Quote:
One wonders what the 109 would have been like to fly without the slats.
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It would have been rather bad in the stall characteristics.
The wing would have stalled all at once instead of root first and the tips receiving an energized boundary layer to keep the flow attached.
The entire wing stalling would be violent and uncontrollable.
Same thing the Spitfire would do without the twist. Major difference being twisting the wing does not energize the boundary layer so the ratio of turbulent to laminar flow remains the same.
The slats increase the amount of turbulent flow over the wing. The turbulent flow portion of the boundary layer is the high energy, high lift portion.