17-Phys-B6 Applied Thermodynamics and Heat Transfer · December 2017
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. 98-Phys-B6 Applied Thermodynamics and Heat Transfer, National Examination December 2017 — 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 4 (the exam's own printed text is ambiguous about whether the piston displacement is 1.00 m³, read here as the intended value) and Question 6 (the external air stream is treated as an effectively infinite, constant-temperature reservoir since no air mass flow rate or duct is specified).
Reference texts. Y. A. Çengel and M. A. Boles, Thermodynamics: An Engineering Approach, 8th ed. (two-phase closed systems, flash chambers, steam turbines, vapour-compression refrigeration, reciprocating compressors); F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (composite cylindrical conduction, internal and external forced convection correlations, natural convection from a vertical plate, heat-exchanger LMTD analysis). Saturation and superheat property values below were computed (Bell et al., IAPWS-95 / REFPROP-quality equations of state for water, ammonia and R134a) and cross-checked against the printed appendix tables on pages 5–8 of the source exam, which they matched to 3–4 significant figures throughout.
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 ideal vapour-compression cycle skeleton (saturated liquid into the expansion valve, dry saturated vapour into the compressor) run at identical condenser/evaporator temperatures and identical cooling duty for two candidate refrigerants; the compressor floor efficiency of 90% applies equally to both, so it scales both fluids' actual work by the same factor and cannot change which fluid needs less power — it is evaluated anyway for a defensible absolute number.
| Quantity | Symbol | Value |
|---|---|---|
| Condenser (saturation) temperature | $T_{cond}$ | $34\,{}^{\circ}\text{C}$ |
| Evaporator (saturation) temperature | $T_{evap}$ | $-16\,{}^{\circ}\text{C}$ |
| Compressor isentropic efficiency | $\eta_c$ | 90% |
| Refrigeration effect | $\dot Q_L$ | 3.5 kJ/s |
Find. Which refrigerant, ammonia or R134a, gives the lower compressor power for the stated cycle and duty.
Approach. For each fluid: state 1 is saturated vapour at $T_{evap}$; state 3 is saturated liquid at $T_{cond}$, and $h_4=h_3$ across the (isenthalpic) expansion valve. Compress isentropically from state 1 to the condenser pressure to get $h_{2s}$, then apply the compressor efficiency to get the actual work; the mass flow rate follows from the refrigeration effect $\dot Q_L=\dot m(h_1-h_4)$, and the compressor power is $\dot m$ times the actual specific work.
| Quantity | Ammonia | R134a |
|---|---|---|
| Refrigeration effect, $h_1-h_4$ | 1081.71 kJ/kg | 141.48 kJ/kg |
| Mass flow rate $\dot m$ | 0.003236 kg/s | 0.02474 kg/s |
| Actual compressor work $w_a$ | 287.29 kJ/kg | 39.34 kJ/kg |
| Compressor power $\dot W_c$ | 0.930 kW | 0.973 kW |
| COP | 3.77 | 3.60 |