Shock Wave Impingement on Boundary Layers at Hypersonic Speeds: Computational Analysis and Uncertainty
Author:
Affiliation:
1. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3143
Reference93 articles.
1. 5Menter, F. R., Improved Two-Equation K-! Turbulence Models for Aerodynamic Flows, NASA TM 103975, Oct. 1992.
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