From 93cc49e414766f2980e06cbe2b9b8be10ec4472d Mon Sep 17 00:00:00 2001
From: blendoit <blendoit@gmail.com>
Date: Tue, 1 Oct 2019 23:29:24 -0700
Subject: Proper package structure

---
 example_airfoil.py | 8 +++++---
 1 file changed, 5 insertions(+), 3 deletions(-)

(limited to 'example_airfoil.py')

diff --git a/example_airfoil.py b/example_airfoil.py
index 08282a3..a5e1cce 100644
--- a/example_airfoil.py
+++ b/example_airfoil.py
@@ -10,8 +10,8 @@ Generate a population of airfoils & optimize.
 """
 
 from resources import materials as mt
-from creator import wing, fuselage, propulsion
-# from evaluator import
+from creator import *
+from evaluator import evaluator
 # from generator import
 
 import time
@@ -41,6 +41,8 @@ NOSE_BOTTOM_STRINGERS = 5
 
 SAVE_PATH = '/home/blendux/Projects/Aircraft_Studio/save'
 
+# Create aircraft instance
+aircraft = base.Aircraft
 # Create airfoil instance
 af = wing.Airfoil(20, 150, mt.aluminium)
 af.add_naca(NACA_NUM)
@@ -69,7 +71,7 @@ af.spar2 = wing.Spar(af, 0.57, mt.aluminium)
 # wing.plot_geom(af, [af.spar1, af.spar2], None)
 
 # Evaluator object contains airfoil analysis results.
-# eval = evaluator.Evaluator(af)
+eval = evaluator.Evaluator(aircraft)
 # The analysis is performed in the evaluator.py module.
 # eval.analysis(1, 1)
 # eval.info_print(2)
-- 
cgit v1.2.3