Boundary-layer separation occurs when the shear stress
at the surface becomes zero. Assume a polynomial representation for the laminar boundary layer of the form, u/U 5 a
1 bλ 1 cλ2 1 dλ3
, where λ 5 y/δ. Specify boundary conditions on the velocity profile at separation. Find appropriate
constants, a, b, c, and d, for the separation profile. Calculate
the shape factor H at separation. Plot the profile and compare
with the parabolic approximate profile.
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