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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 |
| 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 作者: Zhou H(周浩); Li XL(李新亮); Qi H(齐涵); Yu ZP(于长平) Adobe PDF(2907Kb)  |  收藏  |  浏览/下载:380/89  |  提交时间:2020/06/15 |
| 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 |
| 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 作者: 童福林; 孙东; 袁先旭; 李新亮 浏览  |  Adobe PDF(1603Kb)  |  收藏  |  浏览/下载:192/66  |  提交时间: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 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 |
| 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 作者: Lin X(林鑫); Tong FL(童福林); Yu ZP(于长平); Li XL(李新亮) 浏览  |  Adobe PDF(3152Kb)  |  收藏  |  浏览/下载:245/74  |  提交时间:2020/03/11 |
| Numerical study of the pressure wave-induced shedding mechanism in the cavitating flow around an axisymmetric projectile via a compressible multiphase solver 期刊论文 OCEAN ENGINEERING, 2019, 卷号: 187, 页码: 9 作者: Ye BS(叶秉晟); Wang YW(王一伟); Huang CG(黄晨光); Huang J(黄荐) 浏览  |  Adobe PDF(6354Kb)  |  收藏  |  浏览/下载:377/104  |  提交时间:2019/11/12 Cavitation Compressibility Shedding mechanism OpenFOAM (R) |
| 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:405/132  |  提交时间: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 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:259/82  |  提交时间:2019/10/21 Oblique detonation wave Boundary layer Viscosity Detonation initiation Hydrogen-air mixture |