1.
Check the engine tail pipe on metal particles and visible damage.
检查发动机尾喷管无金属颗粒和损坏。
2.
Experiment and Simulation Investigation of Scramjet Nozzle;
超燃冲压发动机尾喷管仿真和试验研究
3.
Parametric sensitivity analysis of scramjet nozzle configuration
超燃冲压发动机尾喷管构型参数灵敏度分析
4.
This engine consists of an inlet, a combustor, and a nozzle.
这台发动机由一个进气道，一个燃烧室和一个尾喷管组成。
5.
The Effects of Controlled Plasma by the External Magnetic Field on Fluid Flow and Heat Transfer of Aeroengine Nozzle;
磁控等离子体对航空发动机尾喷管流动传热的影响
6.
3D afterbody nozzle optimization of air-breathing hypersonic vehicle
吸气式高超声速飞行器三维后体尾喷管优化设计
7.
Numerical Analysis on Inner Flow Field and Thrust Speciality Research of the Asymmetry Quadrate Nozzle
非对称方形尾喷管内流场数值分析与推力特性研究
8.
Three Dimension Two Phase Flow Field Numerical Simulation on Tail-Pipe Nozzle SRM under Spinning Condition
旋转条件下长尾喷管发动机三维两相流场数值模拟
9.
Effects of non-equilibrium chemical reaction flow on the performance of scramjet nozzle
化学非平衡流动对超燃冲压发动机尾喷管性能的影响
10.
The Particle Parameter and Temperature Measurement for the Wake of Solid Propellant Rocket Motor(SRM)
固体火箭发动机喷管出口粒子参数和尾流温度测量方法研究
11.
A projecting part with an opening, as at the end of a hose, for regulating and directing a flow of fluid.
管嘴，喷嘴管子等物件的尾端的带有开口的突起部分，用于控制和引导水流
12.
Four nozzles, canted outboard, split the exhaust of the solid rocket motor into four equal tails.
四个向外倾斜的喷管把固体火箭发动机的排气流分成四个相等的尾巴。
13.
Experimental and Numerical Investigation on the Effect of Trailing Edge Blowing on the Flow of the Wake;
尾部喷气对尾迹区流动影响的实验和数值研究
14.
INVESTIGATION ON INTERACTION NOISE BETWEEN STATOR WAKE AND ROTOR WITH TRAILING EDGE BLOWING
静子尾缘喷气后尾迹与动叶干涉噪声研究
15.
boom drop - pipe
喷杆的下悬[喷]管(喷雾机用的)
16.
a broken pipe spouting(out)water
喷（出）水的坏管子
17.
propulsion by means of the discharge a jet of fluid toward the rear.
通过向尾部喷出流动物而推进。
18.
Spray Satinique Advanced Finishing Spray to the root area for added body. Also, spray a little on your fingers and twist on the hair ends to accentuate the texture.
在发尾喷上仙姬持久造型喷雾，另喷些在指尖，然后抹在发尾增加发丝质感。