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. An actual (irreversible-compression, subcooled-liquid) R-134a cycle with every state pinned by two independent properties, so no assumed process (e.g. isentropic compression) is needed for the ACTUAL cycle — only for its ideal comparison.
| State | Description | Conditions |
|---|---|---|
| 1 | compressor inlet | 0.14 MPa, $-10\,{}^{\circ}\text{C}$ (superheated) |
| 2 | compressor outlet | 0.8 MPa, $50\,{}^{\circ}\text{C}$ |
| 3 | condenser outlet | 0.72 MPa, $26\,{}^{\circ}\text{C}$ (subcooled liquid) |
| 4 | after throttle valve | 0.15 MPa, $h_4=h_3$ |
| $\dot m=0.05$ kg/s | ||
Find. (a) $\dot Q_L$, $\dot W_{in}$, compressor isentropic efficiency, $COP_{actual}$; (b) the ideal-cycle $\dot Q_L$ and $\dot W_{in}$ at the same evaporator/condenser pressures, and the differences.
Approach. For the ideal comparison, replace states 1 and 3 with the SATURATED states at the same two pressures (saturated vapour at $P_1$, saturated liquid at $P_2$) and compress isentropically from the new state 1 to $P_2$.
| Quantity | Actual | Ideal (same pressures) |
|---|---|---|
| Heat removal $\dot Q_L$ | 7.93 kW | 7.18 kW |
| Compressor power $\dot W_{in}$ | 2.02 kW | 1.81 kW |
| COP | 3.93 | 3.97 |
| Compressor isentropic efficiency: 93.7% | Actual exceeds ideal by 0.74 kW ($\dot Q_L$) and 0.21 kW ($\dot W_{in}$) | ||