Question 7 of 9: Charging a Rigid Tank from a Supply Line (R-134a)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exam 04-BS-10, Thermodynamics — May 2013. 3 hours, Closed-Book Exam (approved
calculator and one double-sided 8.5x11-inch aid sheet permitted). 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. 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 7: Charging a Rigid Tank from a Supply Line (R-134a) (15 marks)
Given. Rigid tank, $V=0.2$ m³. Initial state: $T_1=8\ ^\circ\text{C}$, quality $x_1=0.6$ (60% vapor by mass). Supply line: $P_{line}=1$ MPa, $T_{line}=120\ ^\circ\text{C}$ (superheated). Filling stops when tank pressure reaches 800 kPa with the tank contents entirely vapor (i.e. the final state is saturated vapor at 800 kPa — the instant the last liquid droplet flashes away).
Find. (a) final tank temperature $T_2$; (b) mass of refrigerant $m_{in}$ that entered; (c) heat transfer $Q$ between the tank and its surroundings during filling.
Approach
This is an unsteady (transient) uniform-flow first-law problem on a closed control volume with one inlet and no exit: $m_2u_2-m_1u_1=Q+m_{in}h_{line}$ (no boundary work, rigid tank). Fix state 1 (given $T_1,x_1$) and state 2 (saturated vapor at the stated final pressure) to get $m_1,m_2,u_1,u_2$ from $V$ and the specific volumes, then $m_{in}=m_2-m_1$ and $Q$ follow directly from the energy balance.
Initial state 1. At $T_1=8\ ^\circ\text{C}$, $x_1=0.6$: $P_1=387.61$ kPa, $v_1=0.031998$ m³/kg, $u_1=313.85$ kJ/kg.
$$m_1=\frac{V}{v_1}=\frac{0.2}{0.031998}=6.2504\ \text{kg}.$$
Final state 2 — saturated vapor at 800 kPa (part a).
$$\boxed{T_2=T_{sat}(800\ \text{kPa})=31.33\ ^\circ\text{C}},\qquad v_2=0.025625\ \text{m}^3/\text{kg},\qquad u_2=394.96\ \text{kJ/kg}.$$
$$m_2=\frac{V}{v_2}=\frac{0.2}{0.025625}=7.8050\ \text{kg}.$$
Mass entered (part b).
$$m_{in}=m_2-m_1=7.8050-6.2504=\boxed{1.5546\ \text{kg}}.$$
Supply-line enthalpy. At 1 MPa, 120°C: $h_{line}=504.21$ kJ/kg.
Heat transfer (part c). Unsteady-flow energy balance on the tank (rigid, no boundary work, one inlet, no exit):
$$Q=(m_2u_2-m_1u_1)-m_{in}h_{line}=\left[7.8050(394.96)-6.2504(313.85)\right]-1.5546(504.21)$$
$$Q=\boxed{337.1\ \text{kJ}}\ (\text{positive}\Rightarrow\text{heat is transferred }\mathit{into}\text{ the tank from the surroundings}).$$