23-Chem-A2 Unit Operations and Separation Processes · May 2013
Question 6 of 6: Radiative Cooling of a Brass Rod
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exam 04-Chem-A2 Mechanical and Thermal Operations, May 2013 — open-book, 3 hours. Two sections: Section A (Mechanical Operations, A1–A3) and Section B (Thermal Operations, B1–B3); all problems 25 marks. The rubric asks candidates to attempt two problems per section; all six are solved in full below.
Reference texts: McCabe, Smith & Harriott, Unit Operations of Chemical Engineering (7th ed., McGraw-Hill) — pipe-flow friction, loss coefficients, sphericity and the Ergun equation (Tables 7.1, 5.1); de Nevers, Fluid Mechanics for Chemical Engineers (3rd ed.) and Brodkey & Hershey, Transport Phenomena — mechanical-energy balance and sudden expansion/contraction losses; Incropera & DeWitt, Fundamentals of Heat and Mass Transfer (7th ed., Wiley) — composite-wall resistance networks, LMTD/ε–NTU cross-flow exchangers and lumped radiative cooling; Lienhard, A Heat Transfer Textbook and Özişik, Radiative Transfer for the appended correction-factor and emissivity charts.
Compressible-flow note. Water properties at 180 °F are taken as $\rho=60.55\ \mathrm{lb/ft^3}=970\ \mathrm{kg/m^3}$ and $\mu=2.32\times10^{-4}\ \mathrm{lb/(ft\cdot s)}=3.45\times10^{-4}\ \mathrm{Pa\cdot s}$; commercial-steel roughness $\varepsilon=0.0457$ mm (Table A2).
Section A — Mechanical Operations
Question B3: Radiative Cooling of a Brass Rod (25 marks)
Given. Lumped body, radiation only. $\rho=8526\ \mathrm{kg/m^3}$, $C_p=382\ \mathrm{J/(kg\,K)}$, $\sigma=5.67\times10^{-8}\ \mathrm{W/(m^2K^4)}$; rod $D=1$ m, $L=2$ m; radiating fraction 0.95 (trestle shades 5%); oxidized-brass emissivity $\varepsilon\approx0.60$ (Fig. B2 at $\sim\!660\,$°F); $T_i=400\,$°C$=673.15$ K, $T_f=300\,$°C$=573.15$ K.
Find. (a) the governing ODE; (b) the cooling time from 400 to 300 °C.
Figure B3 — The rod is treated as a lumped body radiating from 95% of its surface. The $T^4$ loss gives a separable ODE whose integral yields the cooling time.
Approach. Energy conservation on the lumped body gives the ODE; separate variables and integrate the $T^{-4}$ term between the two temperatures, using the cylinder’s volume-to-(radiating)area ratio.
(a) Governing equation. The stored-enthalpy loss rate equals the radiant loss to the (cold) surroundings: $$\rho V C_p\frac{dT}{dt}=-A\varepsilon\sigma\big(T^4-T_{\text{surr}}^4\big).$$ With $T_{\text{surr}}^4\ll T^4$ (hot body, cool room), this reduces to the required form $$\boxed{(\rho V C_p)\frac{dT}{dt}+A\varepsilon\sigma T^4=0.}$$
Separate and integrate. $$\int_{T_i}^{T_f}\frac{dT}{T^4}=-\frac{A\varepsilon\sigma}{\rho V C_p}\int_0^t dt\;\Rightarrow\;t=\frac{\rho V C_p}{3\,\varepsilon\sigma A}\left(\frac{1}{T_f^{3}}-\frac{1}{T_i^{3}}\right).$$
Geometry. $V=\tfrac{\pi}{4}D^2L=1.571\ \mathrm{m^3}$; total surface $A_{\text{tot}}=\pi DL+2\cdot\tfrac{\pi}{4}D^2=7.85\ \mathrm{m^2}$; radiating area $A=0.95A_{\text{tot}}=7.46\ \mathrm{m^2}$, so $V/A=0.2105$ m.
Evaluate. With $\varepsilon=0.60$, $\sigma=5.67\times10^{-8}$: $$t=\frac{8526(382)}{3(0.60)(5.67\times10^{-8})}(0.2105)\!\left(\frac{1}{573.15^{3}}-\frac{1}{673.15^{3}}\right)=\boxed{1.37\times10^{4}\ \mathrm{s}\approx3.8\ \mathrm{h}.}$$
Quantity
Result
Governing ODE
$(\rho VC_p)\dot T+A\varepsilon\sigma T^4=0$
Volume / radiating area
1.571 m$^3$ / 7.46 m$^2$
Emissivity (oxidized brass)
$\approx$ 0.60
Cooling time (400→300 °C)
≈ $1.37\times10^{4}$ s (3.8 h)
Check — lumped assumption & chart reads The 1-m diameter is taken as printed. Lumped capacitance requires a small radiative Biot number; for high-conductivity brass ($k\approx110\ \mathrm{W/mK}$) $Bi=\varepsilon\sigma T^3 (D/2)/k\approx0.06\ll0.1$, so it is defensible. The time scales as $1/\varepsilon$; reading $\varepsilon=0.55$–0.65 from Fig. B2 shifts $t$ by $\pm8\%$.