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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
作者:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
浏览  |  Adobe PDF(2082Kb)  |  收藏  |  浏览/下载：421/189  |  提交时间：2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty  
An efficient single-loop strategy for reliability-based multidisciplinary design optimization under non-probabilistic set theory 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 148-163
作者:  Wang XJ;  Wang RX(王睿星);  Wang L;  Chen XJ;  Geng XY
浏览  |  Adobe PDF(3200Kb)  |  收藏  |  浏览/下载：480/108  |  提交时间：2018/10/30
Non-probabilistic reliability based  multidisciplinary design optimization  Single loop strategy  Uncertainty multidisciplinary analysis  Non-probabilistic reliability analysis  Translating distance calculation  
Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230
作者:  Chen XJ;  Qiu ZP;  Wang XJ;  Li YL;  Wang RX(王睿星)
浏览  |  Adobe PDF(4860Kb)  |  收藏  |  浏览/下载：390/87  |  提交时间：2018/02/08
Uncertain Reduced-order Modeling  Robust Flutter Analysis  Interval Perturbation Method  Uncertain Aeroelastic System