Aeroacoustics computation for nearly fully expanded supersonic jets using the CE/SE method

6th Aeroacoustics Conference and Exhibit

Volumn , Issue , 2000, Pages

  Loh, Ching Y ^a   Hultgren, Lennart S ^a   Wang, Xiao Y ^a   Chang, Sin Chung ^a   Jorgenson, Philip C E ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894620261     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Chang, S. C., The Method of Space-Time Conservation Element and Solution Element-A New Approach for Solving the Navier-Stokes and Euler Equations," Journal of Computational Physics, vol. 119, pp. 295-324 (1995).
2. Chang, S. C. and To, W. M., "A Brief Description of a New Numerical Framework for Solving Conservation Laws-The Method of Space-Time Conservation Element and Solution Element," Proceedings of the Thirteenth International Conference on Numerical Methods in Fluid Dynamics, Rome, Italy, 1992, M. Napolitano and F. Sabetta, eds., Lecture Notes in Physics 414, Springer-Verlag, pp. 396-400. Also published as NASA TM 105757 (1992).
3. Chang, S. C., Yu, S. T" Himansu, A., Wang, X. Y., Chow, C. Y. and Loh, C. Y "The Method of Space-Time Conservation Element and Solution Element-A New Paradigm for Numerical Solution of Conservation Laws", Computational Fluid Dynamics Review, eds. M. M. Hafez and K. Oshima, Wiley (1997).
4. Chang, S. C., Wang, X. Y. and Chow, C. Y., "The Space-Time Conservation Element and Solution Element Method - A New High-Resolution and Genuine Multidimensional Paradigm for Solving Conservation Laws", J. Comput. Phys. vol. 156, pp. 89-136 (1999).
5. Loh, C. Y., Hultgren, L. S. and Chang, S.-C., "Computing Waves in Compressible Flow Using the Space-Time Conservation Element Solution Element Method," AIAA Paper 98-0369 (1998).
6. Loh, C. Y., Hultgren, L. S., Chang, S.-C. and Jorgenson, P. C. E., "Vortex Dynamics Simulation in Aeroacoustics by the Space-Time Conservation Element Solution Element Method," AIAA Paper 99- 0359(1999).
7. Loh, C. Y., Hultgren, L. S., Chang, S.-C. and Jorgenson, P. C. E., "Noise Computation for a Shock- Containing Supersonic Axisymmetric Jet Using the CE/SE Method" AIAA Paper 2000-0475 (2000).
8. Loh, C. Y., Chang, S. C. and Scott, J. R., "Computational Aeroacoustics via the Space-Time Conservation Element/Solution Element Method", AIAA Paper 96-1687 (1996).
9. Yu, S. T. and Chang, S.-C., "Treatment of Stiff Source Terms in Conservation Laws by the Method of Space-Time Conservation Element and Solution Element", AIAA Paper 97-0435 (1997).
10. Oertel, H., "Mach wave radiation of hot supersonic jets", in Mechanics of Sound Generation in Flows, (ed. E. A. Muller), pp. 275-281, Springer (1979).
11. Oertel, H., "Mach wave radiation of hot supersonic jets investigated by means of the shock tube and new optical techniques", Proceedings of the 12th Intl. Symp. on Shock Tube and Waves, Jerusalem (eds. A. Lifshitz and J. Rom), pp. 266-275 (1980).
12. Oertel, H., "Coherent structures producing Mach waves inside and outside of the supersonic jet", Structure of Complex Turbulent Shear Flow, IU- TAM Symp. Marseille (1982).
13. Tam, C. K. W, and Hu, F. Q., "On the three families of instability waves of high-speed jets", J. Fluid Mech., vol. 201, pp. 447-483 (1989).
14. Shih, S. H., Hixon, D. R. and Mankbadi, R. R., "Zonal Approach for Prediction of Jet Noise", AIAA vol. 13, pp. 745-752 (1997).
15. Troutt, T. R. and McLaughlin, D. K., "Experiments on the flow and acoustic properties of a moderate- Reynolds-number supersonic jet", J. Fluid Mech., vol. 116, pp. 123-156(1982).