AviationTire Principles Of Flight - Aeroplane Subsonic Aerodynamics CLmax augmentation Q 2 / 5

When a trailing edge flap is lowered fully:

the C of P moves to the rear and lift/drag ratio is unaffected.
the C of P moves to the rear and lift/drag ratio is decreased.
the C of P moves forwards and lift/drag ratio is decreased.
the C of P moves to the rear and lift/drag ratio is increased.