Investigation of Transcritical Methane Flow and Heat Transfer in Curved Cooling Channels
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Publisher
American Institute of Aeronautics and Astronautics
Reference26 articles.
1. 2LeBail, F. and Popp, M. “Numerical Analysis of High Aspect Ratio Cooling Passage Flow and Heat Transfer,” AIAA Paper 1993-1829, June 1993, 29th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
2. 4Brown, C. “Conceptual Investigations for a Methane-Fueled Expander Rocket Engine,” AIAA Paper 2004-4210, July 2004, 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
3. Kerosene vs. Methane: A Propellant Tradeoff for Reusable Liquid Booster Stages
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