NUMERICAL EVALUATION OF AN EJECTOR-ENHANCED RESONANT PULSE COMBUSTOR WITH A POPPET INLET VALVE AND A CONVERGING EXHAUST NOZZLE (AIAA 2016-4559)
Joint propulsion conference
01.01.2016
12 pages
Aufsatz (Konferenz)
Englisch
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SAE | 1929
|Engineering Index Backfile | 1929
|British Library Conference Proceedings | 2016
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