This tutorial has two parts. The first part will analyze the flow using Moving Frame of Reference, while the second part will use the Sliding Mesh feature.
To access Part 1 of the tutorial, click here.
The setup for this part 2 of the tutorial has mostly been done during part 1. So it's highly recommended that you go through the first part, as we will start from the same project file.
In this tutorial, you will learn to:
Consider a uniform flow of V = 10m/s passing through a Vertical Axis Wind Turbine (VAWT) as sketched above. The VAWT has a diameter of 12cm and 3 equally spaced blades, each one with a chord length of 2cm. For simplification, consider that it spins with a constant angular velocity of 40 RPM*. The center of each blade is located 0.04m from the center of the hub.
Note that this is a Darrieus VAWT, which is lift based, in contrast to the Savonius VAWT, which is drag based. This is an intensive field of research, and at Cornell we have the Fluid Dynamics Research Laboratory, directed by Prof. Charles Williamson. In the last section we will compare results with the experimental data obtain by the lab.
* Note that this is an important simplification. Here we're considering that the turbine is already spinning independently of the flow, what is clearly not true, since the flow is responsible for spinning the turbine. There is only one stable combination of incoming flow velocity and RPM, given the geometry and mass of the turbine. However, modeling the movement of a geometry caused by the flow is considerably difficult, and requires the use of a method called "6DOF solver." A tutorial on that is intended to be made in the future. For now, let's stick to a simpler analysis, first a steady-state picture of the problem (part 1 of this tutorial), and later a transient analysis (this tutorial).