Dynamic Shock Wave Reflection
Author:
Affiliation:
1. University of the Witwatersrand, Johannesburg 2050, South Africa
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.810
Reference10 articles.
1. Transition between regular and Mach reflection in dynamic compressible flows
2. Experiments on transition of Mach reflexion
3. Transition to Mach reflexion of shock waves in steady and pseudosteady flow with and without relaxation
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