A fully loaded aircraft has a mass of \(5.4 \times 10^{5} \mathrm{~kg}\). Its total wing area is \(500 \mathrm{~m}^{2}\)…

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