Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-6 of 6 Help

Filters                    
Selected(0)Clear Items/Page:    Sort:
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)
Favorite  |  View/Download：89/0  |  Submit date：2024/01/22
High-pressure capturing wing  Subsonic  Numerical simulation  Wing dihedral  Stability  
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)
Adobe PDF(8136Kb)  |  Favorite  |  View/Download：69/9  |  Submit date：2024/03/11
High-pressure capturing wing  Hypersonic  Numerical simulation  Wing dihedral  Stability  
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
Adobe PDF(3584Kb)  |  Favorite  |  View/Download：191/39  |  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
Adobe PDF(2111Kb)  |  Favorite  |  View/Download：185/49  |  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
Adobe PDF(1833Kb)  |  Favorite  |  View/Download：272/73  |  Submit date：2022/11/07
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
Authors:  Yang L(杨磊);  Ye, Zhengyin;  Li WH(李文皓);  Sun QH(孙泉华)
Adobe PDF(4621Kb)  |  Favorite  |  View/Download：279/61  |  Submit date：2021/11/01
Store separation  Aerodynamic modeling  Interference aerodynamics  Dynamic simulation  Air-launch-to-orbit