Mach reflection wave configuration in two-dimensional supersonic jets of overexpanded nozzles

AIAA Journal

Volumn 36, Issue 3, 1998, Pages 488-491

  Li, H ^a   Ben Dor, G ^a  

^a BEN GURION UNIVERSITY OF THE NEGEV   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 1842526557     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.395     Document Type: Article

References (6)

1. Emanuel, G., "Nozzle and Diffuser Flow," Gasdynamics: Theory and Applications, AIAA Education Series, AIAA, New York, 1986, pp. 89-101.
2. Azevedo, D. J., and Liu, C. S., "Engineering Approach to the Prediction of Shock Patterns in Bounded High-Speed Flows," AIAA Journal, Vol. 31, No. 1, 1993, pp. 83-90 .
3. Schotz, M., Levy, A., Ben-Dor, G., and Igra, O., "Analytical Prediction of the Wave Configuration Size in Steady Flow Mach Reflections," Shock Waves, Vol. 7, No. 6, 1997, pp. 363-372.
4. Ben-Dor, G., "Analytical Approaches for Describing Regular and Mach Reflections," Shock Wave Reflection Phenomena, Springer, New York, 1991, pp. 10-16.
5. Chpoun, A., Passeral, D., Lengrand, J. C., Li, H., and Ben-Dor, G., "Mise en Évidence Expérimentale et Numérique d'un Phénoméne d'Hystérésis lors de la Transition Réflexion de Mach-Réflexion Réguliére," Comptes Rendus à l'Académie des Sciences, Vol. 319, Ser. 2, Paris, 1994, pp. 1447-1453 .
6. Vuillon, J., Zeitoun, D., and Ben-Dor, G., "Reconsideration of Oblique Shock Wave Reflection in Steady Flows. Part II: Numerical Investigation," Journal of Fluid Mechanics, Vol. 301, 1995, pp. 37-50.