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04-BS-10 · May 2015

Question 9 of 9: Rigid Tank Charged from a Steam Supply Line

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 9: Rigid Tank Charged from a Steam Supply Line (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. Rigid tank, $m_1=0.5$ kg at $700$ kPa, $320\ ^\circ$C (initial). Supply line: constant $1.5$ MPa, $320\ ^\circ$C. Final tank state: $1.0$ MPa, $320\ ^\circ$C.

Find. (a) $m_2$; (b) $Q$.

Approach

The tank volume is fixed, so the initial specific volume (from the given initial state) fixes the tank volume, and the final specific volume (from the given final state) then gives the final mass directly. The unsteady-flow energy balance for a charging process ($m_2u_2-m_1u_1=Q+\dot m_{in}h_{line}$, with no work crossing the rigid boundary) then isolates the heat transfer, using the supply line's own enthalpy (not internal energy) for the entering mass since flow work at the valve is real.

  1. Tank volume and initial/final specific volumes. At $700$ kPa, $320\ ^\circ$C: $v_1=0.38523$ m$^3$/kg, $u_1=2831.68$ kJ/kg. Tank volume: $$V=m_1v_1=0.5\times0.38523=0.19261\ \text{m}^3.$$ At $1.0$ MPa, $320\ ^\circ$C: $v_2=0.26786$ m$^3$/kg, $u_2=2826.50$ kJ/kg.
  2. Final mass (part a). $$m_2=\frac{V}{v_2}=\frac{0.19261}{0.26786}=\boxed{0.7191\ \text{kg}}.$$
  3. Supply-line enthalpy and entering mass. At the line condition ($1.5$ MPa, $320\ ^\circ$C): $h_{line}=3082.43$ kJ/kg. Entering mass $m_{in}=m_2-m_1=0.7191-0.5=0.2191$ kg.
  4. Heat transfer (part b). Unsteady energy balance, rigid tank (no boundary work): $$Q=(m_2u_2-m_1u_1)-m_{in}h_{line}$$ $$=(0.7191\times2826.50-0.5\times2831.68)-(0.2191\times3082.43)$$ $$=(2032.32-1415.84)-675.15=\boxed{-58.66\ \text{kJ}}.$$ Negative sign: heat is transferred from the steam in the tank to the surroundings.
QuantityResult
(a) $m_2$0.7191 kg
(b) $Q$−58.66 kJ (heat OUT of the tank)
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