EXPERIMENTAL VALIDATION OF NOZZLE FLOW SIMULATIONS FOR ROCKET APPLICATION ROTATING DETONATION ENGINES

EXPERIMENTAL VALIDATION OF NOZZLE FLOW SIMULATIONS FOR ROCKET APPLICATION ROTATING DETONATION ENGINES

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Veröffentlicht in:AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Pressure gain combustion
1. Verfasser: Harroun, Alexis (VerfasserIn)
Weitere Verfasser: Heister, Stephen D. (VerfasserIn), Ruf, Joseph H. (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2020
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