Improvement of the mesh generation and control pt. 1

[GBenedett]

Objective:

• Change the power law to mesh the fluid domain
• Add the feature in CEASIOMpy GUI
• Scale the mesh proportionally to the size of the aircraft (farfield, wing and fuselage)
• Improved the sumo geometry generation
• Switch from cell size to cell factor proportional to aircraft dimensions
• Automatic Aeromap creation (if there isn't in CPACS file)
• Directional refinement or local (specific aircraft part) refinement

[codecov]

Codecov Report

Attention: 52 lines in your changes are missing coverage. Please review.

Comparison is base (0fdd6dc) 68.99% compared to head (cf7dce6) 69.47%.
Report is 5 commits behind head on main.

Files	Patch %	Lines
ceasiompy/CPACS2GMSH/func/mesh_sizing.py	88.37%	20 Missing ⚠️
ceasiompy/SU2Run/func/su2config.py	46.42%	15 Missing ⚠️
ceasiompy/CPACS2SUMO/cpacs2sumo.py	50.00%	10 Missing ⚠️
ceasiompy/SkinFriction/skinfriction.py	0.00%	3 Missing ⚠️
ceasiompy/ExportCSV/exportcsv.py	50.00%	2 Missing ⚠️
ceasiompy/SUMOAutoMesh/sumoautomesh.py	50.00%	2 Missing ⚠️

Additional details and impacted files

@@            Coverage Diff             @@
##             main     #280      +/-   ##
==========================================
+ Coverage   68.99%   69.47%   +0.47%     
==========================================
  Files          82       84       +2     
  Lines        7906     8148     +242     
==========================================
+ Hits         5455     5661     +206     
- Misses       2451     2487      +36     

Flag	Coverage Δ
integrationtests	54.61% <80.22%> (-1.37%)	⬇️
unittests	50.94% <72.10%> (+1.14%)	⬆️

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