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Steady-state high pressure LOx/H2 rocket engine combustion
Institution:1. The University of Adelaide, School of Mechanical Engineering, 5005 Australia;2. DLR Institute of Space Propulsion, 74239, Germany;1. Combustion Chamber Department, Korea Aerospace Research Institute, Daejeon, Republic of Korea;2. School of Mechanical Engineering, Chungbuk National University, 52 Naesudong-ro, Heungdeok-gu, Cheongju, Chungbuk, 361-763, Republic of Korea;1. CERFACS, CFD Team, 42 Av Coriolis, 31057 Toulouse, France;2. Société Nationale d’Etude et de Construction de Moteurs d’Aviation, 77550 Reau, France;3. Centre de Recherche et Technologies: SAFRAN, France;4. IMF Toulouse, INP de Toulouse and CNRS, 31400 Toulouse, France;1. CNRS, UPR 288, Laboratoire d’Energétique Moléculaire et Macroscopique, Combustion (EM2C), Grande Voie des Vignes, 92290 Châtenay-Malabry, France;2. Ecole Centrale Paris, Grande Voie des Vignes, F-92290 Châtenay-Malabry, France;3. Cerfacs, 42, Avenue Gaspard Coriolis, 31057 Toulouse Cedex 01, France
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