DESIGN OF SHAPE TRANSITION NOZZLE FOR DIRECT-CONNECT SUPERSONIC COMBUSTOR

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Veröffentlicht in:AIAA Propulsion and Energy Forum (2021 : Online) High-speed air-breathing propulsion
1. Verfasser: Sung, Bu-Kyeng (VerfasserIn)
Weitere Verfasser: Choi, JeongYeol (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2021
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