Question 9 of 9: Carnot Power Cycle — Air Standard
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exam 04-BS-10, Thermodynamics — December 2018. 3 hours, Closed-Book Exam (approved
calculator and one double-sided 8.5x11-inch aid sheet permitted; property tables and charts supplied
in an appendix, interpolation not required — the closest tabular value may be used). Part A:
answer 2 of Questions 1–3 (20 marks each). Part B: answer 4 of Questions 4–9 (15 marks
each), for a 100-mark paper. Only the first two Part-A and first four Part-B questions as they appear
in the answer book are marked. All nine questions (Part A complete, Part B complete) are solved below
for completeness.
Reference texts: Cengel & Boles, Thermodynamics: An Engineering
Approach, 8th ed.; Moran, Shapiro, Boettner & Bailey, Fundamentals of Engineering
Thermodynamics, 8th ed. All state properties (water/steam, R-134a, air, N₂, O₂, humid
air) were computed from high-accuracy equations of state in place of printed property-table interpolation; every boxed numeric result.
Question 9: Carnot Power Cycle — Air Standard (15 marks)
Given. $m=1.5$ kg air, ideal gas. $\eta_{th}=0.50$. $Q_{in}=40$ kJ (process 1→2,
isothermal expansion at $T_H$). $P_1=700$ kPa, $V_1=0.12$ m³.
Find. (a) $T_H$, $T_L$ [K]; (b) $V_2$ [m³]; (c) $W$, $Q$ for each of the four
processes.
Fig. Q9 — Carnot cycle on the p–v plane: 1→2 isothermal expansion at
$T_H$, 2→3 isentropic expansion, 3→4 isothermal compression at $T_L$, 4→1 isentropic
compression.
Approach
State 1 fixes $T_H$ directly from the ideal-gas law; the given cycle efficiency then fixes $T_L$
from the Carnot relation. The isothermal-expansion heat transfer, combined with the ideal-gas
isothermal work integral, gives $V_2$. The remaining volumes and every process's work/heat follow from
the Carnot cycle's standard four-process bookkeeping.
Maximum and minimum temperature (part a).
$$T_H=\frac{P_1V_1}{mR}=\frac{700\times0.12}{1.5\times0.287}=\boxed{195.12\ \text{K}}$$
$$T_L=T_H(1-\eta_{th})=195.12\times0.50=\boxed{97.56\ \text{K}}.$$
Volume at the end of the isothermal expansion (part b). Isothermal, so
$\Delta U=0\Rightarrow Q_{12}=W_{12}=mRT_H\ln(V_2/V_1)=P_1V_1\ln(V_2/V_1)$:
$$\ln\frac{V_2}{V_1}=\frac{Q_{12}}{P_1V_1}=\frac{40}{700\times0.12}=0.4762
\ \Rightarrow\ V_2=V_1e^{0.4762}=0.12\times1.610=\boxed{0.1932\ \text{m}^3}.$$
Process 1→2 (isothermal expansion at $T_H$).
$$W_{12}=Q_{12}=\boxed{40.00\ \text{kJ}}.$$
Process 2→3 (isentropic expansion, $T_H\to T_L$). $Q_{23}=0$; work equals
the drop in internal energy:
$$W_{23}=-\Delta U=mc_v(T_H-T_L)=1.5\times0.718\times(195.12-97.56)=\boxed{105.07\ \text{kJ}},\qquad
Q_{23}=0.$$
Process 3→4 (isothermal compression at $T_L$). By the Carnot heat-ratio
relation $Q_{out}/Q_{in}=T_L/T_H$:
$$Q_{out}=Q_{12}\frac{T_L}{T_H}=40\times\frac{97.56}{195.12}=20.00\ \text{kJ}
\ \Rightarrow\ Q_{34}=W_{34}=\boxed{-20.00\ \text{kJ}}.$$
Process 4→1 (isentropic compression, $T_L\to T_H$). By symmetry with
2→3 (same $|\Delta T|$, opposite direction):
$$W_{41}=-mc_v(T_H-T_L)=\boxed{-105.07\ \text{kJ}},\qquad Q_{41}=0.$$