I just have a question about the calculation of the airleron deflection angle.
Where do I get this data from?
1. Change in lift with aileron deflection: cldeltaa
2. Airfoil’s lift curve slope: cldelta
3. Section drag coefficient: cdo
Is it possible to calculate them? Or do they come from...
Hi CastMetal,
thank you for this link! It is exactly what I was looking for.
I used google too, but only found very complicated instructions and a lot of mathematical stuff ;)