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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)
Adobe PDF(8067Kb)  |  Favorite  |  View/Download：399/69  |  Submit date：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
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：208/52  |  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)
View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download：351/124  |  Submit date：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
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：309/91  |  Submit date：2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
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
View  |  Adobe PDF(1675Kb)  |  Favorite  |  View/Download：235/47  |  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  
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
Authors:  Wang ZP(王知溥);  Gu HB(顾洪斌);  Cheng L W;  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
View  |  Adobe PDF(2630Kb)  |  Favorite  |  View/Download：263/79  |  Submit date：2019/04/11
supersonic combustion  one-dimensional modelling  heat release  CH* chemiluminescence  
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)
View  |  Adobe PDF(2110Kb)  |  Favorite  |  View/Download：384/138  |  Submit date：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
Authors:  马生虎;  岳连捷;  贾轶楠;  肖雅彬;  张新宇
View  |  Adobe PDF(1677Kb)  |  Favorite  |  View/Download：269/73  |  Submit date：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  
Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor 期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:  Wang X;  Zhong FQ(仲峰泉);  Gu HB(顾宏斌);  Zhang XY(张新宇);  Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(4711Kb)  |  Favorite  |  View/Download：312/134  |  Submit date：2016/01/08
Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
Quasi-One-Dimensional Multimodes Analysis for Dual-Mode Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2014, 卷号: 30, 期号: 6, 页码: 1559-1567
Authors:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Li F(李飞);  Zhang XY(张新宇);  Tian, L (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
View  |  Adobe PDF(7587Kb)  |  Favorite  |  View/Download：596/136  |  Submit date：2014/12/18