1. Change the shape and size of the wing:
a.angle of attack
b.thickness and curvature
c.size of the wing area
2. For each of wing shapes change the external factors that influence lift:
a.position
b.airspeed
c.altitude
3. Record results:
a.Plots of pressure above and below the airfoil surface.
b.Plots of airspeed above and below the airfoil surface.
4. Compare the results and determine which wing shape is the most aerodynamic.