My recollection came from UAS days, but some discussion on it here (NZ CAA website):
https://www.caa.govt.nz/fig/advanced...-stalling.html
By using aileron to stop the roll (a natural tendency), the mean angle of attack increases on the down-going wing. The lift continues to decrease with an increase in angle of attack (past the critical angle), while the drag continues to increase rapidly with any small increase in angle of attack. Show the effect of aileron on the CL and CD curves on the graph.
The use of aileron adversely affects the roll and favours autorotation. This is the reason for maintaining ailerons neutral in the initial stall recovery.