|June 9, 2012, 04:23||
Boundary layer velocity profiles
Join Date: May 2012
Posts: 9Rep Power: 6
how can I get, in a well defined position along the surfaces of an airfoil, the boundary layer velocity profiles, i.e. the values (or the plot directly..) calculated in a direction perpendicular to the considered point tangent?
Of course I already have the flow field calculated with good resolution in the near wall region.
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