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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：346/101  |  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：339/95  |  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  
A numerical study of oblique detonation re-stabilization by expansion waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 122, 页码: 8
Authors:  Yao KP(姚克鹏);  Wang C(王春);  Jiang ZL(姜宗林)
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Oblique detonation  Stationary  Thermal choking  Expansion waves  
An experimental study of formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2022, 卷号: 237, 页码: 5
Authors:  Zhang ZJ(张子健);  Wen, Chihyung;  Yuan CK(苑朝凯);  Liu YF(刘云峰);  Han GL(韩桂来);  Wang C(王春);  Jiang ZL(姜宗林)
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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：179/46  |  Submit date：2022/06/10
Boundary layer correction  High-enthalpy flow  Hypersonic wind tunnel  Nozzle design  Real-gas effects