Given access to the complete geometry, surface pressure and shear stress distribution over a body placed in a uniform flow, one can estimate

The positive high angle-of-attack condition is obtained in a steady pull-out maneuver at the largest permissible angle-of-attack of the wing. Under this conditi...

A Pilot tube mounted on the wing tip of an airplane flying at an altitude of 3 km measures a pressure of 0.72 bar, and the outside air temperature is 268.66 K....