Question 1 of 9: Ideal Regenerative Rankine Cycle — Closed + Open Feedwater Heaters, with Second-Law Efficiency
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 1: Ideal Regenerative Rankine Cycle — Closed + Open Feedwater Heaters, with Second-Law Efficiency (20 marks)
Given. Turbine inlet (state 8) $P=12.5$ MPa, $T=550\ ^\circ$C. First extraction
(state 9) at $P_{e1}=0.8$ MPa to the closed FWH; second extraction (state 10) at $P_{e2}=0.3$ MPa to
the open FWH; condenser (state 11 in, state 1 out) $P=10$ kPa. Closed-FWH feedwater exit (state 5):
$170\ ^\circ$C, 12.5 MPa. Closed-FWH drain (state 6) leaves as saturated liquid at 0.8 MPa and is
trapped (throttled) into the open FWH at state 7. Open-FWH exit (state 3): saturated liquid at 0.3
MPa. Ideal cycle: isentropic turbine stages and pumps. Net power $\dot W_{net}=150$ MW. Source
$T_H=1500$ K, sink $T_L=300$ K, dead-state $T_0=300$ K.
Fig. Q1 — T–s state points for the regenerative Rankine cycle
with closed + open feedwater heaters (2→3 and 6→7 are mixing/throttling steps drawn as
straight connectors for continuity rather than single-stream process lines).
Approach
Fix the turbine-inlet state and follow the isentrope through both extraction pressures and the
condenser pressure to get states 9, 10 and 11. Fix the two feedwater-heater exit/drain states from
the given temperatures and saturation conditions, pump each stream to its next pressure, then close
the closed-FWH energy balance for the extraction fraction $y$ and the open-FWH mixing balance for
$z$. Net specific work, mass flow rate, thermal efficiency and second-law efficiency follow directly.
Turbine-inlet state and isentropic expansion legs. State 8: $h_8=3476.51$ kJ/kg,
$s_8=6.6317$ kJ/kg·K. Following $s=s_8$ down to each pressure: $h_9=2755.03$ kJ/kg (0.8 MPa),
$h_{10}=2578.51$ kJ/kg (0.3 MPa), $h_{11}=2099.96$ kJ/kg (10 kPa).
Condenser exit and Pump I (1→2). Saturated liquid at 10 kPa:
$h_1=191.81$ kJ/kg, $s_1=0.6492$ kJ/kg·K. Pumped isentropically to 0.3 MPa: $h_2=192.10$ kJ/kg.
Open FWH exit and Pump II (3→4). Saturated liquid at 0.3 MPa:
$h_3=561.43$ kJ/kg, $s_3=1.6717$ kJ/kg·K. Pumped isentropically to 12.5 MPa: $h_4=574.48$ kJ/kg.
Closed-FWH states. Feedwater exit (state 5, given): $170\ ^\circ$C, 12.5 MPa
⇒ $h_5=725.60$ kJ/kg. Drain (state 6), saturated liquid at 0.8 MPa: $h_6=720.86$ kJ/kg; trapped
(isenthalpic) into the open FWH, $h_7=h_6=720.86$ kJ/kg.
Closed-FWH energy balance ⇒ extraction fraction $y$. Tube-side feedwater
($\dot m=1$, normalized) rises from $h_4$ to $h_5$; the extraction-steam stream $y$ condenses from $h_9$ to
$h_6$:
$$y(h_9-h_6)=(h_5-h_4)\ \Rightarrow\ y=\frac{725.60-574.48}{2755.03-720.86}=\boxed{0.07429}.$$
Open-FWH mixing balance ⇒ extraction fraction $z$. The open FWH mixes
extraction $z$ (at $h_{10}$), the trapped closed-FWH drain $y$ (at $h_7$), and the remaining
$(1-y-z)$ from Pump I (at $h_2$), to leave as saturated liquid at $h_3$:
$$z\,h_{10}+y\,h_7+(1-y-z)h_2=h_3$$
$$z=\frac{h_3-h_2+y(h_2-h_7)}{h_{10}-h_2}=\frac{561.43-192.10+0.07429\times(192.10-720.86)}{2578.51-192.10}=\boxed{0.13830}.$$
Turbine and pump work, net specific work (part a).
$$w_{turb}=(h_8-h_9)+(1-y)(h_9-h_{10})+(1-y-z)(h_{10}-h_{11})=1261.71\ \text{kJ/kg}.$$
$$w_{pI}=(1-y-z)(h_2-h_1)=0.231\ \text{kJ/kg},\qquad w_{pII}=h_4-h_3=13.055\ \text{kJ/kg}.$$
$$w_{net}=w_{turb}-w_{pI}-w_{pII}=1261.71-0.23-13.06=\boxed{1248.42\ \text{kJ/kg}}.$$
Mass flow rate entering the first-stage turbine (part b).
$$\dot m=\frac{\dot W_{net}}{w_{net}}=\frac{150{,}000\ \text{kW}}{1248.42\ \text{kJ/kg}}\times3600\ \text{s/h}=\boxed{432{,}547\ \text{kg/h}}.$$
Thermal efficiency (part c). Heat is added only in the boiler, $q_{in}=h_8-h_5$:
$$q_{in}=3476.51-725.60=2750.92\ \text{kJ/kg},\qquad \eta_{th}=\frac{w_{net}}{q_{in}}=\frac{1248.42}{2750.92}=\boxed{0.4538\ (45.4\%)}.$$
Second-law (exergy) efficiency (part d). Modeling the heat addition as supplied
from a source at $T_H=1500$ K, the exergy content of $q_{in}$ is
$$x_{in}=q_{in}\left(1-\frac{T_0}{T_H}\right)=2750.92\times\left(1-\frac{300}{1500}\right)=2200.73\ \text{kJ/kg}.$$
$$\eta_{II}=\frac{w_{net}}{x_{in}}=\frac{1248.42}{2200.73}=\boxed{0.5673\ (56.7\%)}.$$