VALIDATION AND APPLICATION OF A REDUCED-ORDER ROTATING DETONATION ENGINE INLET AND FILL ZONE MODEL

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Veröffentlicht in:AIAA SciTech Forum and Exposition (2021 : Online) Pressure gain combustion
1. Verfasser: Bedick, Clinton (VerfasserIn)
Weitere Verfasser: Ferguson, Donald H. (VerfasserIn), Strakey, Peter (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2021
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