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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 tkinter as tk
from tkinter import ttk
class Input:
'''User inputs.'''
def __init__(self, master):
ttk.Frame(master).grid(row=0, column=0)
ttk.Label(master, text='NACA Number').grid(row=0, sticky='W')
ttk.Label(master, text='Chord Length').grid(row=1, sticky='W')
ttk.Entry(master).grid(row=0, column=1)
ttk.Entry(master).grid(row=1, column=1)
class Graph:
'''Graph airfoil.'''
def __init__(self, master):
ttk.Frame(master).grid(row=0, column=1)
def main():
root = tk.Tk()
root.title('MAE 154B - Airfoil Design, Evaluation, Optimization')
root.geometry('1000x400')
Input(root)
Graph(root)
root.mainloop()
return None
if __name__ == '__main__':
main()
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