Computation of crossing shock/turbulent boundary layer interaction at Mach 8.3
Author:
Affiliation:
1. Rutgers University, Piscataway, New Jersey 08855
2. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11784
Reference26 articles.
1. Swept shock/boundary-layer interactions - Tutorial and update
2. Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layer
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