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机译:
Moscow Aviation Institute (National Research University);
Technical University of Munich;
Liquid rocket engine; Kerosene; Oxygen; Favre-averaged Navier-Stokes; Film cooling; Numerical simulation;
机译:Numerical investigations of the nozzle performance for a rocket-based rotating detonation engine with film cooling
机译:Numerical investigation of pentagonal V-shape ribs to enhance heat transfer in hydrogen rocket engine cooling channels
机译:Numerical Approach for the Estimation of Throat Heat Flux in Liquid Rocket Engines