What happen with the left wing AoA when rolling to the right?
Sometimes I read that the AoA is higher because of the deflection of the aileron downwards and every now and then is lower attending to the rolling effect -lift vector tilts back due to the change of the relative wind-.
Can anyone help me to understand this possible contradiction?
Last edited by smthngdffrnt; 12th September 2017 at 15:33.