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中国科学院力学研究所机构知识库
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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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View/Download：454/195
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Submit date：2020/03/21
Hypersonic vehicle
Six sigma robust optimization
Successive response surface
Thermal protection system
Uncertainty
基于浸入边界方法的复杂几何边界湍流壁面模化的大涡模拟
学位论文
博士论文，北京: 中国科学院大学, 2019
Authors:
时北极
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View/Download：743/19
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Submit date：2019/05/30
大涡模拟
浸入边界方法
壁模型
近壁速度重构模型
壁面滑移速度模型
体积力重构模型
