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Numerical Simulation of Tower Rotor Interaction for Downwind Wind Turbine

机译:顺风风力发电机塔转子相互作用的数值模拟

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Downwind wind turbines have lower upwind rotor misalignment, and thus lower turning moment and self-steered advantage over the upwind configuration. In this paper, numerical simulation to the downwind turbine is conducted to investigate the interaction between the tower and the blade during the intrinsic passage of the rotor in the wake of the tower. The moving rotor has been accounted for via ALE formulation of the incompressible, unsteady, turbulent Navier-Stokes equations. The localized Ci>, C;,, and C_D are computed and compared to undisturbed flow evaluated by Panel method. The time history of the Cp, aerodynamic forces (C_L and C_D), as well as moments were evaluated for three cross-sectional tower; asymmetrical airfoil (NACA0012) having four times the rotor's chord length, and two circular cross-sections having four and two chords lengths of the rotor's chord. 5%, 17%, and 57% reductions of the aerodynamic lift forces during the blade passage in the wake of the symmetrical airfoil tower, small circular cross-section tower and large circular cross-section tower were observed, respectively. The pronounced reduction, however, is confined to a short time/distance of three rotor chords. A net forward impulsive force is also observed on the tower due to the high speed rotor motion.
机译:顺风风力涡轮机具有较低的逆风转子偏心度,因此与逆风结构相比具有较低的转弯力矩和自转向优势。在本文中,对下风轮机进行了数值模拟,以研究在塔机尾部转子固有通过过程中塔机与叶片之间的相互作用。通过不可压缩,不稳定,湍流的Navier-Stokes方程的ALE公式解决了运动转子的问题。计算局部的Ci>,C;和C_D并将其与通过Panel方法评估的未扰动流进行比较。对三个横截面塔的Cp的时间历程,空气动力(C_L和C_D)以及弯矩进行了评估。非对称翼型(NACA0012),其翼弦长是其四倍,而两个圆形截面的翼弦长分别为四和二。在对称翼型塔,小型圆形截面塔和大型圆形截面塔之后,叶片通过过程中的气动升力分别降低了5%,17%和57%。然而,明显的减小仅限于三个转子弦的短时间/距离。由于高速转子的运动,在塔架上也观察到净向前冲力。

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