Transition between regular and Mach reflections of shock waves in steady flows
Author:
Affiliation:
1. Russian Academy of Sciences, Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2511
Reference24 articles.
1. Transition to Mach reflexion of shock waves in steady and pseudosteady flow with and without relaxation
2. Transition from regular to Mach reflection of shock waves Part 2. The steady-flow criterion
3. Hysteresis effect in stationary reflection of shock waves
4. Reconsideration of oblique shock wave reflections in steady flows. Part 1. Experimental investigation
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