An airplane flying at a velocity of 130 mi/h at a standard altitude of 5000 ft. At a point on the wing, the pressure is 1750.0 psf. Calculate the velocity at that point, assuming incompressible flow.
An airplane flying at a velocity of 130 mi/h at a standard altitude of 5000 ft. At a point on the wing, the pressure is 1750.0 psf. Calculate the velocity at that point, assuming incompressible flow.