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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：329/96  |  Submit date：2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download：330/88  |  Submit date：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
Control of shock-wave/boundary-layer interaction using abackward-facing step 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 126, 页码: 13
Authors:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW(张伟为)
Adobe PDF(4533Kb)  |  Favorite  |  View/Download：188/50  |  Submit date：2022/12/20
Shock-wave/boundary-layer interaction  Backward-facing step  Flow separation  Hypersonic inlet  
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：194/39  |  Submit date：2022/07/18
Double wedge  Hypersonic flow  Initiation structures  Oblique detonation  Shock interactions  
Thermochemical non-equilibrium effects on hypersonic shock wave/turbulent boundary-layer interaction 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 192, 页码: 1-14
Authors:  Jiang, Hao;  Liu, Jun;  Luo, Shichao;  Huang, Wei;  Wang, Junyuan;  Liu MK(刘美宽)
Adobe PDF(9113Kb)  |  Favorite  |  View/Download：255/43  |  Submit date：2022/05/17
Hypersonic flow  Shock wave/turbulent boundary-layer interactions  Thermochemical non-equilibrium  Turbulence model  
Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2554Kb)  |  Favorite  |  View/Download：168/41  |  Submit date：2022/06/10
Boundary layer correction  High-enthalpy flow  Hypersonic wind tunnel  Nozzle design  Real-gas effects