This page is under construction. Check back for updates. For now, please download the file below to continue working on this simulation
Skip Creating the Geometry and Meshing
If you wish to skip creating the geometry and mesh, then you can download the meshed geometry here shortly. Download the compressed folder, then extract the files to your working directory. If you download the geometry you may skip steps 2 and 3 of this tutorial.
Geometry
Download the Airfoil Coordinates
In this step, we will import the coordinates of the airfoil and create the geometry we will use for the simulation. Begin by downloading this file here and saving it somewhere convenient. This file contains the points of a NACA 0012 airfoil.
Launch Design Modeler
Before we launch the design modeler, we need to specify the problem as a 2D problem. Right click Properties. In the Properties of Schematic A2: Geometry Window, select Analysis Type > 2D. Now, double click to launch the Design Modeler. When prompted, select Meters as the unit of measurement.
and selectAirfoil
First, we will create the geometry of the airfoil. In the menu bar, go to Concept > 3D Curve. In the Details View window, click Geometry File and select the ellipsis to browse to a file. Browse to and select the geometry file you downloaded earlier. Once you have selected the desired geometry file, click to create the curve. Click to get a better look at the curve.
Next, we need to create a surface from the curve we just generated. Go to Concepts > Surfaces from Edges. Click anywhere on the curve you just created, and select Edges > Apply in the Details View Window. Click to create the surface.
Create C-Mesh
Now that the airfoil has been generated, we need to create the meshable surface we will use once we begin to specify boundary conditions. We will begin by creating a coordinate system at the tail of the airfoil - this will help us create the geometry for the C-mesh. Click Type > From Coordinates. For FD11, Point X, enter 1
.
Click Plane 4), then click