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| Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors: Chen KT(陈科挺); Yue LJ(岳连捷) ; Zhang XY(张新宇)
 Adobe PDF(511Kb) |  Favorite | View/Download：226/49 | Submit date：2022/01/12
Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(8067Kb) | Favorite | View/Download：404/71 | Submit date：2021/03/03
Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 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 |
| Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
Authors: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇)
Adobe PDF(5176Kb) | Favorite | View/Download：279/113 | Submit date：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 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 |
| CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization 期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50
Authors: Wang ZP(王知溥); Gu HB(顾洪斌); Cheng L W; Zhong FQ(仲峰泉); Zhang XY(张新宇)
View | Adobe PDF(2630Kb) | Favorite | View/Download：265/79 | Submit date：2019/04/11
supersonic combustion one-dimensional modelling heat release CH* chemiluminescence |
| Numerical Study of Impingement Cooling of Aviation Kerosene at Supercritical Conditions 期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2018, 卷号: 140, 期号: 11, 页码: Ar-112201
Authors: Xing YF(邢云绯); Zhong FQ(仲峰泉); Zhang XY(张新宇)
View | Adobe PDF(2044Kb) | Favorite | View/Download：333/137 | Submit date：2018/12/12
impingement cooling supercritical condition heat transfer kerosene |
| Numerical study on supersonic combustion of hydrogen and its mixture with Ethylene and methane with strut injection 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2018, 卷号: 43, 期号: 15, 页码: 7591-7599
Authors: Ma SG(马素刚); Zhong FQ(仲峰泉); Zhang XY(张新宇)
View | Adobe PDF(2634Kb) | Favorite | View/Download：284/117 | Submit date：2018/07/17
Detached Eddy Simulation Reduced Kinetic Mechanism Supersonic Combustion Hydrogen Hydrocarbon |
| Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors: Yue LJ(岳连捷); Jia YN(贾轶南); Xu X; Zhang XY(张新宇); Zhang P(张鹏)
 Adobe PDF(2110Kb) | Favorite | View/Download：385/138 | Submit date：2018/10/30
Inlet restart Cowl shock Shock wave boundary layer interactions |
| The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Jia YN(贾轶南); Yue LJ(岳连捷); Zhang XY(张新宇); Jia, Yinan(yuelj@imech.ac.cn)
Adobe PDF(566Kb) | Favorite | View/Download：341/74 | Submit date：2018/01/16
Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
