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Numerical Study of Combustion and Cooling Performance of a Gaseous Oxygen and Gaseous Methane Rocket Combustor with the Needle-Bolt Injector

G. D. Zhang, G. X. Li, R. P. Xing,Hu Zhang,G. H. Tang

APPLIED THERMAL ENGINEERING(2023)

引用 5|浏览18
关键词
Liquid rocket engine,Needle-bolt injector,Combustion characteristics,Cooling performance,Computational fluid dynamic
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