22-Mec-A1 Applied Thermodynamics and Heat Transfer · December 2018
Question 6 of 8: Heat generation in a current-carrying conductor
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: National Examination 16-Mec-A1, 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 mixtures, the air-standard Otto cycle, wet-region steam properties, the throttling calorimeter, the steady-flow energy equation, the regenerative gas-turbine (Brayton) cycle and vapour-compression refrigeration; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — radial conduction through composite cylinders, conduction with internal heat generation, internal-flow convection with a constant surrounding-fluid temperature, and the effectiveness–NTU method for shell-and-tube exchangers. Steam properties are IAPWS-consistent (equivalent to the steam tables); ammonia properties are read from the saturated- and superheated-ammonia tables appended to the examination; air and combustion gases are treated as ideal gases with constant specific heats ($\gamma=1.4$, $R=0.287\ \text{kJ/kg}\cdot\text{K}$, $c_p=1.005\ \text{kJ/kg}\cdot\text{K}$).
Question 6 — Heat generation in a current-carrying conductor (Part B, equal value)
Given. Solid cylinder, diameter 75 mm ($r_0=0.0375$ m), $k=70\ \text{W/m°C}$, uniform volumetric generation $\dot q'''$. Fluid $T_\infty=27$ °C, surface coefficient $h=568\ \text{W/m}^2\text{°C}$; peak (centreline) temperature limited to $T_\text{max}=540$ °C.
Find. (a) the maximum generation rate per unit length, (b) the surface temperature.
Figure 6 — Uniform generation gives a parabolic radial temperature profile. The centreline is hottest (limited to 540 °C); the surface sits above the fluid by the convective drop $\dot q'''r_0/2h$.
Approach. For a solid cylinder with uniform generation, the centre-to-surface rise is $\dot q'''r_0^2/4k$ and the surface-to-fluid rise is $\dot q'''r_0/2h$ (from a surface energy balance). Summing them to the 540 °C limit fixes $\dot q'''$; then the surface temperature follows.
Peak-temperature constraint. The centreline temperature is
$$T_c=T_\infty+\underbrace{\frac{\dot q'''r_0}{2h}}_{\text{surface film}}+\underbrace{\frac{\dot q'''r_0^{2}}{4k}}_{\text{conduction in solid}}=540\ ^\circ\text{C}$$
Solving for the generation rate:
$$\dot q'''=\frac{T_c-T_\infty}{\dfrac{r_0}{2h}+\dfrac{r_0^{2}}{4k}}=\frac{513}{3.30\times10^{-5}+5.02\times10^{-6}}=1.349\times10^{7}\ \text{W/m}^3$$
Generation per unit length. Multiply by the cross-sectional area $\pi r_0^2$:
$$\dot q'=\dot q'''\,\pi r_0^{2}=1.349\times10^{7}\,\pi(0.0375)^{2}=5.96\times10^{4}\ \text{W/m}$$
$\dot q'\approx 59.6\ \text{kW/m}$
Surface temperature. From the surface film drop only:
$$T_s=T_\infty+\frac{\dot q'''r_0}{2h}=27+\frac{1.349\times10^{7}(0.0375)}{2(568)}=27+445=472\ ^\circ\text{C}$$
$T_s\approx 472\ ^\circ\text{C}$
As a check, adding the conduction rise $\dot q'''r_0^2/4k=68$ °C recovers the 540 °C centreline. ✓