Air at freestream velocity U∞=16 ms, and free steam temperature T∞=50℃ is flowing over a plate surface that is at temperature Ts=100℃. The velocity and thermal boundary layers developing on the surface have been shown in the figure. Also shown are the tangents to the velocity and temperature profiles at the surface y=0. If the density of air is ρ∞=1.1 kgm3, viscosity μ=1.963×10-5kgm∙s, and thermal conductivity k=0.0274Wm∙K then, calculate
(a) the wall shear stress, τw
(b) coefficient of skin friction, Cf
(c) convection heat transfer coefficient, h
(d) the Nusselt number, if the length of the plate is L=1m.
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