From 7a7c4840386adc45ed84985784d57fe3fc345c07 Mon Sep 17 00:00:00 2001
From: Marius Peter <blendoit@gmail.com>
Date: Sun, 23 Jun 2019 02:17:21 -0700
Subject: bugfix

---
 creator.py | 4 ++--
 main.py    | 6 +++---
 2 files changed, 5 insertions(+), 5 deletions(-)

diff --git a/creator.py b/creator.py
index aa9fcbd..0bfe529 100644
--- a/creator.py
+++ b/creator.py
@@ -198,8 +198,8 @@ class Airfoil(Coordinates):
         x_chord.extend(i for i in range(x_chord_25_percent, self.chord + 1))
         # Reversed list for our lower airfoil coordinate densification
         x_chord_rev = [i for i in range(self.chord, x_chord_25_percent, -1)]
-        ext = [i / 10 for i in range(x_chord_25_percent * 10, -1, -1)]
-        x_chord_rev.extend(ext)
+        extend = [i / 10 for i in range(x_chord_25_percent * 10, -1, -1)]
+        x_chord_rev.extend(extend)
 
         # Generate our airfoil geometry from previous sub-functions.
         for x in x_chord:
diff --git a/main.py b/main.py
index b62b24f..97cd492 100644
--- a/main.py
+++ b/main.py
@@ -23,8 +23,8 @@ import time
 start_time = time.time()
 
 # Airfoil dimensions
-NACA_NUM = 2412
-CHORD_LENGTH = 100
+NACA_NUM = 4412
+CHORD_LENGTH = 133
 SEMI_SPAN = 140
 
 # Airfoil thickness
@@ -106,7 +106,7 @@ def main():
         eval.analysis()
         # eval.info_print(2)
         eval.info_save(SAVE_PATH, _)
-        # evaluator.plot_geom(eval)
+        evaluator.plot_geom(eval)
         # evaluator.plot_lift(eval)
 
     # Print final execution time
-- 
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