Film Cooling in Laminar and Turbulent Supersonic Flows-Reference-Cited by-同舟云学术

Film Cooling in Laminar and Turbulent Supersonic Flows

Published:2013-07 Issue:4 Volume:50 Page:742-753
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Hombsch M.¹,Olivier H.¹

Affiliation:

1. Shock Wave Laboratory, 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.A32346

Reference23 articles.

1. Film Cooling in a High-Pressure Subscale Combustion Chamber

2. Experimental and Numerical Study of Cooling Gas Injection in Laminar Supersonic Flow

3. HeuferK. A. “Untersuchungen zur Filmkühlung in Supersonischen Strömungen,” Ph.D. Thesis, Shock Wave Lab., RWTH Aachen Univ., Aachen, Germany, 2008 (in German).

4. HombschM.OlivierH. “Flow Condition and Cooling Gas Variation for Film Cooling Studies in Hypersonic Flow,” AdamsN. A.RadespielR.SattelmayerT.SchröderW.WeigandB. (eds.), “Annual Report SFB TRR-40, Munich, Germany, 2010, pp. 27–39.

5. Numerical Analysis of Film Cooling in Advanced Rocket Nozzles

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