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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 View  |  Adobe PDF(578Kb)  |  Favorite  |  View/Download:405/76  |  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 |
| 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:362/127  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Study of coupled effect of impingement jet cooling of kerosene with solid structure 期刊论文 SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2019, 卷号: 62, 期号: 11, 页码: 2021-2028 Authors: Du MM(杜蒙蒙); Zhong FQ(仲峰泉); Xing YF(邢云绯); Zhang XY(张新宇) View  |  Adobe PDF(2806Kb)  |  Favorite  |  View/Download:393/101  |  Submit date:2020/03/21 impingement jet cooling hydrocarbon fuel heat transfer enhancement fluid-solid coupling |
| 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:320/96  |  Submit date:2020/03/11 Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| 一种用于风洞中流道壁面切应力的测量装置 专利 发明专利. 一种用于风洞中流道壁面切应力的测量装置, 专利号: ZL201711458666.1, 申请日期: 2017-12-28, Inventors: 孟东东; 顾洪斌; 李东霞; 张新宇; 高占彪 View  |  Adobe PDF(553Kb)  |  Favorite  |  View/Download:161/27  |  Submit date:2020/02/10 |
| 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:378/100  |  Submit date: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 Authors: 孟宇; 顾洪斌; 岳连捷; 张新宇 View  |  Adobe PDF(1057Kb)  |  Favorite  |  View/Download:284/80  |  Submit date: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 |
| 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 Authors: 杜蒙蒙; 仲峰泉; 邢云绯; 张新宇 View  |  Adobe PDF(987Kb)  |  Favorite  |  View/Download:181/66  |  Submit date:2020/09/28 实验研究 冲击射流 航空煤油 强化传热 |
| 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 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇) View  |  Adobe PDF(3918Kb)  |  Favorite  |  View/Download:548/178  |  Submit date:2019/09/09 Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| 一种进气道定堵塞度自起动试验装置 专利 发明专利. 一种进气道定堵塞度自起动试验装置, 专利号: ZL201710941567.2, 申请日期: 2017-10-11, Inventors: 张启帆; 彭辉; 岳连捷; 南轶楠; 张新宇 View  |  Adobe PDF(502Kb)  |  Favorite  |  View/Download:165/31  |  Submit date:2020/02/10 |