Influence of Shock Waves on Supersonic Film Cooling
Author:
Affiliation:
1. Tsinghua University, 100084 Beijing, People ’ s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.38458
Reference9 articles.
1. Film Cooling
2. Turbulent Boundary-Layer Shock Interaction with and without Injection
3. Flowfield measurements in supersonic film cooling including the effect of shock-wave interaction
4. Experimental studies of supersonic film cooling with shock wave interaction
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