estimate the upward force on an airplane's wing?

Question

Use Bernoulli's equation to estimate the upward force on an airplane's wing if the average flow speed of air is 180 m/s above the wing and 155 m/s below the wing. The density of the air is 1.2 kg/m3 and the area of each wing surface is 27 m2

Answer 1

Bernoulli's equation says
p + 0.5ρV^2 + 0.5ρgh = constant where ρ is density.
Ignoring the small effect of the height-dependent pressure difference (since wing thickness isn't given), the pressure difference on the two sides of the wing is
Δp = 0.5ρ(V1^2-V2^2)
Then the force = AΔp where A = wing area