$ new\ V = V\sqrt{G} $ $ G = \frac{1}{cos(Φ)} $ where V is the airspeed, G is the [[Load Factor]], and Φ is the bank angle in degrees. $ new\ V = V\sqrt{\frac{new\ W}{old\ W}} $ where V is the airspeed, and W is the weight of the aircraft. This can be applied to accelerated stalls and maneuvering speed, L/Dmax speed, and minimum sink speed.