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.
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
3.
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
4.
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
5.
nozzle diaphragm
喷管挡栅板 -固体火箭发动机的
6.
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
7.
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
8.
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
9.
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
10.
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
11.
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
12.
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
13.
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。
14.
Stress Field Analysis Near Crack Tip Buried in the Rosette Carbon-Carbon Nozzle of SRM;
固体火箭发动机花瓣铺层碳/碳柔性喷管扩张段裂尖附近应力场研究
15.
air-breathing rocket engine
空气喷气火箭发动机
16.
Allan J.McDonald, "Design evolution of the space shuttle solid rocket motors"
航天飞机固体火箭发动机的设计演变
17.
Investigation of ring aerodynamic throat for solid rocket motor
固体火箭发动机环缝式气动喉部研究
18.
internal ballistics of solid rocket motors
固体火箭发动机内弹道学