Question 2 of 7: The Reversible Adiabatic (Isentropic) Ideal-Gas Process
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 2: The Reversible Adiabatic (Isentropic) Ideal-Gas Process (20 marks)
Find. (a) Show $P_iV_i^{\gamma}=P_fV_f^{\gamma}$. (b) $T_2$ after the adiabatic expansion.
Approach. Combine the first law (adiabatic, $\delta q=0$) with the ideal-gas equation of state to get a separable relation between $T$ and $V$; integrate, then substitute $T=PV/nR$ to re-express purely in $P$ and $V$. Part (b) reuses the same derivation with $V$ eliminated instead, giving the direct $T$–$P$ form.
(a) First law, adiabatic. $\delta q=0\Rightarrow dU=\delta w_{on}=-PdV$ (reversible). With $dU=nC_vdT$ (ideal gas, $C_v$ constant) and $P=nRT/V$ (ideal-gas law):
$$nC_v\,dT=-\frac{nRT}{V}dV\ \Longrightarrow\ C_v\frac{dT}{T}=-R\frac{dV}{V}.$$
Integrate between the initial and final states.
$$C_v\ln\frac{T_f}{T_i}=-R\ln\frac{V_f}{V_i}\ \Longrightarrow\ \left(\frac{T_f}{T_i}\right)^{C_v}=\left(\frac{V_i}{V_f}\right)^{R}.$$
Eliminate $T$ using $T=PV/(nR)$. $\dfrac{T_f}{T_i}=\dfrac{P_fV_f}{P_iV_i}$, so
$$\left(\frac{P_f}{P_i}\right)^{C_v}\left(\frac{V_f}{V_i}\right)^{C_v}=\left(\frac{V_i}{V_f}\right)^{R}\ \Longrightarrow\ \left(\frac{P_f}{P_i}\right)^{C_v}=\left(\frac{V_i}{V_f}\right)^{R+C_v}=\left(\frac{V_i}{V_f}\right)^{C_p}$$
using $R+C_v=C_p$. Raising both sides to the power $1/C_v$ and writing $\gamma=C_p/C_v$:
$$\frac{P_f}{P_i}=\left(\frac{V_i}{V_f}\right)^{\gamma}\ \Longrightarrow\ \boxed{P_iV_i^{\gamma}=P_fV_f^{\gamma}}.\ \blacksquare$$
(b) The equivalent T–P form. Eliminating $V$ instead of $P$ from the same two starting relations gives, by the identical steps,
$$\left(\frac{T_f}{T_i}\right)^{C_p}=\left(\frac{P_f}{P_i}\right)^{R}\ \Longrightarrow\ T_f=T_i\left(\frac{P_f}{P_i}\right)^{R/C_p}.$$
Here $C_v=C_p-R=28.9-8.314=20.586\ \text{J}\,\text{K}^{-1}\text{mol}^{-1}$, $\gamma=C_p/C_v=1.404$, and $R/C_p=8.314/28.9=0.2877$.
Substitute the numbers.
$$T_2=300\left(\frac{60}{80}\right)^{0.2877}=300(0.75)^{0.2877}=300(0.9206)=\boxed{276.2\ \text{K}}.$$
The gas cools on adiabatic expansion, as expected ($T_2