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| Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 14 Authors: Zhou, Lin; Teng, Honghui; Ng, Hoi Dick; Yang PF(杨鹏飞); Jiang ZL(姜宗林) Adobe PDF(6382Kb)  |  Favorite  |  View/Download:235/35  |  Submit date:2021/11/01 Cellular detonation Lead shock evolution Multi-layer perceptron Numerical simulations |
| Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363 Authors: Tong FL(童福林); Sun D(孙栋); Li XL(李新亮) Adobe PDF(4402Kb)  |  Favorite  |  View/Download:217/51  |  Submit date:2021/06/07 Direct numerical simulation Low-frequency unsteadiness Shock waves Turbulent boundary layer Wavy-wall |
| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104 Authors: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童) Adobe PDF(1806Kb)  |  Favorite  |  View/Download:290/61  |  Submit date:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Ma SH(马生虎); Zhang QF(张启帆); Zhang, Peng; Zhang XY(张新宇) Adobe PDF(3937Kb)  |  Favorite  |  View/Download:212/53  |  Submit date:2021/03/30 Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文 NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207 Authors: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒) Adobe PDF(1090Kb)  |  Favorite  |  View/Download:270/101  |  Submit date:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows 期刊论文 ACTA MECHANICA SINICA, 2020, 页码: 9 Authors: Qi H(齐涵); Li XL(李新亮); Yu ZP(于长平) Adobe PDF(2084Kb)  |  Favorite  |  View/Download:362/83  |  Submit date:2020/07/06 Large-eddy simulation Subgrid-scale model Rotating turbulent channel flow |
| 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:660/296  |  Submit date:2019/12/17 Kerosene Supersonic combustion Large eddy simulation Skeletal mechanism Scramjet |
| 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) View  |  Adobe PDF(2806Kb)  |  Favorite  |  View/Download:381/96  |  Submit date:2020/03/21 impingement jet cooling hydrocarbon fuel heat transfer enhancement fluid-solid coupling |
| 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:312/92  |  Submit date:2020/03/11 Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| 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:325/101  |  Submit date:2019/04/11 direct numerical simulation velocity-temperature correlation supersonic flow channel flow thermally perfect gas strong Reynolds analogy |