同轴式喷注器
- Coaxial injector;【航天】concentric tube injector
同轴式喷注器
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大流量同轴式喷注器雾化过程及喷雾两相流数值模拟研究
Studies on atomization process of large flux coaxial injector and numerical simulation of spray two-phase flow
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以同轴式喷嘴为喷注器的液氢液氧火箭发动机的高频不稳定燃烧现象有可能是喷嘴自激振荡引起燃烧室中压力振荡的结果。
At last , the comparison between phenomena of the self-oscillation and some experiments of LRE indicates that some instability phenomena in Oxygen / Hydrogen propellant rocket engine may be the result of self-oscillation in coaxial swirl injectors .