Liquid Rocket Motor
Liquid Rocket Motor-
Numerical Simulation and Experimental Validation of Chemical Reaction Viscous Turbulent Flow Field in the Nozzle of Liquid Rocket Motor
液体火箭发动机喷管化学反应黏性流场数值模拟和实验验证
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Bipropellant liquid rocket motor
双元液体推进剂火箭发动机
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A transient burning model of solid propellants and its application to liquid quench of rocket motor
固体推进剂瞬态燃烧模型及其在液体喷射熄火研究中的应用
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It is found from this theoretical study that there is a critical value of injection pressure drop required , for the liquid quench of rocket motor .
理论研究发现液体喷射瞬变燃烧存在着临界喷射压降。
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Determination of liquid quantity required for liquid quench of solid rocket motor
固体火箭发动机液体喷射熄火液量的确定
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