A hot liquid $\left(c_{p}=1000 \mathrm{~J} / \mathrm{kg} \cdot
\mathrm{K}\right)\( flows at a flow rate of \)0.05 \mathrm{~kg} / \mathrm{s}$
inside a copper pipe with an inner diameter of \(45 \mathrm{~mm}\) and a wall
thickness of \(5 \mathrm{~mm}\). At the pipe exit, the liquid temperature
decreases by \(10^{\circ} \mathrm{C}\) from its temperature at the inlet. The
outer surface of the \(5-\mathrm{m}\)-long copper pipe is black oxidized, which
subjects the outer surface to radiation heat transfer. The air temperature
surrounding the pipe is \(10^{\circ} \mathrm{C}\). Assuming that the properties
of air can be evaluated at \(35^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\)
pressure, determine the outer surface temperature of the pipe. Is $35^{\circ}
\mathrm{C}$ an appropriate film temperature for evaluation of the air
properties?