My Taylor Mono Plane (almost identical to the KR1 except my horizontal stab is larger) has a forward c of g condition depending on fuel loading ( I have a rear fuel tank as well as forward. Can any one tell me with experience how much of a forward c of g they have flown and how did it perform?
I'm looking at a 18.2% MAC full fuel in forward tank with zero in aft tank. My target is 11.40-15.90 of the RAF48" cord Or 23.75 to 33.125% of MAC If I can provide flying surface dimensions could some one run them on one of the good airplane design soft ware packages for me? Darren Pond Taylor Mono Plane CF-VML KR2 C-GGGW
