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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：387/65  |  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：198/49  |  提交时间：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
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)
Adobe PDF(3862Kb)  |  收藏  |  浏览/下载：338/118  |  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)
Adobe PDF(4075Kb)  |  收藏  |  浏览/下载：297/86  |  提交时间：2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
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
作者:  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)  |  收藏  |  浏览/下载：364/96  |  提交时间：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration  
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
作者:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
Adobe PDF(3918Kb)  |  收藏  |  浏览/下载：529/169  |  提交时间：2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
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
作者:  Wang ZP(王知溥);  Gu HB(顾洪斌);  Cheng L W;  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
Adobe PDF(2630Kb)  |  收藏  |  浏览/下载：257/77  |  提交时间：2019/04/11
supersonic combustion  one-dimensional modelling  heat release  CH* chemiluminescence  
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
作者:  Tian L;  Chen LH(陈立红);  Chen Q(陈强);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1162Kb)  |  收藏  |  浏览/下载：333/83  |  提交时间：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
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
作者:  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.
Adobe PDF(4711Kb)  |  收藏  |  浏览/下载：304/132  |  提交时间：2016/01/08
Supersonic Combustor  Convective Heat Transfer  Numerical Study  Wall Heat Flux  
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1112Kb)  |  收藏  |  浏览/下载：544/226  |  提交时间：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas