Q. The speed of air flow on the upper and lower surfaces of a wing of an aeroplane are
v1 and
v2 respectively. If A is the cross section area of the wing and
ρ is the density of air, then the upward lift is :
- 12ρA(v1+v2)
- 12ρA(v1−v2)
- 12ρA(v21−v22)
- 12ρA(v21+v22)