3 files changed, 6 insertions, 61 deletions
diff --git a/README.md b/README.md
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--- /dev/null
+++ b/README.md
@@ -0,0 +1,6 @@
+# UCLA_MAE_154B
+UCLA Spring 2019, MAE 154B
+
+Code enables the creation of NACA airfoils;
+the evaluation of the airfoil's structural properties;
+the optimization via genetic algorithm of a population of airfoils, usign standard GA algorithms.
diff --git a/evaluate.py b/evaluate.py
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index 4065c5a..0000000
--- a/evaluate.py
+++ /dev/null
@@ -1,16 +0,0 @@
-# This file is part of Marius Peter's airfoil analysis package (this program).
-#
-# This program is free software: you can redistribute it and/or modify
-# it under the terms of the GNU General Public License as published by
-# the Free Software Foundation, either version 3 of the License, or
-# (at your option) any later version.
-#
-# This program is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
-# GNU General Public License for more details.
-#
-# You should have received a copy of the GNU General Public License
-# along with this program.  If not, see <https://www.gnu.org/licenses/>.
-
-import airfoil as af
diff --git a/main.py b/main.py
deleted file mode 100644
index 7a5a20b..0000000
--- a/main.py
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@@ -1,45 +0,0 @@
-# This file is part of Marius Peter's airfoil analysis package (this program).
-#
-# This program is free software: you can redistribute it and/or modify
-# it under the terms of the GNU General Public License as published by
-# the Free Software Foundation, either version 3 of the License, or
-# (at your option) any later version.
-#
-# This program is distributed in the hope that it will be useful,
-# but WITHOUT ANY WARRANTY; without even the implied warranty of
-# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
-# GNU General Public License for more details.
-#
-# You should have received a copy of the GNU General Public License
-# along with this program.  If not, see <https://www.gnu.org/licenses/>.
-
-import creator
-import random
-
-import time
-start_time = time.time()
-
-CHORD_LENGTH = 100
-SEMI_SPAN = 200
-
-POP_SIZE = 1
-SAVE_PATH = 'C:/Users/blend/Desktop/python/airfoils'
-
-
-def main():
-    # Create coordinate system specific to airfoil dimensions.
-    creator.Coordinates(CHORD_LENGTH, SEMI_SPAN)
-    for airfoil_number in range(1, POP_SIZE + 1):
-        foo = creator.Airfoil()
-        foo.naca(2412)
-        # foo.print_geometry(4)
-        foo.spar = creator.Spar()
-        foo.spar.add_spar(foo.coordinates, 'aluminium', 0.15)
-        creator.plot(foo, foo.spar)
-        # foo.save_values(airfoil_number, SAVE_PATH)
-
-    print("--- %s seconds ---" % (time.time() - start_time))
-
-
-if __name__ == '__main__':
-    main()