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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
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：184/43  |  提交时间：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Experimental and numerical investigation on flow and heat transfer of impingement jet cooling of kerosene 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2020, 卷号: 116, 页码: 8
作者:  Du MM(杜蒙蒙);  Zhong FQ(仲峰泉);  Xing YF(邢云绯);  Zhang XY(张新宇)
Adobe PDF(2316Kb)  |  收藏  |  浏览/下载：262/105  |  提交时间：2020/08/26
Impingement jets  Kerosene  Heat transfer coefficient  Pressure loss  Reynolds number  
High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
作者:  Yang L;  岳连捷;  张启帆;  张新宇
Adobe PDF(1289Kb)  |  收藏  |  浏览/下载：200/48  |  提交时间：2021/01/12
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
作者:  张启帆;  岳连捷;  贾轶楠;  张新宇;  李欣;  高雄
浏览  |  Adobe PDF(1675Kb)  |  收藏  |  浏览/下载：204/44  |  提交时间：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 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
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
作者:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
浏览  |  Adobe PDF(2110Kb)  |  收藏  |  浏览/下载：367/135  |  提交时间：2018/10/30
Inlet restart  Cowl shock  Shock wave boundary layer interactions  
隔离段抽吸引起的激波迟滞现象研究 期刊论文
推进技术, 2017, 卷号: 38, 期号: 04, 页码: 732-739
作者:  马生虎;  岳连捷;  贾轶楠;  肖雅彬;  张新宇
浏览  |  Adobe PDF(1677Kb)  |  收藏  |  浏览/下载：250/66  |  提交时间：2017/12/22
超燃冲压发动机  隔离段  激波反射迟滞  边界层分离迟滞  
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate 期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
作者:  Zhong FQ(仲峰泉);  Ma SG;  Zhang XY(张新宇);  Sung CJ;  Niemeyer KE;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1318Kb)  |  收藏  |  浏览/下载：287/91  |  提交时间：2016/01/08
Reduced Chemistry  Hydrocarbons  Directed Relation Graph  Ignition Delay Time  
Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 85, 页码: 1003-1011
作者:  Dang GX;  Zhong FQ(仲峰泉);  Zhang YJ;  Zhang XY(张新宇);  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(2856Kb)  |  收藏  |  浏览/下载：462/135  |  提交时间：2015/06/12
Supercritical Kerosene  Convective Heat Transfer  Turbulent Flow  Numerical Study