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Ground effect on the power extraction performance of a flapping wing biomimetic energy generator

机译:地面效应对襟翼仿生能量发生器功率提取性能的影响

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In this study the ground effect on the power extraction by a flapping wing based biomimetic energy generator was numerically investigated. The use of flapping wings, which derives inspiration from the study of biomimetics, has been considered as an alternative approach to developing an energy generation system that is completely different from the traditional turbine-based power generation unit. A NACA0015 airfoil, which is commonly used to model the wing cross-section, was placed in a two-dimensional laminar flow system and imposed with a harmonic plunge and pitch rotary motion. To carry out numerical simulations, the immersed boundary-lattice Boltzmann method was employed. At a Reynolds number of 1100 and with the position of the airfoil pitching axis at one third of the chord length from the leading edge, the influence of the clearance between the airfoil pitching axis and the ground (c <= h(0) <= 5c, c is the chord length of the airfoil), the amplitude (h(m)=0.5c and c, alpha(n) = 10 degrees and 20 degrees) and frequency (0.05 <= St <= 0.5) of motion on the force behavior and power extraction were systematically evaluated. Compared to the situation in which there was no ground effect, the airfoil placed in close proximity to the ground gave improved power extraction performance. For given amplitude, as the clearance decreased the power extraction efficiency improved. The maximum efficiency improved by 28.6%. Moreover, it was found that the contribution to efficiency improvement was essentially from the increased plunging component of the power extraction, resulting from the generation of high lift force, rather than that of pitching. (C) 2014 Elsevier Ltd. All rights reserved.
机译:在本研究中,数值研究了基于襟翼的仿生能量发生器对地面功率提取的影响。襟翼的使用是仿生学研究的灵感,已被认为是开发与传统涡轮机发电装置完全不同的能源发电系统的替代方法。将通常用于机翼横截面建模的NACA0015机翼放置在二维层流系统中,并施加谐波骤降和俯仰旋转运动。为了进行数值模拟,采用了浸入边界格子Boltzmann方法。雷诺数为1100且机翼俯仰轴的位置位于距前缘的弦长的三分之一处时,机翼俯仰轴与地面之间的间隙的影响(c <= h(0)<=在图5c中,c是翼型的弦长),振幅(h(m)= 0.5c和c,alpha(n)= 10度和20度)和频率(0.05 <= St <= 0.5)系统评估了受力行为和功率提取。与没有地面影响的情况相比,靠近地面放置的机翼提高了功率提取性能。对于给定的幅度,随着间隙减小,功率提取效率提高。最大效率提高了28.6%。此外,已经发现,对效率提高的贡献主要来自功率提取的下降分量的增加,这是由产生高升力而不是俯仰产生的。 (C)2014 Elsevier Ltd.保留所有权利。

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