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| Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor 期刊论文 International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410 作者: Meng Y(孟宇); Gu HB(顾洪斌); Zhang XY(张新宇) Adobe PDF(3187Kb)  |  收藏  |  浏览/下载:213/77  |  提交时间:2021/10/29 |
| 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 作者: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(8067Kb)  |  收藏  |  浏览/下载:376/61  |  提交时间: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 作者: 贺理浩; 张启帆; 岳连捷; 张新宇; 王卫星; 谭慧俊 Adobe PDF(9600Kb)  |  收藏  |  浏览/下载:233/33  |  提交时间: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 作者: 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)  |  收藏  |  浏览/下载:183/43  |  提交时间: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 作者: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇) Adobe PDF(5176Kb)  |  收藏  |  浏览/下载:251/102  |  提交时间:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Experimental and numerical investigation on flow and heat transfer of impingement jet cooling of kerosene 期刊论文 INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2020, 卷号: 116, 页码: 8 作者: Du MM(杜蒙蒙); Zhong FQ(仲峰泉); Xing YF(邢云绯); Zhang XY(张新宇) Adobe PDF(2316Kb)  |  收藏  |  浏览/下载:262/105  |  提交时间:2020/08/26 Impingement jets Kerosene Heat transfer coefficient Pressure loss Reynolds number |
| 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 作者: Yang L; 岳连捷; 张启帆; 张新宇 Adobe PDF(1289Kb)  |  收藏  |  浏览/下载:199/47  |  提交时间:2021/01/12 |
| 激光诱导荧光聚焦纹影系统及超声速燃烧流场应用 期刊论文 气体物理, 2020, 卷号: 5, 期号: 02, 页码: 14-19 作者: 周芮旭; 连欢; 顾洪斌; 张新宇 浏览  |  Adobe PDF(2073Kb)  |  收藏  |  浏览/下载:284/67  |  提交时间:2020/05/06 聚焦纹影 激光诱导荧光 准稳态/非定常 超声速燃烧场 |
| 微波增强滑移电弧等离子体辅助超声速燃烧 期刊论文 航空学报, 2020, 卷号: 41, 期号: 2, 页码: 123345 作者: 孟宇; 顾洪斌; 孙文明; 张新宇 浏览  |  Adobe PDF(945Kb)  |  收藏  |  浏览/下载:223/31  |  提交时间:2019/12/16 超燃冲压发动机 超声速燃烧 等离子体助燃 滑移电弧 微波 |
| 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 作者: Zhang X(张旭); Yue LJ(岳连捷); Huang TL(黄庭隆); Zhang QF(张启帆); Zhang XY(张新宇) 浏览  |  Adobe PDF(3862Kb)  |  收藏  |  浏览/下载:329/113  |  提交时间:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |