Air at \(10^{\circ} \mathrm{C}\) enters an \(18-\mathrm{m}\)-long rectangular duct
of cross section \(0.15 \mathrm{~m} \times 0.20 \mathrm{~m}\) at a velocity of
\(4.5 \mathrm{~m} / \mathrm{s}\). The duct is subjected to uniform radiation
heating throughout the surface at a rate of \(400 \mathrm{~W} /
\mathrm{m}^{3}\). The wall temperature at the exit of the duct is
(a) \(58.8^{\circ} \mathrm{C}\)
(b) \(61.9^{\circ} \mathrm{C}\)
(c) \(64.6^{\circ} \mathrm{C}\)
(d) \(69.1^{\circ} \mathrm{C}\)
(e) \(75.5^{\circ} \mathrm{C}\)
(For air, use \(k=0.02551 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K},
\operatorname{Pr}=0.7296, v=1.562 \times\) \(10^{-5} \mathrm{~m}^{2} /
\mathrm{s}, c_{p}=1007 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, \rho=1.184
\mathrm{~kg} / \mathrm{m}^{3}\).)