Comparison of Shock/Cooling-Film Interaction for Cooled and Isoenergetic Injection
Author:
Affiliation:
1. RWTH Aachen University, 52062 Aachen, Germany
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference26 articles.
1. Film Cooling
2. Velocity and Temperature Profiles in Turbulent Boundary Layers With Tangential Injection
3. Flowfield measurements in supersonic film cooling including the effect of shock-wave interaction
4. Large-Eddy Simulation of Shock/Cooling-Film Interaction
5. Turbulent Boundary-Layer Shock Interaction with and without Injection
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