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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：841/164  |  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  
A micro diffuser/nozzle pump with fins on the sidewall 会议论文
4th International Conference on Solid-State Sensors, Actuators and Microsystems, TRANSDUCERS and EUROSENSORS '07, Lyon, France, June 10, 2007 - June 14, 2007
作者:  Li XH;  Yu XM;  Zhang DC;  Li ZH;  Xu WH
浏览  |  Adobe PDF(402Kb)  |  收藏  |  浏览/下载：148/55  |  提交时间：2017/06/01
Diffuser/nozzle  Diffuser/nozzle Pump  Fins  Flow Efficiency  International Conferences  Key Parts  Novel Methods  Pump Performance  Silicon Micro-machining  Solid-state Sensors