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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)
 View |  Adobe PDF(9586Kb) |  Favorite | View/Download：685/303 | Submit date：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
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：427/107 | 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：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：227/83 | 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 |
| A high performance fifth-order multistep WENO scheme 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2019, 卷号: 91, 期号: 4, 页码: 159-182
Authors: Ceng FJ(曾方军); Shen YQ(申义庆); Liu SP(刘升平); Liu, L
View | Adobe PDF(1578Kb) | Favorite | View/Download：361/115 | Submit date：2019/10/21
critical point high performance low-dissipation multistep WENO scheme transition point |
| 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)
View | Adobe PDF(4075Kb) | Favorite | View/Download：335/101 | Submit date：2020/03/11
Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 93, 页码: 9
Authors: Fu YW(符耀威); Yu ZP(于长平); Yan Z(闫正); Li XL(李新亮)
View | Adobe PDF(2894Kb) | Favorite | View/Download：427/155 | Submit date：2020/03/21
Supersonic combustion Turbulence jet Direct numerical simulations Coherent structures |
| 高温非平衡流动中的氧分子振动态精细分析 期刊论文
力学学报, 2019, 页码: 14
Authors: 洪启臻; 王小永; 孙泉华
View | Adobe PDF(1760Kb) | Favorite | View/Download：490/126 | Submit date：2019/12/16
高温非平衡，振动松弛，态-态计算，驻点线模型 |
| 设计参数对幂次乘波体纵向静稳定性的影响 期刊论文
宇航学报, 2019, 期号: 08, 页码: 887-896
Authors: 王晓朋; 张陈安; 刘文; 王发民; 叶正寅
View | Adobe PDF(663Kb) | Favorite | View/Download：435/65 | Submit date：2019/09/12
纵向静稳定性 幂次乘波体 高超声速滑翔飞行器 |
| 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)
View | Adobe PDF(1085Kb) | Favorite | View/Download：301/96 | Submit date：2019/10/21
Oblique detonation wave Boundary layer Viscosity Detonation initiation Hydrogen-air mixture |
