Fast-oad-cs25

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Fixed:

- Fixed tail geometry (**Warning**: slight but noticeable changes in tail CG, hence in overall data). (45)

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Added:

- Compatibility with Python 3.11. (43)

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Changed:

- More control on calculation of load factors. (38)
- Update on geometry of tail planes (36)

Fixed:

- Restored the default solver behaviors of v0.4 for models with inner loop. (39)

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Changed:

- Allowing deactivation of inner solvers. (33)
- Having ISA temperature offset as input of engine deck. (31)

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Changed:

- FAST-OAD-CS25 is now officially compatible with Python 3.10. Support of Python 3.7 has been abandoned. (26)
- Trailing edge of wing inner part can now have a non-zero sweep angle.(27)
- Now the criteria for computation of wing can be controlled through options. (29)
- Computation of wing geometry now uses sub-models and has now an option for (de)activating the computation of wing thickness. (29)

Fixed:

- Fixed component for computing global positions of wing chords, which is now a sub-model of geometry module (28)

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Changed:

- OpenMDAO 3.18+ is now required. (18)
- Submodels have been introduced in module "fastoad.loop.wing_area". (7)
- Load factors are now explicitly in output data. (23)

Fixed:

- Unit of variable "data:weight:aircraft:additional_fuel_capacity" has been corrected to "kg". (18)
- Unit of "*:CL_alpha" variables is now consistently "1/rad". (21)
- Unit for "data:load_case:lc2:Vc_EAS" has been corrected to "m/s". (23)