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Numerical analysis on transitions and symmetry-breaking in the wake of a flapping foil 期刊论文
Acta Mechanica Sinica, 2012, 卷号: 28, 期号: 6, 页码: 1551-1556
Authors:  He GY;  Wang Q;  Zhang X(张星);  Zhang SG;  Zhang X(张星);  LNM, Institute of Mechanics,Chinese Academy of Sciences,100190 Beijing, China
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Flapping Motion  Immersed Boundary Method  Wake  Symmetry-breaking  
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:862/170  |  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  
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:1813/1236  |  Submit date:2013/03/01