Reconsideration of oblique shock wave reflections in steady flows. Part 1. Experimental investigation-Reference-Cited by-同舟云学术

Reconsideration of oblique shock wave reflections in steady flows. Part 1. Experimental investigation

Published:1995-10-25 Issue: Volume:301 Page:19-35
ISSN:0022-1120
Container-title:Journal of Fluid Mechanics
language:en
Short-container-title:J. Fluid Mech.

Author:

Chpoun A.,Passerel D.,Li H.,Ben-Dor G.

Abstract

The reflection of shock waves over straight reflecting surfaces in steady flows was investigated experimentally using the supersonic wind tunnel of Laboratoire d'Aerothermique du CNRS, Meudon, France. The results for a flow Mach number M0 = 4.96 contradict the state of the art regarding the regular [harr ] Mach reflection transition in steady flows. Not only was a hysteresis found to exist in this transition, but, unlike previous reports, regular reflection configurations were found to be stable in the dual-solution domain in which theoretically both regular and Mach reflection are possible.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

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