Airleron angle
Airleron angle
(OP)
Hello,
does someone know where to find how the airleron angle is calculated?
I mean the maximum deflection of the airleron wich is needed.
does someone know where to find how the airleron angle is calculated?
I mean the maximum deflection of the airleron wich is needed.





RE: Airleron angle
http://w
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RE: Airleron angle
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 ;)
RE: Airleron 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 flight tests?
RE: Airleron angle
airfoil Cl is generally available (for the wing airfoil and the aileron airfoil; also Cd. look up the airfoil data (maybe on the NACA/NASA site).