Coupled numerical simulation for the later period of the stage separation of a multi-stage rocket

被引：0
|
作者：
Gao, Li-Hua [1 ]
Zhang, Bing [2 ]
Quan, Xiao-Bo [2 ]
Fu, Song [1 ]
机构：
[1] School of Aerospace, Tsinghua Univ., Beijing 100084, China
[2] Beijing Inst. of Space System Engineering, Beijing 100076, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2010年 / 31卷 / 02期
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摘要：
9
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页码：129 / 133
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