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)
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 $T_s$.
Quantity
Value
Panel height (characteristic length), $H$
0.75 m
Panel length
1.5 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
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 $T_s$.
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 $h(T_s-20)=306.7$.
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,
$$Ra_H = \frac{g\beta\Delta T\,H^3}{\nu\alpha} \approx 1.64\times10^{9}$$
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.