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| 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)
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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：212/53 | Submit date：2021/03/30
Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| 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)
Adobe PDF(3862Kb) | Favorite | View/Download：355/125 | 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)
Adobe PDF(2806Kb) | Favorite | View/Download：379/96 | Submit date：2020/03/21
impingement jet cooling hydrocarbon fuel heat transfer enhancement fluid-solid coupling |
| 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)
Adobe PDF(3099Kb) | Favorite | View/Download：371/98 | Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| 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
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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)
Adobe PDF(3918Kb) | Favorite | View/Download：541/173 | Submit date：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| 真实气体效应对Ma10级进气道流动的影响 期刊论文
推进技术, 2019, 卷号: 40, 期号: 05, 页码: 1042-1050
Authors: 张启帆; 岳连捷; 贾轶楠; 张新宇; 李欣; 高雄
Adobe PDF(1675Kb) | Favorite | View/Download：238/47 | Submit date：2019/09/12
真实气体效应 高马赫数进气道 化学非平衡气体模型 热完全气体模型 前缘钝化 再起动性能 |
| 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
Authors: Xing YF(邢云绯); Zhong FQ(仲峰泉); Zhang XY(张新宇)
Adobe PDF(2044Kb) | Favorite | View/Download：331/135 | Submit date：2018/12/12
impingement cooling supercritical condition heat transfer kerosene |
| Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors: Yue LJ(岳连捷); Jia YN(贾轶南); Xu X; Zhang XY(张新宇); Zhang P(张鹏)
Adobe PDF(2110Kb) | Favorite | View/Download：385/138 | Submit date：2018/10/30
Inlet restart Cowl shock Shock wave boundary layer interactions |
