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Modern Engineering Thermodynamics

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15.5 Standard Reference State 603<br />

If moisture enters the combustion process as humidity in the inlet air, this moisture is carried through the<br />

reaction as an inert element and adds to the combustion water in the products. This has the net effect of raising<br />

the dew point temperature. This is illustrated in the next example.<br />

EXAMPLE 15.5<br />

During the automobile engine fuel combustion test discussed in Example 15.3, the dry bulb and wet bulb temperatures of<br />

the inlet air were measured to be 90.0°F and 75.0°F, respectively. Determine (a) the amount of water carried into the engine<br />

in the form of inlet humidity and (b) the new dew point temperature of the exhaust products. Assume the exhaust is at a<br />

total pressure of 14.7 psia.<br />

Solution<br />

From the psychrometric chart, Figure D.6a of Thermodynamic Tables to accompany <strong>Modern</strong> <strong>Engineering</strong> <strong>Thermodynamics</strong>, we find<br />

that, for T DB = 90°F andT WB = 76°F, the relative humidity ϕ = 50% and the humidity ratio, ω = (105 grains of H 2 O per lbm of<br />

dry air) × (1 lbm/7000. grains) = 0.0150 lbm H 2 O/lbm dry air. On a molar basis, the humidity ratio is<br />

ω = ð0:0150 lbm H 2 O/lbm dry airÞ = 0:0241 lbmole H 2 O/lbmole dry air<br />

<br />

28:97 lbm dry air/lbmole dry air<br />

18:016 lbm H 2 O/lbmole H 2 O<br />

From the balanced reaction equation of part a of Example 15.3, we find that the amount of dry air used per mole of fuel is<br />

21.9(1 + 3.76) = 104 moles, and this now carries with it 0.0241(104) = 2.51 moles of water. Assuming this water passes<br />

through the reaction unchanged, the total amount of water now in the exhaust is 9:00 + 2:51 = 11:5 moles per mole of fuel.<br />

Consequently, the total moles of product are 111.5, the mole fraction of water vapor in the exhaust is now<br />

χ H2O = n H2O<br />

= 11:5/111:5 = 0:103<br />

n total<br />

and Eq. (12.23) gives the partial pressure of the water vapor in the exhaust as<br />

p H2O = 0:103ð14:7Þ = 1:52 psia<br />

Again, interpolating in Table C.1a in Thermodynamic Tables to accompany <strong>Modern</strong> <strong>Engineering</strong> <strong>Thermodynamics</strong>, we find<br />

T sat ð1:52 psiaÞ = T DP = 116°F = 46:5°C<br />

Exercises<br />

13. What happens to the water vapor in the engine’s exhaust in Example 15.5 if the surrounding air temperature is 20.0°C?<br />

Answer: It condenses into liquid water, since the surrounding air temperature is less than the dew point temperature of<br />

the water vapor.<br />

14. If the inlet air in Example 15.5 contains 3.214 moles of water vapor per mole of fuel burned (instead of 2.50 moles of<br />

H 2 O per mole of fuel), determine the new dew point temperature. Answer: T DP = 118°F.<br />

15. If the inlet air in Example 15.5 has a relative humidity of 100.% and a dry bulb temperature of 90.0°F, what is the new<br />

exhaust dew point temperature? Answer: T DP = 123°F.<br />

<br />

By comparing the results of Examples 15.4 and 15.5, we see that combustion air with 50.0% relative humidity<br />

has a dew point temperature 7.6°F (4.2°C) higher than that of dry combustion air.<br />

15.5 STANDARD REFERENCE STATE<br />

Because we deal with a variety of elements and compounds in combustion reactions, it is necessary to define<br />

a common thermodynamic reference state for all these substances. Recall that, in developing the steam tables,<br />

we chose the triple point of water as the reference state and arbitrarily set the specific internal energy of<br />

liquid water equal to zero at that point. Therefore, the values of u and h in the steam tables are not the actual<br />

specific internal energies and enthalpies of steam, they are only relative values. This is sufficient, since most of<br />

our formulae use u 2 − u 1 or h 2 − h 1 for changes occurring within a system and the effect of the reference<br />

state cancels out in the subtraction process. In the case of the gas tables, we take 0 K and 1 atm as the<br />

thermodynamic reference state and arbitrarily set the specific internal energy equal to zero at this state. However,<br />

in the case of combustion processes, a more pragmatic thermodynamic reference state of 25.0°C and<br />

0.100 MPa (approximately 1 atm) is chosen. This is called the standard reference state (SRS) for combustion<br />

reactions. However, since most of the calorimeters used to study combustion processes are steady state, steady<br />

flow, open systems, it is more convenient to set the specific enthalpy rather than the specific internal energy of<br />

the elements equal to zero at this state.

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