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| 超燃冲压发动机加速过程及等离子体对超声速火焰结构的影响 学位论文
博士论文，北京: 中国科学院大学, 2019
作者: 孟宇
 Adobe PDF(11443Kb) |  收藏 | 浏览/下载：693/44 | 提交时间：2019/11/07
超燃冲压发动机，燃烧模态，火焰结构，加速过程，微波，滑移电弧，等离子体 |
| Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
作者: Zhang X(张旭); Yue LJ(岳连捷); Huang TL(黄庭隆); Zhang QF(张启帆); Zhang XY(张新宇)
 浏览 |  Adobe PDF(3862Kb) | 收藏 | 浏览/下载：343/121 | 提交时间：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Numerical study of wedge-induced oblique detonations in unsteady flow 期刊论文
JOURNAL OF FLUID MECHANICS, 2019, 卷号: 876, 页码: 264-287
作者: Yang PF(杨鹏飞); Ng HD; Teng HH(滕宏辉)
浏览 | Adobe PDF(1356Kb) | 收藏 | 浏览/下载：369/125 | 提交时间：2019/09/09
detonations |
| A high performance fifth-order multistep WENO scheme 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2019, 卷号: 91, 期号: 4, 页码: 159-182
作者: Ceng FJ(曾方军); Shen YQ(申义庆); Liu SP(刘升平); Liu, L
浏览 | Adobe PDF(1578Kb) | 收藏 | 浏览/下载：323/96 | 提交时间：2019/10/21
critical point high performance low-dissipation multistep WENO scheme transition point |
| Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
作者: Fan WH(范文慧); Zhong FQ(仲峰泉); Ma SG(马素刚); Zhang XY(张新宇)
浏览 | Adobe PDF(4075Kb) | 收藏 | 浏览/下载：301/88 | 提交时间：2020/03/11
Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2019, 卷号: 44, 期号: 41, 页码: 23429-23435
作者: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民)
浏览 | Adobe PDF(1085Kb) | 收藏 | 浏览/下载：271/88 | 提交时间：2019/10/21
Oblique detonation wave Boundary layer Viscosity Detonation initiation Hydrogen-air mixture |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇)
浏览 | Adobe PDF(3918Kb) | 收藏 | 浏览/下载：534/172 | 提交时间：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| Numerical investigation on the initiation of oblique detonation waves in stoichiometric acetylene-oxygen mixtures with high argon dilution 期刊论文
COMBUSTION AND FLAME, 2019, 卷号: 204, 页码: 391-396
作者: Zhang YH; Fang YS(方宜申); Ng HD; Teng HH(滕宏辉)
浏览 | Adobe PDF(1597Kb) | 收藏 | 浏览/下载：255/112 | 提交时间：2019/11/27
Oblique detonation Acetylene-oxygen mixture Argon dilution Initiation structure |
| Numerical study of chemically reacting flow in a shock tube using a high-order point-implicit scheme 期刊论文
COMPUTERS & FLUIDS, 2019, 卷号: 184, 页码: 107-118
作者: Chen S; Sun QH(孙泉华); Klioutchnikov I; Olivier H
浏览 | Adobe PDF(1365Kb) | 收藏 | 浏览/下载：317/119 | 提交时间：2019/06/10
Shock wave/boundary-layer interactions Real gas effects Chemical nonequilibrium High-order scheme |
| Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者: Wang Q(汪球); Lu P(卢盼); Li JW(栗继伟); Wu S(吴松); Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林)
Adobe PDF(299Kb) | 收藏 | 浏览/下载：91/36 | 提交时间：2023/03/17 |
