The very first step in the simulation of ice accretion on a wind turbine blade is the accurate prediction of the flow field around\r\nit and the performance of the turbine rotor. The paper addresses this prediction using RANS equations with a proper turbulence\r\nmodel. The numerical computation is performed using a commercial CFD code, and the results are validated using experimental\r\ndata for the 3D flow field around the NREL Phase VI HAWT rotor. For the flow simulation, a rotating reference frame method,\r\nwhich calculates the flow properties as time-averaged quantities, has been used to reduce the time spent on the analysis. A basic\r\ngrid convergence study is carried out to select the adequate mesh size. The two-equation turbulence models available in ANSYS\r\nFLUENT are compared for a 7 m/s wind speed, and the one that best represents the flow features is then used to determine\r\nmoments on the turbine rotor at five wind speeds (7 m/s, 10 m/s, 15 m/s, 20 m/s, and 25 m/s). The results are validated against\r\nexperimental data, in terms of shaft torque, bending moment, and pressure coefficients at certain spanwise locations. Streamlines\r\nover the cross-sectional airfoils have also been provided for the stall speed to illustrate the separation locations. In general, results\r\nhave shown good agreement with the experimental data for prestall speeds.
Loading....