Rewrote the formula necessary to compute the turboprop geometry, fuel consumption and maximum thrsut under the form of an OpenMDAO problem. The rationale behind it is that it seems to be quicker to solve it like this which would reduce the computation time of what is right the longest module in FAST-OAD_CS23. Now, what's left to do is implement the use of these components (whose validity were checked in another project) and optimize the implementation, using results caching or a smarter breakdown of the maps

The turboprop sizing has been tested and implemented as a nested problem whose setup is done only once and only when needed

As for the problem, the geometry parameter are computed only when needed

The 4 different problems that will help computing the max thrust at all altitudes have now been implement as was done for the sizing of the turboprop. Note that a problem for the case where propeller thrust is limiting has been added. Their use in the max_thrust function has not yet been implemented !

Reworked the max thrust function so that it uses the nested problem. The main assumption is that, if limits are reached, they are reached in this order : power, opr, itt, propeller thrust.
Also added a small cache to the max thrust function for cases like cruise where altitude and speed don't vary

The 2 different problems that will help computing the fuel consumed have now been implement as was done for the sizing of the turboprop. There is a problem with a linesearch algorithm that can be used but will not be favored if possible. There implementation in the sfc function have not yet been implemented

There some differences with the previous version of the code although it is in the order of magnitude of 1-2% for a significant gain in time

Max power is basically computed using the same problem as max thrust is. Except intead of extracting the thrust required we extract shaft power

Remove methods that were previously used and not necessary anymore

Implemented a test to check the stauration of the cache

Reworked the cnstruction of the sfc map for the turboprop and checked tested, only minor difference on predicted sfc with new map generation for a considerable speedup (7m to 30s). Now we will test and rework the reading of those maps. Btw `scipy.interpolate.interp2d` is gonna be deprecated so it was changed

Tested the turboprop map construction and read on the TBM900 sizing process. Minimal change on the fuel consumed. Also implemented more widely the use of LinearNDInterpolator to replace interp2d