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Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:  Zhang WS(张文硕);  Zhang, Zijian;  Jiang ZL(姜宗林);  Han X(韩信);  Liu, Yunfeng;  Wang, Chun
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Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文
SHOCK WAVES, 2021, 页码: 8
Authors:  Wang Q(汪球);  Li JP(李进平);  Luo K(罗凯);  Li JW(栗继伟);  Zhao W(赵伟)
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Hypersonic  Aerodynamic heating  Detached bow shock  Shock tube  expansion tube  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
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Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:  Zhang ZJ(张子健);  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(3599Kb)  |  Favorite  |  View/Download：363/92  |  Submit date：2021/03/03
Oblique detonation wave  Combustor  Oblique detonation engine  Normal detonation wave  Boundary layer separation  
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download：348/176  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:  Jiang ZL(姜宗林);  Li JP(李进平);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Yu HR(俞鸿儒)
Adobe PDF(1090Kb)  |  Favorite  |  View/Download：271/101  |  Submit date：2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
Authors:  Yuan CK(苑朝凯);  Zhou K(周凯);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Numerical simulation of the interaction of two shear layers in double backward-facing steps 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 5, 页码: 15
Authors:  Deng F(邓放);  Han GL(韩桂来);  Liu MK(刘美宽);  Ding, J;  Weng, PF;  Jiang ZL(姜宗林)
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Experimental investigation of liquid film cooling in hypersonic flow 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10
Authors:  Yuan CK(苑朝凯);  Li JP(李进平);  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
View  |  Adobe PDF(4383Kb)  |  Favorite  |  View/Download：454/132  |  Submit date：2019/06/10