1. + + u(z) = 6z - 4z3, 2 = y 16 (4) I n the present study, we have used equation (4) since it i s possible t o evaluate a l l integrals across the boundary layer analytically.
2. 2 fl = 0.7611 t 0.4211 6 = -5.5 + 2.511+ @.mn B = o.6n - 0.33
3. v )[(nlcl+ e) -(2 + 3.1667nItl
4. In reference 16, satisfactory predictions have also been shown for several cases includinq flat-plate, favorable pressure gradient, and moderate adverse pressure gradient unseparated flows selected from the Proceedings of the Stanford Conference.