(c) $p_{1} + \frac{1}{2}\rho\ v_{1}^{2} = p_{2} + \frac{1}{2}\rho\ v_{2}^{2}$
Or $p_{1} - p_{2} = \frac{1}{2}\rho\ (v_{2}^{2} - v_{1}^{2})$
$= \frac{1}{2} \times 1.3 \times (120^{2} - 90^{2})$
$= 4.095 \times 10^{3}\ Nm^{- 2}$
Gross lift on the wing $= (p_{1} - p_{2}) \times$ area
$= 4.095 \times 10^{3} \times 10 \times 2$
$= 81.9 \times 10^{3}$ N