Dynamics models for the combustor component in liquid rocket engine

被引：0
|
作者：
Liu, Shang [1 ]
Liu, Hong-Jun [1 ]
Chen, Hong-Yu [1 ]
机构：
[1] Xi'an Aerospace Propulsion Institute, Xi'an 710100, China
来源：
Yuhang Xuebao/Journal of Astronautics | 2012年 / 33卷 / 10期
关键词：
Combustors;
D O I：
10.3873/j.issn.1000-1328.2012.10.022
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1512 / 1518
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