|
Selected(0)Clear
Items/Page: Sort: |
| 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：227/49 | Submit date：2022/01/12
Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| 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：213/54 | 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：281/113 | Submit date：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 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：355/125 | Submit date：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors: Meng Y(孟宇); Gu HB(顾洪斌); Zhuang JH(庄金衡); Sun WM(孙文明); Gao ZB(高占彪); Lian H(连欢); Yue LJ(岳连捷); Chang XY(张新宇)
View | Adobe PDF(3099Kb) | Favorite | View/Download：371/98 | Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| 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：542/174 | Submit date：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| Comment on "Mechanics of Combustion Mode Transition in a Direct-Connect Ramjet-Scramjet Experiment" 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 2, 页码: 550-551
Authors: Chen KT(陈科挺); Yue LJ(岳连捷); Chang XY(张新宇)
View | Adobe PDF(148Kb) | Favorite | View/Download：264/90 | Submit date：2018/10/30 |
| 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)
View | Adobe PDF(2110Kb) | Favorite | View/Download：386/138 | Submit date：2018/10/30
Inlet restart Cowl shock Shock wave boundary layer interactions |
| The vitiation effects of water vapor and carbon dioxide on the autoignition characteristics of kerosene 期刊论文
Acta Mechanica Sinica, 2014, 卷号: 30, 期号: 4, 页码: 485-494
Authors: Liang JH(梁金虎); Wang S(王苏); Zhang ST(张胜涛); Yue LJ(岳连捷); Fan BC(范秉诚); Zhang XY(张新宇); Cui JP(崔季平); Wang S(王苏)
View | Adobe PDF(1351Kb) | Favorite | View/Download：893/221 | Submit date：2014/08/14
Ignition Delay Vitiation Effect Kerosene Water Carbon Dioxide Shock Tube |
| Flow characteristics of hypersonic inlets with different cowl-lip blunting methods 期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors: Lu HB(卢洪波); Yue LJ(岳连捷); Zhang XY(张新宇); Yue LJ(岳连捷)
View | Adobe PDF(1133Kb) | Favorite | View/Download：944/261 | Submit date：2014/04/15
Hypersonic Inlet Cowl-lip Bluntness Flow Characteristics Shock Pattern Shock Interference |
