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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 Authors: Meng Y(孟宇) ; Gu HB(顾洪斌) ; Zhang XY(张新宇)![](/image/person.jpg)
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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)![](/image/person.jpg)
Adobe PDF(511Kb)  |   Favorite  |  View/Download:238/54  |  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)![](/image/person.jpg)
Adobe PDF(8067Kb)  |   Favorite  |  View/Download:423/80  |  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:279/43  |  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)![](/image/person.jpg)
Adobe PDF(3937Kb)  |   Favorite  |  View/Download:230/61  |  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)![](/image/person.jpg)
Adobe PDF(5176Kb)  |   Favorite  |  View/Download:292/115  |  Submit date: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 Authors: Du MM(杜蒙蒙); Zhong FQ(仲峰泉) ; Xing YF(邢云绯) ; Zhang XY(张新宇)![](/image/person.jpg)
Adobe PDF(2316Kb)  |   Favorite  |  View/Download:295/119  |  Submit date:2020/08/26 Impingement jets Kerosene Heat transfer coefficient Pressure loss Reynolds number |
| 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 Authors: 孟宇 ; 顾洪斌 ; 孙文明; 张新宇![](/image/person.jpg)
View  |   Adobe PDF(945Kb)  |   Favorite  |  View/Download:254/37  |  Submit date: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 |
| 斜爆轰波的波角和法向速度-曲率关系初步探究 期刊论文 航空学报, 2020, 卷号: 41, 页码: 123701 Authors: 杨理; 岳连捷 ; 张新宇![](/image/person.jpg)
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| 微波对超声速燃烧火焰结构的影响 期刊论文 航空学报, 2019, 卷号: 40, 期号: 12, 页码: 88-96 Authors: 孟宇 ; 顾洪斌 ; 张新宇![](/image/person.jpg)
View  |   Adobe PDF(578Kb)  |   Favorite  |  View/Download:409/79  |  Submit date:2020/01/08 超燃冲压发动机 超声速燃烧 火焰结构 微波 火焰边界 分形几何 |