17-Phys-B6 Applied Thermodynamics and Heat Transfer · December 2013
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. 98-Phys-B6 Applied Thermodynamics and Heat Transfer, National Examination December 2013 — a three-hour open-book examination; candidates are expected to bring both a thermodynamics text and a heat-transfer text to make use of the property tables. A complete examination is five questions — either three from Part A (Thermodynamics, Q1–Q4) and two from Part B (Heat Transfer, Q5–Q8), or two from Part A and three from Part B — every question carrying equal value; all eight are solved below as a complete study set. Candidates are invited to state any assumptions where a question is open to interpretation; this licence is used explicitly in Question 1(b) (standard air properties, not printed directly) and Question 7 (a printed convective "rate" read as a heat-transfer coefficient with a temperature unit omitted in print — the same omission the paper shows in Question 6's specific-heat units).
Reference texts. Y. A. Çengel and M. A. Boles, Thermodynamics: An Engineering Approach, 8th ed. (ideal-gas processes, vapour power cycles, gas-turbine/Brayton cycles, vapour-compression refrigeration); F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (conduction, natural convection, lumped-capacitance transient conduction, radiation exchange between surfaces, heat-exchanger LMTD analysis).
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. Flat baseplate, thickness 0.5 cm, area 0.03 m², $\rho=2770$ kg/m³, $C_p=875$ J/kg·K (the source's printed "J/k C" is read as the standard J/kg·K), $\alpha=7.3\times10^{-5}$ m²/s, surface coefficient $h=12$ W/m²·K, 85% of the 1000 W heater output reaching the baseplate, starting from thermal equilibrium with $22\,{}^{\circ}\text{C}$ air.
| Quantity | Symbol | Value |
|---|---|---|
| Baseplate thickness | $\delta$ | 0.5 cm |
| Surface area | $A$ | 0.03 m² |
| Density | $\rho$ | 2770 kg/m³ |
| Specific heat | $C_p$ | 875 J/kg·K |
| Thermal diffusivity | $\alpha$ | $7.3\times10^{-5}$ m²/s |
| Surface coefficient | $h$ | 12 W/m²·K |
| Heater power reaching plate | $\dot Q_{in}$ | $0.85\times1000=850$ W |
| Ambient / initial temperature | $T_\infty$ | $22\,{}^{\circ}\text{C}$ |
Find. (a) Time to heat from $22\,{}^{\circ}\text{C}$ to $140\,{}^{\circ}\text{C}$ with the heater on; (b) time for the plate to cool from $140\,{}^{\circ}\text{C}$ back down to $125\,{}^{\circ}\text{C}$ with the heater off.
Approach. The thin plate (Biot-number-favourable geometry) is treated with lumped-capacitance transient analysis. With the heater on, the energy balance $mC_p\,dT/dt=\dot Q_{in}-hA(T-T_\infty)$ integrates to an exponential approach toward a (very high, never-reached) steady-state temperature; with the heater off, it reduces to plain Newtonian cooling. Both parts use the same time constant $\tau=mC_p/(hA)$.
| Quantity | Value |
|---|---|
| Time constant $\tau$ | 1009.9 s |
| (a) Time to reach $140\,{}^{\circ}\text{C}$ | 51.8 s |
| (b) Heater-off duration ($140\to125\,{}^{\circ}\text{C}$) | 137.3 s |