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04-BS-10 · May 2018

Question 7 of 9: Simple Brayton Cycle, Constant Specific Heats

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

Notes on this paper

National Exam 04-BS-10, Thermodynamics — May 2018. 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, H₂, humid air) were computed from high-accuracy equations of state in place of printed property-table interpolation; every boxed numeric result.

Question 7: Simple Brayton Cycle, Constant Specific Heats (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. $T_1=310$ K (compressor inlet), $T_3=900$ K (turbine inlet), $r_p=P_2/P_1=8$, $\dot m=460$ kg/s, $\eta_c=0.80$, $\eta_t=0.86$. Constant specific heats at room temperature: $c_p=1.005$ kJ/kg·K, $k=1.4$. Simple (non-regenerative) cycle.

Find. $\dot W_{net}$ [MW].

Approach

With constant specific heats the isentropic temperature ratios reduce to closed-form power-law expressions in $r_p$; compute the isentropic compressor/turbine work directly, divide/multiply by the respective isentropic efficiencies to get actual work, and take the difference weighted by the mass flow rate.

  1. Isentropic compressor exit and actual work. $$T_{2s}=T_1\,r_p^{(k-1)/k}=310\times8^{0.2857}=\boxed{561.6\ \text{K}}.$$ $$w_{c,s}=c_p(T_{2s}-T_1)=1.005\times(561.6-310)=252.8\ \text{kJ/kg}.$$ $$w_{c,a}=\frac{w_{c,s}}{\eta_c}=\frac{252.8}{0.80}=\boxed{316.0\ \text{kJ/kg}}.$$
  2. Isentropic turbine exit and actual work. $$T_{4s}=\frac{T_3}{r_p^{(k-1)/k}}=\frac{900}{8^{0.2857}}=\boxed{496.8\ \text{K}}.$$ $$w_{t,s}=c_p(T_3-T_{4s})=1.005\times(900-496.8)=405.2\ \text{kJ/kg}.$$ $$w_{t,a}=\eta_t\,w_{t,s}=0.86\times405.2=\boxed{348.5\ \text{kJ/kg}}.$$
  3. Net specific work and net power output. $$w_{net}=w_{t,a}-w_{c,a}=348.5-316.0=32.4\ \text{kJ/kg}.$$ $$\dot W_{net}=\dot m\,w_{net}=460\times32.4=14{,}924\ \text{kW}=\boxed{14.9\ \text{MW}}.$$
QuantityResult
$\dot W_{net}$14.9 MW