Optimal Design of Rocket Nozzle Parameters with Consideration of Gas-Particle Two Phase Flow Effect
Inst. of Aerospace & Material Engineering , National University of Defence Technology, Changsha 410073, China;Inst. of Aerospace & Material Engineering , National University of Defence Technology, Changsha 410073, China;Inst. of Aerospace & Material Engineering , National University of Defence Technology, Changsha 410073, China;Inst. of Aerospace & Material Engineering , National University of Defence Technology, Changsha 410073, China
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