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Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  Favorite  |  View/Download:420/79  |  Submit date:2022/08/24
Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels  
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:331/89  |  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  
高超声速电离绕流中电子密度的静电探针测量方法研究 期刊论文
实验流体力学, 2013, 卷号: 27, 期号: 6, 页码: 64-69+85
Authors:  汪球;  赵伟;  余西龙;  姜宗林
Adobe PDF(487Kb)  |  Favorite  |  View/Download:908/236  |  Submit date:2014/01/24
静电探针  电子密度  高超声速  高焓激波风洞  Electrostatic Probe  Electron Density  Hypersonic  High Enthalpy Shock Tunnel  
Approximate analytic solution of heat conduction in hollow semi-spheres flying at hypersonic speed 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2013, 卷号: 43, 页码: 46-52
Authors:  Han GL(韩桂来);  Jiang ZL(姜宗林);  Han, GL (reprint author), Chinese Acad Sci, Stake Key Lab High Temp Gas Dynam LHD, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(548Kb)  |  Favorite  |  View/Download:1115/333  |  Submit date:2013/05/31
Heat Conduction  Theoretical Investigation  Approximate Solution  Hypersonic