Experimental Investigations of Film Cooling in a Conical Nozzle Under Rocket-Engine-Like Flow Conditions
Author:
Affiliation:
1. RWTH Aachen University, 52056 Aachen, Germany
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057486
Reference31 articles.
1. Influence of injectant Mach number and temperature on supersonic film cooling
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3. Supersonic film cooling
4. Film Cooling
5. Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow
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