Consider the flow of a liquid metal past a flat plate (Pr
<< 1). We have shown that for a constant wall teemperature,
T_o, the Nusselt number is given by Nu = 0.564*(Re^1/2)*(Pr^1/2).
Show that if the surface is not a constant temperature, but is
instead providing a constant heat flux, that the Nusselt number
becomes Nu = 0.886*(Re^1/2)*(Pr^1/2). Start with the following
expression for the temperature profile within a semi-infinite body
with a constant heat flux boundary condition T...