Transonic Flow: RAE2822 Airfoil Using Overset Mesh

This tutorial demonstrates how to use an overset mesh to simulate transonic flow over the RAE2822 airfoil.

The physics models, initial, and boundary conditions are the same as in the Transonic Flow tutorial. By using an overset mesh for the region surrounding the airfoil, this tutorial shows how the angle of attack is changed without having to generate a mesh. This approach greatly simplifies the case setup for parametric studies.