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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
View  |  Adobe PDF(2082Kb)  |  Favorite  |  View/Download：465/197  |  Submit date：2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty  
An integration design of gas exchange, bubble separation, and flow control in a space cell culture system on board the SJ-10 satellite 期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2019, 卷号: 90, 期号: 7, 页码: 12
Authors:  Sun SJ(孙树津);  Wang CZ(王成之);  Bi YZ(毕于振);  Li N(李宁);  Lv DY(吕东媛);  Chen Q(陈琴);  Chen J(陈娟);  Long M(龙勉)
Adobe PDF(9094Kb)  |  Favorite  |  View/Download：345/187  |  Submit date：2019/09/09