AviationTire Principles Of Flight - Aeroplane Subsonic Aerodynamics Means to decrease the CL - CD ratio, increasing drag Q 3 / 5

The optimum angle of attack for a typical airfoil is about..., and the actual angle of attack will be close to this optimum angle during...

4° , a stall.
16° , a stall.
4° , cruise.
16° , cruise.