1.
Study on infrared properties of low altitude multi-nozzle engine exhaust plume
低空多喷管发动机喷焰红外特性研究
2.
Numerical Investigation on Characteristic of Multi-tube Pulse Detonation Engines with Different Common Nozzles
多管脉冲爆震发动机共用喷管特性的数值模拟
3.
ducted-fan (jet) engine
导管风扇式喷气发动机
4.
Study on Canted Scarfed Flow-backward Multi-nozzle SRM;
小型斜置倒流多喷管固体火箭发动机研究
5.
ramjet exhaust nozzle
冲压式喷气发动机排气喷管
6.
Development of the CA6102B MPI Engine;
CA6102B多点电喷发动机的设计开发
7.
A simple, essentially tubular jet engine, such as a ramjet.
压式喷气发动机一种简单的，主要为管道式的喷气发动机，如喷压式发动机
8.
nozzle diaphragm
喷管挡栅板 -固体火箭发动机的
9.
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。
10.
A METHOD FOR DESIGN OF SMALL BEVEL NOZZLE OF ROCKET ENG INES
火箭发动机小斜切角喷管的设计方法
11.
The Research on the Performance of Timed Manifold Injection Hydrogen-Fueled Engine;
进气歧管喷射式氢气发动机性能研究
12.
The Development of Integral Design of Solid Rocket Motor Nozzle;
固体火箭发动机喷管热结构CAD设计
13.
Research progress of CMC used in rocket motor nozzle and nozzle throat
火箭发动机喷管喉衬用CMC研究进展
14.
Investigation on Noise Elimination Nozzle with Micro-Perforated Panel in Pulse Detonation Engine
脉冲爆震发动机微穿孔消声喷管研究
15.
Estimation Method of Nozzle Exit Speed for Torpedo Turbine Engine
涡轮发动机喷管出口速度的估计方法
16.
Fracture Analysis of Igniter Nozzle Tube of Aeroengine Afterburner
某型发动机加力点火喷嘴管断裂分析
17.
airless injection engine
无气喷射式发动机，机械喷油式发动机
18.
Investigation of Aft-End Internal Flows in Solid Rocket Motors with Submerged Nozzle;
固体火箭发动机潜入喷管背壁区流动研究