Question 1 of 7: First-Law Bookkeeping for a Monatomic Ideal Gas — Isobaric–Isochoric–Isothermal Cycle
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams — May 2015 — 10-Met-A1 Metallurgical Thermodynamics. Three-hour, closed-book exam using an approved (Casio or Sharp) calculator; candidates were told to state any interpretive assumptions. Any five of the seven questions constitute a complete paper — all seven are solved below for completeness. All questions are of equal value (20 marks each out of 100).
Reference texts: Gaskell, D. R., Introduction to the Thermodynamics of Materials (2nd–5th ed.) — the exam's own Ellingham diagram (Fig. 9-3) is reproduced from this text, which also supplies the standard-state enthalpy/entropy data used below; supporting 298 K entropies for the elements, CO, CO₂, H₂, H₂O(g) and Cu₂O/Cr₂O₃/TiO₂/SiO₂ from the NIST–JANAF Thermochemical Tables.
Question 1: First-Law Bookkeeping for a Monatomic Ideal Gas — Isobaric–Isochoric–Isothermal Cycle (20 marks)
Given. $n=1$ mol monatomic ideal gas, $C_v=20.8\ \text{J}\,\text{K}^{-1}\text{mol}^{-1}$ (so $C_p=C_v+R=29.11\ \text{J}\,\text{K}^{-1}\text{mol}^{-1}$). State A: $P_A=100$ kPa, $V_A=25$ L. Step 1 (isobaric) to state B: $P_B=100$ kPa, $V_B=100$ L. Step 2 (isochoric) to state C: $V_C=100$ L. Step 3 (isothermal) returns C→A, which fixes $T_C=T_A$.
Find. $q$, $w$ (on the system), $\Delta E\,(=\Delta U)$ and $\Delta H$ for each of the three steps and for the closed cycle.
Figure 1 — The A→B→C→A cycle in the P–V plane, drawn to the state values found in Step 1 below (isobar, isochor, then the $P=2500/V$ isotherm closing back to A).
Approach. Pin down every state's temperature and pressure from the ideal-gas law (using $T_C=T_A$ from Step 3's own description), then apply the standard constant-P, constant-V and isothermal-reversible work/heat relations leg by leg, and sum for the cycle.
State temperatures and $P_C$. $T_A=\dfrac{P_AV_A}{nR}=\dfrac{(100{,}000)(0.025)}{8.314}=300.7$ K; $T_B=\dfrac{P_BV_B}{nR}=\dfrac{(100{,}000)(0.100)}{8.314}=1202.8$ K. Step 3 returns isothermally to A, so $T_C=T_A=300.7$ K, and
$$P_C=\frac{nRT_C}{V_C}=\frac{(8.314)(300.7)}{0.100}=\boxed{25.0\ \text{kPa}}.$$
(c) Step 3 (C→A, isothermal, reversible). Ideal gas at constant $T$: $\Delta U=\Delta H=0$. Work done on the system during the reversible compression $V_C\to V_A$:
$$w=-nRT_C\ln\!\frac{V_A}{V_C}=-(8.314)(300.7)\ln\!\frac{25}{100}=-2500\ln(0.25)=\boxed{+3465.7\ \text{J}}.$$
Since $\Delta U=0$, $q=-w=\boxed{-3465.7\ \text{J}}$ (heat is rejected as the gas is compressed isothermally).
(d) The cycle. Summing the three legs, and separately confirming $\Delta U$ and $\Delta H$ close to zero because A→B→C→A returns to the identical starting state:
$$q_{cyc}=26{,}263.5-18{,}763.5-3465.7=\boxed{+4034.3\ \text{J}},\qquad w_{cyc}=-7500+0+3465.7=\boxed{-4034.3\ \text{J}},$$
$$\Delta U_{cyc}=\Delta H_{cyc}=\boxed{0}.$$
Check: $q_{cyc}+w_{cyc}=4034.3-4034.3=0=\Delta U_{cyc}$. ✓