Investigation of Film Cooling Efficiency in a High Pressure Subscale LOX/H2 Combustion Chamber-Reference-Cited by-同舟云学术

Investigation of Film Cooling Efficiency in a High Pressure Subscale LOX/H2 Combustion Chamber

Published:2011-07-31 Issue: Volume: Page:
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Container-title:47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Suslov D.,Arnold R.,Haidn O.

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. Progress in Astronautics and Aeronautics;Huzel D. K.,1992

2. Effects of Liquid-Oxygen Post Biasing on SSME Injector Wall Compatibility

3. Suslov, D., Woschnak, A., Sender, J., and Oschwald, M. Test Specimen Design and Measurement Technique for Investigation of Heat Transfer Processes in Cooling Channels of Rocket Engines under Real Thermal Conditions," 24th International Symposium on Space Technology and Science ISTS, Miyazaki, Japan, May 30th-June 6th 2004, ISTS 2004-e-40.

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