evaluate wing & main file

2 files changed, 61 insertions, 0 deletions

diff --git a/evaluate.py b/evaluate.py
new file mode 100644
index 0000000..8ea1579
--- /dev/null
+++ b/evaluate.py
@@ -0,0 +1,16 @@
+# 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
new file mode 100644
index 0000000..dd6b179
--- /dev/null
+++ b/main.py
@@ -0,0 +1,45 @@
+# 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()