Protuberance interference heating in high-speed flow
Author:
Affiliation:
1. Aerospace Corp., Thermal Control Dept., El Segundo, CA
2. Rockwell International Corp., Aerothermodynamics Dept., Downey, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1724
Reference23 articles.
1. Shock Impingement Caused by Boundary-Layer Separation Ahead of Blunt Fins
2. Effect of Transition on Three-Dimensional Shock- Wave/Boundary-Layer Interaction
3. The Structure of Three-Dimensional Separated Flows in Obstacle-Boundary Layer Interactions.
4. Step induced boundary-layer separation phenomena
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