reaction nozzle

Numerical solutions of full Navier-Stokes equations with chemical reaction flow were established for the nozzle flow of the LOX/ HTPB hybrid rocket motor.

利用二维轴对称N-S方程和组分方程对选用液氧/端羟基聚丁二烯推进剂的固液混合火箭发动机喷管流动进行了计算。

A jet propulsion model was designed and the structural dimensions of its reaction chamber and jet nozzle were determined referring to the operating principle of the jet engine in the exploration and investigation of the newfashioned propulsion for the watercraft.

在舰船用新型推进器的研究和探索中，依据火箭喷气式发动机的工作原理，设计了一种喷气式推进模型，并确定了推进模型反应室和喷嘴的结构尺寸。

The reaction assembly generates a compound gas stream for compound nozzle towards a target substrate.

反应装置能产生用于喷向目标基片的化合物气体流.

Reaction part uses efficient KH-2 pulverization nozzle, promote beforehand paragraph and stop reaction establishment quickly.

反应部分采用高效KH-2雾化喷嘴 、 预提升段和快速终止反应设施.

Gear method for calculation of one dimensional chemical reaction nozzle flow

一维喷管化学反应流的吉尔方法研究

The key component of the homogeneously catalyzed micro monopropellant thruster is its micro thrust chamber, which consists of the catalytic reaction tank and the micro nozzle. The impulse output resolution of the experimental prototype is better than 80 μ Ns.

同相催化的单组元液体推进器，其关键部件是微小型推力室，包括催化反应腔和喷管等结构，试验样机的冲量输出分辨率优于80μNs。

Numerical Simulation and Experimental Validation of Chemical Reaction Viscous Turbulent Flow Field in the Nozzle of Liquid Rocket Motor

液体火箭发动机喷管化学反应黏性流场数值模拟和实验验证