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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:227/49  |  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:406/73  |  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:216/56  |  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:282/113  |  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:356/125  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 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:543/175  |  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:265/91  |  Submit date:2018/10/30 |
| 隔离段抽吸引起的激波迟滞现象研究 期刊论文 推进技术, 2017, 卷号: 38, 期号: 04, 页码: 732-739 Authors: 马生虎; 岳连捷; 贾轶楠; 肖雅彬; 张新宇 View  |  Adobe PDF(1677Kb)  |  Favorite  |  View/Download:274/75  |  Submit date:2017/12/22 超燃冲压发动机 隔离段 激波反射迟滞 边界层分离迟滞 |
| 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:946/262  |  Submit date:2014/04/15 Hypersonic Inlet Cowl-lip Bluntness Flow Characteristics Shock Pattern Shock Interference |