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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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(7258Kb)  |  收藏  |  浏览/下载：79/15  |  提交时间：2024/01/15
Two-stage-to-orbit  Wind tunnel test  Numerical simulation  Stage separation  Hypersonic  Shock waves  
Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9327Kb)  |  收藏  |  浏览/下载：192/62  |  提交时间：2023/05/26
Two-stage-to-orbit  Hypersonic  Numerical simulation  Stage separation  Aerodynamic interaction  Unsteady flow  Center of gravity  
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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  收藏  |  浏览/下载：365/69  |  提交时间：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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9707Kb)  |  收藏  |  浏览/下载：297/85  |  提交时间：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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  收藏  |  浏览/下载：309/82  |  提交时间：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  
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
作者:  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.
浏览  |  Adobe PDF(1654Kb)  |  收藏  |  浏览/下载：346/83  |  提交时间：2017/10/25
Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution  
Influence of Thermal Sensor Installation on Measuring Accuracy at Stagnation Points 期刊论文
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2017, 卷号: 31, 期号: 2, 页码: 318-323
作者:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(419Kb)  |  收藏  |  浏览/下载：428/114  |  提交时间：2017/10/27
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
作者:  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)  |  收藏  |  浏览/下载：1097/326  |  提交时间：2013/05/31
Heat Conduction  Theoretical Investigation  Approximate Solution  Hypersonic  
Concept of non-ablative thermal protection system for hypersonic vehicles 期刊论文
AIAA Journal, 2013, 卷号: 51, 期号: 3, 页码: 584-590
作者:  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(5046Kb)  |  收藏  |  浏览/下载：1383/495  |  提交时间：2013/04/07
Flow Fields  Flow Visualization  Hypersonic Aerodynamics  Hypersonic Vehicles  Mach Number  Shock Waves  Thermal Insulating Materials  Engineering Applications  Experimental Datum  Hypersonic Wind Tunnels  Numerical Results  Stagnation Points  Thermal Protection  Thermal Protection System  Working Pressures  
On the transition pattern of the oblique detonation structure 期刊论文
JOURNAL OF FLUID MECHANICS, 2012, 卷号: 713, 页码: 659-669
作者:  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Teng, HH;  Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1414Kb)  |  收藏  |  浏览/下载：1233/360  |  提交时间：2013/01/18
Detonations  Reacting Flows  Numerical-simulation  Shock-waves  Wedge  Combustion  Stability