Side Slip /wing blanking/dihedral/change in wing profile realative to the wind.
HiTech
So you are applying enough yaw force to move the longitudinal axis fast enough and far enough across the velocity vector to blank the wing enough to stall it at the tip?
The force required to do that at 230 mph is tremendous.
In reality, the airfoil needs to be close to its critical AOA before a rudder kick will stall it (a little up aileron will help on the side of the kick) and the speed needs to be low enough that the rudder kick doesn't knock the tail off.
Snap rolls are violent things, involving high G on the wing and large forces on the vertical stabilizer. You have to stall (or get very very close) the wing with back stick and induce the autorotation with rudder or it is just a high G barrel roll.
And this is where I will bow out.
There is no room for a point of view other than "it matches reality now" so no point in further discussion.
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