diff options
Diffstat (limited to 'example_airfoil.py')
| -rw-r--r-- | example_airfoil.py | 9 |
1 files changed, 5 insertions, 4 deletions
diff --git a/example_airfoil.py b/example_airfoil.py index 9626f6f..2828b27 100644 --- a/example_airfoil.py +++ b/example_airfoil.py @@ -18,9 +18,6 @@ import generator import time start_time = time.time() -# Airfoil dimensions (in) -NACA_NUM = 2412 - # Thicknesses SPAR_THICKNESS = 0.4 SKIN_THICKNESS = 0.1 @@ -46,7 +43,7 @@ eval = evaluator.Evaluator("eval") ac = creator.base.Aircraft(eval, "ac") af = creator.wing.Airfoil(ac, 'af') -af.add_naca(NACA_NUM) +af.add_naca(2412) # af.info_print(2) af.info_save() spar1 = creator.wing.Spar(af, 'spar1') @@ -59,10 +56,14 @@ spar2.info_save() ac2 = creator.base.Aircraft(eval, "ac2") af2 = creator.wing.Airfoil(ac2, 'af2') af2.add_naca(3412) +af2.info_save() spar3 = creator.wing.Spar(af2, 'spar3', 0.23) spar4 = creator.wing.Spar(af2, 'spar4', 0.67) +spar3.info_save() +spar4.info_save() for aircraft in eval.aircrafts: + print(aircraft) print(aircraft.wing) for spar in aircraft.wing.spars: print(spar.material["name"]) |