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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
Authors: Yao W(姚卫)
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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
Authors: 孟宇
 Adobe PDF(11443Kb) | Favorite | View/Download：736/44 | Submit date：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
Authors: Zhang X(张旭); Yue LJ(岳连捷); Huang TL(黄庭隆); Zhang QF(张启帆); Zhang XY(张新宇)
View | Adobe PDF(3862Kb) | Favorite | View/Download：376/134 | Submit date：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 超声速膨胀角入射激波/湍流边界层干扰直接数值模拟研究 期刊论文
航空学报, 2019, 页码: 21
Authors: 童福林; 孙东; 袁先旭; 李新亮
View | Adobe PDF(1603Kb) | Favorite | View/Download：228/84 | Submit date：2019/12/16
激波/湍流边界层干扰 膨胀角 本征正交分解 直接数值模拟 |
| 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
Authors: Fan WH(范文慧); Zhong FQ(仲峰泉); Ma SG(马素刚); Zhang XY(张新宇)
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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
Authors: 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)
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Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| JF12激波风洞高Mach数超燃冲压发动机实验研究 期刊论文
气体物理, 2019, 卷号: 4, 期号: 05, 页码: 25-31
Authors: 姚轩宇; 王春; 喻江; 苑朝凯; 姜宗林; 司徒明
View | Adobe PDF(2036Kb) | Favorite | View/Download：432/107 | Submit date：2020/01/08
超燃冲压发动机 高Mach数 激波风洞 纯净空气 JF12风洞 |
| Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 92, 页码: 676-684
Authors: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民); Deng, X
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Oblique detonation wave Blunt wedge Initiation Hydrogen |
| Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors: Zhu JJ; Wang XJ; Zhang HG; Li YW; Wang RX(王睿星); Qiu ZP
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Hypersonic vehicle Six sigma robust optimization Successive response surface Thermal protection system Uncertainty |
| 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
Authors: 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)
View | Adobe PDF(2651Kb) | Favorite | View/Download：443/144 | Submit date：2019/09/09
Heat flux measurement Kerosene Supersonic combustion Scramjet Heat flux sensor |
