I've read this whole thread and I think that both sides are right and are simply not seeing the other's point of view.
It's like the old parable of several blind men touching an elephant, feeling different parts (softball for 6PC), and then being in complete disagreement about the characteristics of the elephant. They're experiences are all true, but none of them are totally true. (No insult meant by reference to "blind men").
From my inexperienced mind -
The bank angle produces a horizontal component of lift that brings the RW in at an angle that cause the plane, left to its own devices, to "turn" along a curved flight path because the tail will continually try to face the plane into the RW.
The application of opposite rudder, however, can be used to prevent the tail from weathervaning to face the plane into the RW and, I think this observation is important (and hopefully correct
), also directs the thrust vector at an angle relative to the plane's direction of travel (i.e. at an angle relative to the RW).
All that said, isn’t it true that the pilot can skillfully control the relative amount of aileron and opposite rudder in a slipping flight condition to do any one of the following?:
(1) “turn” the plane in either direction, while slipping, in the sense that the plane follows a curved flight path by continuously maintaining an imbalanced force vector in the horizontal plane; or
(2) “side slip” the plane in either direction, while slipping, in the sense that the plane moves left or right while essentially staying on a parallel flight path, by applying those same horizontal force vectors in a more balanced, more subtle manner; or
(3) "forward slip" the plane along a continuous course, while slipping, by keeping the horizontal forces that would otherwise "turn" or "side slip" the plane in complete balance?
Seems to my newbie-mind that all three scenarios are possible just by varying the relative amount of aileron and rudder in a skillful and timely manner.