*ARCHIVED* development moved to aircraft-studio.
no graph
main.py
@@ -75,7 +75,7 @@
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af.stringer.print_info(2)
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# Plot components with matplotlib
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Removed:
creator.plot(af, af.spar, af.stringer)
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Added:
# creator.plot(af, af.spar, af.stringer)
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# Save component info
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af.save_info(SAVE_PATH, _)
@@ -83,7 +83,7 @@
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af.stringer.save_info(SAVE_PATH, _)
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# Evaluate previously created airfoil(s).
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Removed:
total_mass = evaluator.get_total_mass(af, af.spar, af.stringer)
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Added:
# total_mass = evaluator.get_total_mass(af, af.spar, af.stringer)
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# Iteratively evaluate airfoils by defining genetic generations.
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# pass