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Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration 期刊论文
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(7258Kb)  |  Favorite  |  View/Download：91/18  |  Submit date：2024/01/15
Two-stage-to-orbit  Wind tunnel test  Numerical simulation  Stage separation  Hypersonic  Shock waves  
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:  Dai, Chunliang;  Sun, Bo;  Yue LJ(岳连捷);  Zhou, Shengbing;  Zhuo, Changfei;  Zhou, Changsheng;  Yu, Jianyi
Adobe PDF(5674Kb)  |  Favorite  |  View/Download：46/6  |  Submit date：2024/02/19
Scramjet inlet  Starting ability  Thermochemical  Work performance  
激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
Authors:  王粤;  汪运鹏;  姜宗林
Adobe PDF(6797Kb)  |  Favorite  |  View/Download：380/39  |  Submit date：2022/12/01
两级入轨  轨迹捕获  激波风洞  多体分离  动态试验  试验技术  
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：396/75  |  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  
一种并联两级入轨飞行器纵向分离方案的数值研究 期刊论文
航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634
Authors:  王粤;  汪运鹏;  王春;  姜宗林
Adobe PDF(4901Kb)  |  Favorite  |  View/Download：593/87  |  Submit date：2022/07/11
两级入轨  高超声速  纵向分离  气动干扰  非定常流动  
基于主动射流控制的高超声速进气道再起动性能研究（英文） 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:  靳一超;  姚卫
Adobe PDF(1844Kb)  |  Favorite  |  View/Download：164/40  |  Submit date：2023/02/09
高超声速进气道  不起动  再起动  主动射流  流动控制  
Experimental study of the high-power laser resistance of ablative material-filled sandwich panels with truss cores under hypersonic airflow 期刊论文
COMPOSITE STRUCTURES, 2022, 卷号: 301, 页码: 116139
Authors:  Yuan W(袁武);  Wang JT(王江涛);  Wang RX(王睿星);  Wang Z(王喆);  Song HW(宋宏伟);  Huang CG(黄晨光)
Adobe PDF(9765Kb)  |  Favorite  |  View/Download：189/49  |  Submit date：2022/10/23
Sandwich panel  Thermal insulation  Lightweight structure  Failure point  
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：317/93  |  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：325/86  |  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  
GPU 加速的超大规模可压缩湍流直接数值模拟研究 学位论文
博士论文，北京: 中国科学院大学, 2022
Authors:  党冠麟
Adobe PDF(39646Kb)  |  Favorite  |  View/Download：454/15  |  Submit date：2023/02/06
软件，湍流，高超声速，直接数值模拟，图形处理器