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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：80/15  |  提交时间：2024/01/15
Two-stage-to-orbit  Wind tunnel test  Numerical simulation  Stage separation  Hypersonic  Shock waves  
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
作者:  Yao KP(姚克鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(1789Kb)  |  收藏  |  浏览/下载：211/37  |  提交时间：2022/06/10
Oblique detonation  Stationary  Thermal choking  Expansion waves  
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
作者:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(5104Kb)  |  收藏  |  浏览/下载：239/45  |  提交时间：2017/05/05
Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow  
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  
Analytical and numerical investigations of the reflection of asymmetric nonstationary shock waves 期刊论文
SHOCK WAVES, 2012, 卷号: 22, 期号: 5, 页码: 435-449
作者:  Yang Y(杨旸);  Wang C(王春);  Jiang ZL(姜宗林);  Yang, Y;  Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(1485Kb)  |  收藏  |  浏览/下载：854/195  |  提交时间：2013/01/18
Asymmetric Shock Waves  Mach Reflection  Detachment Criterion  Mach Reflection  Transition  Boundaries  Domains  Gas