New structural G-limit feature

[AndyJWest]

Bellator, I understand what you are saying, but I'd be a bit wary of taking such figures too literally - they seem to imply (a) that there is a fixed ratio between G force necessary to cause airframe damage and that needed to cause failure, and (b) this ratio differed between Allied and Luftwaffe aircraft.

It's worth noting, at least in passing, that there are suggestions in the thread that early Spitfires were designed for 10 G loads, and actual tests on wings exceeded this.