23-Chem-A2 Unit Operations and Separation Processes · May 2014
Question 4 of 6: Heater Between Two Composite Walls
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 2014 — open-book, 3 hours. Two sections: Section A (Mechanical Operations, A1–A3) and Section B (Thermal Operations, B1–B3); all problems are worth 25 marks. The rubric asks candidates to attempt two problems per section; all six are solved in full below as a study resource.
Reference texts: McCabe, Smith & Harriott, Unit Operations of Chemical Engineering (7th ed., McGraw-Hill) — pipe-flow friction and loss coefficients, agitator power correlations (Fig. 9.13, Table 9.3), and filtration theory; de Nevers, Fluid Mechanics for Chemical Engineers (3rd ed.) and Brodkey & Hershey, Transport Phenomena — mechanical-energy balance, fitting equivalent lengths, and the appended Fanning chart; Coulson & Richardson, Chemical Engineering Vol. 2 — rotary-drum filtration; Incropera & DeWitt, Fundamentals of Heat and Mass Transfer (7th ed., Wiley) and Lienhard, A Heat Transfer Textbook — composite-wall resistance networks, the Colburn (Chilton–Colburn) analogy, and LMTD/ε–NTU cross-flow exchangers.
Property note. Water properties are as printed in each question; the appended Table A.2 loss coefficients ($k$) and Table A3 turbine constants ($K_T$) are used directly, and pipe-friction factors are taken from Colebrook (identical to the appended Fanning chart, Fig. A1) so the numbers are reproducible without reading a graph.
Question B1: Heater Between Two Composite Walls (25 marks)
Given. One heater feeding two parallel conduction paths that share the same surface temperature $T_{\text{htr}}$ and the same ambient $T_\infty=25\ \mathrm{^\circ C}$; $A=(0.5)^2=0.25\ \mathrm{m^2}$.
Layer (from heater outward)
$t$ (mm)
$k$ (W/m·K)
$t/k$ (m$^2$K/W)
Left: aluminum
20
237
$8.4\times10^{-5}$
Left: glass
6
1.4
$4.29\times10^{-3}$
Left film $1/h$
—
$h=50$
$2.0\times10^{-2}$
Right: copper
15
97
$1.55\times10^{-4}$
Right: alumina
4
30
$1.33\times10^{-4}$
Right: Teflon
6
0.35
$1.71\times10^{-2}$
Right film $1/h$
—
$h=150$
$6.67\times10^{-3}$
Find. (a) left-side flux; (b) right-side flux; (c) interface temperatures $T_1\!\ldots\!T_6$; (d) qualitative discussion of the temperature drops.
[Figure not reproduced: Figure B1 — Although the layers are drawn stacked, the two composite walls are parallel resistances driven from the common heater surface $T_{\text{htr}}$ to a common ambient. $T_3$ is the heater itself; $T_1,T_2$ and $T_4,T_5,T_6$ march outward on the aluminum and copper sides, as labell. See the official exam paper.]
Read from the exam figure On the printed drawing the 4 mm shaded layer against the copper is labelled alumina ($k=30$) and the 6 mm outer layer Teflon ($k=0.35$); the $T_3$ leader ends on the heater, $T_4$ on the copper/alumina face, $T_5$ on the alumina/Teflon face and $T_6$ on the Teflon outer face. The heater is thin and drawn without a dimension, so it is taken as isothermal at $T_3$.
Approach. The heater surface is a single temperature feeding two independent series stacks that both dump to $25\ \mathrm{^\circ C}$; treat them as two resistances in parallel. Find $T_{\text{htr}}$ from the total flux and the parallel resistance, split the flux by each side's resistance, then march the temperatures outward layer by layer.
Total flux and side resistances. $q''_{\text{tot}}=Q/A=6500/0.25=26{,}000\ \mathrm{W/m^2}$. Summing $t/k$ (plus the film) on each side, $$R_{\text{Al}}=\tfrac{0.020}{237}+\tfrac{0.006}{1.4}+\tfrac{1}{50}=0.02437\ \mathrm{m^2K/W},\quad R_{\text{Cu}}=\tfrac{0.015}{97}+\tfrac{0.004}{30}+\tfrac{0.006}{0.35}+\tfrac{1}{150}=0.02410\ \mathrm{m^2K/W}.$$ The two sides turn out almost equally resistive: the Al side is dominated by its weak $h=50$ film, the Cu side by its 6 mm of Teflon.
Heater temperature. The two sides are parallel, so $q''_{\text{tot}}=(T_3-T_\infty)\big(\tfrac{1}{R_{\text{Al}}}+\tfrac{1}{R_{\text{Cu}}}\big)$: $$T_3=25+\frac{26{,}000}{41.03+41.50}=25+315.0=340.0\ \mathrm{^\circ C}.$$
(a),(b) Side fluxes. Each side carries $q''=(T_3-T_\infty)/R$: $$q''_{\text{Al}}=\frac{315.0}{0.02437}=1.293\times10^{4}\ \mathrm{W/m^2},\qquad q''_{\text{Cu}}=\frac{315.0}{0.02410}=1.307\times10^{4}\ \mathrm{W/m^2}.$$ They sum to $26{,}000\ \mathrm{W/m^2}$ ✓ (i.e. 3232 W and 3268 W through the 0.25 m$^2$ faces). Al side $\approx 12.9\ \mathrm{kW/m^2}$; Cu side $\approx 13.1\ \mathrm{kW/m^2}$
(c) Copper-side temperatures. From $T_3=340.0\ \mathrm{^\circ C}$ with $\Delta T=q''_{\text{Cu}}(t/k)$: $$T_4=340.0-13{,}073\tfrac{0.015}{97}=338.0,\quad T_5=338.0-13{,}073\tfrac{0.004}{30}=336.3,\quad T_6=336.3-13{,}073\tfrac{0.006}{0.35}=112.2\ \mathrm{^\circ C}.$$ (Convection check: $150(112.2-25)=13{,}080\approx13{,}073\ \mathrm{W/m^2}$ ✓.)
(d) Where the gradients land. The high-$k$ metals barely drop at all (aluminum $1.1\ \mathrm{^\circ C}$, copper $2.0\ \mathrm{^\circ C}$), while the low-$k$ glass drops $55.4\ \mathrm{^\circ C}$ and the Teflon $224.1\ \mathrm{^\circ C}$. But conductivity is not the only factor: each drop is $q''\,t/k$, so thickness and flux matter as well. The alumina ($k=30$, three times lower than copper) drops only $1.7\ \mathrm{^\circ C}$, less than the copper, because it is 4 mm thick against 15 mm. The convective films also act as resistances: the weak $h=50$ film on the aluminum side takes $258.5\ \mathrm{^\circ C}$, the largest drop anywhere in the system.
Quantity
Result
(a) Aluminum-side flux
$1.29\times10^{4}\ \mathrm{W/m^2}$
(b) Copper-side flux
$1.31\times10^{4}\ \mathrm{W/m^2}$
(c) $T_1,\,T_2$ (Al side)
283.5 °C, 338.9 °C
(c) $T_3$ (heater)
340.0 °C
(c) $T_4,\,T_5,\,T_6$ (Cu side)
338.0 °C, 336.3 °C, 112.2 °C
(d) Largest drops
Al-side film 258.5 °C, Teflon 224.1 °C, glass 55.4 °C