22-Mec-A1 Applied Thermodynamics and Heat Transfer · December 2019
Question 8 of 8: Two-shell-pass, twelve-tube-pass oil cooler
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: National Examination 16-Mec-A1 Applied Thermodynamics and Heat Transfer, 3 hours, open book. Eight questions of equal value: Part A — Thermodynamics (Q1–Q4) and Part B — Heat Transfer (Q5–Q8). A complete paper is any five questions (three from one part and two from the other).
Reference texts: Çengel & Boles, Thermodynamics: An Engineering Approach (9th ed., McGraw-Hill) — ideal-gas processes and entropy generation, polytropic compression, rigid-vessel charging, the reciprocating air compressor, throttling/flash separation, the steam turbine, and vapour-compression refrigeration/heat-pump cycles; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — steady radial conduction through a cylindrical wall with convection, conduction with uniform internal generation, transient (lumped) cooling by combined convection and radiation, and the effectiveness–NTU method for shell-and-tube exchangers. Steam and Freon-12 (R-12) properties are evaluated, which reproduces the IAPWS steam tables and the standard R-12 property tables to graphing accuracy; enthalpy differences (the only quantities used) are datum-independent. Air and combustion gases are treated as ideal with constant specific heats ($\gamma=1.4$, $R=0.287\ \text{kJ/kg}\cdot\text{K}$, $c_p=1.005$, $c_v=0.718\ \text{kJ/kg}\cdot\text{K}$).
2 shell / 12 tube passes, $D=0.018$ m, $L=3.8$ m/pass
Overall coefficient
$U=340$ W/m²·°C
Find. Heat-transfer rate and both exit temperatures.
Water (the lower heat-capacity rate) is $C_\text{min}$; the multi-pass arrangement permits the water outlet (110.6 °C) to exceed the oil outlet (72 °C) — a temperature cross a single pass could not achieve.
Approach. Compute the two heat-capacity rates and identify $C_\text{min}$; find the area and NTU; apply the $n$-shell-pass effectiveness relation to get $\varepsilon$; then $\dot Q=\varepsilon C_\text{min}\Delta T_\text{max}$ and close the two energy balances for the exit temperatures.
Area and NTU. $A=12\,\pi D L=12\pi(0.018)(3.8)=2.578\ \text{m}^2$:
$$\text{NTU}=\frac{UA}{C_\text{min}}=\frac{340(2.578)}{418}=2.097$$
Effectiveness (2 shell passes). First one shell pass at $\text{NTU}_1=\text{NTU}/2=1.048$:
$$\varepsilon_1=\frac{2}{(1+C_r)+\sqrt{1+C_r^2}\,\dfrac{1+e^{-\text{NTU}_1\sqrt{1+C_r^2}}}{1-e^{-\text{NTU}_1\sqrt{1+C_r^2}}}}=0.478$$
then combine two identical passes:
$$\varepsilon=\frac{\left(\dfrac{1-\varepsilon_1 C_r}{1-\varepsilon_1}\right)^{2}-1}{\left(\dfrac{1-\varepsilon_1 C_r}{1-\varepsilon_1}\right)^{2}-C_r}=\boxed{0.652}$$
The paper prints the tube length as "3.8 cm", which is physically impossible (it gives $A=0.026$ m² and a negligible NTU); it is read as 3.8 m per pass, consistent with a real shell-and-tube unit. Note the computed water outlet, 110.6 °C, exceeds 100 °C — at atmospheric pressure the tube water would begin to boil, so a real installation would run pressurised (or with a higher water flow). The calculation is reported as posed; the boiling caveat is flagged rather than folded into the answer.