1) common nozzle
共用尾喷管
1.
Numerical investigation of multi-tube pulse detonation engine with common nozzle;
共用尾喷管多管脉冲爆震发动机数值模拟研究
2) Nozzle
[英]['nɔzl] [美]['nɑzḷ]
尾喷管
1.
Parallel design of turbo engine and three-dimensional nozzle;
发动机总体与尾喷管三维并行设计研究
2.
Effect of magnetic plasma on heat transfer characteristics of nozzle wall;
磁控等离子体对尾喷管壁传热特性的影响
3.
Experimental investigation on pulse detonation engine nozzles;
脉冲爆震发动机尾喷管的实验
3) long-tail nozzle
长尾喷管
1.
Numerical simulation on 3D two-phase flow field in SRM with dual burning rate star-pore grain and long-tail nozzle;
双燃速星孔药柱长尾喷管发动机三维两相流场数值模拟
4) tail-pipe nozzle
长尾喷管
1.
Numerical simulations of axisymmetric two-phase flow field of tail-pipe nozzle segment in SRM were carried out by using stochastic trajectory model.
应用随机轨道模型对长尾喷管发动机长尾段内的轴对称两相流动进行了数值模拟,并对确定轨道和随机轨道获得的计算结果进行了对比分析,研究了10、30、50、80、100μm不同直径颗粒及3种不同颗粒直径分布下颗粒的运动轨迹和颗粒在壁面聚集浓度的区别。
2.
The differences of the particle trace and particle concentration along the wall of tail-pipe nozzle between the different diameters 10 μm,40 μm,70 μm,100 μm and different spinning velocities 0,100 r/min,300 r/min,500 r/min,1 000 r/min are studied.
针对旋转条件下长尾喷管发动机的三维两相流场开展了一体化数值模拟,进行了旋转速度为0、100 r/min、300 r/min、500 r/min和1 000 r/min,颗粒直径为10μm、40μm、70μm和100μm条件下颗粒运动轨迹和聚集浓度分布影响的研究。
5) jet pipe
喷射管，[尾]喷管
6) inner-tailpipe nozzle
内涵尾喷管
补充资料：共用
1.共同使用。
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