The wing of an airplane has an average cross-sectional area of 11 m2 and experiences a lift force of 72,000 N. What is the average difference in the air pressure between the top and bottom of the wing?
Pressure = Force / area
Net force = 72000 N ( Force Difference )
Area = 11m2
Pressure difference = Force difference / area
72000/11 N/m 2
= 6545.45 Pa