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| author | blendoit <blendoit@gmail.com> | 2019-10-04 11:47:39 -0700 |
|---|---|---|
| committer | blendoit <blendoit@gmail.com> | 2019-10-04 11:47:39 -0700 |
| commit | 7683b492ba9791c8a0ce2fc6c1820d69cbdfc652 (patch) | |
| tree | ba09cf28c7a2d9e33daf857af623777b17734b1e /example_airfoil.py | |
| parent | b6cbe69cd70050bd88c789b3b80131bb87bc7886 (diff) | |
Start work under Pypy3
Diffstat (limited to 'example_airfoil.py')
| -rw-r--r-- | example_airfoil.py | 2 |
1 files changed, 1 insertions, 1 deletions
diff --git a/example_airfoil.py b/example_airfoil.py index 14cf916..3488eb9 100644 --- a/example_airfoil.py +++ b/example_airfoil.py @@ -69,7 +69,7 @@ af.spar2 = creator.wing.Spar(af, 0.57, mt.aluminium) # af.stringer.info_save(SAVE_PATH, 'foo_name') # Plot components with matplotlib -# wing.plot_geom(af, [af.spar1, af.spar2], None) +# creator.wing.plot_geom(af, [af.spar1, af.spar2], None) # Evaluator object contains airfoil analysis results. eval = evaluator.Evaluator(aircraft) |