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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
Adobe PDF(738Kb)  |  Favorite  |  View/Download：869/173  |  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  
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)
View  |  Adobe PDF(361Kb)  |  Favorite  |  View/Download：434/119  |  Submit date：2014/04/02
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