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04-BS-10 · May 2014

Question 7 of 9: Insulated Steam Turbine — Isentropic Efficiency from Given Actual Work

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

National Exam 04-BS-10, Thermodynamics — May 2014. 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). 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 (R-134a, water/steam, moist air, N₂, O₂, air) were computed from high-accuracy equations of state in place of printed property-table interpolation; every boxed numeric result.

Question 7: Insulated Steam Turbine — Isentropic Efficiency from Given Actual Work (15 marks)

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. $P_1=1.0$ MPa, $T_1=320\ ^\circ$C, $\dot m=10$ kg/s, $P_2=20$ kPa, $w_{actual}=630$ kJ/kg. Adiabatic (insulated), steady-state, steady-flow.

Find. (a) $\eta_t$; (b) $T_2$; (c) $x_2$; (d) reversible or not?

Approach

Fix the inlet state, follow the isentrope to the exit pressure to get the ideal exit enthalpy and isentropic work, then compare with the given actual work to get the isentropic efficiency directly. Back out the actual exit enthalpy from the actual work, locate it on the 20 kPa isobar (checking whether it falls in the two-phase dome), and compare actual and inlet entropy to assess reversibility.

  1. Inlet state. $P_1=1.0$ MPa, $T_1=320\ ^\circ$C (superheated): $$h_1=3094.36\ \text{kJ/kg},\qquad s_1=7.1979\ \text{kJ/kg}\cdot\text{K}.$$
  2. Isentropic exit state and isentropic work. At $P_2=20$ kPa with $s_{2s}=s_1$: $$h_{2s}=2372.59\ \text{kJ/kg},\qquad w_s=h_1-h_{2s}=3094.36-2372.59=721.78\ \text{kJ/kg}.$$
  3. Isentropic efficiency (part a). $$\eta_t=\frac{w_{actual}}{w_s}=\frac{630}{721.78}=\boxed{0.8728\ (87.3\%)}.$$
  4. Actual exit state. $h_2=h_1-w_{actual}=3094.36-630=2464.36$ kJ/kg. At 20 kPa, $h_f=251.42$ kJ/kg and $h_g=2608.94$ kJ/kg, so $h_f
  5. Exit quality (part c). $$x_2=\frac{h_2-h_f}{h_g-h_f}=\frac{2464.36-251.42}{2608.94-251.42}=\boxed{0.9387\ (93.87\%)}.$$
  6. Reversibility (part d). Exit entropy at $(P_2,x_2)$: $s_2=7.4733$ kJ/kg·K. Since the turbine is adiabatic ($q=0$), any entropy generation shows up directly as $\Delta s>0$: $$s_2-s_1=7.4733-7.1979=0.2754\ \text{kJ/kg}\cdot\text{K}>0\ \Rightarrow\ \boxed{\text{not reversible}}.$$ This is consistent with $\eta_t=87.3\%<100\%$: any isentropic efficiency below unity in an adiabatic device is itself proof of internal irreversibility (friction, flow separation in the blading, etc.).
QuantityResult
(a) $\eta_t$0.8728 (87.3%)
(b) $T_2$60.06°C (saturation temp. at 20 kPa)
(c) $x_2$0.9387 (93.87%)
(d) Reversible?No — $s_2 > s_1$ ($\Delta s=0.2754$ kJ/kg·K)