Originally Posted by PJ2
I wonder if you meant pitch attitude? The AoA at stall is, just guessing, going to be around 14 to 18deg perhaps a bit higher given the wing:
At FL350 ?
Never been there by chance but would be very surprised by such AoA figures ... !?
For 212k kg, FL350 the pitch attitude at AlphaProt is almost 9deg
To me your CBT autoflight software is not really representative performance wise, a simulator would be a better reference.
I believe the numbers produced by HN39 for the AoA make more sense, I would be interested to know how he did estimate them ?
ww, you're pretty close ...