Affiliation:
1. University of California
Publisher
American Institute of Aeronautics and Astronautics
Cited by
3 articles.
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1. Steady and Unsteady Shock Interactions by Shock Fitting Approach;Shock Wave and High Pressure Phenomena;2017
2. Direct Numerical Simulations of Turbulent Flow Interactions with Strong Shocks Using Shock-Fitting Method;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2011-01-04
3. Numerical Simulation of Shock-Turbulence Interactions Using High-Order Shock-Fitting Algorithms;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04