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| Study of coupled effect of impingement jet cooling of kerosene with solid structure 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2019, 卷号: 62, 期号: 11, 页码: 2021-2028
Authors: Du MM(杜蒙蒙); Zhong FQ(仲峰泉) ; Xing YF(邢云绯); Zhang XY(张新宇)
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impingement jet cooling hydrocarbon fuel heat transfer enhancement fluid-solid coupling |
| 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
Authors: Yang PF(杨鹏飞); Ng HD; Teng HH(滕宏辉)
View | Adobe PDF(1356Kb) | Favorite | View/Download：381/128 | Submit date：2019/09/09
detonations |
| 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 |
| 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)
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Heat flux measurement Kerosene Supersonic combustion Scramjet Heat flux sensor |
| 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
Authors: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民)
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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
Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇)
View | Adobe PDF(3918Kb) | Favorite | View/Download：539/173 | Submit date：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
Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
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Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
| External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
Authors: Chen H; Tan H; Liu YZ; Zhang QF(张启帆)
View | Adobe PDF(4679Kb) | Favorite | View/Download：279/97 | Submit date：2019/09/09 |
| Combustion states distinction of the methane/oxygen laminar co-flow diffusion flame at high pressure 期刊论文
FUEL, 2019, 卷号: 243, 页码: 221-229
Authors: Ge YF(葛逸飞); Li S(李森); Wei XL(魏小林)
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Diffusion flame Co-flow Laminar Pulsation High pressure |
| Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules 期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
Authors: Zhong K; Yan C; Chen SS; Wang XY(王小永); Ju SJ
View | Adobe PDF(8635Kb) | Favorite | View/Download：232/73 | Submit date：2019/05/29
Aeroheating Heatshield configuration Sphere-cone angle Mars Turbulent |
