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Modern Engineering Thermodynamics

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382 CHAPTER 11: More Thermodynamic Relations<br />

EXAMPLE 11.11 (Continued )<br />

33. Determine an expression for the specific entropy of the material in Example 11.11 in the superheated region. Answer:<br />

where B = B 1 – B 2 /T.<br />

s = s 0 +<br />

Z T<br />

c 0 Z v<br />

<br />

<br />

v<br />

T dT + ∂p<br />

= s 0 + c<br />

∂T<br />

v0 vdv 0 v ln T <br />

+ R ln v<br />

<br />

+ exp½BŠ 1 − B <br />

2 1<br />

T 0 v 0<br />

T v − 1 <br />

v 0<br />

T0<br />

11.9 GAS TABLES<br />

We now move from the region of the vapor dome and its immediate surroundings out into the region where<br />

the material behaves as an “ideal gas.” However, we need to incorporate the temperature dependence of the<br />

ideal gas’s specific heats.<br />

When the concept of an ideal gas was introduced in Chapter 3, it was noted that ideal gases generally do not<br />

have constant specific heats. Therefore, one of the simplest steps we can take to make the ideal gas equations<br />

more accurate is to take into account their temperature-dependent specific heats. This is what is done for you in<br />

Tables C.16 and C.17 in Thermodynamic Tables to accompany <strong>Modern</strong> <strong>Engineering</strong> <strong>Thermodynamics</strong>.<br />

The specific internal energy and enthalpy values listed in thegastablesaredetermined from an integration of<br />

Eqs. (3.37) and (3.40) by incorporating an accurate specific heat vs. temperature data curve fit as<br />

and<br />

Z T<br />

u = u o + c v dT<br />

T o<br />

Z T<br />

h = h o + c p dT<br />

T o<br />

where u o , h o ,andT o are the arbitrarily chosen reference state values, all of which are set equal to zero in these<br />

tables.<br />

Since the ideal gas specific entropy depends on more than just temperature, it is not listed in these tables. However,<br />

the temperature-dependent part of the specific entropy is listed as the ϕ function, where<br />

and, from Eq. (7.35), we have<br />

Z T<br />

ϕ = c p /T dT (11.34)<br />

T o<br />

Z T<br />

s = s o + ðc p /TÞdT − R ln ðp/p o Þ<br />

T o<br />

= s o + ϕ − R ln ðp/p o Þ<br />

(7.35)<br />

In the gas tables, s o and T o are both arbitrarily set equal to zero, and p o is set equal to 1 atm. As always, the arbitrarily<br />

chosen reference states for u, h, ands cancel out when we calculate the changes u 2 – u 1 , h 2 – h 1 , and s 2 – s 1 .<br />

Such changes are calculated directly from values taken from the gas tables for u and h, but the change in entropy<br />

is given by combining the previous equations as<br />

or an isentropic process, s 2 = s 1 ; Eq. (11.35) then gives<br />

s 2 − s 1 = ϕ 2 − ϕ 1 − R ln ðp 2 /p 1 Þ (11.35)<br />

ðϕ 2 − ϕ 1 Þ/R = ln ðp 2 /p 1 Þ = ln p 2p o<br />

= ln ðp r2 /p r1 Þ<br />

p 1 p o

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