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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:376/61  |  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: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:252/102  |  提交时间: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 作者: 周芮旭; 连欢; 顾洪斌; 张新宇 浏览  |  Adobe PDF(2073Kb)  |  收藏  |  浏览/下载:285/67  |  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 |
| 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 |
| 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 作者: Fan WH(范文慧); Zhong FQ(仲峰泉); Ma SG(马素刚); Zhang XY(张新宇) 浏览  |  Adobe PDF(4075Kb)  |  收藏  |  浏览/下载:290/84  |  提交时间:2020/03/11 Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| 航空煤油冲击射流强化传热的实验研究 会议论文 中国航天第三专业信息网第四十届技术交流会暨第四届空天动力联合会议, 中国云南昆明, 2019-08-14 作者: 杜蒙蒙; 仲峰泉; 邢云绯; 张新宇 浏览  |  Adobe PDF(987Kb)  |  收藏  |  浏览/下载:165/58  |  提交时间:2020/09/28 实验研究 冲击射流 航空煤油 强化传热 |
| Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781 作者: Zhong FQ(仲峰泉); Cheng LW(程柳维); Gu HB(顾洪斌); Zhang XY(张新宇) Adobe PDF(2032Kb)  |  收藏  |  浏览/下载:292/83  |  提交时间:2019/05/29 Supersonic combustor Hydrocarbon Mixture fuel Flame structure Ignition |
| Numerical Study of Impingement Cooling of Aviation Kerosene at Supercritical Conditions 期刊论文 JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2018, 卷号: 140, 期号: 11, 页码: Ar-112201 作者: Xing YF(邢云绯); Zhong FQ(仲峰泉); Zhang XY(张新宇) 浏览  |  Adobe PDF(2044Kb)  |  收藏  |  浏览/下载:296/114  |  提交时间:2018/12/12 impingement cooling supercritical condition heat transfer kerosene |