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中国科学院力学研究所机构知识库
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Indexed By：SCI
Language：英语
Funding Organization：National Nature Science Foundation of China
Funding Project：Defence Industrial Technology Development Programs of China[JCKY2017601B001]
Document Type：期刊论文
Community：流固耦合系统力学重点实验室
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Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors:
Zhu JJ
;
Wang XJ
;
Zhang HG
;
Li YW
;
Wang RX(王睿星)
;
Qiu ZP
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Submit date：2020/03/21
Hypersonic vehicle
Six sigma robust optimization
Successive response surface
Thermal protection system
Uncertainty
