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SIMULATION: ANSYS WB - Modal Analysis of an Airfoil a Wing - Panel
SIMULATION: ANSYS WB - Modal Analysis of an Airfoil a Wing - Panel

Mesh

Open the Mesher

To open the mesher, double click . This will load ANSYS Mechanical. You should now be able to see the airfoil geometry.

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The first thing we are going to need to do when the mesher opens is specify the thickness of the airfoil walls. In the Outline window, expand Geometry and select Part 1. In the Details window, change the thickness to 0.01 m.

Mapped Face Meshing

To apply a mapped face meshing, first click on Mesh in the Outline window. This will bring up the Meshing Menu Bar at the top of the screen. Next, select Mesh Control > Mapped Face Meshing. Select the 2 faces of the mesh by holding down the left mouse button and dragging over the entire geometry. In the Details window, click Geometry > Apply - it should say 2 faces are selected.

Edge Sizing

In the Meshing Menu, click Meshing Control > Sizing. Click the edge selection filter . Select the 4 curved edges on the outside of the geometry that make up the shape of the NACA 0012 Airfoil as the picture shows:

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