Originally Posted by
Agus Rosales
You will see that this angle is constant for both wings during the whole path on each, this means that the relative wind will hit both wings with the same angle, so same AOA.
Agus.
I would suggest that's not correct either, the AoA won't be and neither will the local slide slip angle. If your looking for a good example of the later, consider why large aircraft often have body gear steering.
Whether this effect is significant I don't know. Sorry not very helpful
I think your question was, though not sure
If you maintain a banked turn, cut thrust, and try to maintain altitude? Would the entire plane stall or would one wing fall first?
Neither, one section of the wing will start to stall before the other, typically the root. But does it really matter? At some point a significant reduction in lateral stability and roll damping will occur. I would suggest this is what really matters.
From a flight instruction point of view you must reduce the AoA.
That's probably enough from me