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04-BS-10 · May 2015

Question 8 of 9: Air-Standard 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 2015. 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, air, N₂, CO₂) were computed from high-accuracy equations of state in place of printed property-table interpolation; every boxed numeric result.

Question 8: Air-Standard 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. $P_1=100$ kPa, $T_1=290$ K, $V_1=400$ cm$^3=4\times10^{-4}$ m$^3$. $T_3=2200$ K (max). Compression ratio $r=8$. Ideal air-standard Otto cycle, variable specific heats.

Find. (a) $Q_{in}$ [kJ]; (b) $W_{net}$ [kJ]; (c) $\eta_{th}$; (d) MEP [kPa].

Approach

Find the actual air mass trapped in the cylinder from the ideal-gas law at state 1, then use variable-specific-heat root-finding (the isentropic relation $s^\circ(T_2)-s^\circ(T_1)=R\ln[(T_2/T_1)(v_1/v_2)]=0$) to fix both isentropic states 2 and 4. Internal energies at all four states give the heat addition, heat rejection, and net work directly; converting to total (not per-mass) quantities and dividing by the displacement volume gives the mean effective pressure.

  1. Trapped mass. $$m=\frac{P_1V_1}{RT_1}=\frac{100{,}000\times4\times10^{-4}}{287\times290}=\boxed{4.806\times10^{-4}\ \text{kg}}.$$
  2. Isentropic compression (1→2) and expansion (3→4). Root-solving the variable-cp isentropic condition for compression ratio $r=8$: $T_2=651.59$ K ($u_2=600.85$ kJ/kg); for the expansion leg ($v$-ratio $=1/8$ from $T_3=2200$ K): $T_4=1159.21$ K ($u_4=1023.58$ kJ/kg). Also $u_1=333.03$ kJ/kg (at $T_1=290$ K), $u_3=1998.06$ kJ/kg (at $T_3=2200$ K).
  3. Heat addition (part a). Constant-volume heat addition 2→3: $$q_{in}=u_3-u_2=1998.06-600.85=1397.21\ \text{kJ/kg},\qquad Q_{in}=m\,q_{in}=4.806\times10^{-4}\times1397.21=\boxed{0.6715\ \text{kJ}}.$$
  4. Heat rejection and net work (part b). Constant-volume rejection 4→1: $$q_{out}=u_4-u_1=1023.58-333.03=690.55\ \text{kJ/kg},\qquad w_{net}=q_{in}-q_{out}=706.66\ \text{kJ/kg}.$$ $$W_{net}=m\,w_{net}=4.806\times10^{-4}\times706.66=\boxed{0.3396\ \text{kJ}}.$$
  5. Thermal efficiency (part c). $$\eta_{th}=\frac{w_{net}}{q_{in}}=\frac{706.66}{1397.21}=\boxed{0.5058\ (50.6\%)}.$$
  6. Mean effective pressure (part d). Displacement volume $V_d=V_1(1-1/r)=4\times10^{-4}\times0.875=3.5\times10^{-4}$ m$^3$: $$\text{MEP}=\frac{W_{net}}{V_d}=\frac{0.3396}{3.5\times10^{-4}}=\boxed{970.3\ \text{kPa}}.$$
QuantityResult
(a) $Q_{in}$0.6715 kJ
(b) $W_{net}$0.3396 kJ
(c) $\eta_{th}$0.5058 (50.6%)
(d) MEP970.3 kPa