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22-Mec-A1 Applied Thermodynamics and Heat Transfer · December 2016

Question 7 of 8: Electrically Heated Pipe — Power to Hold 30 °C

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Reference texts: Çengel & Boles, Thermodynamics: An Engineering Approach (9th ed., McGraw-Hill) — closed- and open-system energy balances, boundary work, reciprocating-compressor and vapour/gas power cycles, and gas-turbine refrigeration; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — radial composite-wall conduction, internal-flow decay, natural convection with radiation from a horizontal cylinder, and the ε–NTU cross-flow heat-exchanger method. Air and steam properties are evaluated from IAPWS-IF97 / ideal-air data; the gas-turbine cycle uses cold-air-standard constant specific heats.

Paper format: National Examination 07-Mec-A1, December 2016, 3 hours, open book. Part A — Thermodynamics (Q1–4); Part B — Heat Transfer (Q5–8). Each answer carries equal value; a complete paper is any five (three from one part and two from the other). All eight questions are solved in full below.

Question 7: Electrically Heated Pipe — Power to Hold 30 °C (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.

QuantityValue
Pipe diameter / surface temp$D=0.30$ m, $T_s=30$ °C (303.15 K)
Ambient air temperature$T_\infty=20$ °C (293.15 K)
Surroundings (radiation)$T_\text{sur}=25$ °C (298.15 K)
Emissivity$\varepsilon=0.8$
Air properties at $T_f=25$ °C$\nu=1.558\times10^{-5}$ m²/s, $\alpha=2.202\times10^{-5}$ m²/s, $k=0.02625$ W/m·K, $Pr=0.707$
Tₛ=30°Cε=0.8, D=0.3 mnatural convection to air 20°C+ radiation to surroundings 25°Cq′ = h·πD·(Tₛ−T∞) + εσ·πD·(Tₛ⁴−T_sur⁴)
Figure 7 — The heated horizontal pipe loses heat by natural convection to the 20 °C air and by radiation to the 25 °C surroundings; the electrical input per metre must balance the sum of the two.

Approach. At steady state the electrical power per metre equals the natural-convection loss (Churchill–Chu horizontal-cylinder correlation) plus the radiation loss to the surroundings.

  1. Rayleigh number. At film temperature $T_f=25$ °C, with $\beta=1/T_f$ and $\Delta T=10$ °C, $$Ra_D=\frac{g\beta\,\Delta T\,D^3}{\nu\alpha}=2.59\times10^{7}$$
  2. Convection coefficient (Churchill–Chu). $$Nu_D=\left\{0.60+\frac{0.387\,Ra_D^{1/6}}{\big[1+(0.559/Pr)^{9/16}\big]^{8/27}}\right\}^{2}=37.5,\qquad h=\frac{Nu_D\,k}{D}=3.28\ \text{W/m}^2\text{}\cdot\text{K}$$
  3. Convective loss per metre. $q'_\text{conv}=h(\pi D)(T_s-T_\infty)=3.28(\pi\cdot0.3)(10)=30.9$ W/m.
  4. Radiative loss per metre. $$q'_\text{rad}=\varepsilon\sigma(\pi D)\big(T_s^4-T_\text{sur}^4\big)=0.8(5.67\times10^{-8})(\pi\cdot0.3)(303.15^4-298.15^4)=23.2\ \text{W/m}$$
  5. Total electrical power per metre. $$q'=q'_\text{conv}+q'_\text{rad}=30.9+23.2$$ ==**$q'\approx54$ W/m must be supplied.**==
Check
Radiation contributes ≈ 43 % of the loss here even though $\Delta T$ is only 5–10 °C — at near-ambient temperatures the two mechanisms are comparable, so neglecting radiation would under-size the heating by nearly half. Air properties are at the 25 °C film temperature; the small 10 °C driving difference keeps $h$ modest (≈ 3.3 W/m²·K).
QuantityResult
Rayleigh number $Ra_D$≈ 2.6 × 10⁷
Convection coefficient $h$≈ 3.28 W/m²·K
Convective loss≈ 30.9 W/m
Radiative loss≈ 23.2 W/m
Total power per metre≈ 54 W/m