What would you expect the typical lift force and coefficient of lift and drag to be for a A320 at cruise?
Considering flight at 36,000 ft, mass approximately 72 tons, velocity 230 m/s with a surface area of 122.6 m² and density 0.366 kg/m³.
The results I've calculated seem a little high, CL=0.666 and L=724 kN