THREE-DIMENSIONAL NUMERICAL SIMULATION ON HYDROGEN/AIR ROTATING DETONATION ENGINE WITH AEROSPIKE NOZZLE: EFFECTS OF NOZZLE GEOMETRIES

THREE-DIMENSIONAL NUMERICAL SIMULATION ON HYDROGEN/AIR ROTATING DETONATION ENGINE WITH AEROSPIKE NOZZLE: EFFECTS OF NOZZLE GEOMETRIES

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Veröffentlicht in:AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Pressure gain combustion
1. Verfasser: Kurita, Nobuhiro (VerfasserIn)
Weitere Verfasser: Jourdaine, Nicolas H. (VerfasserIn), Tsuboi, Nobuyuki (VerfasserIn), Ozawa, Kohei (VerfasserIn), Hayashi, Koichi A. (VerfasserIn), Kojima, Takayuki (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2020
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