Most people know the standard, "At a 60 degree bank, an aircraft experiences 2G's" checkpoint for load-factor on an airplane.
I assume that this statement has an underlying, unspoken assumption that the aircraft is maintaining a constant altitude in the bank.
This leads on to matters of increased stall speed during turns.
My question is, if no pitch adjustment is made while in a coordinated turn, which I think means that no additional load-factor is acting on the aircraft, is the stall speed still affected?