Question 7 of 9: Adiabatic Steam Turbine, Efficiency from a Measured Work Output
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exam 04-BS-10, Thermodynamics — May 2016. 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). 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, CO₂,
moist air) were computed from high-accuracy equations of state in place of printed property-table interpolation; every boxed numeric result.
Question 7: Adiabatic Steam Turbine, Efficiency from a Measured Work Output (15 marks)
Fix the inlet state, then find the isentropic exit enthalpy at 20 kPa from the inlet entropy to
get the isentropic (maximum possible) work. The isentropic efficiency is the ratio of the actual
measured work to that isentropic work. The actual exit enthalpy follows directly from the actual
work by an energy balance, which fixes the actual exit state (and its entropy, for the
reversibility check).
Inlet state. At 1.0 MPa, 320°C: $h_1=3094.36$ kJ/kg, $s_1=7.1979$
kJ/kg·K.
Isentropic exit and efficiency (part a). At 20 kPa with $s_{2s}=s_1=7.1979$
kJ/kg·K, the exit is wet: $h_{2s}=2372.59$ kJ/kg, giving isentropic work
$w_s=h_1-h_{2s}=3094.36-2372.59=721.78$ kJ/kg.
$$\eta_t=\frac{w_{actual}}{w_s}=\frac{630}{721.78}=\boxed{0.8728\ (87.3\%)}.$$
Actual exit state (parts b, c). Energy balance on the adiabatic turbine:
$$h_2=h_1-w_{actual}=3094.36-630=2464.36\ \text{kJ/kg}.$$
At 20 kPa, $h_f=251.42$ kJ/kg and $h_g=2608.94$ kJ/kg, so $h_2$ lies between them — a two-phase
mixture, with $T_2=T_{sat}(20\ \text{kPa})=\boxed{60.06\ ^\circ\text{C}}$ and
$$x_2=\frac{h_2-h_f}{h_g-h_f}=\frac{2464.36-251.42}{2608.94-251.42}=\boxed{0.9387}.$$
Reversibility check (part d). Entropy at the actual exit state:
$s_2=s_f+x_2 s_{fg}=7.4733$ kJ/kg·K. Since $s_2=7.4733>s_1=7.1979$ kJ/kg·K, entropy
increased across this adiabatic turbine, so
$$\boxed{\text{the process is irreversible}}$$
(consistent with $\eta_t=87.3\%<100\%$ — a truly reversible adiabatic turbine would be
isentropic, $s_2=s_1$, and would achieve $\eta_t=100\%$).