*ARCHIVED* development moved to aircraft-studio.
typos
Changed files
example_airfoil.py
@@ -44,7 +44,7 @@
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af = creator.Airfoil.from_dimensions(CHORD_LENGTH, SEMI_SPAN)
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af.add_naca(NACA_NUM)
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af.add_mass(AIRFOIL_MASS)
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Removed:
# af.info_print(2)
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af.info_print(2)
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af.info_save(SAVE_PATH, 'foo_name')
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# Create spar instance
@@ -56,7 +56,7 @@
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af.spar.add_spar_caps(SPAR_CAP_AREA)
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af.spar.add_mass(SPAR_MASS)
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af.spar.add_webs(SPAR_THICKNESS)
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Removed:
# af.spar.info_print(2)
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af.spar.info_print(2)
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af.spar.info_save(SAVE_PATH, 'foo_name')
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# Create stringer instance
@@ -70,7 +70,7 @@
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af.stringer.add_area(STRINGER_AREA)
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af.stringer.add_mass(STRINGER_MASS)
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af.stringer.add_webs(SKIN_THICKNESS)
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Removed:
# af.stringer.info_print(2)
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af.stringer.info_print(2)
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af.stringer.info_save(SAVE_PATH, 'foo_name')
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# Plot components with matplotlib
@@ -80,16 +80,16 @@
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eval = evaluator.Evaluator(af)
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# The analysis is performed in the evaluator.py module.
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eval.analysis(1, 1)
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Removed:
# eval.info_print(2)
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eval.info_print(2)
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eval.info_save(SAVE_PATH, 'foo_name')
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# evaluator.plot_geom(eval)
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Removed:
# evaluator.plot_lift(eval)
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evaluator.plot_lift(eval)
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pop = generator.Population(10)
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# print(help(creator))
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# print(help(evaluator))
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# print(help(generator))
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print(help(creator))
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print(help(evaluator))
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print(help(generator))
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# Print final execution time
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print("--- %s seconds ---" % (time.time() - start_time))
tools/creator.py
@@ -401,7 +401,7 @@
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plt.gca().legend(bbox_to_anchor=(1, 1),
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bbox_transform=plt.gcf().transFigure)
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Removed:
if view == True:
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if view is True:
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plt.show()
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else:
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pass