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| -rw-r--r-- | evaluate.py | 16 | ||||
| -rw-r--r-- | main.py | 45 |
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 @@ -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() |