Numerical Simulation of Hot-Gas Side Heat Transfer Enhancement in Thrust Chambers by Wall Ribs
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Publisher
American Institute of Aeronautics and Astronautics
Reference21 articles.
1. 1Pugh, R. “The Many Factes of the RL-10 Liquid Rocket Engine, a Continuing Success Story,” 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 13-15July 1998, Cleveland, OH. AIAA-98-3680.
2. 2Peery, S. and Minick, A. “Design and Development of an Advanced Expander Combustor,” 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 13-15July 1998, Cleveland, OH. AIAA-98-3675.
3. 3Rachuk, V. and Titkov, N. “The First Russian LOX-LH2Expander Cycle LRE: RD0146,” 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 9-12July 2006, Sacramento, CA. AIAA-2006-4904.
4. 4Fujita, M., Aoki, H., Nakagawa, T., Tokunaga, T., Yasui, M., and Iwama, K. “Upper Stage Propulsion System for H-IIA Launch Vehicle,” 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7-10July 2002, Indianapolis, IN. AIAA-2002-4212.
5. 5Knab, O., Frohlich, A., Wennerberg, D., and Haslinger, W. “Advanced Cooling Circuit Layout for the VINCI Expander Cycle Thrust Chamber,” 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7-10July 2002, Indianapolis, IN. AIAA-2002-4005.
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1. Coupled Heat Transfer Analysis in Regeneratively Cooled Thrust Chambers;Journal of Propulsion and Power;2014-03
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