Computation of hypersonic boundary-layer response to external disturbances
Author:
Affiliation:
1. High Technology Corp., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-411
Reference48 articles.
1. Turbulence amplification in shock-wave boundary-layer interaction
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4. Linear and nonlinear stability of the Blasius boundary layer
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