1.
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
2.
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
3.
Numerical simulation of gas-particle flow in nozzle of solid rocket motor
固体火箭发动机喷管气固两相流动的数值模拟
4.
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
5.
Integrated numerical simulation and software implementation on two-phase flow field and structure temperature field of solid rocket motor nozzle
固体火箭发动机喷管两相流场与结构温度场一体化数值模拟与软件实现
6.
nozzle diaphragm
喷管挡栅板 -固体火箭发动机的
7.
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
8.
air-breathing rocket engine
空气喷气火箭发动机
9.
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
10.
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
11.
Mechanical Capability Study on Conical Nozzle of Rocket Engine by ANSYS
火箭发动机锥形喷管ANSYS力学性能分析研究
12.
Simulation and Experiment of Thrust Performance for Solid Rocket Motor with Angle-cut Nozzle
斜切喷管固体火箭发动机推力特性仿真与试验
13.
forward force produced by a propeller,jet engine,rocket,etc
（推进器、喷气发动机、火箭等的）推力.
14.
The Study of Atomization Character of Coaxial Injector in Rocket Engine;
火箭发动机同轴式喷嘴雾化特性研究
15.
Thermal and Thermal-Structural Couple Analysis of the Rosette Carbon-Carbon Nozzle in SRM;
碳/碳固体火箭发动机柔性喷管热及热－结构耦合作用研究
16.
Upgrade the Performance of Single Combustion Chamber Dual Thrust SRM by Unilateralism Nozzle Throat Area Control
利用定向可调喷管提升单室双推固体火箭发动机性能
17.
Starting with the invention of the bicycle, going on to sports cars, cars with jet engines, rocket-powered cars, attempts to break the sound barrier, and rocket-engine airplanes.
从发明自行车开始，一直到赛车，喷气发动机汽车，火箭动力汽车，尝试突破声障和火箭动力飞机。
18.
Simulation of Random Launch and Flight Dynamics of MLRS
多管火箭随机发射与飞行动力学仿真