Numerical simulation of pintle thruster combustion and heat transfer for MMH/NTO hypergolic bipropellant

被引：0
|
作者：
Zhang, Lian-Bo [1 ]
Mao, Xiao-Fang [2 ]
Wang, Feng-Shan [2 ]
Xu, Xu [1 ]
机构：
[1] School of Astronautics, School of Astronautics, Beijing,100191, China
[2] Beijing Institute of Control Engineering, Beijing,100190, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2015年 / 36卷 / 10期
关键词：
Drops - Numerical models - Pressure drop - Flow fields - Turbulence models - Atomization - Heat transfer - Numerical methods - Rockets - Combustors - Fluid structure interaction - Particle size;
D O I：
10.13675/j.cnki.tjjs.2015.10.006
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1487 / 1494
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