The span area of the wings of an aeroplane is 50 m^(2). When it is running on the runway the pressure of air at the bottom and top of the wings are found to be 0.75x10^(5) pascal and 0.70x10^(5) pascal respectively. Find the dynamic lift on the wings.

The span area of the wings of an aeroplane is 50 m^(2). When it is run

1.	The span area of the wings of an aeroplane is 50 m^(2). When it is running on the runway the pressure of air at the bottom and top of the wings are found to be 0.75x10^(5) pascal and 0.70x10^(5) pascal respectively. Find the dynamic lift on the wings.
Answer» SOLUTION :`2.5xx10^(5)N`