Sotm
Member
BEHIND the wing TE? Yeah, that is WAAAAY too aft. Something's amiss there...
But yes, I do have an answer: CG range should be 5.38" - 6.76" (15% MAC - 25% MAC) from the wing root LE.
The blue line is the 15% MAC location, and the red line is 25% MAC. I maidened the first one in Ohio and the second one at home both closer to the 15% mark, and they were quite nose heavy. I think it should go back closer to the 25% MAC location.
View attachment 101108
I use this "Flying Wing CG Calculator" to get quick CG and MAC calc's for the wing-alone: http://fwcg.3dzone.dk
Not sure a flying wing COG is correct. went back to my on-line and used the one panel wing instead of the two panel. Got very different result. 8.46 fro LE. The flying wing one of yours gave me 8.11 from LE. Pretty similar but different from your 5.38 to 6.76. I did lengthen the wing 1 1/2 inches on each side though for a total of 3 inches more span/and aft sweep. Could be the difference. Maybe I'll just try my friend's "Drop" test. Hold it level in flight ready condition and drop it. See how it drops, nose down or tail down. LOL Seriously I know a dude that CGs his scratch builds that way.