Looking at the Pressure and Mach Number Distribution

Summary of the above video:

1. Change Units in CFD Post
2. Edit → Options → Units → English Engineering
3. Create Pressure Coefficient Contours on the wing surface
4. Reflect across symmetry plane
5. Create Pressure Coefficient Contours on the symmetry plane
6. Disable contour bands
7. Create Mach Number Contours on the wing surface