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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:214/77  |  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:377/61  |  提交时间: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 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:187/44  |  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:254/103  |  提交时间:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 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:330/114  |  提交时间:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 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 作者: 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) 浏览  |  Adobe PDF(3099Kb)  |  收藏  |  浏览/下载:361/94  |  提交时间:2019/10/15 Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| 超燃冲压发动机加速过程中燃烧不稳定性研究 会议论文 中国力学大会, 中国浙江杭州, 2019年8月25-28日 作者: 孟宇; 顾洪斌; 岳连捷; 张新宇 浏览  |  Adobe PDF(1057Kb)  |  收藏  |  浏览/下载:252/68  |  提交时间:2019/11/21 超燃冲压发动机 不稳定性 加速过程 直连台 实验研究 |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22 作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇) 浏览  |  Adobe PDF(3918Kb)  |  收藏  |  浏览/下载:521/165  |  提交时间:2019/09/09 Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| 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 作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(714Kb)  |  收藏  |  浏览/下载:31/15  |  提交时间:2023/03/17 |
| 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 作者: Wang ZP(王知溥); Gu HB(顾洪斌); Cheng L W; Zhong FQ(仲峰泉); Zhang XY(张新宇) 浏览  |  Adobe PDF(2630Kb)  |  收藏  |  浏览/下载:250/75  |  提交时间:2019/04/11 supersonic combustion one-dimensional modelling heat release CH* chemiluminescence |