any use of aileron will cause some sideslip
My brain is starting to hurt a little now, but would co-ordinated rudder not negate/minimise this? Or are we saying that rolling an aircraft creates sideslip..? Or that an aircraft at any bank angle (even if co-ordinated) is slipping? If so, how? Not trying to be flippant, but just increase my level of understanding! Thanks in advance for any answers.
I also seem to recall an EASA/CAA document doing the rounds a couple of years ago re: reducing AoA, then increasing power, as opposed to "powering out". Will try find reference.