Angle of Attack and its pratical use in airline jets..
It seems it would be more efficient to use angle of attack indicators (like the carrier Navy). Referencing V speeds for different weights would be eliminated and max a/c performance could be realized, for all phases of flight, even engine failures.
But, how is AOA used with take off decision speed? And, how is AOA used with high speed flight. AOA would be great for approach, but what about climb to the flight levels.
I may have answered my own question, somewhat, but I would like some in depth discussion.