Aerospace Engineering > GATE 2015 > Boundary Layer Theory
The velocity profile of an incompressible laminar boundary layer over a flat plate developing under constant pressure is given by u(y)/Uα=3y/(2δ)-1/2(y/δ)3. The freestream velocity U∞=10 m/s and the dynamic viscosity of the fluid μ=1.8×10-skg/(ms) At a streamwise station where the boundary layer thickness δ=5 mm, the wall shear stress is _______ ×10-3Pa
Correct : 53.9 to 54.1
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