Z. Dong, "A study of the short wave components in computational acoustics," J. Comput. Acoust. 1, 1 (1993). JCOAEJ 0218-396X 10.1142/S0218396X93000020
22. C. K. W. Tam and H. Shen, "Direct computation of nonlinear acoustic pulses using high order finite difference schemes," AIAA Paper No. 1993-4325 (1993).
23. C. K. W. Tam, "Advances in numerical boundary conditions for computational aeroacoustics," J. Comput. Acoust. 6, 377 (1998). JCOAEJ 0218-396X
24. C. K. W. Tam and Z. Dong, "Radiation and outflow boundary conditions for direct computation of acoustic and flow disturbances in a nonuniform mean flow," J. Comput. Acoust. 4, 175 (1996). JCOAEJ 0218-396X
25. C. K. W. Tam and Z. Dong, "Wall boundary conditions for high-order finite-difference schemes in computational aeroacoustics," Theor. Comput. Fluid Dyn. 6, 303 (1994). TCFDEP 0935-4964 10.1007/BF00311843
26. M. Lummer, H. A. Grogger, and J. M. Delfs, "Using RANS mean flow fields in numerical aeroacoustics simulations (CAA)," in NATO RTO-AVT Symposium on Ageing Mechanism and Control, Part A-Developments in Computational Aero- and Hydro-Acoustics, Manchester, UK, 8-11 October 2001.
27. J. Panda and R. G. Seasholtz, "Measurement of shock structure and shock-vortex interaction in underexpanded jets using Rayleigh scattering," Phys. Fluids PHFLE6 11, 3761 (1999). 1070-6631 10.1063/1.870247
28. J. Panda, G. Raman, and K. B. M. Q. Zaman, "Underexpanded screeching jets from circular, rectangular and elliptic nozzles," NASA Tech. Memo. 212481 (2003).