Question 8 of 9: Rigid Tank, N₂/O₂ Ideal-Gas Mixture
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Examinations — 04-BS-10, Thermodynamics. Three hours. Closed-book exam with one
8.5×11 in. double-sided sheet of notes allowed and an approved Casio or Sharp calculator;
property tables and charts are supplied and interpolation is not necessary — the closest tabular
value may be used. Part A: two of three 20-mark questions; Part B: four of six 15-mark questions.
Every question is answered in full.
Reference texts. Cengel & Boles, Thermodynamics: An Engineering
Approach, 8th ed. (Vapor Power Cycles Ch. 10; Gas Power Cycles Ch. 9; Refrigeration Cycles
Ch. 11; Gas Mixtures Ch. 13; Psychrometrics Ch. 14; Exergy Ch. 8).
Check — paper format. The paper is headed "National Examination – May 2019 / 04-BS-10, Thermodynamics, 3 Hours Duration": four question pages followed by a 22-page appendix of property tables and a psychrometric chart. All nine questions are answered in full (Part A questions 1–3 at 20 marks each, Part B questions 4–9 at 15 marks each; the paper asks for two of Part A and four of Part B). Two wording notes from the printed page: Question 2's final sub-part is printed "(d) the second law efficiency" after an earlier "(d)", i.e. the paper repeats the letter, and Question 3(d) is printed "in kJ/K" for a quantity that is a rate of exergy destruction in kJ/s.
Find. (a) mass fractions; (b) mole fractions; (c) partial pressures
(at state 1); (d) the mixture pressure; (e) $Q$ to reach $127\ ^\circ\text{C}$.
Approach
Mass fractions come directly from the given masses; converting each to moles ($n=m/M$) gives the
mole fractions. Each species' partial pressure follows from its own ideal-gas law using the shared
tank volume and temperature (Dalton's model). Heat transfer at constant volume uses the mixture's
mass-weighted $c_v$.
Mass fractions — part (a). $m_{tot}=0.7+1.1=1.8$ kg.
$$mf_{N_2}=\frac{0.7}{1.8}=\boxed{0.3889\ (38.9\%)},\qquad mf_{O_2}=\frac{1.1}{1.8}=\boxed{0.6111\ (61.1\%)}.$$
Partial pressures at state 1 — part (c). Each species occupies the full
tank volume at $T_1$ (Dalton's model), $R_i=\bar R/M_i$:
$$P_{N_2}=\frac{m_{N_2}R_{N_2}T_1}{V}=\frac{0.7\times0.2968\times300.15}{0.1}=\boxed{623.6\ \text{kPa}}$$
$$P_{O_2}=\frac{m_{O_2}R_{O_2}T_1}{V}=\frac{1.1\times0.2598\times300.15}{0.1}=\boxed{857.8\ \text{kPa}}$$
Mixture pressure — part (d). By Dalton's law the mixture pressure is the sum
of the partial pressures (equivalently $P=n_{tot}\bar RT_1/V=0.05936\times8.314\times300.15/0.1$):
$$P_{tot}=P_{N_2}+P_{O_2}=623.6+857.8=\boxed{1481.4\ \text{kPa}}.$$
Heat transfer to $127\ ^\circ$C — part (e). Constant volume, so all the
heat goes to raising internal energy; use the mass-weighted mixture $c_v$:
$$c_{v,mix}=mf_{N_2}c_{v,N_2}+mf_{O_2}c_{v,O_2}=0.3889\times0.743+0.6111\times0.658=0.6911\ \text{kJ/kg}\cdot\text{K}.$$
$$Q=m_{tot}\,c_{v,mix}(T_2-T_1)=1.8\times0.6911\times(400.15-300.15)=\boxed{124.4\ \text{kJ}}.$$