Mach number and temperature effects on Mach wave emission from supersonic jets

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn , Issue , 2008, Pages

  Nonomura, Taku ^a,c   Fujii, Kozo ^b,c  

^a UNIVERSITY OF TOKYO   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c Department of Aeronautics and Astronautics ^*

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC EMISSIONS; ACOUSTIC FIELDS; ACOUSTIC VARIABLES MEASUREMENT; ACOUSTIC WAVE TRANSMISSION; AVIATION; FLOW FIELDS; MACH NUMBER; NOZZLE DESIGN; ROCKET NOZZLES; ROCKETS; STROUHAL NUMBER; SUPERSONIC AERODYNAMICS; TEMPERATURE;

COMPACT SCHEMES; FLUID ANALYSIS; INCREASING TEMPERATURES; MACH WAVE EMISSION; NUMBER EFFECTS; ROCKET PLUMES; SOUND PRESSURE LEVEL; SUPERSONIC JETS;

FIGHTER AIRCRAFT;

EID: 77957774118     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-6587     Document Type: Conference Paper

References (21)

1. Eldred, K. M., "Acoustic Loads Generated by Propulsion System," SP 8072, NASA, 1971.
2. Varnier, J., "Experimental Study and Simulation of Rocket Engine Freejet Noise," AIAA Journal, Vol. 39, No. 10, 2001, pp. 1851-1859.
3. Kawai, S., Tsutsumi, S., Takaki, R., and Fujii, K., "Computational Aeroacoustics Analysis of Overexpanded Supersonic Jet Impingement on a Flat Plate With/Without Hole," ASME FEDSM 2007-27563, 2007.
4. Tsutsumi, S., Shima, E., Takaki, R., and Fujii, K., "Generation and Propagation of Pressure Waves from H-IIA Launch Vehicle at Lift-off," AIAA Paper 2008-390, 2008.
5. Bodony, D. J. and Lele, S. K., "Review of the Current Status of Jet Noise Prediction Using Large-Eddy Simulation," AIAA Paper 2006-0468, 2006.
6. Nonomura, T. and Fujii, K., "Computational Analysis of Characteristics and Mach Number Effects on Noise Emission from Ideally Expanded Highly Supersonic Free-Jet," ASME FEDSM 2007-37539, 2007.
7. Nonomura, T. and Fujii, K., "Over-expansion Effects on Mach 3.0 Supersonic Jet Acoustics," AIAA paper 2008-2836, 2008.
8. Jiang, G.-S. and Shu, C.-W., "Efficient implementation of weighted ENO schemes," Journal of Computational Physics, Vol. 126, 1996, pp. 202-228.
9. Lele, S. K., "Compact Finite Difference Schemes with Spectral-like Resolution." Journal of Computational Physics, Vol. 103, No. 1, 1992, pp. 16-42.
10. Deng, X. G. and Zhang, H., "Developing High-order Weighted Compact Nonlinear Schemes," Journal of Computational Physics, Vol. 165, 2000, pp. 22-44.
11. Nonomura, T., Iizuka, N., and Fujii, K., "Uniform Flow Preserving Property of High Order Upwind Scheme on Generalized Coordinate System," Proceedings of International Conference on Computational Fluid Dynamics, 2006.
12. Shima, E. and Jounouchi, T., "Role of CFD in Aeronautical Engineering (No.14) -AUSM type Upwind Schemes-," Proceedings of the 14th NAL Symposium on Aircraft Computational Aerodynamics, NAL, 1997, pp. 7-12.
13. Liou, M. S. and Steffen, Jr, C., "A New Flux Splitting Scheme," Journal of Computational Physics, Vol. 107, 1993, pp. 23-39.
14. Visbal, M. R. and Gaitonde, D. V., "On the Use of Higher-Order Finite-Difference Schemes on Curvilinear and Deforming Meshes," Journal of Computational Physics, Vol. 181, 2002, pp. 155-185.
15. Boris, J. P., Grinstein, F. F., Oran, E., and Kolbe, R. J., "New Insights Into Large Eddy Simulation," Fluid Dynamics Research, Vol. 10, 1992, pp. 199-228.
16. Ishiko, K., Ohnishi, N., and Sawada, K., "Implicit LES for Two-Dimensional Turbulence Using Shock Capturing Monotone Scheme," AIAA paper 2006-703, 2006.
17. Ishiko, K., Ohnishi, N., and Sawada, K., "Implicit LES of Compressible Turbulent Flow," AIAA Paper 2007-920, 2007.
18. Nonomura, T., Characteristics of Acoustic Waves Generated by Flow Instability of Supersonic Jets, Ph.D. thesis, University of Tokyo, 2008.
19. Papamoschou, D. and Roshko, A., "The Compressible Turbulent Shear Layer: An Experimental Study," Journal of Fluid Mechanics, Vol. 197, 1988, pp. 453-477.
20. Freund, J. B., Lele, S. K., and Moin, P., "Compressibility Effects in a Turbulent Annular Mixing Layer. Part2. Mixing of a passive scalar," Journal of Fluid Mechanics, Vol. 421, 2000, pp. 269-292.
21. Troutt, T. R. and McLaughlin, D. K., "Experiments on the flow and acoustic properties of a moderate-Reynolds-number supersonic jet," Journal of Fluid Mechanics, Vol. 116, 1982, pp. 123-156.