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| Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
作者: Yao W(姚卫)
 浏览 |  Adobe PDF(9586Kb) |  收藏 | 浏览/下载：644/293 | 提交时间：2019/12/17
Kerosene Supersonic combustion Large eddy simulation Skeletal mechanism Scramjet |
| 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：679/44 | 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：330/114 | 提交时间：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 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：293/85 | 提交时间：2020/03/11
Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
作者: Meng Y(孟宇); Gu HB(顾洪斌); Zhuang JH(庄金衡); Sun WM(孙文明); Gao ZB(高占彪); Lian H(连欢); Yue LJ(岳连捷); Chang XY(张新宇)
浏览 | Adobe PDF(3099Kb) | 收藏 | 浏览/下载：361/94 | 提交时间：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| Numerical investigations of fully nonlinear water waves generated by moving bottom topography 期刊论文
Theoretical & Applied Mechanics Letters, 2019, 卷号: 9, 页码: 35-44
作者: Wang M(王冕)
Adobe PDF(3436Kb) | 收藏 | 浏览/下载：114/25 | 提交时间：2021/06/10
Underwater landslide Surface gravity waves Euler equations |
| Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor 期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11
作者: Cheng D(程迪); Wang J(王晶); Lu Y(陆阳); Li L(李龙); Yao W(姚卫); Fan XJ(范学军)
浏览 | Adobe PDF(2651Kb) | 收藏 | 浏览/下载：404/132 | 提交时间：2019/09/09
Heat flux measurement Kerosene Supersonic combustion Scramjet Heat flux sensor |
| 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：521/165 | 提交时间：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| 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
作者: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
浏览 | Adobe PDF(2165Kb) | 收藏 | 浏览/下载：396/92 | 提交时间：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| 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：244/107 | 提交时间：2019/11/27
Oblique detonation Acetylene-oxygen mixture Argon dilution Initiation structure |
