Total area of wings, A = 2 × 25 = 50m2
speed of air lover the longer wing,
V1 = 180 km/h = 50 m/s
speed of air over the upper wings,
V2 = 243 km/h = 65 m/s
Density of air, ρ =1kg/m3
Let P1 and P2 be the pressure of air over the lower wing and upper wing respectively.
From Bimoull’s equation,
∴ pressure difference, ∆P
The upward force on the plane, F = (∆P) A
= 862.5 × 50
= 43125 N
We know that the upward force balances the weight of the plane
∴ F = mg
43125 = m × 9.8
⇒ m = 4400.51 kg.