Comparison of a two-dimensional shock impingement computation with experiment
Author:
Affiliation:
1. Iowa State University, Ames, Iowa
2. NASA Ames Research Center, Moffett Field, Calif.
3. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7125
Reference3 articles.
1. Numerical Computation of Two-Dimensional Viscous Blunt Body Flows with an Impinging Shock
2. ANOMALOUS HEAT TRANSFER AND PRESSURE DISTRIBUTIONS ON BLUNT BODIES AT HYPERSONIC SPEEDS IN THE PRESENCE OF AN IMPINGING SHOCK.
3. A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactions
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