Space-time VMS computation of wind-turbine rotor and tower aerodynamics

被引:108
作者
Takizawa, Kenji [1 ,2 ]
Tezduyar, Tayfun E. [3 ]
McIntyre, Spenser [3 ]
Kostov, Nikolay [3 ]
Kolesar, Ryan [3 ]
Habluetzel, Casey [3 ]
机构
[1] Waseda Univ, Dept Modern Mech Engn, Shinjuku Ku, Tokyo 1698050, Japan
[2] Waseda Univ, Waseda Inst Adv Study, Shinjuku Ku, Tokyo 1698050, Japan
[3] Rice Univ, Houston, TX 77005 USA
关键词
Space-time VMS method; DSD/SST-VMST; Wind-turbine rotor and tower aerodynamics; Mesh motion; Remeshing; Temporal NURBS functions; ST/NURBS Mesh Update Method; STNMUM; FLUID-STRUCTURE-INTERACTION; FINITE-ELEMENT COMPUTATIONS; SLIP MESH UPDATE; MOVING BOUNDARIES; STABILIZATION PARAMETERS; FLOW PROBLEMS; ISOGEOMETRIC ANALYSIS; 3D SIMULATION; FORMULATIONS; INTERFACES;
D O I
10.1007/s00466-013-0888-x
中图分类号
O1 [数学];
学科分类号
0701 ; 070101 ;
摘要
We present 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 flows, 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 flows 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 flexibility 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.
引用
收藏
页码:1 / 15
页数:15
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