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… analysis (few things are remaining)
using DVConstraints for computing the volume of the deformed wing instead of generating surface maesh in plot3d format for each volume evaluation
removed if condition for checking fail analysis when alpha is implicit since the runscript does that automatically now
added write solution options for solve cl function, using the dict returnred from solve CL for check cl convergence
now user can add LE, TE, and other FFD points separately. This enables to fix the LE and TE due to local FFD changes
added a feature so that user can mention whether to extract the lift distribution or not for wing module
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