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Modern Engineering Thermodynamics

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11.7 Constructing Tables and Charts 379<br />

Curve fit 2: p = pðv, TÞðfor superheated and saturated vaporÞ<br />

Curve fit 3: v f = v f ðT sat Þ<br />

Curve fit 4: c 0 v = c0 v ðTÞðfor superheated and saturated vaporÞ (11.31d)<br />

(11.31b)<br />

(11.31c)<br />

C. If a very low-pressure reference state (p 0 , v 0 , T 0 ) is chosen such that ðc v Þ 0 = c 0 v , then Eqs. (11.19), (3.17), and<br />

(11.24) are used to calculate values for u, h, and s relative to this reference state as<br />

Z T Z v<br />

<br />

u = u 0 + c 0 v dT + T ∂p<br />

T 0 v 0<br />

∂T<br />

<br />

− p<br />

v<br />

<br />

dv (11.32)<br />

h = u + pv (3.17)<br />

and<br />

s = s 0 +<br />

Z T<br />

T 0<br />

<br />

c 0 <br />

v<br />

dT +<br />

T<br />

Z v<br />

v 0<br />

<br />

∂p<br />

∂T<br />

<br />

dv (11.33)<br />

v<br />

where u 0 and s 0 are the internal energy and entropy values of the reference state. Note that these reference<br />

state properties always cancel out in a typical internal energy change (u 2 – u 1 ) or entropy change (s 2 – s 1 )<br />

calculation, so their values can be arbitrarily chosen and need not be made known to the user of the table<br />

or chart. Typically u 0 and s 0 are chosen so as to make h f and s f zero at the reference temperature T 0 , and T 0 is<br />

often taken to be the triple point temperature (see, for example, the first row of values for water in Table C.1a),<br />

because the triple point is a well-defined and easily reproducible reference state. Therefore, u 0 and s 0 are seldom<br />

chosen to be zero themselves. The generation of the tables can now be carried out as follows.<br />

11.7.1 Saturation tables<br />

A temperature entry saturation table can be constructed as follows:<br />

1. A temperature T = T sat is chosen at which the properties are to be determined.<br />

2. Next, p sat is calculated from Eq. (11.31a).<br />

3. Equation (11.31b), which must be valid for saturated vapor as well as superheated vapor, is used to<br />

calculate v g at these p sat and T sat values.<br />

4. Chose a reference temperature T o and assign arbitrary values to u o and s o .<br />

5. The expression for (dp/dT) sat is determined by differentiating Eq. (11.31a). 3 The values of u g , h g , and s g are<br />

then calculated from Eqs. (11.32), (3.17), and (11.33) by setting (∂p/∂T) v = (dp/dT) sat .<br />

6. Equation (11.31c) is used to calculate v fg = v g – v f at the T sat value.<br />

7. The remaining saturated liquid properties are determined from the Clapeyron and Gibbs Eqs. (11.17) and<br />

(11.10) as follows:<br />

<br />

dp<br />

h f = h g − h fg = h g − T sat v fg<br />

dT<br />

and<br />

sat<br />

u f = u g − u fg = u g − ðh fg − p sat v fg Þ<br />

s f = s g − s fg = s g − h fg /T sat<br />

This sequence of operations is repeated for a variety of T sat values, and the compilation of all these results<br />

gives a temperature entry saturation table like Table C.1a or C.1b in Thermodynamic Tables to accompany<br />

<strong>Modern</strong> <strong>Engineering</strong> <strong>Thermodynamics</strong>.<br />

Beginning the calculation sequence with a p = p sat value and calculating the corresponding T sat value<br />

from Eq. (11.31a) and continuing as just described produces a pressure entry saturation table like<br />

Table C.2a or C.2b.<br />

3 Note that Eq. (11.31b) should yield the same values of p sat and T sat as Eq (11.31a). However, they both are both empirical equations<br />

and may not yield the same values of (dp/dT) sat . In this case, Eq. (11.31a) is preferable.

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