Quote:
Originally Posted by Letum
This is not the case. If airframe strength was not considered, the zero would
be able to take nearly 3x the G of the F6, based on it's weight.
The strength of the airframe has certainly been considered. Directly or indirectly.
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Well, do not known. Only TD can answer. But i almost remenber they wrote that g limits were not especific for each design.