A fully loaded boeing aircraft has a mass of \( 5.4 \times 10^{5}\ \text{kg} \). Its total wing area is \( 500\ \text{m}^{2} \). It is in level flight with a speed of \( 1080\ \text{km/h} \). If the density of air \( \rho \) is \( 1.2\ \text{kg m}^{-3} \), the fractional increase in the speed of the air on the upper surface of the wing relative to the lower surface in percentage will be: \( (g = 10\ \text{m/s}^{2}) \)