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# 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 evaluator
import generator
import tkinter as tk
import tkinter.ttk as ttk
from matplotlib.backends.backend_tkagg import (
FigureCanvasTkAgg, NavigationToolbar2Tk)
def main():
root = tk.Tk()
root.wm_title('MAE 154B - Airfoil Design, Evaluation, Optimization')
# root.geometry('1000x400')
# # User inputs
l_naca = ttk.Label(root, text='NACA Number')
e_naca = ttk.Entry(root)
l_chord = ttk.Label(root, text='Chord Length')
e_chord = ttk.Entry(root)
af = generator.default_airfoil()
# # Graph window
fig, ax = creator.plot_geom(af, False)
plot = FigureCanvasTkAgg(fig, master=root)
plot.draw()
plot.get_tk_widget().pack(side=tk.TOP, fill=tk.BOTH, expand=1)
toolbar = NavigationToolbar2Tk(plot, root)
toolbar.update()
plot.get_tk_widget().pack(side=tk.TOP, fill=tk.BOTH, expand=1)
# # Layout
l_naca.pack()
e_naca.pack()
l_chord.pack()
e_chord.pack()
root.mainloop()
if __name__ == '__main__':
main()
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