You are correct that the new airfoil can change the cg limits...the aft cg
limit is based on the wing...not the aircraft...so a different airfoil
might affect the c.g. range. I looked through a selection of different
aircraft and 15%-35% mac is a pretty common range.
https://sites.google.com/site
>...the kr2s should actually have a
>smaller cg range than the kr2. This is because the kr2s has a shorter mean
>aerodynamic chord. 15% to 35% mac is a smaller range on the kr2s than a
>kr2.
+++
Where is the center of lift on the new airfo
2 matches
Mail list logo
