The span area of the wings of an aeroplane is 50 cm. When it is running on the runway the pessure 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 cm. When it is runnin

1.	The span area of the wings of an aeroplane is 50 cm. When it is running on the runway the pessure 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`