Knegel/Hosenose,
Does this help at all? The F4U-1/4 can pull 2G's (instantanious) at 110Knots (126MPH) at 12,000LBS no power/no flaps. The CAS/IAS chart for the F4U shows no error at that speed so that is a real number. When power is applied the stall number comes way down as airflow increases over the wing from the prop. In postwar test of the F4U it could reach 3G's with no flaps at just over 100Knots IAS. These are examples of turning without flaps.
With flaps the drag from the flaps can be used to slow the airplane from higher speeds however the thrust/drag curve starts to change at lower speeds the parasite drag from the flaps becomes less of a force and the lift is more powerful especially when combined with the airflow created from the 2,000HP up front. Evident of this is the ability to take off with a 4,000LBS payload. If the drag was more powerfull than the lift the airplane could not takeoff in such a loading condition.
IMHO what should happen is what does happen: as you add flaps and turn you slow from 170MPH down to 110MPH when you no longer deccelerate and you seem to accelerate through the turn because your lift and thrust far exceed the drag and G force being applied at low speed.
So basically the flaps add drag at low speed but not enough to overcome 2,000HP and the lift of the wing and flaps which is also considerable.