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Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner 期刊论文
COMPUTERS & FLUIDS, 2020, 卷号: 198, 页码: 18
Authors:  Tong FL(童福林);  Li XL(李新亮);  Yuan XX;  Yu ZP(于长平)
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Shock wave  Turbulent boundary layer  Unsteadiness  Expansion corner  
超声速膨胀角入射激波/湍流边界层干扰直接数值模拟 期刊论文
航空学报, 2020, 卷号: 41, 期号: 3, 页码: 123328
Authors:  童福林;  孙东;  袁先旭;  李新亮
Favorite  |  View/Download:36/0  |  Submit date:2020/06/01
超声速膨胀角入射激波/湍流边界层干扰直接数值模拟研究 期刊论文
航空学报, 2019, 页码: 21
Authors:  童福林;  孙东;  袁先旭;  李新亮
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激波/湍流边界层干扰  膨胀角  本征正交分解  直接数值模拟  
Heterogeneous lamella structure unites ultrafine-grain strength with coarse-grain ductility 期刊论文
PROCEEDINGS OF THE NATIONAL ACADEMY OF SCIENCES OF THE UNITED STATES OF AMERICA, 2015, 卷号: 112, 期号: 47, 页码: 14501-14505
Authors:  Wu XL(武晓雷);  Yang MX;  Yuan FP(袁福平);  Wu GL;  Wei YJ(魏宇杰);  Huang XX;  Zhu YT;  Wu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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Back-stress Hardening  Heterogeneous Lamella Structure  Ductility  Strength  Strain Partitioning  
Behavior of interface crack in layered structure under actions of both stress wave and residual stress 会议论文
13th International Conference on Fracture(ICF13), 中国北京, 2013-06-16
Authors:  Wu CW(吴臣武);  Cheng XX(程欣欣);  Yuan YC(袁雨辰)
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Layered  Initially  Singularity  Stressed  Relaxation  Thereby  
高速列车通风设计方法的研究 期刊论文
北京航空航天大学学报, 2000, 卷号: 26, 期号: 1, 页码: 52
Authors:  庄达民;  林国华;  袁修干;  王晓新
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通风  射流  数值计算  高速列车