NivaarExam PrepOfficial exam papers ↗

22-Mec-A1 Applied Thermodynamics and Heat Transfer · December 2017

Question 7 of 8: Surface temperature of a natural-convection heating panel

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) — closed-system energy balances, wet-region steam properties, flash/separator processes, isentropic turbine and compressor efficiency, vapour-compression refrigeration, and reciprocating-compressor clearance analysis; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — transient lumped-capacitance cooling, radial composite-cylinder conduction, internal-flow and external cross-flow convection, natural convection from a vertical plate, and the LMTD method for condensers. Water/steam and air properties are taken from standard tables (IAPWS-consistent); ammonia and R-134a properties are read from the saturation and superheat tables appended to the examination paper.

Question 7 — Surface temperature of a natural-convection heating panel (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. A thin vertical panel, height $H=0.75$ m, length $L_w=1.5$ m, dissipating 690 W by natural convection from both faces into still air at 20 °C. Find. the panel surface temperature $T_s$.

QuantityValue
Panel height (characteristic length), $H$0.75 m
Panel length1.5 m
Total area (both faces)2 × (0.75 × 1.5) = 2.25 m²
Heat dissipated, $\dot Q$690 W
Air temperature, $T_\infty$20 °C
Oil panel, 690 W$H=0.75$ mbuoyant airstill air, 20 °C
Figure 7 — Thin vertical panel losing heat by natural convection from both faces; the boundary layers rise along the 0.75 m height, which is the characteristic length for the Rayleigh number.

Approach. Balance the dissipated power against natural-convection loss from both faces, using the Churchill–Chu vertical-plate correlation with air properties at the film temperature, and iterate on $T_s$.

  1. Energy balance. $\dot Q = h\,A_\text{tot}(T_s-T_\infty)$ with $A_\text{tot}=2.25\ \text{m}^2$, so the required flux is $\dot Q/A_\text{tot}=306.7\ \text{W/m}^2$ and $h(T_s-20)=306.7$.
  2. Rayleigh number (film properties). At the converged film temperature $T_f\approx 48.8$ °C, air has $\nu\approx1.79\times10^{-5}$, $\alpha\approx2.54\times10^{-5}\ \text{m}^2/\text{s}$, $k\approx0.0280$, $Pr\approx0.71$. With $\beta=1/T_f$ and $\Delta T\approx57.5$ °C, $$Ra_H = \frac{g\beta\Delta T\,H^3}{\nu\alpha} \approx 1.64\times10^{9}$$
  3. Churchill–Chu Nusselt number (all-$Ra$ vertical plate). $$Nu = \left\{0.825 + \frac{0.387\,Ra_H^{1/6}}{\left[1+(0.492/Pr)^{9/16}\right]^{8/27}}\right\}^2 \approx 143$$ $$h = Nu\,k/H \approx 5.33\ \text{W/m}^2\text{}\cdot\text{°C}$$
  4. Solve the balance. Iterating $T_s$ until $h(T_s-20)=306.7$ converges gives $$T_s - 20 = \frac{306.7}{5.33} \approx 57.5\ \text{°C}$$ $T_s \approx 77.5\ ^\circ\text{C}$
Check — radiation neglected.
Only natural convection is counted, as the question states. If the panel also radiated ($\varepsilon\approx0.9$) it would shed extra heat and the true surface temperature would be somewhat lower; the convection-only figure is the conservative (higher) surface temperature the question asks for.
QuantityResult
Required convective flux306.7 W/m²
Rayleigh number $Ra_H$≈ 1.64 × 10⁹
Nusselt number / $h$≈ 143 / 5.33 W/m²·°C
Surface temperature $T_s$≈ 77.5 °C