Now the viscous solver is created after the interface. This allows less user inputs and avoids conflict between parameters. The blSolverInterface class was reworked and documentation was improved. The sections can now have no wake or only one side (for fuselage for example). Bug fix here and there and ajusted tests. Only the onera validation case is up to date.

The data structures of the viscous solver have been reworked to avoid lists of lists of lists... Users now have the possibility to automatically generate sections on wing or to use prescribed section from another mesh. First option requires to identified upper and lower sides and this information is also used by the rbf interpolator.

Removed the requirement of a transfinite surface mesh to generate viscous section. They are now generated by interpolation of the convex hull (wing) using scipy. This works best if we identify the upper and lower sides of the wing. 2 tests are given; NACA0012 airfoil in 2D with RBF interpolation and RAE2822 wing in 3D with rbf as well.  There might be a problem with parallel run of tests. Validation cases are not updated yet. Usage of LFS mesh is prevented on purpose so the 3D validation cases will fail.

Avoid modifying install path if the project is a submodule. In that case, installation is handled by the top project.

Avoid forcing installation location

Pipeline should fail

Changes are relative to adjoint and api modifications.

Following commit that removes VII from dartflo

Modified CMakeLists.txt files to find amfe in dartflo subdirectory and linked dart, tbox and fwk libs with blast through swig. Changed root run.py file to find amfe.

Switched to branch <paul> for dartflo submodule

Removed amfe and added dartflo as submodule