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Wind Turbine Blade FSI (Part 1)

Created using ANSYS 15.0 (also works in 14.5)

To access Part 2 of the tutorial, click here

Problem Specification

Overview

This tutorial considers the deformation due to aerodynamic loading of a wind turbine blade by performing a steady-state 1-way FSI (Fluid-Structure Interaction) analysis. Part 1 of the tutorial uses ANSYS Fluent to develop the aerodynamics loading on the blade. In part 2, the pressures on the wetted areas of the blade are passed as pressure loads to ANSYS Mechanical to determine stresses and deformations on the blade. 

 

The blade is 42.3 meters long and starts with a cylindrical shape at the root and then transitions to the airfoils S818, S825 and S826 for the root, body and tip, respectively. This blade also has pitch to vary as a function of radius, giving it a twist and the pitch angle at the blade tip is 4 degrees. This blade was created to be similar in size to a GE 1.5XLE turbine. For more information on the dimension characteristics of this blade, please see this M.Eng report (note that model in the present tutorial has an additional 2 meter cylindrical extension at the root to make it more realistic). 

The blade is made out of an orthotropic composite material, it has a varying thickness and it also has a spar inside the blade for structural rigidity. These specs, which are important for the FEA simulation, are described in  more details in Part 2 of the tutorial.

The turbulent wind is flows towards the negative z-direction (into the page on the above diagram) at 12 m/s which is a typical rated wind speed for a turbine this size. This incoming flow makes the blade rotate at an angular velocity of -2.22 rad/s about the z-axis (the blade is thus spinning clockwise when looking at it from the front, like most real wind turbines). The blade root is offset from the axis of rotation by 1 meter to make it more representative of an actual turbine where the blades would connect to the hub. Note that to represent the blade being connected to a hub, the blade root is offset from the axis of rotation by 1 meter.

 


Part 1

In this section of the tutorial, the blade geometry is imported, a mesh is created around the blade and the Fluent solver is then used to find the aerodynamics loading on the blade, the fluid streamlines and the torque generated. We will use air at standard conditions (15 degree celcius). Its density is 1.225 kg/m^3 and its viscosity is 1.7894e-05 kg/m*s.

Using periodicity, we will simulate the flow around one blade and extrapolate the solution to two more blades in order to visualize the results for a 3 blade rotor. Here's a sneak peak of a particular result that you will obtain at the end of this tutorial. The figure is showing a pressure contour plot on the back surface of the blades.

Are you ready? Let's go!

Go to Step 1: Pre-Analysis & Start-Up

Go to all FLUENT Learning Modules

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