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The streamwise velocity component of a steady, incompressible, flat plate boundary layer of boundary layer thickness is approximated by the simple linear expression, u =

The streamwise velocity component of a steady, incompressible, flat plate boundary
layer of boundary layer thickness is approximated by the simple linear expression,
u=U(y) for y, and u=U for y>. Generate expressions for displacement
thickness and momentum thickness as functions of and compare them with the
displacement and momentum thicknesses for turbulent boundary layer where u=
U(y)17.
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