There geo file for naca 0012 was updated by adding the growth ratio as input parameter instead of the farfield mesh size.

Boundary layer c++ objects are created in python with swig and are manipulated by the interface. The initial condition of the viscous solver was changed. All test cases have been adapted. A decrease in the number of iterations is globally observed. Results are slightly improved especially for the RAE validation case.

Added test case on the rae2822 3D finite wing thattests the 3D functionnalities of the code with vtk writing

Contains 2D and 3D developements as well as the api.