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Space-Time VMS Computation of Wind-Turbine Rotor and Tower Aerodynamics.

机译:风力涡轮机转子和塔架空气动力学的时空VMS计算。

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摘要

This thesis is on the space{time variational multiscale (ST-VMS) computation of wind-turbine rotor and tower aerodynamics. The rotor geometry is that of the NREL 5MW offshore baseline wind turbine. We compute with a given wind speed and a specified rotor speed. The computation is challenging because of the large Reynolds numbers and rotating turbulent ows, and computing the correct torque requires an accurate and meticulous numerical approach. The presence of the tower increases the computational challenge because of the fast, rotational relative motion between the rotor and tower. The ST-VMS method is the residual-based VMS version of the Deforming-Spatial-Domain/Stabilized ST (DSD/SST) method, and is also called "DSD/SST-VMST" method (i.e., the version with the VMS turbulence model). In calculating the stabilization parameters embedded in the method, we are using a new element length definition for the diffusion-dominated limit. The DSD/SST method, which was introduced as a general-purpose moving-mesh method for computation of ows with moving interfaces, requires a mesh update method. Mesh update typically consists of moving the mesh for as long as possible and remeshing as needed. In the computations reported here, NURBS basis functions are used for the temporal representation of the rotor motion, enabling us to represent the circular paths associated with that motion exactly and specify a constant angular velocity corresponding to the invariant speeds along those paths. In addition, temporal NURBS basis functions are used in representation of the motion and deformation of the volume meshes computed and also in remeshing. We name this "ST/NURBS Mesh Update Method (STNMUM)." The STNMUM increases computational efficiency in terms of computer time and storage, and computational exibility in terms of being able to change the time-step size of the computation. We use layers of thin elements near the blade surfaces, which undergo rigid-body motion with the rotor. We compare the results from computations with and without tower, and we also compare using NURBS and linear finite element basis functions in temporal representation of the mesh motion.
机译:本文主要研究风轮机转子和塔架空气动力学的时空多尺度(ST-VMS)计算。转子的几何形状是NREL 5MW海上基准风力涡轮机的几何形状。我们以给定的风速和指定的转子速度进行计算。由于大的雷诺数和旋转的湍流,因此计算具有挑战性,并且计算正确的扭矩需要精确而细致的数值方法。由于转子和塔架之间的快速旋转相对运动,塔架的存在增加了计算难度。 ST-VMS方法是“变形空间域/稳定ST(DSD / SST)”方法的基于残差的VMS版本,也称为“ DSD / SST-VMST”方法(即具有VMS湍流的版本)模型)。在计算方法中嵌入的稳定参数时,我们使用新的元素长度定义作为扩散主导的极限。 DSD / SST方法是一种通用的移动网格方法,用于计算带有移动接口的流,它需要一种网格更新方法。网格更新通常包括尽可能长时间地移动网格并根据需要重新网格化。在此处报告的计算中,NURBS基函数用于转子运动的时间表示,使我们能够精确地表示与该运动相关的圆形路径,并指定与沿这些路径的不变速度相对应的恒定角速度。此外,时间NURBS基函数用于表示所计算的体积网格的运动和变形以及重新网格化。我们将其命名为“ ST / NURBS网格更新方法(STNMUM)”。 STNMUM在计算机时间和存储方面提高了计算效率,在能够更改计算的时间步长方面提高了计算的灵活性。我们在叶片表面附近使用薄元件层,该薄层元件随转子而发生刚体运动。我们比较了有塔和无塔的计算结果,并在网格运动的时间表示中使用了NURBS和线性有限元基础函数进行了比较。

著录项

  • 作者

    McIntyre, Spenser W.;

  • 作者单位

    Rice University.;

  • 授予单位 Rice University.;
  • 学科 Engineering Mechanical.;Engineering Aerospace.
  • 学位 M.S.
  • 年度 2013
  • 页码 78 p.
  • 总页数 78
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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