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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 |
| Subgrid-scale model for large-eddy simulation of transition and turbulence in compressible flows 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 12, 页码: 14
Authors: Zhou H(周浩); Li XL(李新亮); Qi H(齐涵); Yu ZP(于长平)
Adobe PDF(2907Kb) | Favorite | View/Download：408/100 | Submit date：2020/06/15 |
| 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：358/126 | Submit date：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
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 |
| Statistical analysis of temperature distribution on vortex surfaces in hypersonic turbulent boundary layer 期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 10, 页码: 7
Authors: Lin X(林鑫); Tong FL(童福林); Yu ZP(于长平); Li XL(李新亮)
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| 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：428/139 | Submit date：2019/09/09
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：545/176 | Submit date：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711
Authors: Chen XP; Li XL(李新亮); Zhu ZC
View | Adobe PDF(1844Kb) | Favorite | View/Download：328/102 | Submit date：2019/04/11
direct numerical simulation velocity-temperature correlation supersonic flow channel flow thermally perfect gas strong Reynolds analogy |
| 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)
 Adobe PDF(2165Kb) | Favorite | View/Download：420/98 | Submit date：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
