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Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9707Kb)  |  Favorite  |  View/Download:340/100  |  Submit date:2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
Oblique detonation wave triggered by a double wedge in hypersonic flow 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184
Authors:  Teng, Honghui;  Zhang, Yuhang;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(1747Kb)  |  Favorite  |  View/Download:199/41  |  Submit date:2022/07/18
Double wedge  Hypersonic flow  Initiation structures  Oblique detonation  Shock interactions  
TSTO马赫7安全级间分离问题的数值研究 期刊论文
力学学报, 2022, 卷号: 54, 期号: 2, 页码: 526-542
Authors:  王粤;  汪运鹏;  薛晓鹏;  姜宗林
Adobe PDF(3565Kb)  |  Favorite  |  View/Download:394/81  |  Submit date:2021/12/23
两级入轨  高超声速  分离流动  气动干扰  级间分离  
高超声速高焓条件下的内嵌式温敏漆测量方法 期刊论文
力学学报, 2022, 卷号: 54, 期号: 01, 页码: 48-58
Authors:  苑朝凯;  姜宗林
Adobe PDF(1381Kb)  |  Favorite  |  View/Download:144/32  |  Submit date:2022/03/16
温敏漆  热流密度场  辐射效应  高超声速流动  辨识方法