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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
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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  
Spanwise stretching and collapse motions stabilize leading-edge vortex in slow-flying bats 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:  Wang SZ(王士召);  He GW(何国威);  Zhang X(张星)
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Stretching  Stabilize  Flying  Leading  Collapse  Vortex  Oscillating  Stable  Slowing  Still  Simulate  Observed  Morphology  Around  Motion  Where  Taken  Method  Study  
Investigation of traveling wave in vortex-induced vibrations of long flexible cylinders 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:  Wu XD(武晓东);  Ge F(葛斐);  Hong YS(洪友士)
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Flexible  Cylinders  0traveling  Vortex  Induced  Fitting  Standing  Vibration  Ident  Overall  Transform  Distribution  Individual  Method  Values  Ratio  Hilbert  Based  Worked  Engineering  
Intrinsic lengths govern failure mode transition in metallic glasses 会议论文
ICTAM, 北京, 2012-8
Authors:  Dai LH(戴兰宏);  Chen Y(陈艳)
Adobe PDF(691Kb)  |  Favorite  |  View/Download：1823/1241  |  Submit date：2013/03/01