Sorry to both of you, but your answers do not satisfy me yet.
You see, I am questioning wether a lighter than gross loaded airplane should be restrained at the same level of G limits as the fully loaded example.
Let´s imagine you are given the task to design the structure of the wing of an...
Can somebdy out there explain to me why is Maneuvering Speed G-limted and not Load-limited as a function of weight ?
Please see
http://www.ec.erau.edu/cce/faculty/sf335ch3_2.ppt
As far as I knew, a wing is, for this purpose, the limiting factor. A wing, as a beam, can only support a certain...