What happen to the dynamic pressure if speed es doubled?
Dynamic pressure will be 4 times larger.
On a CAMBERED aerofoil, what happen to the total reaction and the centre of pressure (CP) if the angle of attack (AoA) is increased?
The magnitude of the total pressure would increase and the CP would move forwards.
On a SYMMETRICAL aerofoil, what happen to the total reaction and the centre of pressure (CP) if the angle of attack (AoA) is increased?
The magnitude of the total pressure would increase and the CP would NOT move.
What happen if the camber increase?
The pressure between the upper and lower surfaces would change.