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Reconsideration of oblique shock wave reflections in steady flows. Part 2. Numerical investigation

Published online by Cambridge University Press:  26 April 2006

J. Vuillon
Affiliation:
Systemes Energetiques et Transferts Thermiques, Universite de Provence, Marseille, France
D. Zeitoun
Affiliation:
Systemes Energetiques et Transferts Thermiques, Universite de Provence, Marseille, France
G. Ben-Dor
Affiliation:
Pearlstone Center for Aeronautical Engineering Studies, Department of Mechanical Engineering, Ben-Gurion University of the Negev, Beer Sheva, Israel

Abstract

The reflection of shock waves over straight reflecting surfaces in steady flows was investigated numerically with the aid of the LCPFCT algorithm. The findings completely supported the experimental results which were reported in Part 1 of this paper (Chpoun et al. 1995). In addition, the dependence of the resulting shock wave configuration on the distance between the trailing edge of the reflecting wedge and the bottom surface, inside the dual-solution domain, was studied. As a result of this study, as well as the one reported in Part 1, the state of the art of shock wave reflections in steady flows was reconsidered.

Type
Research Article
Copyright
© 1995 Cambridge University Press

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