T-6/Harvard wing attach angle manufacturing technique

[italian harvard]

I am aware that Titanium is harder on milling equipment, and has a different thermal expansion coefficient. With that aside, would the angle hold up?

My last post on this subject... Yes it would hold up. Would the adjacent structure? Titanium is much stiffer than aluminum. It could cause a stress concentration in the wing skins and stiffener attachments because the attach angle would not flex as much (be as soft) spanwise. Why keep trying to reinvent the wheel?...

couldnt say it any better than this..

Alex