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| A theoretical method for solving shock relations coupled with chemical equilibrium and its applications 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors: Zhang, Zijian; Wen, Chihyung; Zhang WS(张文硕) ; Liu YF(刘云峰); Jiang ZL(姜宗林)
 Adobe PDF(3178Kb) |  Favorite | View/Download：253/60 | Submit date：2022/07/18
Chemical equilibrium Detonation Dissociated air Shock relation Theoretical solution |
| Mechanisms of the destabilized Mach reflection of inviscid oblique detonation waves before an expansion corner 期刊论文
JOURNAL OF FLUID MECHANICS, 2022, 卷号: 940, 页码: 39
Authors: Zhang, Zijian; Liu YF(刘云峰); Wen, Chihyung
Adobe PDF(1777Kb) | Favorite | View/Download：183/50 | Submit date：2022/05/17
detonation waves |
| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors: Lin MY(林明月); Wang C(王春); Peng J(彭俊); Jiang ZL(姜宗林)
Adobe PDF(4805Kb) | Favorite | View/Download：348/68 | Submit date：2022/01/12 |
| 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)
Adobe PDF(1158Kb) | Favorite | View/Download：284/64 | Submit date：2021/05/17
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)
Adobe PDF(1806Kb) | Favorite | View/Download：295/65 | Submit date：2021/05/17
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：382/94 | 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：357/178 | 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：279/101 | Submit date：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
 View | Adobe PDF(2165Kb) | Favorite | View/Download：424/99 | Submit date：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| 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)
View | Adobe PDF(5760Kb) | Favorite | View/Download：564/92 | Submit date：2019/10/21 |
