Flow separation and side-load in nozzle

被引：0
|
作者：
Lin, Zhen [1 ]
Wang, Changhui [1 ]
Liu, Yu [1 ]
Xu, Xiaoyong [2 ]
机构：
[1] School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
[2] Beijing Aerospace Propulsion Institute, Beijing 100076, China
来源：
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2010年 / 36卷 / 03期
关键词：
Rocket engines - Flow fields - Wall flow - Rockets - Rocket nozzles - Numerical models;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：307 / 310
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