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1 Introduction. - MIT

1 Introduction. - MIT

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At in nity (outside the boundary layer), away from the plate, we have that u!Uas y!1: (3.26) For the ow along a at plate parallel to the stream velocity U, we assume no pressure gradient, so the momentum equation in the xdirection for steady motion in the boundary layer is u @u @x + v @u @y = @2u @y2 (3.27) and the appropriate boundary ...

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