= 3. If u = U2 2y +*) where too, 8 represent the freestream velocity and boundary layer thickness respectively for flow

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3 If U U2 2y Where Too 8 Represent The Freestream Velocity And Boundary Layer Thickness Respectively For Flow 1 (26.12 KiB) Viewed 20 times

= 3. If u = U2 2y +*) where too, 8 represent the freestream velocity and boundary layer thickness respectively for flow over a flat plate, find the displacement thickness, momentum thickness, wall shear stress and skin friction coefficient approximately at x = 0.05 m if u. 1 m/s, p = 1000 kg/mº, u = 10 Pa.s. The boundary layer thickness can be estimated from Blasius solution. The velocity distribution in the boundary layer is given by 3 y 1 28 2 I u 3 का U.CO