How can one calculate the maximum instantaneous bank angle a plane can do in a certain time? I know that there is a limitation to do an instantaneous banking angle a plane can do. These limitations are due to the airplane (infrastructure - aerodynamics) and limitation on the pilot (due to his ability to withstand a certain maneuvering calculated in g), so how can one calculate an accurate or approximate value for the maximum instantaneous bank angle taking into account the (military and civilian) planes infrastructure and also taking into account the pilot (with or without) a g-suit.

Also i want to know how long can a pilot withstand that instantaneous bank angle?

Thanks in advance.
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