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| 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:399/69  |  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:208/52  |  Submit date:2021/03/30 Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文 4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020 Authors: Yang L; 岳连捷; 张启帆; 张新宇 Adobe PDF(1289Kb)  |  Favorite  |  View/Download:221/55  |  Submit date:2021/01/12 |
| 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:351/124  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 真实气体效应对Ma10级进气道流动的影响 期刊论文 推进技术, 2019, 卷号: 40, 期号: 05, 页码: 1042-1050 Authors: 张启帆; 岳连捷; 贾轶楠; 张新宇; 李欣; 高雄 View  |  Adobe PDF(1675Kb)  |  Favorite  |  View/Download:235/47  |  Submit date:2019/09/12 真实气体效应 高马赫数进气道 化学非平衡气体模型 热完全气体模型 前缘钝化 再起动性能 |
| Numerical Study of Heat Transfer on Confined Under-Expanded Impinging Jet from Slot into a Plenum 会议论文 31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(714Kb)  |  Favorite  |  View/Download:36/17  |  Submit date:2023/03/17 |
| 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:384/138  |  Submit date:2018/10/30 Inlet restart Cowl shock Shock wave boundary layer interactions |
| 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:269/73  |  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 |
| Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Ma SH; Jia YN(贾轶南); Zhang XY(张新宇); Yue, Lianjie(yuelj@imech.ac.cn) View  |  Adobe PDF(704Kb)  |  Favorite  |  View/Download:273/93  |  Submit date:2018/01/16 Spacecraft |
| 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) View  |  Adobe PDF(566Kb)  |  Favorite  |  View/Download:338/74  |  Submit date:2018/01/16 Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |