Choked Flow in a Converging/Diverging Rotating Detonation Engine Exit
AIAA SciTech Forum ; 2023 ; National Harbor, Md.; Online
2023
Conference paper
English
Raketentriebwerk , Erhöhung , Verbrennung , Turbine , Druck
Numerical simulation of converging-diverging nozzle flow in pulse detonation rocket engine
British Library Online Contents | 2007
|British Library Conference Proceedings | 2014
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