Originally Posted by RRR
"At Take off aProt is equal to aMAX for 5s."
By which time, the SRS will have commanded about V2+10.
With one engine inoperative?
If we assume Cl is proportional to AoA then, ...
Is that a valid assumption? In the landing configuration AoA for Cl=0 is almost certainly some significant negative value. Also Cl-alpha is non-linear near Clmax.