Originally Posted by
SrTelemaster150
Usually the CG should be located @ the main wing spar or the thickest part of the airfoil.
Well l get that, BUT! This is a canard, main wing is on the back & the stab is on the front? I know most kits, the CG is at the 25-30% or main spar. I set my CG on most planes l go from the LE to TE & mark the halfway point. then l go from the halfway point to the LE and mark it halfway. That would be 25% and on a flying wing, l go from the LE to the 25% mark and mark it ageen and that is where l start. BUT! This is a hole new dog??
