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Numerical Study of A Flapping Flat Plate For Power Extraction

机译:拍打式拍打平板的数值研究

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摘要

Flapping-foils offer an alternative to rotary turbines in generating power from fluid flows. This thesis examined the flapping-foil concept using numerical simulations with the aim of improving performance, by considering streamlined foils and a flat plate of different leading and trailing edge configurations, control of the effective angle of attack, and optimum kinematic parameter values in laminar and turbulent flows. The flat plate, anticipated to be cheaper and easier to manufacture, has been found to generate higher power compared to streamlined foils using sinusoidal plunge and pitch motions. This is largely a result of (i) the ability of a flat plate to harvest the energy of LEVs, by the uniform thickness along its chord length. Investigation into the active control of the effective angle of attack is implemented with sinusoidal plunge motion, with the pitch motion adjusted to achieve the desired effective angle of attack profile. A square wave effective angle of attack profile is found to be superior for a flat plate with the maximum effective angle of attack 21⁰ or less. This is a result of the reduction in the pitch rate and the increase in moment acting in the same direction as the pitch motion during the stroke reversals. A cosine variation is best for maximum effective angle of attack of at least 46⁰ because the moment of the flat plate nearer the end of the pitch-reversal-stroke and into the beginning of a new pitch stroke opposes the moment for the pitch motion, as the cosine profile moves towards a square wave profile. Optimisation of five kinematic parameters of a flat plate flapping-foil turbine is performed with a “multi-fidelity” evolutionary algorithm for a single objective function. The multi-fidelity algorithm is found to be good in predicting near optimum solutions with reduced overall computational cost compared to single fidelity algorithms. However, in the search for optimum solutions of power generation and efficiency and the values of five kinematic parameters, the surrogates did not predict the optimum solutions and five kinematic parameter values accurately as result of a non-linear relationship between the five kinematic parameters and each objective function.
机译:拍打箔为旋转涡轮提供了一种替代方案,可以从流体流中产生动力。本文通过数值模拟研究了拍打箔的概念,旨在通过考虑流线型箔片和具有不同前缘和后缘构型的平板,控制有效攻角以及在层流中优化运动学参数值来提高翼片的性能。湍流。与使用正弦波切入和俯仰运动的流线型箔片相比,预计将更便宜,更易于制造的平板可产生更高的功率。这主要是由于(i)平板沿弦长均匀的厚度来收集LEV能量的能力。对正攻角的主动控制的研究是通过正弦突降运动进行的,调整俯仰运动以获得所需的正攻角曲线。发现对于最大有效迎角为21°或更小的平板来说,方波有效迎角轮廓更好。这是由于在冲程反转期间俯仰率降低和作用在与俯仰运动相同的方向上的力矩增加的结果。余弦变化最有利于最大有效攻角至少为46°,因为平板靠近俯仰反转冲程末端并进入新的俯仰冲程开始的时刻与俯仰运动的时刻相反,因为余弦轮廓向方波轮廓移动。利用“多保真”进化算法对单个目标函数执行了平板拍打叶轮机的五个运动学参数的优化。与单保真度算法相比,发现多保真度算法可以更好地预测接近最优的解决方案,同时降低总体计算成本。但是,在寻找发电和效率的最佳解以及五个运动学参数值时,由于五个运动学参数与每个运动学参数之间存在非线性关系,因此代理人无法准确预测最优解和五个运动学参数值。目标函数。

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