The relations of thrust and specific impulse to inlet air flow and temperature are derived from theoretical analysis of solid fuel ramjet (SFRJ) performance.
在固体燃料冲压发动机性能分析基础上，推导了某发动机的推力和比冲与入口流量和温度之间的关系式。
Theoretical research on specific impulse performance and chamber length of hydroreactive metal fuel motor;
水反应金属燃料发动机系统构型研究需要以燃烧数值模拟作为研究基础。
Theoretical research on specific impulse performance and chamber length of hydroreactive metal fuel motor;
水反应金属燃料发动机系统构型研究需要以燃烧数值模拟作为研究基础。
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