基于谐波法的高流入湍流和尾迹风力机气动分析

S. W. Naung, M. Rahmati, H. Farokhi
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引用次数: 8

摘要

本文采用计算流体力学(CFD)方法对某型水平轴风力机进行了气动仿真分析。选择墨西哥(受控条件下模型转子实验)实验风力机进行仿真,因为实验数据可以用于验证所使用的CFD模型。CFD方法已被许多研究用来预测风力机的气动特性。然而,大多数研究都认为入口处有稳定的气流。有时,当气流不稳定或附近有其他风力涡轮机时,情况就不是这样了。本文首先在不考虑进气道尾迹的情况下,采用不同的湍流模型进行了定常模拟。然后在进气道处产生谐波尾迹,进行非定常CFD模拟。非定常CFD模拟通常需要较长的运行时间,因此本研究采用谐波(频域)法进行非定常计算,谐波(频域)法是一种研究非定常周期流动的高效计算方法,其计算代价以定常解为阶。本文首先讨论了有和无谐波尾迹时进气道压力系数的分布,并与实验结果进行了比较。在此基础上,从子午和叶片间两种角度对非定常谐波尾迹作用下的叶片绕流进行了详细分析。其次,简要讨论了压力分布对叶片结构的影响。最后根据气动分析结果以及气动载荷对叶片结构的影响进行了总结。
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Aerodynamic Analysis of a Wind Turbine With Elevated Inflow Turbulence and Wake Using Harmonic Method
This paper presents aerodynamic simulation and analysis of a horizontal axis wind turbine using Computational Fluid Dynamics (CFD) method. The MEXICO (Model Rotor Experiments In Controlled Conditions) Experiment wind turbine is selected for simulation as the experimental data are available and can be used for validation of the CFD model used. CFD method has been used by a number of studies to predict aerodynamic behaviour of wind turbines. However, the majority of studies consider a steady wind flow at the inlet. Sometimes this is not the case when the wind flow is not steady or there are other wind turbines nearby. In this paper, the steady simulations are first conducted using different turbulence models without considering inflow wake at the inlet. Afterwards, a harmonic wake is generated at the inlet and unsteady CFD simulation is performed. Unsteady CFD simulation usually requires long runtime and therefore harmonic (frequency domain) method, which is an efficient computational method to study unsteady periodic flow at a computational cost in the order of steady-state solutions, is used for unsteady computation in this study. This paper first discusses the pressure coefficient distributions with and without harmonic wake at the inlet and compares them against the experiment. Afterwards the detailed analysis of flow around the blade subject to the unsteady harmonic wake is conducted in the meridional view and the blade-to-blade view. Next, the effect of pressure distribution on the blade structure is briefly discussed. Finally this paper concludes based on the results from the aerodynamic analysis as well as the analysis of the effect of aerodynamic loads on the blade structure.
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