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Study on Flame Stabilization in a Dual-Mode Combustor Using Optical Measurements 期刊论文
JOURNAL OF PROPULSION AND POWER, 2015, 卷号: 31, 期号: 6, 页码: 1524-1531
作者:  Yuan YM(袁越明);  Zhang TC(张泰昌);  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(578Kb)  |  收藏  |  浏览/下载:480/133  |  提交时间:2016/03/21
Large-eddy simulation of orientation and rotation of ellipsoidal particles in isotropic turbulent fows 期刊论文
Journal of turbulence, 2015, 卷号: 17, 期号: 3, 页码: 308-326
作者:  Chen JC(陈进财);  Jin GD(晋国栋);  Zhang J(张健)
浏览  |  Adobe PDF(2831Kb)  |  收藏  |  浏览/下载:426/141  |  提交时间:2015/12/23
湍流大涡模拟的时空关联方法 期刊论文
中国科学: 物理学 力学 天文学, 2015, 卷号: 45, 期号: 12, 页码: 124702
作者:  晋国栋;  陈进财;  时北极;  何国威
浏览  |  Adobe PDF(3034Kb)  |  收藏  |  浏览/下载:1020/148  |  提交时间:2015/12/23
湍流  大涡模拟  时空关联  湍流噪声  携带颗粒湍流  Turbulent Flows  Large-eddy Simulation  Space-time Correlation  Turbulent Noise  Particle-laden Turbulent Flows  
Aerothermal characteristics of bleed slot in hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
作者:  Yue LJ(岳连捷);  Lu HB;  Xu X;  Chang XY;  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
Improvement of weighted compact scheme with multi-step strategy for supersonic compressible flow 期刊论文
COMPUTERS & FLUIDS, 2015, 卷号: 115, 页码: 2841-2849
作者:  Peng J(彭峻);  Shen YQ(申义庆);  Shen, YQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Numerical Method  Supersonic Compressible Flow  Weighted Compact Scheme  Multi-step Strategy  
Experimental study on spectrum and multi-scale nature of wall pressure and velocity in turbulent boundary layer 期刊论文
CHINESE PHYSICS B, 2015, 卷号: 24, 期号: 6, 页码: 64702
作者:  Zheng Xiao-Bo;  Jiang Nan;  Jiang, N (reprint author), Tianjin Univ, Dept Mech, Tianjin 300072, Peoples R China.
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Multi-scale Coherent Structures  Hot Wire Anemometry  Microphone  Wavelet Transform  
Direct Numerical Simulation on Mach Number and Wall Temperature Effects in the Turbulent Flows of Flat-Plate Boundary Layer 期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 17, 期号: 1, 页码: 189-212
作者:  Liang X;  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(860Kb)  |  收藏  |  浏览/下载:760/239  |  提交时间:2015/06/12
Hypersonic  Directly Numerical Simulation  Compressibility Effects  Turbulent Boundary Layer  Strong Reynolds Analogy