17-Phys-B6 Applied Thermodynamics and Heat Transfer · May 2016
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. 98-Phys-B6 Applied Thermodynamics and Heat Transfer, National Examination May 2016 — 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 and charts. 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. Where the exam's own "state your assumptions" licence applies (Part A cold-air-standard properties in Question 3; the rectangular-case geometry read from the printed illustration in Question 7), the assumption is flagged explicitly in a check callout rather than hedged inside the answer.
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 with convective boundaries, internal/external convection correlations, natural convection, radiation exchange, cross-flow heat-exchanger effectiveness–NTU 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. 40 tubes, $D=1$ cm, in a 1 m × 1 m duct. Water (tube-side, hence UNMIXED — each tube's stream never contacts another): $c_p=4180$ J/kg°C, $T_{c,in}=18\,{}^{\circ}\text{C}$, $V=3$ m/s. Air (duct-side, open cross-section, hence MIXED): $c_p=1010$ J/kg°C, $T_{h,in}=130\,{}^{\circ}\text{C}$, 105 kPa, $V=12$ m/s. $U=80$ W/m2°C.
| Quantity | Symbol | Value |
|---|---|---|
| Number of tubes / diameter | $N,\,D$ | 40 / 1 cm |
| Duct cross-section | — | 1 m × 1 m |
| Water specific heat / inlet temp / velocity | $c_{p,w},\,T_{c,in},\,V_w$ | 4180 J/kg°C / $18\,{}^{\circ}\text{C}$ / 3 m/s |
| Air specific heat / inlet temp / velocity | $c_{p,a},\,T_{h,in},\,V_a$ | 1010 J/kg°C / $130\,{}^{\circ}\text{C}$ / 12 m/s |
| Air inlet pressure | $P_a$ | 105 kPa |
| Overall heat transfer coefficient | $U$ | 80 W/m2°C |
Find. The water and air outlet temperatures and the total heat-transfer rate.
Approach. Compute both capacity rates $C=\dot{m}c_p$ from the given velocities and cross-sections, identify $C_{\min}/C_{\max}$, form $\text{NTU}=UA/C_{\min}$ with $A=N\pi DL$, apply the effectiveness–NTU relation for the one-fluid-mixed/one-unmixed cross-flow configuration (air mixed, water unmixed), then back out both outlet temperatures.
The temperature changes are small because the given $U$ (80 W/m2°C) and area (1.26 m2) together give a very small NTU relative to the large capacity rates on both sides — this is a genuinely undersized/lightly-loaded exchanger for the flow rates specified, not a computational error (confirmed by the $\varepsilon\approx\text{NTU}$ self-check above).
| Quantity | Value |
|---|---|
| Water capacity rate, $C_w$ | 39,340 W/K |
| Air capacity rate, $C_a$ | 11,000 W/K |
| NTU / effectiveness | 0.00914 / 0.00909 |
| Heat-transfer rate, $q$ | 11.19 kW |
| Water outlet temperature, $T_{c,out}$ | $18.29\,{}^{\circ}\text{C}$ |
| Air outlet temperature, $T_{h,out}$ | $128.98\,{}^{\circ}\text{C}$ |