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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：840/163  |  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  
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
作者:  Wang SZ(王士召);  He GW(何国威);  Zhang X(张星)
浏览  |  Adobe PDF(361Kb)  |  收藏  |  浏览/下载：408/110  |  提交时间：2014/04/02
Stretching  Stabilize  Flying  Leading  Collapse  Vortex  Oscillating  Stable  Slowing  Still  Simulate  Observed  Morphology  Around  Motion  Where  Taken  Method  Study  
Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
作者:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟)
浏览  |  Adobe PDF(199Kb)  |  收藏  |  浏览/下载：472/73  |  提交时间：2014/04/02
Vehicle  Leading  0algorithm  Genetic  Hypersonic  Optimization  Aerothermal  Based  Method  Design  Attack  Novel  Around  Angle  Evaluated  Greatly  About  Fluid  Result  Differ