Chapter 9: Problem 72
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?