Supersonic flow around wing

Developers, developers, developers!

So for my master thesis I’m trying to simulate supersonic flow around 3d wing. I already have some results from supersonic panel method and finite difference method from Fluent.
I would also like to use FR method and compare results.
Now the question is, do you have maybe an example on how to use PyFR for 3D case? And if so can you share it?

Regards