17-Phys-B6 Applied Thermodynamics and Heat Transfer · Undated paper
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. 17-Phys-B6 Applied Thermodynamics and Heat Transfer, National Examinations, May 2019 — 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 graphs the exam supplies. 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.
Reference texts. Y. A. Çengel and M. A. Boles, Thermodynamics: An Engineering Approach, 8th ed. (polytropic closed-system processes, throttling, Rankine-cycle reheat/extraction turbines, air-standard Brayton-cycle energy balances, vapour-compression refrigeration); F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (composite plane-wall conduction with convection and radiation at both faces, combined entry-length internal convection, natural convection with radiation from a vertical plate, shell-and-tube heat exchanger sizing via the LMTD correction-factor method). Ammonia, steam and R-134a property values were computed (Bell et al., IAPWS-95 / REFPROP-quality equations of state) and cross-checked against the printed saturated-ammonia appendix table on page 6 of the source exam, which it matched to 3–4 significant figures.
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 1-shell-pass, N-tube-pass exchanger heats tube-side water using shell-side water as the hot fluid; the tube-side mass flow and the given velocity/density fix how many tubes must run in parallel, while the required heat-transfer AREA (from the duty and a corrected LMTD) fixes how many passes of the length-limited tubes are needed.
| Quantity | Symbol | Value |
|---|---|---|
| Tube-side (heated) flow rate | $\dot m_t$ | 3.8 kg/s |
| Tube-side inlet / outlet temperature | $T_{t,i}/T_{t,o}$ | $38\,{}^{\circ}\text{C}/55\,{}^{\circ}\text{C}$ |
| Shell-side flow rate, inlet temperature | $\dot m_s,\ T_{s,i}$ | 1.9 kg/s, $94\,{}^{\circ}\text{C}$ |
| Overall heat-transfer coefficient | $U$ | 1420 W/m²·K |
| Tube inside diameter | $d$ | 1.905 cm |
| Tube-side density, velocity | $\rho,\ V$ | 961 kg/m³, 0.386 m/s |
| Maximum length per pass | $L_{max}$ | 2.44 m |
Find. The number of tubes $N$ and the number of tube passes.
Approach. Get the duty from the tube side, the shell-side outlet temperature from its own energy balance, then the counter-flow LMTD and its 1-shell/N-tube-pass correction factor $F$ to size the total heat-transfer AREA. Separately, the given velocity and density fix how many tubes must run in parallel to carry $\dot m_t$; dividing the required area by that many tubes' available length-per-pass (capped at 2.44 m) gives the number of passes.
| Quantity | Value |
|---|---|
| Heat duty $\dot Q$ | 270.1 kW |
| Required area $A_{req}$ | 7.28 m² |
| Number of tubes $N$ | 36 |
| Number of tube passes | 2 |
| Actual tube length per pass | 1.69 m |