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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:392/185  |  Submit date:2020/03/21 Hypersonic vehicle Six sigma robust optimization Successive response surface Thermal protection system Uncertainty |
| Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor 期刊论文 JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11 Authors: Cheng D(程迪); Wang J(王晶); Lu Y(陆阳); Li L(李龙); Yao W(姚卫); Fan XJ(范学军) Adobe PDF(2651Kb)  |  Favorite  |  View/Download:395/127  |  Submit date:2019/09/09 Heat flux measurement Kerosene Supersonic combustion Scramjet Heat flux sensor |
| Comparison of the reliability-based and safety factor methods for structural design 期刊论文 APPLIED MATHEMATICAL MODELLING, 2019, 卷号: 72, 页码: 68-84 Authors: Wang XJ; Shi QH; Fan WC; Wang RX(王睿星); Wang L Adobe PDF(1921Kb)  |  Favorite  |  View/Download:339/70  |  Submit date:2019/09/09 Safety factor method Reliability-based design optimization Structural design Uncertainty |
| 一种用于超声速然烧的直连台的气膜冷却装置 专利 发明专利. 一种用于超声速然烧的直连台的气膜冷却装置, 专利号: ZL201611135726.1, 申请日期: 2016-12-12, Inventors: 樊川; 王晶; 孟令瑾; 范学军 Adobe PDF(336Kb)  |  Favorite  |  View/Download:225/44  |  Submit date:2020/02/09 |
| An interval updating model for composite structures optimization 期刊论文 COMPOSITE STRUCTURES, 2019, 卷号: 209, 页码: 177-191 Authors: Shi QH; Wang XJ; Wang RX(王睿星); Chen X; Ma YJ Adobe PDF(1806Kb)  |  Favorite  |  View/Download:253/68  |  Submit date:2019/04/11 Composite structural design Model updating Uncertainty Progressive failure analysis |