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17-Phys-B6 Applied Thermodynamics and Heat Transfer · May 2016

Question 1 of 8: Stepped-Piston Force Balance; Isothermal Expansion of Saturated Steam

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. 98-Phys-B6 Applied Thermodynamics and Heat Transfer, National Examination May 2016 — a three-hour open-book examination; candidates are expected to bring both a thermodynamics text and a heat-transfer text to make use of the property tables and charts. A complete examination is five questions — either three from Part A (Thermodynamics, Q1–Q4) and two from Part B (Heat Transfer, Q5–Q8), or two from Part A and three from Part B — every question carrying equal value; all eight are solved below as a complete study set. Where the exam's own "state your assumptions" licence applies (Part A cold-air-standard properties in Question 3; the rectangular-case geometry read from the printed illustration in Question 7), the assumption is flagged explicitly in a check callout rather than hedged inside the answer.

Reference texts. Y. A. Çengel and M. A. Boles, Thermodynamics: An Engineering Approach, 8th ed. (ideal-gas processes, vapour power cycles, gas-turbine/Brayton cycles, vapour-compression refrigeration); F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (conduction with convective boundaries, internal/external convection correlations, natural convection, radiation exchange, cross-flow heat-exchanger effectiveness–NTU analysis).

Question 1: Stepped-Piston Force Balance; Isothermal Expansion of Saturated Steam

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. Part (a): a two-diameter piston separating gas A (top, 200 kPa) from gas B (bottom, unknown) with atmospheric air (100 kPa) acting on the annular shoulder exposed between the two cylinder bores; piston mass 10 kg, static equilibrium. Part (b): 0.01 m3 of saturated water vapour at 200°C expands at constant temperature to a final pressure of 200 kPa.

Given data
QuantitySymbolPart (a)Part (b)
Diameter A / initial temperature$D_A,\,T_1$100 mm$200\,{}^{\circ}\text{C}$
Diameter B / initial volume$D_B,\,V_1$25 mm0.01 m3
Gas A pressure / final pressure$P_A,\,P_2$200 kPa200 kPa
Atmospheric pressure$P_o$100 kPa—
Piston mass$m$10 kg—

[Figure not reproduced: Stepped piston connecting cylinders A and B, with atmospheric air acting on the exposed shoulder. See the official exam paper or the cited reference text.]

Fig. 1 — stepped piston (as printed): gas A above the wide face, gas B below the narrow face, atmospheric air on the exposed annular shoulder.

Find. (a) The gas pressure $P_B$ in cylinder B. (b) The boundary work $W$ done by the real steam during the isothermal expansion, and the percentage error of an ideal-gas estimate of the same work.

Approach. (a) Sum vertical forces on the piston in static equilibrium, with gas A and the piston weight acting down and gas B and atmospheric air (on the shoulder) acting up. (b) Use real steam properties (mass fixed from $V_1/v_1$) to trace the actual $T=200\,{}^{\circ}\text{C}$ isotherm from saturation down to 200 kPa and numerically integrate $W=m\int P\,dv$, then compare against the ideal-gas closed-form $W_{\text{ideal}}=mRT\ln(P_1/P_2)$.

  1. Areas of the two piston faces. $$A_A=\frac{\pi}{4}D_A^2=\frac{\pi}{4}(0.100\text{ m})^2=7.854\times10^{-3}\text{ m}^2,\qquad A_B=\frac{\pi}{4}D_B^2=\frac{\pi}{4}(0.025\text{ m})^2=4.909\times10^{-4}\text{ m}^2$$ The exposed shoulder (where atmospheric air pushes up on the piston) has area $A_A-A_B=7.363\times10^{-3}\text{ m}^2$.
  2. Force balance on the piston. Gas A presses down on the wide face and the weight acts down; gas B presses up on the narrow face and atmospheric air presses up on the shoulder: $$P_A A_A + mg = P_B A_B + P_o(A_A-A_B)$$ Solving for $P_B$: $$P_B=\frac{P_A A_A + mg - P_o(A_A-A_B)}{A_B}$$
  3. Substitute. $$P_B=\frac{(200{,}000)(7.854\times10^{-3}) + (10)(9.81) - (100{,}000)(7.363\times10^{-3})}{4.909\times10^{-4}}$$ $$P_B=\frac{1570.8+98.1-736.3}{4.909\times10^{-4}}=\frac{932.6}{4.909\times10^{-4}}\text{ Pa}$$ $$\boxed{P_B \approx 1900\text{ kPa} \;(1.90\text{ MPa})}$$
  4. State 1 (b): saturated vapour at 200°C. From steam tables/property data, $P_{\text{sat}}(200\,{}^{\circ}\text{C})=1554.9$ kPa and $v_1=v_g=0.12721\text{ m}^3/\text{kg}$, so the (fixed) mass is $$m=\frac{V_1}{v_1}=\frac{0.01}{0.12721}=0.07861\text{ kg}$$
  5. State 2: superheated at $200\,{}^{\circ}\text{C}$, 200 kPa. $v_2=1.08048\text{ m}^3/\text{kg}$, so $V_2=mv_2=0.08494\text{ m}^3$ — a large expansion at essentially constant mass.
  6. Real boundary work: integrate along the isotherm. The pressure–volume path is NOT a simple polytropic curve for real steam, so $W=m\int_{v_1}^{v_2}P\,dv$ is evaluated by tracing $v(P)$ at $T=200\,{}^{\circ}\text{C}$ from $P_1=1554.9$ kPa down to $P_2=200$ kPa (400 points) and integrating numerically: $$\boxed{W_{\text{actual}}\approx 35.3\text{ kJ}}$$ This is confirmed independently through the first law: $Q=mT_1(s_2-s_1)=41.9$ kJ and $W=Q-m(u_2-u_1)$ reproduce the same 35.3 kJ to three figures.
  7. Ideal-gas comparison, same $m$, $T$, endpoints. For an ideal gas undergoing the same isothermal process, $W_{\text{ideal}}=mRT\ln(P_1/P_2)$ with $R_{\text{water}}=8.3145/18.015=0.4615\text{ kJ/kg}\cdot\text{K}$: $$W_{\text{ideal}}=(0.07861)(0.4615)(473.15)\ln\!\left(\frac{1554.9}{200}\right)=35.2\text{ kJ}$$ $$\text{error}=\frac{W_{\text{ideal}}-W_{\text{actual}}}{W_{\text{actual}}}\times100\%=\boxed{-0.4\%}$$

The error is surprisingly small even though state 1 (saturated vapour) itself deviates from ideal-gas behaviour by about 10% (compressibility $Z_1\approx0.90$). Most of the volume swept during the expansion happens at the LOW-pressure end of the path, where the steam is far into the superheated region and nearly ideal ($Z_2\approx0.99$); that low-pressure portion dominates the work integral and pulls the aggregate error down to well under 1%, even though a single-state comparison at $P_1$ alone would suggest a much bigger discrepancy.

Question 1 — results
QuantityValue
(a) Gas pressure in cylinder B, $P_B$≈ 1900 kPa (1.90 MPa)
(b) Mass of steam, $m$0.07861 kg
(b) Actual boundary work, $W_{\text{actual}}$35.3 kJ
(b) Ideal-gas boundary work, $W_{\text{ideal}}$35.2 kJ
(b) Error of the ideal-gas estimate−0.4%
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