Influence of Cooling-Gas Properties on Film-Cooling Effectiveness in Supersonic Flow
Author:
Affiliation:
1. Institut für Aero- und Gasdynamik, University of Suttgart, 70550 Stuttgart, Germany
2. Stoß Wellenlabor, RWTH Aachen University, 52056 Aachen, Germany
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.A33203
Reference38 articles.
1. Redesign of the Vulcain 2 Nozzle Extension
2. Experimental Study of Active Cooling in 8 Laminar Hypersonic Flows
3. Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow
4. Numerical Investigations of Film Cooling
5. Numerical Simulation of Coolant Variation in Laminar Supersonic Film Cooling
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