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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：107/19  |  Submit date：2024/01/15
Two-stage-to-orbit  Wind tunnel test  Numerical simulation  Stage separation  Hypersonic  Shock waves  
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：403/40  |  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  
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：608/92  |  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  
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  
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)
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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：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  
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：387/80  |  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  
JF-12激波风洞在火星进入环境下的运行特性 期刊论文
航空学报, 2021, 卷号: 42, 期号: 03, 页码: 189-200
Authors:  韩子健;  彭俊;  胡宗民;  韩桂来;  姜宗林
Adobe PDF(5070Kb)  |  Favorite  |  View/Download：367/94  |  Submit date：2021/04/19
火星探测  反向爆轰驱动激波风洞  二氧化碳  缝合运行状态  驻室压力  
高超声速溢流冷却实验研究 期刊论文
力学学报, 2018, 卷号: 50, 期号: 1, 页码: 1-8
Authors:  苑朝凯;  李进平;  陈宏;  姜宗林;  俞鸿儒
View  |  Adobe PDF(570Kb)  |  Favorite  |  View/Download：409/97  |  Submit date：2018/10/24
高超声速热防护  主动冷却  溢流冷却  液膜  
Shock relations in gases of heterogeneous thermodynamic properties 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭俊);  Li JP(李进平);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1654Kb)  |  Favorite  |  View/Download：376/94  |  Submit date：2017/10/25
Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution