Generally speaking about WW2 era aircraft, as you burn fuel, your CG moves towards the rear and the separation point of lift and drag on the wing to the rear because of the slight change in AOA. The only exception to this is the "ponie", which, when you burn fuselage tank first, as you should, it will move forward,(the CG) and then as you burn wing tanks, it will move rearward again. At least that is what my engineering buddies toward me, back when "dirt" was invented! LOL
I was wondering if you were talking about the max alpha or the chordwise location of the separation point. Sounds like you meant the latter. If so, then no, my recollection is, as the AoA increases, the separation point will actually move forward. This will continue until you reach a critical angle, after which, the flow will become almost completely separated and lift will decrease dramatically.
As for the fuel distribution, I'm used to flying 109s. The tank is behind and the cg moves forward, IIRC. The Pony, also IIRC, is as you state - marginally stable at full fuel, more stable as you burn off the tank.
Mind, I'm going back some years as well. aero engin school for me was back in the 80's.