Vectoring thrust and two-dimensional nozzle
推力矢量和二元喷管
A Study on the Two-Dimensional Thrust Vectoring Nozzle with Secondary Flow Injection
基于次流喷射控制推力矢量喷管的实验及数值研究
Two-dimensional axisymmetric transient thermal analysis for a composite construction nozzle of solid rocket motor is performed by finite element method in this paper.
以固体火箭发动机复合结构喷管为对象,用有限元法进行了二维轴对称瞬态热分析。
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