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| 升阻比对可重复使用运载器爬升特性影响 期刊论文
中国科学:技术科学, 2019, 期号: 08, 页码: 891-900
Authors: 崔凯 ; 徐应洲; 李广利; 肖尧; 王浩祥
 View |  Adobe PDF(508Kb) |  Favorite | View/Download：89/9 | Submit date：2019/09/12
可重复使用运载器 水平发射 两级入轨 弹道分析 升阻比 |
| 全乘波背部进气高超声速飞机新概念构型研究 学位论文
博士论文，北京: 中国科学院大学, 2018
Authors: 肖尧
 Adobe PDF(10334Kb) | Favorite | View/Download：365/9 | Submit date：2018/05/24
高超声速飞行器 乘波体 背部进气布局 升阻比 气动设计与优化 |
| 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
View | Adobe PDF(665Kb) | Favorite | View/Download：124/38 | Submit date：2018/10/30 |
| 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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| 上置翼调节装置及高速飞行器 专利
发明专利. 上置翼调节装置及高速飞行器, 专利号: ZL201410557661.4, 申请日期: 2014-10-20, 授权日期: 2017-02-22
Inventors: 崔凯; 李广利; 肖尧
View | Adobe PDF(734Kb) | Favorite | View/Download：163/25 | Submit date：2017/03/03 |
| 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
View | Adobe PDF(5584Kb) | Favorite | View/Download：164/28 | 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 |
| 一种组合前缘乘波体设计方法及组合前缘乘波体 专利
发明专利. 一种组合前缘乘波体设计方法及组合前缘乘波体, 专利号: ZL201510079522.X, 申请日期: 2015-02-13, 授权日期: 2017-01-04
Inventors: 崔凯; 李广利; 肖尧
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| Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Xiao Y(肖尧); Cui K(崔凯); Li GL(李广利); Xu YZ(徐应洲)
View | Adobe PDF(639Kb) | Favorite | View/Download：124/38 | Submit date：2018/01/16
Aerodynamics Air Engines Aspect Ratio Computational Fluid Dynamics Drag Engines Hypersonic Aerodynamics Lift Lift Drag Ratio Propulsion Spacecraft Vehicles |
| Study on Compression Surface Deformation of Waveriders 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Xu YZ(徐应洲); Cui K(崔凯); Li GL(李广利); Xiao Y(肖尧)
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Aerodynamic Configurations Aerodynamics Computational Fluid Dynamics Deformation Evolutionary Algorithms Fluid Dynamics Hypersonic Aerodynamics Optimization Spacecraft |
| 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：144/24 | 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 |
