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	Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
	Zhu, Jingjing; Wang, Xiaojun; Zhang, Haiguo; Li, Yuwen; Wang, Ruixing; Qiu, Zhiping
刊名	CHINESE JOURNAL OF AERONAUTICS
	2019
卷号	32页码:2095-2108
关键词	Hypersonic vehicle Six sigma robust optimization Successive response surface Thermal protection system Uncertainty
ISSN号	1000-9361
DOI	10.1016/j.cja.2019.04.009
URL标识	查看原文
收录类别	SCIE
WOS记录号	WOS:000492014900006
内容类型	期刊论文
URI标识	http://www.corc.org.cn/handle/1471x/5916459
专题	北京航空航天大学
推荐引用方式 GB/T 7714	Zhu, Jingjing,Wang, Xiaojun,Zhang, Haiguo,et al. Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method[J]. CHINESE JOURNAL OF AERONAUTICS,2019,32:2095-2108.
APA	Zhu, Jingjing,Wang, Xiaojun,Zhang, Haiguo,Li, Yuwen,Wang, Ruixing,&Qiu, Zhiping.(2019).Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method.CHINESE JOURNAL OF AERONAUTICS,32,2095-2108.
MLA	Zhu, Jingjing,et al."Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method".CHINESE JOURNAL OF AERONAUTICS 32(2019):2095-2108.

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