No when the boundary layer separates the center of lift moves aft and flow on the undeside of the wing is allowed to curl up over the trailing edge, this simly causes turbulence behind the wing.
Light buffet comes from the separation but for most aircraft the significant stall buffet is from the turbulent air impinging on the tailplane.
Washout is what prevents the tips of the wing stalling before the inboard.
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as our drag goes up, so does our lift
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This is the part I'm most curious about, sounds counter intuitive, increased lift increases induced drag, past the stall then form drag increases but I have never heard of an increase in drag inceasing lift?..