Three-dimensional effects on shock wave reflections in steady flows

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Sudani, Norikazu ^a   Sato, Mamoru ^a   Watanabe, Mitsunori ^a   Noda, Junichi ^a   Tate, Atsushi ^a   Karasawa, Toshio ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ASPECT RATIO; DATA VISUALIZATION; SHOCK WAVES;

DEFLECTION ANGLES; DUAL SOLUTIONS; HYSTERESIS EFFECT; MACH REFLECTION; NEUMANN CONDITION; REFLECTION CONFIGURATION; SHOCK WAVE REFLECTION; THREE DIMENSIONAL EFFECT;

THREE DIMENSIONAL COMPUTER GRAPHICS;

EID: 84983138430     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Hornung, H. G., Oertel, H., and Sandeman, R. J., “Transition to Mach Reflexion of Shock Waves in Steady and Pseudosteady Flow With and Without Relaxation,” J. Fluid Mech., Vol. 90, Part 3, 1979, pp. 541-560.
2. Hornung, H. G. and Robinson, M. L., “Transition From Regular to Mach Reflection of Shock Waves. Part 2. The Steady-Flow Criterion,” J. Fluid Mech., Vol. 123, 1982, pp. 155-164.
3. Ivanov, M. S., Gimelshein, S. F., and Beylich, A. E., “Hysteresis Effect in Stationary Reflection of Shock Waves,” Phys. Fluids, Vol. 7, No. 4, 1995, pp. 685-687.
4. Vuillon, V, Zeitoun, D., and Ben-Dor, G., “Numerical Investigation of Shock Wave Reflections in Steady Flows,” AIAA Journal, Vol. 34, No. 6,1996, pp. 1167-1173.
5. Ivanov, M. S., Gimelshein, S. F., Markelov, G. N., and Beylich, A. E., “Numerical Investigation of Shock-Wave Reflection Problems in Steady Flows,” Proceedings of the 20th International Symposium on Shock Waves (Pasadena, 1995), World Scientific, Vol. 2, 1996, ppT 471-476.
6. Hornung, H. G., “On the Stability of Steady-Flow Regular and Mach Reflection,” Shock Waves, Vol. 7, No. 2, 1997, pp. 123-125.
7. Sudani, N. and Hornung, H. G., “Stability and Analogy of Shock Wave Reflection in Steady Flow,” Shock Waves (to be published).
8. Chpoun, A., Passerel, D., Li, H., and Ben-Dor, G., “Reconsideration of Oblique Shock Wave Reflections in Steady Flows. Part 1. Experimental Investigation,” J. Fluid Mech., Vol. 301, 1995, pp. 19-35.
9. Chpoun, A. and Lengrand, J. C, “Experimental Confirmation of the Hysteresis Phenomenon in the Case of Interaction of Two Non-Symmetrical Oblique Shocks,” C. R. Acad. Sci. Paris. 324, Serie 2, 1997, pp. 1-8.
10. Fomin, V. M., Ivanov, M. S., Kharitonov, A. M., Klemenkov, G. P., Kudryavtsev, A. N., Pavlov, A. A., and Hornung, H. G., “The Study of Transition Between Regular and Mach Reflection of Shock Waves in Different Wind Tunnels,” Proceedings of the 12th International Mach Reflection Symposium (Johannesburg, 1996).
11. Ivanov, ~M. S., Gimelshein, S. F., Kudryavtsev, A. N., and Markelov, G. N., “Transition From Regular to Mach Reflection in Two- and Three-Dimensional Flows,” Proceedings of the 21st International Symposium on Shock Waves (Great Keppel Island, 1997).
12. Skews, B. W., “Aspect Ratio Effects in Wind Tunnel Studies of Shock Wave Reflection Transition,” Shock Waves, Vol. 7, 1997, pp. 373-383.
13. Li, H. and Ben-Dor, G., “A Parametric Study of Mach Reflection in Steady Flows,” J. Fluid Mech., Vol. 341, 1997, pp. 101-125.
14. Vuillon, J., Zeitoun, D., and Ben-Dor, G., “Reconsideration of Oblique Shock Wave Reflections in Steady Flows. Part 2. Numerical Investigation,” J. Fluid Mech., Vol. 301, 1995, pp. 37-50.
15. Quirk, J. J., “Amrita-A Computational Facility for CFD Modelling,” VKI 29th CFD Lecture Series, von Karman Inst, for Fluid Dynamics, Feb. 1998.