THREE-DIMENSIONAL NUMERICAL SIMULATION ON HYDROGEN/AIR ROTATING DETONATION ENGINE WITH AEROSPIKE NOZZLE: EFFECTS OF NOZZLE GEOMETRIES
AIAA SciTech Forum and Exposition ; 2020 ; Orlando, Fla.
2020
Conference paper
English
Raketentriebwerk , Erhöhung , Verbrennung , Turbine , Druck
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