Flowfield Calculation Coupled with Fuel Surface Regression in Combustion Chamber for Swirling-Oxidizer-Type Hybrid Rocket Engine
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
2013-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2013
|NUMERICAL SIMULATION OF SWIRLING FLOWFIELD IN COMBUSTION CHAMBER FOR HYBRID ROCKET ENGINE
British Library Conference Proceedings | 2010
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