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| Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16 Authors: Chang SY(常思源); Xiao Y(肖尧); Li GL(李广利) ; Tian ZW(田中伟); Cui K(崔凯)![](/image/person.jpg)
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| Numerical study on hypersonic aerodynamic characteristics of the high-pressure capturing wing configuration with wing dihedral 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 15 Authors: Chang SY(常思源) ; Xiao Y(肖尧); Li GL(李广利) ; Tian ZW(田中伟); Cui K(崔凯)![](/image/person.jpg)
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| 翼反角对高压捕获翼构型高超气动特性的影响 期刊论文 航空学报, 2023, 卷号: 44, 期号: 08, 页码: 45-58 Authors: 常思源 ; 肖尧; 李广利 ; 田中伟; 张凯凯 ; 崔凯![](/image/person.jpg)
Adobe PDF(3584Kb)  |   Favorite  |  View/Download:206/42  |  Submit date:2022/10/17 高压捕获翼 高超声速 数值模拟 上/下反角 稳定性 |
| 机体尾缘形状对高压捕获翼构型亚声速特性影响 期刊论文 航空学报, 2023, 卷号: 44, 期号: 06, 页码: 10.7527/S1000-6893.2022.27215 Authors: 王浩祥; 肖尧; 张凯凯 ; 李广利 ; 常思源 ; 田中伟; 崔凯![](/image/person.jpg)
Adobe PDF(2111Kb)  |   Favorite  |  View/Download:193/53  |  Submit date:2022/10/17 高压捕获翼 亚声速 流动特性 流动分离 数值模拟 |
| 翼反角对高压捕获翼构型亚声速气动特性影响分析研究 期刊论文 力学学报, 2022, 卷号: 54, 期号: 10, 页码: 2760-2772 Authors: 常思源 ; 肖尧; 李广利 ; 田中伟; 崔凯![](/image/person.jpg)
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| 高压捕获翼构型亚跨超流动特性数值研究 期刊论文 力学学报, 2021, 卷号: 53, 期号: 11, 页码: 3056-3070 Authors: 王浩祥; 李广利 ; 杨靖 ; 肖尧; 王小永; 徐应洲; 许先贵 ; 崔凯![](/image/person.jpg)
Adobe PDF(2607Kb)  |   Favorite  |  View/Download:306/80  |  Submit date:2022/03/16 高压捕获翼 计算流体力学 宽速域 流动分离 气动干扰 |
| Hypersonic I-shaped aerodynamic configurations 期刊论文 SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2018, 卷号: 61, 期号: 2, 页码: 24722 Authors: Cui K(崔凯) ; Xiao Y(肖尧); Xu YZ; Li GL![](/image/person.jpg)
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| High-Pressure Capturing Wing Configurations 期刊论文 AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919 Authors: Cui K(崔凯) ; Li GL ; Xiao Y(肖尧) ; Xu YZ; Cui,K(reprint author), Chinese Acad Sci, Inst Mech
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| 乘波体压缩面变化对其气动性能影响分析 期刊论文 力学学报, 2017, 卷号: 49, 期号: 01, 页码: 75-83 Authors: 崔凯 ; 徐应洲; 肖尧 ; 李广利![](/image/person.jpg)
View  |   Adobe PDF(5584Kb)  |   Favorite  |  View/Download:380/95  |  Submit date:2017/12/22 乘波体 优化设计 增量参数化方法 微分演化算法 计算流体力学 |
| Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Li GL(李广利) ; Cui K(崔凯) ; Xiao Y(肖尧) ; Xu YZ(徐应洲)
View  |   Adobe PDF(664Kb)  |   Favorite  |  View/Download:412/102  |  Submit date:2018/01/16 Aerodynamics Angle Of Attack Angle Of Attack Indicators Boundary Layers Drag Drag Coefficient High Pressure Effects Hypersonic Aerodynamics Hypersonic Flow Spacecraft |