Numerical simulation of the generation of axisymmetric mode jet screech tones

AIAA Journal

Volumn 36, Issue 10, 1998, Pages 1801-1807

  Shen, Hao ^a   Tam, Christopher K W ^a,b  

^a FLORIDA STATE UNIVERSITY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000365708     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.295     Document Type: Article

References (19)

1. Tam, C. K. W., "Supersonic Jet Noise," Annual Review of Fluid Mechanics. Vol. 21, 1995, pp. 17-43.
2. Powell, A., "On the Mechanism of Choked Jet Noise," Proceedings of the Physical Society, London, Vol. 66, 1953, pp. 1039-1056.
3. Tam, C. K. W., Shen, H., and Raman, G., "Screech Tones of Supersonic Jets from Bevelled Rectangular Nozzles," AIAA Journal, Vol. 35, No. 7, 1997, pp. 1119-1125.
4. Tam, C. K. W., "Computational Aeroacoustics: Issues and Methods," AIAA Journal, Vol. 33, No. 10, 1995, pp. 1788-1796.
5. Thies, A. T., and Tam, C. K. W., "Computation of Turbulent Axisymmetric and Nonaxisymmetric Jet Flows Using the k-ε Model," AIAA Journal, Vol. 34, No. 2, 1996, pp. 309-316.
6. Tam, C. K. W., and Webb, J. C., "Dispersion-Relation-Preserving Finite Difference Schemes for Computational Acoustics," Journal of Computational Physics, Vol. 107, Aug. 1993, pp. 262-281.
7. Dong, Z., "Fundamental Problems in Computational Acoustics," Ph.D. Thesis, Dept. of Mathematics, Florida State Univ., Tallahassee, FL, Spring 1994.
8. Tam, C. K. W., "Advances in Numerical Boundary Conditions for Computational Aeroacoustics," AIAA Paper 97-1774, June 1997; see also Journal of Computational Acoustics (to be published).
9. Tam, C. K. W., "Advances in Numerical Boundary Conditions for Computational Aeroacoustics," AIAA Paper 97-1774, June 1997; see also Journal of Computational Acoustics (to be published).
10. Tam, C. K. W., and Dong, Z., "Radiation and Outflow Boundary Conditions for Direct Computation of Acoustic and Flow Disturbances in a Nonuniform Mean Flow," Journal of Computational Acoustics, Vol. 4, June 1996, pp. 175-201.
11. Tam, C. K. W., and Dong, Z., "Wall Boundary Conditions for High-Order Finite Difference Schemes in Computational Aeroacoustics," Theoretical and Computational Fluid Dynamics, Vol. 8, Oct. 1994, pp. 303-322.
12. Tam, C. K. W., Webb, J. C., and Dong, Z., "A Study of the Short Wave Components in Computational Acoustics," Journal of Computational Acoustics, Vol. 1, March 1993, pp. 1-30.
13. Tam, C. K. W., and Shen, H., "Direct Computation of Nonlinear Acoustic Pulses Using High-Order Finite Difference Schemes," AIAA Paper 93-4325, Oct. 1993.
14. Westley, R., and Woolley, J. H., "An Investigation of the Near Noise Fields of a Choked Axisymmetric Air Jet," Proceedings of AFOSR-UTIAS Symposium on Aerodynamic Noise, Univ. of Toronto Press, Toronto, ON, Canada, 1968, pp. 147-167.
15. Norum, T. D., "Screech Suppression in Supersonic Jets," AIAA Journal, Vol. 21, No. 2, 1983, pp. 235-240.
16. Ponton, M. K., and Seiner, J. M., "The Effects of Nozzle Exit Lip Thickness on Plume Resonance," Journal of Sound and Vibration, Vol. 154, No. 3, 1992, pp. 531-549.
17. Lau, J. C., "Effects of Exit Mach Number and Temperatures on MeanFlow and Turbulence Characteristics in Round Jets," Journal of Fluid Mechanics, Vol. 105, 1981, pp. 193-218.
18. Norum, T. D., and Brown, M. C., "Simulated High-Speed Flight Effects on Supersonic Jet Noise," AIAA Paper 93-4388, Oct. 1993.
19. Tam, C. K. W., and Burton, D. E., "Sound Generated by Instability Waves of Supersonic Flows: Part 1, Two Dimensional Mixing Layers; Part 2, Axisymmetric Jets," Journal of Fluid Mechanics, Vol. 135, 1984, pp. 249-295.