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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:369/58  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 高速进气道低马赫数不起动特性及马赫数影响规律 期刊论文 推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217 Authors: 贺理浩; 张启帆; 岳连捷; 张新宇; 王卫星; 谭慧俊 Adobe PDF(9600Kb)  |  Favorite  |  View/Download:220/31  |  Submit date:2021/11/12 高速进气道 低马赫数不起动 非定常 气动力 自起动 |
| 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:172/40  |  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:243/97  |  Submit date:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 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:185/44  |  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:324/112  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 一种进气道定堵塞度自起动试验装置 专利 发明专利. 一种进气道定堵塞度自起动试验装置, 专利号: ZL201710941567.2, 申请日期: 2017-10-11, Inventors: 张启帆; 彭辉; 岳连捷; 南轶楠; 张新宇 View  |  Adobe PDF(502Kb)  |  Favorite  |  View/Download:140/21  |  Submit date:2020/02/10 |
| 内压缩波系对高超声速进气道自起动性能影响研究 期刊论文 实验流体力学, 2019, 卷号: 33, 期号: 03, 页码: 60-67 Authors: 贾轶楠; 张启帆; 仝晓通; 岳连捷; 张新宇 View  |  Adobe PDF(2765Kb)  |  Favorite  |  View/Download:336/39  |  Submit date:2019/09/12 自起动性能 肩部膨胀扇 侧压式 边界层厚度 几何喉道 气动喉道 |
| 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:189/41  |  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 |