22-Mec-A1 Applied Thermodynamics and Heat Transfer · May 2014
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper: National Examinations — 07-Mec-A1 Applied Thermodynamics and Heat Transfer, May 2014. Open-book, 3-hour paper. 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, all of equal value. Full worked solutions to all eight questions are given below.
Reference texts: Çengel & Boles, Thermodynamics: An Engineering Approach (9th ed., McGraw-Hill) — closed- and open-system energy balances, steam tables, gas power cycles, reciprocating compressors and vapour-compression refrigeration; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — composite-wall conduction, internal-flow and cross-flow convection correlations, natural convection with radiation, and the ε–NTU heat-exchanger method. Freon-12 property data are taken from the appendix supplied with the exam; steam and air data from standard tables.
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 real (irreversible, with line pressure drops) vapour-compression cycle. The compressor runs 1→2 and rejects $q_\text{out}=4\ \text{kJ/kg}$; the condenser exit / throttle inlet is state 5; throttling holds enthalpy so $h_7=h_6=h_5$; the evaporator absorbs heat 7→8. Enthalpies from the supplied Freon-12 tables:
| State | Condition | $h\ (\text{kJ/kg})$ |
|---|---|---|
| 1 — compressor inlet | 125 kPa, −10 °C (superheated) | 185.2 |
| 2 — compressor exit | 1.20 MPa, 100 °C (superheated) | 245.5 |
| 5 — throttle inlet | ≈ sat. liquid, 40 °C | 74.5 |
| 7 — evaporator inlet | 140 kPa, $h_7=h_5$ | 74.5 |
| 8 — evaporator exit | 100 kPa, −20 °C (superheated) | 179.9 |
Find. The cycle coefficient of performance, $\text{COP}=q_L/w_\text{in}$.
Approach. Write the first law over the compressor (heat loss increases the work input), take the refrigeration effect as the evaporator enthalpy rise with $h_7=h_5$ from the throttle, then form the COP.
| Quantity | Result |
|---|---|
| Compressor work input | 64.4 kJ/kg |
| Refrigeration effect $q_L$ | 105.3 kJ/kg |
| Coefficient of performance | ≈ 1.64 |