This program calculates the motion of an airfoil attached to an ornithopter wing. The airfoil undergoes a sinusoidal oscillation and its angle is found through a torque balance. With this angle, the lift and drag of the airfoil are calculated along with their subsequent torque. It's assumed the airfoil is subject to the inertial reaction of its mass, an aerodynamic force, and a damped angular spring. Each of these forces/torques can be adjusted along with the amplitude and frequency of the oscillation. Therefore, it's possible to try out different parameters and observe how they affect the x and y components of the aerodynamic force.
The scripts were written in Python 3.9.5 and require the following libraries:
To execute the program, open the terminal/command prompt and browse to the folder containing main.py and run the command:
>> python3 main.py
If you are using windows, you can simply double click interface.py and to open it with IDLE.
To adjust the calculations, open input_parameters.py with a text editor and change the variables.
