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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) Adobe PDF(3187Kb)  |  Favorite  |  View/Download:246/84  |  Submit date: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 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:395/68  |  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:205/52  |  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:273/111  |  Submit date:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 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 Authors: 周芮旭; 连欢; 顾洪斌; 张新宇 View  |  Adobe PDF(2073Kb)  |  Favorite  |  View/Download:304/73  |  Submit date: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 Authors: 孟宇; 顾洪斌; 孙文明; 张新宇 View  |  Adobe PDF(945Kb)  |  Favorite  |  View/Download:236/33  |  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 |
| 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:346/121  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文 ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953 Authors: Fan WH(范文慧); Zhong FQ(仲峰泉); Ma SG(马素刚); Zhang XY(张新宇) View  |  Adobe PDF(4075Kb)  |  Favorite  |  View/Download:306/90  |  Submit date:2020/03/11 Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文 Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316 Authors: Meng Y(孟宇); Gu HB(顾洪斌); Zhuang JH(庄金衡); Sun WM(孙文明); Gao ZB(高占彪); Lian H(连欢); Yue LJ(岳连捷); Chang XY(张新宇) View  |  Adobe PDF(3099Kb)  |  Favorite  |  View/Download:370/98  |  Submit date:2019/10/15 Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization 期刊论文 INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50 Authors: Wang ZP(王知溥); Gu HB(顾洪斌); Cheng L W; Zhong FQ(仲峰泉); Zhang XY(张新宇) View  |  Adobe PDF(2630Kb)  |  Favorite  |  View/Download:262/79  |  Submit date:2019/04/11 supersonic combustion one-dimensional modelling heat release CH* chemiluminescence |