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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)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

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: aluminum20237$8.4\times10^{-5}$
Left: glass61.4$4.29\times10^{-3}$
Left film $1/h$—$h=50$$2.0\times10^{-2}$
Right: copper1597$1.55\times10^{-4}$
Right: alumina430$1.33\times10^{-4}$
Right: Teflon60.35$1.71\times10^{-2}$
Right film $1/h$—$h=150$$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.

  1. 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.
  2. Heater temperature. The two sides are parallel, so $q''_{\text{tot}}=(T_3-T_\infty)\big(\tfrac{1}{R_{\text{Al}}}+\tfrac{1}{R_{\text{Cu}}}\big)$: $$T_3=25+\frac{26{,}000}{41.03+41.50}=25+315.0=340.0\ \mathrm{^\circ C}.$$
  3. (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 $\approx 13.1\ \mathrm{kW/m^2}$
  4. (c) Aluminum-side temperatures. Marching outward from $T_3=340.0\ \mathrm{^\circ C}$ with $\Delta T=q''_{\text{Al}}(t/k)$: $$T_2=340.0-12{,}927\tfrac{0.020}{237}=338.9\ \mathrm{^\circ C},\qquad T_1=338.9-12{,}927\tfrac{0.006}{1.4}=283.5\ \mathrm{^\circ C}.$$ (Convection check: $q''=h(T_1-T_\infty)=50(258.5)=12{,}925\ \mathrm{W/m^2}$ ✓.)
  5. (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: $150(112.2-25)=13{,}080\approx13{,}073\ \mathrm{W/m^2}$ ✓.)
  6. (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.
QuantityResult
(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 dropsAl-side film 258.5 °C, Teflon 224.1 °C, glass 55.4 °C