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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 s​hell-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)

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. 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.

conductor, $\dot q'''$ $r_0$ $T_c=540$ °C $h,T_\infty$ $r$ (−$r_0$ … +$r_0$)$T$ 540 °C (centre) 472 °C (surface)
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.

  1. 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: $$\dot q'''=\frac{T_c-T_\infty}{\dfrac{r_0}{2h}+\dfrac{r_0^{2}}{4k}}=\frac{513}{3.30\times10^{-5}+5.02\times10^{-6}}=1.349\times10^{7}\ \text{W/m}^3$$
  2. Generation per unit length. Multiply by the cross-sectional area $\pi r_0^2$: $$\dot q'=\dot q'''\,\pi r_0^{2}=1.349\times10^{7}\,\pi(0.0375)^{2}=5.96\times10^{4}\ \text{W/m}$$ $\dot q'\approx 59.6\ \text{kW/m}$
  3. 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. ✓
QuantityResult
Volumetric generation $\dot q'''$$1.35\times10^{7}$ W/m³
Generation per unit length $\dot q'$59.6 kW/m
Surface temperature $T_s$472 °C