Question

an aeroplane has a mass of 15 tonnes. At cruising speed,air flows over the top of it's wing at 150 m/s and under the wing at 120m/s. Calculate the pressure in difference between the top and the bottom of the wing and the surface area underside the wing

Related Questions

1. A road sign says that no vehicles over 7.5 tonnes may use a bridge. My lorry weighs 4 tonnes, and... an aeroplane of mass 8000kg flying at 600km.h-1 fires a projectile of mass 100kg at a speed of 900 k... The aerodynamic drag on an aeroplane is given by D=bv^2. The power output of the aeroplane cruising... An aeroplane has a mass of 15 tonnes. At cruising speed, air flows over the top of its wings at 150...