Pressure*areawings=weightaircraft
Pressure*500=3.3E6 kg* 9.8N/kg
solve for pressure difference in Newtons
Please help
A fully loaded aircraft has a mass of 3.3×10^5 kg.its total wing area is 500m2 . It is in level flight with a speed of 960km/h.
Calculate the pressure difference between the lower and upper surface of the wings.
Thank you!
1 answer