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Parametric Study of an Oscillating Airfoi in a Power-Extraction Regime

机译:动力提取系统中的摆动翼型的参数研究

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A wing that is heaving and pitching simultaneously may extract energy from an oncoming flow, thus acting as a turbine. The theoretical performance of such a concept is investigated here through unsteady two-dimensional laminar-flow simulations using the commercial finite volume computational fluid dynamics code FLUENT. Computations are performed in the heaving reference frame of the airfoil, thus leaving only the pitching motion of the airfoil to be dealt with through a rigid-body mesh rotation and a circular nonconformal sliding interface. Unsteady aerodynamics basics of the oscillating airfoil are first exposed, with a description of the operating regimes. Effects of unsteadiness are stressed and the inadequacy of a quasi-steady approach to take them into account is exposed. We present a mapping of power-extraction efficiency for a single oscillating airfoil in the frequency and pitching-amplitude domain: 0 < fc/U_∞ < 0.25 and 0 < θ_0 < 90deg for a NACA 0015 airfoil at a Reynolds number of Re = 1100,aheaving amplitude of one chord (H_0 = c), and a pitching axis at the third chord (x_p = c/3). Remarkably, efficiency as high as 34% is observed, as well as a large parametric region at θ_0 > 55 deg in which efficiencies are higher than 20%. Results from a parametric study are then provided and discussed. It is found that motion-related parameters such as heaving amplitude and frequency have the strongest effects on airfoil performances, whereas geometry and viscous parameters turn out to play a secondary role.
机译:同时起伏和俯仰的机翼可能会从迎面而来的气流中吸收能量,从而充当涡轮机。通过使用商业有限体积计算流体动力学代码FLUENT的非稳态二维层流模拟,在此研究了这种概念的理论性能。计算是在机翼的起伏参考系中进行的,因此仅剩下机翼的俯仰运动可通过刚体网格旋转和圆形不规则的滑动界面来处理。首先介绍了摆动翼型的不稳定空气动力学基础知识,并介绍了运行方式。强调了不稳定的影响,并暴露了将其纳入考虑的准稳定方法的不足。我们在频域和俯仰幅度域中给出了单个振荡机翼的功率提取效率的映射:对于Re = 1100的雷诺数的NACA 0015机翼,0 55度的大参数区域,其中效率高于20%。然后提供并讨论了参数研究的结果。发现与运动相关的参数(例如升幅和频率)对机翼性能的影响最大,而几何形状和粘性参数却起着次要作用。

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