Three-dimensional laminar boundary-layer separation on a flat plate due to a flow confrontation with a half cone at incidence

The incompressible, three-dimensional, laminar boundary layer flow on a flat plate about a half-cone protuberance has been investigated bath by experiment in the NAE water tunnel and by analysis using Cooke's small cross-flow momentum integral method. Three half cones of semi-apex angles 7½, 10° and 12½, were tested at a Reynolds number of 2 x...

Theree-dimensional flow separation of a plane, incompressible, laminar boundary layer caused by a half-delta wing on a flat plate