Structure of supersonic turbulent flow past a sharp fin
Author:
Affiliation:
1. Rutgers University, New Brunswick, New Jersey
2. NASA Ames Research Center, Moffett Field, California
3. Princeton University, Princeton, New Jersey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9787
Reference27 articles.
1. The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary Layer
2. Three-Dimensional Shock Wave-Turbulent Boundary Layer Interactions at Mach 6
3. An experimental study of the interaction between a glancing shock wave and a turbulent boundary layer
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