水动力学研究与进展A辑
水動力學研究與進展A輯
수동역학연구여진전A집
Journal of Hydrodynamics
2015年
4期
460-465
,共6页
振动翼%能量采集%边界元%椭圆正弦函数
振動翼%能量採集%邊界元%橢圓正絃函數
진동익%능량채집%변계원%타원정현함수
oscillatory foil%energy harvesting%boundary element%elliptic sine function
振动翼作为一种有效的潮流能、风能换能装置,可将潮流或风的动能转化为机械动能推动电机发电。该文通过调整机翼的周期性垂向运动与旋转运动实现机翼与来流的有效攻角控制,来流对机翼的流体动升力可推动机械装置往复运动并转换为电机的转动。假定机翼表面的边界层极薄,黏性仅在边界层内部作用,泻出涡仅从机翼的尾缘处泻出,引入势流理论,采用边界元法与泻出涡模型模拟机翼边界层的外部流场。主要分析了机翼以椭圆正弦为有效攻角运动的振动运动的能量采集性能,计算NACA0012机翼在不同运动频率、振动幅值与有效攻角时的能量采集效率,并分析了椭圆正弦K 参数对能量采集的影响,研究实现高效率能量采集的机理。
振動翼作為一種有效的潮流能、風能換能裝置,可將潮流或風的動能轉化為機械動能推動電機髮電。該文通過調整機翼的週期性垂嚮運動與鏇轉運動實現機翼與來流的有效攻角控製,來流對機翼的流體動升力可推動機械裝置往複運動併轉換為電機的轉動。假定機翼錶麵的邊界層極薄,黏性僅在邊界層內部作用,瀉齣渦僅從機翼的尾緣處瀉齣,引入勢流理論,採用邊界元法與瀉齣渦模型模擬機翼邊界層的外部流場。主要分析瞭機翼以橢圓正絃為有效攻角運動的振動運動的能量採集性能,計算NACA0012機翼在不同運動頻率、振動幅值與有效攻角時的能量採集效率,併分析瞭橢圓正絃K 參數對能量採集的影響,研究實現高效率能量採集的機理。
진동익작위일충유효적조류능、풍능환능장치,가장조류혹풍적동능전화위궤계동능추동전궤발전。해문통과조정궤익적주기성수향운동여선전운동실현궤익여래류적유효공각공제,래류대궤익적류체동승력가추동궤계장치왕복운동병전환위전궤적전동。가정궤익표면적변계층겁박,점성부재변계층내부작용,사출와부종궤익적미연처사출,인입세류이론,채용변계원법여사출와모형모의궤익변계층적외부류장。주요분석료궤익이타원정현위유효공각운동적진동운동적능량채집성능,계산NACA0012궤익재불동운동빈솔、진동폭치여유효공각시적능량채집효솔,병분석료타원정현K 삼수대능량채집적영향,연구실현고효솔능량채집적궤리。
Oscillatory foil is an effective energy harvesting device to extract energy from incoming flow, including current and wind. By adjusting the periodical vertical and rotational motion, the effective attack angle can be controlled;and the fluid loads can be utilized to drive the reciprocating motion of mechanical device. Assuming that the boundary layer is thin and the viscosity only has effects within the layer, the velocity potential is introduced to simulate the outer fluid flow through boundary element method and vortex shedding scheme. The energy harvesting performance of NACA0012 foil in oscillatory motion, where the effective attack angle is elliptic sine function, is analyzed. The energy extraction efficiency at various heave amplitude, the effective attack angle and Strouhal number is calculated, the effects of K parameter on the energy efficiency have been analyzed;the mechanics to achieve high efficiency is investigated.