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04-BS-10 · May 2016

Question 4 of 9: Ideal Otto Cycle, Variable Specific Heats

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 4: Ideal Otto Cycle, Variable 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. Compression ratio $r=8$. $T_1=310$ K (BDC, minimum), $T_3=1600$ K (after combustion, maximum). Constant volume heat addition/rejection; variable specific heats for air.

Find. (a) $q_{in}$ [kJ/kg]; (b) $w_{net}$ [kJ/kg]; (c) $\eta_{th}$.

Approach

With variable specific heats, the isentropic compression/expansion legs are solved using the ideal-gas relative-specific-volume function $v_r(T)=T\,e^{-s^\circ(T)/R}$, for which $v_2/v_1=v_r(T_2)/v_r(T_1)$ exactly along any isentrope — this replaces the constant-$k$ formula $T_2=T_1r^{k-1}$. Internal energies at each of the four corner states then give the two heat-transfer legs directly.

  1. Isentropic compression (1→2), $v_1/v_2=r=8$. Solving $v_r(T_2)=v_r(T_1)/8$ by root-finding gives $T_2=692.86$ K. Internal energies: $u_1=347.40$ kJ/kg, $u_2=633.08$ kJ/kg.
  2. Heat addition (2→3, constant volume) — part (a). $u_3=1424.59$ kJ/kg at $T_3=1600$ K. $$q_{in}=u_3-u_2=1424.59-633.08=\boxed{791.50\ \text{kJ/kg}}.$$
  3. Isentropic expansion (3→4), $v_4/v_3=r=8$. Solving $v_r(T_4)=v_r(T_3)\times8$ gives $T_4=809.88$ K, $u_4=726.72$ kJ/kg.
  4. Heat rejection (4→1, constant volume). $$q_{out}=u_4-u_1=726.72-347.40=379.32\ \text{kJ/kg}.$$
  5. Net work (part b). $$w_{net}=q_{in}-q_{out}=791.50-379.32=\boxed{412.18\ \text{kJ/kg}}.$$
  6. Thermal efficiency (part c). $$\eta_{th}=\frac{w_{net}}{q_{in}}=\frac{412.18}{791.50}=\boxed{0.5208\ (52.1\%)}.$$ For comparison, the constant-cold-air-standard result $\eta_{th}=1-r^{1-k}=1-8^{-0.4}=0.5647$ overstates the true efficiency, since variable specific heats rise with temperature and thus reduce the effective temperature ratio's leverage on efficiency.
QuantityResult
(a) $q_{in}$791.50 kJ/kg
(b) $w_{net}$412.18 kJ/kg
(c) $\eta_{th}$0.5208 (52.1%)