Experimental studies of supersonic film cooling with shock wave interaction
Author:
Affiliation:
1. National Aerospace Laboratory, Kakuda, Miyagi 981-15, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13060
Reference14 articles.
1. Effect of film cooling/regenerative cooling on scramjet engine performances
2. Turbulent Boundary-Layer Shock Interaction with and without Injection
3. Experimental studies of shock wave/wall jet interaction in hypersonic flow
4. Experimental results for film cooling in 2-D supersonic flow including coolant delivery pressure, geometry, and incident shock effects
5. Flowfield measurements in supersonic film cooling including the effect of shock-wave interaction
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