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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
作者:  Qi DW;  He GW(何国威);  Liu YM
Adobe PDF(738Kb)  |  收藏  |  浏览/下载：845/166  |  提交时间：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  
Two-way coupling model for shock-induced laminar boundary-layer flows of a dusty gas 期刊论文
Acta Mechanica Sinica, 2005, 卷号: 21, 期号: 6, 页码: 557-563
作者:  Wang BY(王柏懿);  Xiong X;  Osiptsov AN;  Wang, BY (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
Adobe PDF(164Kb)  |  收藏  |  浏览/下载：700/143  |  提交时间：2009/08/03
Shock Wave  Dusty Gas  Two-phase Boundary Layer  Two-way Coupling  Numerical Modeling  Initial-stages  Lift Force  Particle  Waves  Air