1) exhaust extension
排气延伸管
2) Extension GP-exhaust
排气延伸管总成
3) turbojet engine extention pipes
涡轮喷气发动机延伸管
4) extendible nozzle
延伸喷管
1.
Analysis on tail flow field of solid rocket motor with extendible nozzle under stage separation condition;
级间热分离条件下带有延伸喷管的固体火箭发动机尾部流场分析
2.
Provided thermodynamic characteristics of the rocket engine burning products and engine performances, the temperature and stress analysis of the extendible nozzle are finished by finite element method.
对该延伸喷管建立二维轴对称有限元计算模型后,对工作时间内瞬态温度场和热应力进行分析计算。
3.
Flow field of unfold course for a solid rocket engine with extendible nozzle was analyzed by approach numerical solution of the 2-D axis symmetry N-S equation through AF method.
文中通过AF方法求解二维轴对称N-S方程,对采用延伸喷管的固体火箭发动机级间展开过程地面单试的流场进行了数值分析。
5) extended management
延伸管理
6) extension pipe
伸延管
补充资料：涡轮风扇喷气发动机
见导弹推进系统。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条