Gary wrote: > From my plans, the CG is 15% to 40% of the wing chord. That was the old > wing. Is it the same with to AS5048 wing?
I don't ever remember seeing that number before. Is that for a KR1, or just an early set of plans? My plans also say 15%-35%, and that's the range that extends too far aft to be safe (according to an analysis by Richard Mole and also experience by pilots). The AS50xx series airfoils are designed to have a similar lift coefficient and range (15%-35%) as the RAF 48 (minus those aft two inches). Mark Langford ML at N56ML.com http://www.n56ml.com
