介绍了差分流量调节的计算方法和内喷管与塞锥推力矢量变化的分析过程，计算产生的俯仰力矩。
The computing method of differential throttling and the analytical process of thrust vector of inner nozzle and plug were introduced. The generated moments of pitch were given.
平行度检测利用测距传感器检测距喷管与发动机法兰之间的距离来调节两平面的平行度。
The parallelism examination is completed by making use of the range finder sensor examining the distance between the range finder and nozzle and the engine flange to adjust two planes parallelism.
在同等壁面热条件下，随着动量调节系数的增加，喷管粘性损失增大，喷管的推力和比冲都将下降；
Under the same wall heat condition, with the increase of momentum correction coefficient, viscosity loss of the nozzle increases, but thrust and specific impulse decrease.
围绕组合喷管及其流量分配调节和推力矢量技术，本文开展了系统性研究。
Systematic researches on combined nozzle and its flow regulation, as well as thrust vector technologies are carried out in this dissertation.
本文叙述气动调节喷管性能计算的分析程序。
An analytical procedure for computing the performance of aerodynamically variable geometry exhaust nozzle is presented in this paper.
本文叙述气动调节喷管性能计算的分析程序。
An analytical procedure for computing the performance of aerodynamically variable geometry exhaust nozzle is presented in this paper.
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