Effects of Combustion and Shock Impingement on Supersonic Film Cooling by Hydrogen
Author:
Affiliation:
1. Tohoku University, Sendai 980-8579, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.843
Reference27 articles.
1. Effect of film cooling/regenerative cooling on scramjet engine performances
2. Numerical study of film cooling in supersonic flow
3. Effects of shock wave impingement on supersonic film cooling
4. Flowfield measurements in supersonic film cooling including the effect of shock-wave interaction
5. Influence of injectant Mach number and temperature on supersonic film cooling
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