Two-phase flow numerical calculation of H2O2/HTPB hybrid rocket engine with diaphragm in grain

被引：0
|
作者：
Wang, Peng-Fei [1 ]
Tian, Hui [1 ]
Yu, Nan-Jia [1 ]
Cai, Guo-Biao [1 ]
机构：
[1] School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2013年 / 28卷 / 11期
关键词：
Diaphragms;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
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页码：2621 / 2626
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