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| Effects of inflow Mach number on oblique detonation initiation with a two-step induction-reaction kinetic model 期刊论文
COMBUSTION AND FLAME, 2018, 卷号: 193, 页码: 246-256
Authors: Yang PF; Teng HH(滕宏辉) ; Jiang ZL(姜宗林); Ng HD
 View |  Adobe PDF(2840Kb) |  Favorite | View/Download：784/128 | Submit date：2018/10/30
Oblique detonation Induction-reaction kinetics Initiation length Initiation structure |
| Shock/shock interactions between bodies and wings 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors: Xiang GX(项高翔); Wang C(王春); Teng HH(腾宏辉); Jiang ZL(姜宗林)
View | Adobe PDF(1161Kb) | Favorite | View/Download：318/76 | Submit date：2018/10/30
Body And Wing Flow Field Hypersonic Flow Shock/shock Interaction Wave Configurations |
| Numerical investigation of the axial impulse load during the startup in the shock tunnel 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
Authors: Meng BQ(孟宝清); Han GL(韩桂来); Luo ZT(罗长童); Jiang ZL(姜宗林)
View | Adobe PDF(1937Kb) | Favorite | View/Download：270/87 | Submit date：2018/10/30
Hypersonic Shock tunnel Start-up process Impulse force Vibration |
| A numerical study on the instability of oblique detonation waves with a two-step induction–reaction kinetic model 期刊论文
Proceedings of the Combustion Institute, 2018
Authors: Yang PF(杨鹏飞); Teng HH(滕红辉); Ng HD; Jiang ZL(姜宗林)
View | Adobe PDF(1827Kb) | Favorite | View/Download：308/58 | Submit date：2019/01/09 |
