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
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
Quantity
Symbol
Part (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 mm
0.01 m3
Gas A pressure / final pressure
$P_A,\,P_2$
200 kPa
200 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 $W_{\text{ideal}}=mRT\ln(P_1/P_2)$.
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 $A_A-A_B=7.363\times10^{-3}\text{ m}^2$.
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 $P_B$:
$$P_B=\frac{P_A A_A + mg - P_o(A_A-A_B)}{A_B}$$
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
$$m=\frac{V_1}{v_1}=\frac{0.01}{0.12721}=0.07861\text{ kg}$$
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.
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.
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.