From 2c8e6e632eb03cd6545de51d72aaebe0df9bf7ee Mon Sep 17 00:00:00 2001
From: Marius Peter <blendoit@gmail.com>
Date: Sat, 22 Jun 2019 21:07:02 -0700
Subject: airfoil coordinates

---
 main.py | 68 ++++++++++++++++++++++++++++++++---------------------------------
 1 file changed, 34 insertions(+), 34 deletions(-)

(limited to 'main.py')

diff --git a/main.py b/main.py
index fd8855f..09d33e6 100644
--- a/main.py
+++ b/main.py
@@ -24,8 +24,8 @@ start_time = time.time()
 
 # Airfoil dimensions
 NACA_NUM = 2412
-CHORD_LENGTH = 40
-SEMI_SPAN = 50
+CHORD_LENGTH = 12
+SEMI_SPAN = 20
 
 # Airfoil thickness
 T_UPPER = 0.1
@@ -41,9 +41,9 @@ SPAR_CAP_AREA = 0.3  # sqin
 STRINGER_AREA = 0.1  # sqin
 
 # Amount of stringers
-TOP_STRINGERS = 0
+TOP_STRINGERS = 2
 BOTTOM_STRINGERS = 18
-NOSE_TOP_STRINGERS = 0
+NOSE_TOP_STRINGERS = 5
 NOSE_BOTTOM_STRINGERS = 5
 
 # population information & save path
@@ -71,42 +71,42 @@ def main():
         af.add_naca(NACA_NUM)
         af.add_mass(AIRFOIL_MASS)
         # af.info_print(2)
-        # af.info_save(SAVE_PATH, _)
-
-        # Create spar instance
-        af.spar = creator.Spar()
-        # Define the spar coordinates and mass, stored in single spar object
-        af.spar.add_coord(af, 0.15)
-        af.spar.add_coord(af, 0.55)
-        # Automatically adds spar caps for all spars previously defined
-        af.spar.add_spar_caps(SPAR_CAP_AREA)
-        af.spar.add_mass(SPAR_MASS)
-        # af.spar.info_print(2)
-        # af.spar.info_save(SAVE_PATH, _)
-
-        # Create stringer instance
-        af.stringer = creator.Stringer()
-        # Compute the stringer coordinates from their quantity in each zone
-        af.stringer.add_coord(af,
-                              NOSE_TOP_STRINGERS,
-                              TOP_STRINGERS,
-                              NOSE_BOTTOM_STRINGERS,
-                              BOTTOM_STRINGERS)
-        af.stringer.add_area(STRINGER_AREA)
-        af.stringer.add_mass(STRINGER_MASS)
-        # af.stringer.info_print(2)
-        # af.stringer.info_save(SAVE_PATH, _)
+        af.info_save(SAVE_PATH, _)
+
+        # # Create spar instance
+        # af.spar = creator.Spar()
+        # # Define the spar coordinates and mass, stored in single spar object
+        # af.spar.add_coord(af, 0.15)
+        # af.spar.add_coord(af, 0.55)
+        # # Automatically adds spar caps for all spars previously defined
+        # af.spar.add_spar_caps(SPAR_CAP_AREA)
+        # af.spar.add_mass(SPAR_MASS)
+        # # af.spar.info_print(2)
+        # # af.spar.info_save(SAVE_PATH, _)
+        #
+        # # Create stringer instance
+        # af.stringer = creator.Stringer()
+        # # Compute the stringer coordinates from their quantity in each zone
+        # af.stringer.add_coord(af,
+        #                       NOSE_TOP_STRINGERS,
+        #                       TOP_STRINGERS,
+        #                       NOSE_BOTTOM_STRINGERS,
+        #                       BOTTOM_STRINGERS)
+        # af.stringer.add_area(STRINGER_AREA)
+        # af.stringer.add_mass(STRINGER_MASS)
+        # # af.stringer.info_print(2)
+        # # af.stringer.info_save(SAVE_PATH, _)
 
         # Plot components with matplotlib
-        # creator.plot_geom(af)
+        creator.plot_geom(af)
 
         # Evaluator object contains airfoil analysis results.
-        eval = evaluator.Evaluator(af)
+        # eval = evaluator.Evaluator(af)
         # The analysis is performed in the evaluator.py module.
-        eval.analysis()
+        # eval.analysis()
         # eval.info_print(2)
-        eval.info_save(SAVE_PATH, _)
-        evaluator.plot_geom(eval)
+        # eval.info_save(SAVE_PATH, _)
+        # evaluator.plot_geom(eval)
         # evaluator.plot_lift(eval)
 
     # Print final execution time
-- 
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