The question may be stupid, but I cannot find any clear definition of both generalized and localized cracking.
Does anybody know the difference, preferably in aircraft structures?
Thank you.
Hi all,
Automated drilling for fastener installation has been used in airplane assembly for long time. It is known (or believed) it provides better fatigue life. Particularly, I mean wing box stringer-skin joints.
I want to quantify the advantage of the automated drilling process over the...
