Sal, I was always here, just nothing to contribute and Dick said things better than I could.
Just looked over former posts and found #76 where I estimated the neutral point to be at the wing's trailing edge. Since the balance is already ahead of it, you now have a pitch-stable airplane, which would be even flyable if it were unstable. Static stability margin might be 8% now - not too bad. So I wouldn't add more weight but rather keep wing loading low.
Burkhard
Last edited by UStik; 02-28-2016 at 06:53 AM.