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The streamwise velocity component of a steady, incompressible, flat plate boundaryFor the previous problem if the flow is air at T = 2 0 C
The streamwise velocity component of a steady, incompressible, flat plate boundaryFor the previous problem if the flow is air at that flows with a velocity of
which solution substitute by the with the following relations to get the laminar and
turbulent displacement and momentum thicknesses at and Write a
comment on which result laminar or turbulent is more accurate at each case.
layer of boundary layer thickness is approximated by the simple linear expression,
for and for 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
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