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A new solver for granular avalanche simulation: Indoor experiment verification and field scale case study 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2017, 卷号: 60, 期号: 12
作者:  Wang XL(王晓亮);  Li JC(李家春);  Li, JC (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.;  Li, JC (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Avalanche  Landslide  Waf  Tvd  
Numerical studies of static aeroelastic effects on grid fin aerodynamic performances 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314
作者:  Huang CD(黄程德);  Liu W(刘文);  Yang GW(杨国伟)
浏览  |  Adobe PDF(4021Kb)  |  收藏  |  浏览/下载:328/98  |  提交时间:2017/11/29
Aeroelasticity  Fluid-structure Interpolation  Grid Fin  Mesh Deformation  Radial Basis Function  
Shock relations in gases of heterogeneous thermodynamic properties 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
作者:  Hu ZM(胡宗民);  Zhou K(周凯);  Peng J(彭俊);  Li JP(李进平);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1654Kb)  |  收藏  |  浏览/下载:341/81  |  提交时间:2017/10/25
Shock Wave  Imperfect Gas  Heterogeneous  Theoretical Solution  
基于过程变量-火焰面模型的湍流燃烧大涡模拟 期刊论文
中国科学:物理学 力学 天文学, 2017, 卷号: 47, 期号: 07, 页码: 79-90
作者:  张健;  刘柽钰;  杨涛
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湍流燃烧  大涡模拟  火焰面模型  过程变量方法  
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel 期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
作者:  Liu YF(刘云峰);  Wang YP(汪运鹏);  Yuan CK(苑朝凯);  Luo ZT(罗长童);  Jiang ZL(姜宗林);  Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1080Kb)  |  收藏  |  浏览/下载:512/126  |  提交时间:2017/08/22
Aerodynamic Force And Moment Measurement  10° Half-angle Cone Model  Jf12  Real-gas Effects  Shock Tunnel  
振动激发对高超声速气动力/热影响 期刊论文
力学学报, 2017, 卷号: 49, 期号: 03, 页码: 616-626
作者:  张子健;  刘云峰;  姜宗林
Adobe PDF(711Kb)  |  收藏  |  浏览/下载:363/73  |  提交时间:2017/12/22
振动激发  气动力/热  边界层  高温气体效应  
Effect of peak perforation on flow past a conic cylinder at Re=100: drag lift and Strouhal number 期刊论文
CHINA OCEAN ENGINEERING, 2017, 卷号: 31, 期号: 3, 页码: 330-340
作者:  Lin LM(林黎明);  Zhong XF(钟兴福);  Wu YX(吴应湘)
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Vortex-induced Vibration  Perforation  Conic Disturbance  Drag  Lift  Strouhal Number