Question: Question 5 : Consider a steady, incompressible ( = constant ) , laminar boundary layer flow over a surface with free - stream velocity U

Question 5: Consider a steady, incompressible ( = constant), laminar boundary layer flow over a surface with free-stream velocity U(x), which may vary with the distance from the leading edge, x. Assuming negligible body forces and constant fluid viscosity: (a) Show that the pressure in the boundary layer will be: ()=0+2(02()2) where P0 and U0 are the velocity and pressure at x=0. List the assumptions you made in showing the result.

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