Load Factor is proportional to lift which is in turn proportional to V^2
LFnew / LForiginal = (Vnew
/ Voriginal)^2
LFnew = LForiginal x (120 / 100)^2
= 1 x 1.2^2 = 1.44
The LF will therefore initially increase to 1.44 if the angle of attack
remains constant.