F106DeltaDart
Elite member
I should probably clarify that I meant 1/4 MEAN (average) aerodynamic chord, not root chord. It ends up being at around 1/3 root chord for wings due to the sweep, depending on angle. That's why I linked to the wing CG calculator. Much easier to calculate that using the site then do it by hand every time .Thanks... good information. I was going to aim for 1/3 cord, kind of like CG. But now.. maybe I'll do it right.
I am looking forward to both of your canard builds, really seeing some awesome aircraft surface for this challenge!