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Numerical simulation of 30p30n multi-element airfoil using delayed detached-eddy simulation 会议论文
AIAA AVIATION 2020 FORUM, 15 June 2020 through 19 June 2020
Authors:  Jin Y;  廖飞, Cai JS
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Investigation of high-order cell-centered finite difference method for aeroacoustics 会议论文
25th AIAA/CEAS Aeroacoustics Conference, 2019, Delft, Netherlands, May 20, 2019 - May 23, 2019
Authors:  Jin Y;  Liao F(廖飞);  Cai JS;  Morris PJ
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Uncertainties in pressurized thermal shock analyses 会议论文
ASME 2019 Pressure Vessels and Piping Conference, PVP 2019, San Antonio, TX, United states, July 14, 2019 - July 19, 2019
Authors:  Niffenegger M;  Garrido OC;  Mora DF;  Qian GA(钱桂安);  Mukin R;  Sharabi M;  Lafferty N;  Niceno B
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Computational fluid dynamics  Finite element method  Pressurized thermal shock  Probabilistic fracture mechanics  Warm pre-stressing  
CONSTRAINT ASSESSMENT FOR CRUCIFORM SPECIMENS WITH A SEMI ELLIPTICAL CRACK 会议论文
ASME Pressure Vessels and Piping Conference (PVP 2018), Prague, CZECH REPUBLIC, JUL 15-20, 2018
Authors:  Cao YP.;  Qian GA(钱桂安);  He YB.;  Chao YJ.
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A Finite Element Model of 18650 Lithium-Ion Battery for Explosion Caused by Internal Short Circuit 会议论文
35th ASME International Conference on Ocean, Offshore and Arctic Engineering, Busan, SOUTH KOREA, JUN 19-24, 2016
Authors:  Wang LB;  Liu BH;  Xu J;  Wang, LB (reprint author), Beihang Univ, Dept Automot Engn, Sch Transportat Sci & Engn, Beijing 100191, Peoples R China.;  Wang, LB (reprint author), Beihang Univ, AVRC, Beijing 100191, Peoples R China.
View  |  Adobe PDF(2388Kb)  |  Favorite  |  View/Download：396/139  |  Submit date：2017/05/12
Cell  Behavior  Fracture  
A numerical study on responses of submerged floating structures undergoing vortex-induced vibration and seismic excitation 会议论文
2nd International Symposium on Submerged Floating Tunnels and Underwater Tunnel Structures (SUFTUS), Chongqing, PEOPLES R CHINA, DEC, 2016
Authors:  Kang L(康凌);  Ge F(葛斐);  Wu XD(武晓东);  Hong YS(洪友士);  Ge, F (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1245Kb)  |  Favorite  |  View/Download：266/70  |  Submit date：2017/05/12
Fluid-structure Interaction  Nonlinearity  Tether Spacing  Tunnel Prototype  China  
Faceted crack initiation characteristics for high-cycle and very-high-cycle fatigue of a titanium alloy under different stress ratios 会议论文
5th International Conference on Crack Paths (CP), Ferrara, ITALY, SEP, 2015
Authors:  Liu XL(刘小龙);  Sun CQ(孙成奇);  Hong YS(洪友士);  Hong, YS (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
View  |  Adobe PDF(2579Kb)  |  Favorite  |  View/Download：395/79  |  Submit date：2017/05/12
Ti-6al-4v Alloy  Faceted Crack Initiation  Very-high-cycle Fatigue  Stress Ratio  Cluster Of Primary Alpha Grains  Competing Failure Modes  Poisson Defect Statistics  Ti-6al-4v Alloy  Structural-materials  Mean Stress  Strength  Microstructure  Behavior  Duality  Surface  
On bifurcation of homogenous deformation in metallic glasses 会议论文
13th International Conference on Fracture 2013, ICF 2013, Beijing, China, June 16, 2013 - June 21, 2013
Authors:  Chen Y(陈艳);  Dai LH(戴兰宏)
View  |  Adobe PDF(273Kb)  |  Favorite  |  View/Download：232/66  |  Submit date：2018/11/08
Bifurcation (mathematics)  Continuum mechanics  Elasticity  Fracture  Glass  Glass transition  Metallic glass  Nanotechnology  Shear bands  Bifurcation condition  Bifurcation theory  Deformation localization  Homogeneous deformation  Inelastic deformation  Loss of ellipticity  Pressure sensitivities  Structural evolution  
Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300 会议论文
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012
Authors:  Qi DW;  He GW(何国威);  Liu YM
Adobe PDF(738Kb)  |  Favorite  |  View/Download：860/169  |  Submit date：2013/02/26
Aerospace Engineering  Deformation  Exhibitions  Flexible Wings  Reynolds Number  Rigidity  Vortex Flow  Aerodynamic Forces  Chord-based Reynolds Number  Flexural Rigidities  Free Stream  Free-stream Flow  Lattice Boltzmann  Leading-edge Vortices  Lift Coefficient  Lift Force  Particle Methods  Pitch Rate  Power Efficiency  Reduced Frequency  Three Dimensional Space  Time-periods  Tip Edge  Trailing Edges  Trailing Vortex  
Size effect of failure modes in composite laminates under compression 会议论文
28th Congress of the International Council of the Aeronautical Sciences 2012 (ICAS 2012), Brisbane, Australia, SEP 23-28, 2012
Authors:  Wang B;  Xu F;  Wei YJ(魏宇杰);  Wang B.
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