CORC  > 北京航空航天大学
31 Transient simulation of regression rate on thrust regulation process in hybrid rocket motor
Tian Hui; Li Yijie; Zeng Peng
刊名CHINESE JOURNAL OF AERONAUTICS
2014
卷号27页码:1343-1351
关键词Dynamic mesh Flow throttling process Hybrid rocket motor Numerical simulation Transient regression rate
ISSN号1000-9361
DOI10.1016/j.cja.2014.08.016
URL标识查看原文
收录类别SCIE ; EI ; ISTICCSCD
WOS记录号WOS:000348588300001
内容类型期刊论文
URI标识http://www.corc.org.cn/handle/1471x/6548446
专题北京航空航天大学
推荐引用方式
GB/T 7714
Tian Hui,Li Yijie,Zeng Peng. 31 Transient simulation of regression rate on thrust regulation process in hybrid rocket motor[J]. CHINESE JOURNAL OF AERONAUTICS,2014,27:1343-1351.
APA Tian Hui,Li Yijie,&Zeng Peng.(2014).31 Transient simulation of regression rate on thrust regulation process in hybrid rocket motor.CHINESE JOURNAL OF AERONAUTICS,27,1343-1351.
MLA Tian Hui,et al."31 Transient simulation of regression rate on thrust regulation process in hybrid rocket motor".CHINESE JOURNAL OF AERONAUTICS 27(2014):1343-1351.
个性服务
查看访问统计
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。


©版权所有 ©2017 CSpace - Powered by CSpace