Combution

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CHAPTER 3

FUELS AND COMBUSTION

3.1 Introduction to Combustion

Combustion Basics

The last chapter set forth the basics of the Rankine cycle and the principles of operation
of steam cycles of modern steam power plants. An important aspect of power
generation involves the supply of heat to the working fluid, which in the case of steam
power usually means turning liquid water into superheated steam. This heat comes from
an energy source. With the exception of nuclear and solar power and a few other exotic
sources, most power plants are driven by a chemical reaction called combustion, which
usually involves sources that are compounds of hydrogen and carbon. Process
industries, businesses, homes, and transportation systems have vast heat requirements
that are also satisfied by combustion reactions. The subject matter of this chapter
therefore has wide applicability to a variety of heating processes.

Combustion is the conversion of a substance called a fuel into chemical compounds
known as products of combustion by combination with an oxidizer. The combustion
process is an exothermic chemical reaction, i.e., a reaction that releases energy as it
occurs. Thus combustion may be represented symbolically by:

Fuel + Oxidizer Y Products of combustion + Energy

Here the fuel and the oxidizer are reactants, i.e., the substances present before the
reaction takes place. This relation indicates that the reactants produce combustion
products and energy. Either the chemical energy released is transferred to the
surroundings as it is produced, or it remains in the combustion products in the form of
elevated internal energy (temperature), or some combination thereof.
Fuels are evaluated, in part, based on the amount of energy or heat that they
release per unit mass or per mole during combustion of the fuel. Such a quantity is
known as the fuel's heat of reaction or heating value.
Heats of reaction may be measured in a calorimeter, a device in which chemical
energy release is determined by transferring the released heat to a surrounding fluid.
The amount of heat transferred to the fluid in returning the products of combustion to
their initial temperature yields the heat of reaction.

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In combustion processes the oxidizer is usually air but could be pure oxygen, an
oxygen mixture, or a substance involving some other oxidizing element such as
fluorine. Here we will limit our attention to combustion of a fuel with air or pure
oxygen.
Chemical fuels exist in gaseous, liquid, or solid form. Natural gas, gasoline, and
coal, perhaps the most widely used examples of these three forms, are each a complex
mixture of reacting and inert compounds. We will consider each more closely later in
the chapter. First let's review some important fundamentals of mixtures of gases, such
as those involved in combustion reactions.

Mass and Mole Fractions

The amount of a substance present in a sample may be indicated by its mass or by the
number of moles of the substance. A mole is defined as the mass of a substance equal to
its molecular mass or molecular weight. A few molecular weights commonly used in
combustion analysis are tabulated below. For most combustion calculations, it is
sufficiently accurate to use integer molecular weights. The error incurred may easily be
evaluated for a given reaction and should usually not be of concern. Thus a gram-mole
of water is 18 grams, a kg-mole of nitrogen is 28 kg, and a pound-mole of sulfur is 32
lbm.
_____________________________________________________________________
Molecule Molecular Weight
-------------------------------------------
C 12
N2 28
O2 32
S 32
H2 2
_____________________________________________________________________

The composition of a mixture may be given as a list of the fractions of each of the
substances present. Thus we define the mass fraction, of a component i, mfi, as the
ratio of the mass of the component, mi, to the mass of the mixture, m:

mfi = mi /m

It is evident that the sum of the mass fractions of all the components must be 1. Thus

mf1 + mf2 + ... = 1

Analogous to the mass fraction, we define the mole fraction of component i, xi, as
the ratio of the number of moles of i, ni, to the total number of moles in the mixture, n:

xi = ni /n

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The total number of moles, n, is the sum of the number of moles of all the components
of the mixture:

n = n1 + n2 + ...

It follows that the sum of all the mole fractions of the mixture must also equal 1.

x1 + x2 + ... = 1

The mass of component i in a mixture is the product of the number of moles of i and its
molecular weight, Mi. The mass of the mixture is therefore the sum, m = n1M1 + n2M2 +
..., over all components of the mixture. Substituting xin for ni, the total mass becomes

m = (x1M1 + x2M2 + ...)n

But the average molecular weight of the mixture is the ratio of the total mass to the
total number of moles. Thus the average molecular weight is

M = m /n = x1M1 + x2M2 + ...

EXAMPLE 3.1

Express the mass fraction of component 1 of a mixture in terms of: (a) the number of
moles of the three components of the mixture, n1, n2, and n3, and (b) the mole fractions
of the three components. (c) If the mole fractions of carbon dioxide and nitrogen in a
three component gas containing water vapor are 0.07 and 0.38, respectively, what are
the mass fractions of the three components?

Solution
(a) Because the mass of i can be written as mi = niMi , the mass fraction of component
i can be written as:

mfi = niMi /(n1M1 + n2M2 + ..) [dl]

For the first of the three components, i = 1, this becomes:

mf1 = n1M1/(n1M1 + n2M2 + n3M3)

Similarly, for i = 2 and i = 3:

mf2 = n2M2/(n1M1 + n2M2 + n3M3)

mf3 = n3M3/(n1M1 + n2M2 + n3M3)

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(b) Substituting n1 = x1 n, n2 = x2 n, etc. in the earlier equations and simplifying, we
obtain for the mass fractions:

mf1 = x1M1/(x1M1 + x2M2 + x3M3)

mf2 = x2M2/(x1M1 + x2M2 + x3M3)

mf3 = x3M3 /(x1M1 + x2M2 + x3M3)

(c) Identifying the subscripts 1, 2, and 3 with carbon dioxide, nitrogen, and water
vapor, respectively, we have x1 = 0.07, x2 = 0.38 and x3 = 1 – 0.07 – 0.038 = 0.55.
Then:

mf1 = (0.07)(44)/[(0.07)(44) + (0.38)(28) + (0.55)(18)]

= (0.07)(44)/(23.62) = 0.1304

mf2 = (0.38)(28)/(23.62) = 0.4505

mf3 = (0.55)(18)/(23.62) = 0.4191

As a check we sum the mass fractions: 0.1304 + 0.4505 + 0.4191 = 1.0000.
________________________________________________________________

For a mixture of gases at a given temperature and pressure, the ideal gas law
shows that pVi = niúT holds for any component, and pV = núT for the mixture as a
whole. Forming the ratio of the two equations we observe that the mole fractions have
the same values as the volume fraction:

xi = Vi /V = ni /n [dl]

Similarly, for a given volume of a mixture of gases at a given temperature, piV = niúT
for each component and pV = núT for the mixture. The ratio of the two equations
shows that the partial pressure of any component i is the product of the mole fraction
of i and the pressure of the mixture:

pi = pni /n = pxi

EXAMPLE 3.2

What is the partial pressure of water vapor in Example 3.1 if the mixture pressure is
two atmospheres?

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Solution
The mole fraction of water vapor in the mixture of Example 3.1 is 0.55. The partial
pressure of the water vapor is therefore (0.55)(2) = 1.1 atm.
_____________________________________________________________________

Characterizing Air for Combustion Calculations

Air is a mixture of about 21% oxygen, 78% nitrogen, and 1% other constituents by
volume. For combustion calculations it is usually satisfactory to represent air as a 21%
oxygen, 79% nitrogen mixture, by volume. Thus for every 21 moles of oxygen that
react when air oxidizes a fuel, there are also 79 moles of nitrogen involved. Therefore,
79/21 = 3.76 moles of nitrogen are present for every mole of oxygen in the air.
At room temperature both oxygen and nitrogen exist as diatomic molecules, O2
and N2, respectively. It is usually assumed that the nitrogen in the air is nonreacting at
combustion temperatures; that is, there are as many moles of pure nitrogen in the
products as there were in the reactants. At very high temperatures small amounts of
nitrogen react with oxygen to form oxides of nitrogen, usually termed NOx. These small
quantities are important in pollution analysis because of the major role of even small
traces of NOx in the formation of smog. However, since these NOx levels are
insignificant in energy analysis applications, nitrogen is treated as inert here.
The molecular weight of a compound or mixture is the mass of 1 mole of the
substance. The average molecular weight, M, of a mixture, as seen earlier, is the linear
combination of the products of the mole fractions of the components and their
respective molecular weights. Thus the molecular weight for air, Mair, is given by the
sum of the products of the molecular weights of oxygen and nitrogen and their
respective mole fractions in air. Expressed in words:

Mair = Mass of air/Mole of air = (Moles of N2 /Mole of air)(Mass of N2 /Mole of N2)

+ (Moles of O2/Mole of air)(Mass of O2 /Mole of O2)
or

Mair = 0.79 Mnitrogen + 0.21 Moxygen

= 0.79(28) + 0.21(32) = 28.84

The mass fractions of oxygen and nitrogen in air are then

mfoxygen = (0.21)(32)/28.84 = 0.233, or 23.3%

and

mfnitrogen = (0.79)(28)/28.84 = 0.767, or 76.7%

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3.2 Combustion Chemistry of a Simple Fuel

Methane, CH4, is a common fuel that is a major constituent of most natural gases.
Consider the complete combustion of methane in pure oxygen. The chemical reaction
equation for the complete combustion of methane in oxygen may be written as:

CH4 + 2O2 Y CO2 + 2H2O (3.1)

Because atoms are neither created nor destroyed, Equation (3.1) states that methane
(consisting of one atom of carbon and four atoms of hydrogen) reacts with four atoms
of oxygen to yield carbon dioxide and water products with the same number of atoms
of each element as in the reactants. This is the basic principle involved in balancing all
chemical reaction equations.
Carbon dioxide is the product formed by complete combustion of carbon through
the reaction C + O2 Y CO2. Carbon dioxide has only one carbon atom per molecule.
Since in Equation (3.1) there is only one carbon atom on the left side of the equation,
there can be only one carbon atom and therefore one CO2 molecule on the right.
Similarly, water is the product of the complete combustion of hydrogen. It has two
atoms of hydrogen per molecule. Because there are four hydrogen atoms in the
reactants of Equation (3.1), there must be four in the products, implying that two
molecules of water formed. These observations require four atoms of oxygen on the
right, which implies the presence of two molecules (four atoms) of oxygen on the left.
The coefficients in chemical equations such as Equation (3.1) may be interpreted as
the number of moles of the substance required for the reaction to occur as written.
Thus another way of interpreting Equation (3.1) is that one mole of methane reacts
with two moles of oxygen to form one mole of carbon dioxide and two moles of water.
While not evident in this case, it is not necessary that there be the same number of
moles of products as reactants. It will be seen in numerous other cases that a different
number of moles of products is produced from a given number of moles of reactants.
Thus although the numbers of atoms of each element must be conserved during a
reaction, the total number of moles need not. Because the number of atoms of each
element cannot change, it follows that the mass of each element and the total mass must
be conserved during the reaction. Thus, using the atomic weights (masses) of each
element, the sums of the masses of the reactants and products in Equation (3.1) are
both 80:

CH4 + 2O2 Y CO2 + 2H2O
[12 + 4(1)] + 4(16) Y [12 + 2(16)] + 2[2(1) + 16] = 80

Other observations may be made with respect to Equation (3.1). There are 2 moles of
water in the 3 moles of combustion products, and therefore a mole fraction of water in
the combustion products of xwater = 2/3 = 0.667. Similarly, xCarbon dioxide = 1/3 = 0.333
moles of CO2 in the products.
There are 44 mass units of CO2 in the 80 mass units of products for a mass

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fraction of CO2 in the products,

mfcarbon dioxide = 44/80 = 0.55

Likewise, the mass fraction of water in the products is 2(18)/80 = 0.45.
We also observe that there are 12 mass units of carbon in the products and
therefore a carbon mass fraction of 12/80 = 0.15. Note that because the mass of any
element and the total mass are conserved in a chemical reaction, the mass fraction of
any element is also conserved in the reaction. Thus the mass fraction of carbon in the
reactants is 0.15, as in the products.

Combustion in Air

Let us now consider the complete combustion of methane in air. The same combustion
products are expected as with combustion in oxygen; the only additional reactant
present is nitrogen, and it is considered inert. Moreover, because we know that in air
every mole of oxygen is accompanied by 3.76 moles of nitrogen, the reaction equation
can be written as

CH4 + 2O2 + 2(3.76)N2 Y CO2 + 2H2O + 2(3.76)N2 (3.2)

It is seen that the reaction equation for combustion in air may be obtained from the
combustion equation for the reaction in oxygen by adding the appropriate number of
moles of nitrogen to both sides of the equation.
Note that both Equations (3.1) and (3.2) describe reactions of one mole of
methane fuel. Because the same amount of fuel is present in both cases, both reactions
release the same amount of energy. We can therefore compare combustion reactions in
air and in oxygen. It will be seen that the presence of nitrogen acts to dilute the
reaction, both chemically and thermally. With air as oxidizer, there are 2 moles of water
vapor per 10.52 moles of combustion products, compared with 2 moles of water per 3
moles of products for combustion in oxygen. Similarly, with air, there is a mass fraction
of CO2 of 0.1514 and a carbon mass fraction of 0.0413 in the combustion products,
compared with 0.55 and 0.15, respectively, for combustion in oxygen.
The diluting energetic effect of nitrogen when combustion is in air may be reasoned
as follows: The same amount of energy is released in both reactions, because the same
amount of fuel is completely consumed. However, the nonreacting nitrogen molecules
in the air have heat capacity. This added heat capacity of the additional nitrogen
molecules absorbs much of the energy released, resulting in a lower internal energy per
unit mass of products and hence a lower temperature of the products. Thus the energy
released by the reaction is shared by a greater mass of combustion products when the
combustion is in air.
Often, products of combustion are released to the atmosphere through a chimney,
stack, or flue. These are therefore sometimes referred to as flue gases. The flue gas
composition may be stated in terms of wet flue gas (wfg) or dry flue gas (dfg), because

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under some circumstances the water vapor in the gas condenses and then escapes as a
liquid rather than remaining as a gaseous component of the flue gas. When liquid water
is present in combustion products, the combustion product gaseous mass fractions may
be taken with respect to the mass of flue gas products, with the product water present
or omitted. Thus, for Equation (3.2), the mass of dry combustion products is 254.56.
Hence the mass fraction of carbon dioxide is 44/254.56 = 0.1728 with respect to dry
flue gas, and 44/290.56 = 0.1514 with respect to wet flue gas.
In combustion discussions reference is frequently made to higher and lower heating
values. The term higher heating value, HHV, refers to a heating value measurement in
which the product water vapor is allowed to condense. As a consequence, the heat of
vaporization of the water is released and becomes part of the heating value. The lower
heating value, LHV, corresponds to a heating value in which the water remains a
vapor and does not yield its heat of vaporization. Thus the energy difference between
the two values is due to the heat of vaporization of water, and

HHV = LHV + (mwater /mfuel)hfg [Btu/lbm | kJ/kg]

where mwater is the mass of liquid water in the combustion products, and hfg is the latent
heat of vaporization of water.

Air-Fuel Ratio

It is important to know how much oxygen or air must be supplied for complete
combustion of a given quantity of fuel. This information is required in sizing fans and
ducts that supply oxidizer to combustion chambers or burners and for numerous other
design purposes. The mass air-fuel ratio, A/F, or oxygen-fuel ratio, O/F, for complete
combustion may be determined by calculating the masses of oxidizer and fuel from the
appropriate reaction equation. Let’s return to Equation (3.2):

CH4 + 2O2 + 2(3.76)N2 Y CO2 + 2H2O + 2(3.76)N2 (3.2)

The A/F for methane is [(2)(32) + (2)(3.76)(28)]/(12 + 4) = 17.16 and the O/F is
2(32)/(12 + 4) = 4. Thus 4 kg of O2 or 17.16 kg of air must be supplied for each
kilogram of methane completely consumed.
Of course it is possible, within limits, to supply an arbitrary amount of air to a
burner to burn the fuel. The terms stoichiometric or theoretical are applied to the
situation just described, in which just enough oxidizer is supplied to completely convert
the fuel to CO2 and H2O. Thus the stoichiometric O/F and A/F ratios for methane are
4.0 and 17.16, respectively. If less than the theoretical amount of air is supplied, the
products will contain unburned fuel. Regardless of the magnitude of A/F, when
unburned fuel remains in the products (including carbon, carbon monoxide, or
hydrogen), combustion is said to be incomplete. Because air is virtually free and fuel is
expensive, it is usually important to burn all of the fuel by using more air than the
theoretical air-fuel ratio indicates is needed. Thus most burners operate with excess air.

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The actual air-fuel ratio used in a combustor is frequently stated as a percentage of
the theoretical air-fuel ratio

% theoretical air = 100(A/F)actual /(A/F)theor (3.3)

Thus, for methane, 120% of theoretical air implies an actual mass air-fuel ratio of
(120/100)(17.16) = 20.59.
Excess air is defined as the difference between the actual and the theoretical air
supplied. Accordingly, the percentage of excess air is

% excess air = 100[(A/F)actual – (A/F)theor ]/(A/F)theor (3.4)

Thus, for methane, 120% of theoretical air implies

% excess air = (100)(20.59 – 17.16)/17.16 = 20%.

Note also that combining Equations (3.4) and (3.3) yields the following general result:

% excess air = % theoretical air – 100% (3.5)

Again, the excess air percentage is 120% – 100% = 20%. Table 3.1 shows examples of
ranges of excess air used with certain fuels and combustion systems.
The air/fuel parameters just discussed emphasize the amount of air supplied to burn
a given amount of fuel relative to the theoretical requirement. An alternate approach
considers a given amount of air and indicates the mass of fuel supplied , the fuel-air
ratio, F/A, which is the inverse of the air-fuel ratio. A measure of how much fuel is
actually supplied, called the equivalence ratio, is the ratio of the actual fuel-air ratio to
the theoretical fuel-air ratio:

M = (F/A)actual / (F/A)theor = (A/F)theor / (A/F)actual

= 100/( % theoretical air)

Thus 100% theoretical air corresponds to an equivalence ratio of 1, and 20% excess air
to M = 100/120 = 0.833. When the equivalence ratio is less than 1, the mixture is called
lean; when greater than 1, it is called rich.
This section has dealt with the application of combustion chemistry or
stoichiometry applied to methane gas. Other fuels for which a reaction equation such as
Equation (3.1) or (3.2) is available may be treated in a similar way. Before considering
more complex combustion problems, it is appropriate to investigate the nature and
description of the various types of fossil fuels.

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3.3 Fossil Fuel Characteristics

Most chemical fuels are found in nature in the form of crude oil, natural gas, and coal.
These fuels are called fossil fuels because they are believed to have been formed by the
decay of vegetable and animal matter over many thousands of years under conditions of
high pressure and temperature and with a deficiency or absence of oxygen. Other fuels
such as gasoline, syngas (synthetic gas), and coke may be derived from fossil fuels by
some form of industrial or chemical processing. These derived fuels are also called
fossil fuels.

Coal

Coal is an abundant solid fuel found in many locations around the world in a variety of
forms. The American Society for Testing Materials, ASTM, has established a ranking
system (ref. 3) that classifies coals as anthracite (I), bituminous (II), subbituminous
(III), and lignite (IV), according to their physical characteristics. Table 3.2 lists

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seventeen of the many United States coals according to this class ranking.
Coal is formed over long periods of time, in a progression shown from left to right
in Figure 3.1. The bars on the ordinate show the division of the combustibles between
fixed carbon and volatile matter in the fuels. “Fixed carbon” and “volatile matter”
indicate roughly how much of the fuel burns as a solid and as a thermally generated gas,
respectively. It is seen that the volatile matter and oxygen contained in the fuels
decrease with increasing age.
Peat is a moist fuel, at the geologically young end of the scale, that has a relatively
low heating value. It is not considered a coal but, nevertheless, follows the patterns of
characteristics shown in the figure. Peat is regarded as an early stage or precursor of
coal. At the other extreme, anthracite is a geologically old, very hard, shiny coal with
high carbon content and high heating value. Bituminous is much more abundant than
anthracite, has a slightly lower carbon content, but also has a high heating value.
Subbituminous coal, lignite, and peat have successively poorer heating values and
higher volatile matter than bituminous.
Coal is a highly inhomogeneous material, of widely varying composition, found in
seams (layers) of varying thickness at varying depths below the earth's surface. The
wide geographic distribution of coal in the United States is shown in Figure 3.2.

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According to reference 1, the average seam in the United States is about 5.5 ft. thick.
The largest known seam is 425 ft. thick and is found in Manchuria.

Coal Analyses

It is often difficult to obtain representative samples of coal because of composition
variations from location to location even within a given seam. As a result there are
limits on the accuracy and adequacy of coal analyses in assessing coal behavior in a
given application. Before discussing the nature of these analyses, it is important to
establish the basis on which they are conducted.
Coal contains varying amounts of loosely held moisture and noncombustible
materials or mineral matter (ash), which are of little or no use. The basis of an analysis
helps to specify the conditions under which the coal is tested. The coal sample may be
freshly taken from the mine, the as-mined basis. It may have resided in a coal pile for
months, and be analyzed just before burning, the as-fired basis. It may be examined
immediately after transport from the mine, the as-received basis. Exposure to rain or
dry periods, weathering, and separation and loss of noncombustible mineral matter
through abrasion and the shifting of loads during transport and storage may cause the
same load of coal to have changing mineral matter and moisture content over time. It is
therefore important to specify the basis for any test that is conducted. Published
tabulations of coal properties are frequently presented on a dry, ash-free, or dry and
ash-free basis, that is, in the absence of water and/or noncombustible mineral matter.
Coal ranking and analysis of combustion processes rely on two types of analysis of
coal composition: the proximate analysis and the ultimate analysis. The proximate
analysis starts with a representative sample of coal. The sample is first weighed, then
raised to a temperature high enough to drive off water, and then reweighed. The weight

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loss divided by the initial weight gives the coal moisture content, M. The remaining
material is then heated at a much higher temperature, in the absence of oxygen, for a
time long enough to drive off gases. The resulting weight-loss fraction gives the
volatile matter content, VM, of the coal. The remainder of the sample is then burned in
air until only noncombustibles remain. The weight loss gives the fixed carbon, FC, and
the remaining material is identified as non-combustible mineral matter or ash, A.
The proximate analysis may be reported as percentages (or fractions) of the four
quantities moisture, ash, volatile matter, and fixed carbon, as in Table 3.2, or without
ash and moisture and with the FC and VM normalized to 100%. Sulfur, as a fraction of
the coal mass, is sometimes reported with the proximate analysis. The proximate
analysis, while providing very limited information, can be performed with limited
laboratory resources.
A more sophisticated and useful analysis is the ultimate analysis, a chemical
analysis that provides the elemental mass fractions of carbon, hydrogen, nitrogen,
oxygen, and sulfur, usually on a dry, ash-free basis. The ash content of the coal and
heating value are sometimes provided also.
Data from a dry, ash-free analysis can be converted to another basis by using the
basis adjustment factor, 1 - A - M, as follows. The mass of coal is the mass of ultimate
or proximate analysis components plus the masses of water (moisture) and ash:

m = mcomp + mash + mmoist [lbm | kg]

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Dividing through by the total mass m and rearranging, we get the following as the ratio
of the mass of components to the total mass:

mcomp / m = 1 – A – M [dl]

where A is the ash fraction and M is the moisture fraction of the total coal mass. A
component of a coal analysis may be converted from the dry, ash-free basis to some
other basis by forming the product of the component fraction and the basis adjustment
factor. Thus an equation for the wet and ashy volatile matter fraction in the proximate
analysis may be determined from the dry, ash-free proximate analysis by using

VMas-fired = (Mass of combustibles/Total mass)VMdry,ashfree

= ( 1 - A - M ) VMdry,ash-free (3.6)

where A and M are, respectively, the ash and moisture fractions for the as-fired coal.
Here the as-fired (wet, ashy) mass fraction of volatile matter is the product of the dry,
ash-free mass fraction and the basis adjustment factor. Fixed carbon, heating values,
and components of the ultimate analysis may be dealt with in a similar way.
Table 3.3 gives proximate and ultimate analyses for a number of United States
coals on a dry basis. Another extensive tabulation of the characteristics of American
and world coals is given in Appendix E.

EXAMPLE 3.3

If the as-fired moisture fraction for Schuylkill, Pa. anthracite culm characterized in
Table 3.3 is 4.5%, determine the as-fired proximate and ultimate analysis and heating
value of the coal. (Culm is the fine coal refuse remaining from anthracite mining.)

Solution
The FC, VM, and ash contents are given in Table 3.3. Because ash is already present in
the analysis, the appropriate adjustment factor is 1 - A - M = 1 – 0.0 – 0.045 = 0.955.
Using Equation (3.6) and the data from Table 3.3, we get

VMas-fired = (0.955)(8.3) = 7.927
FCas-fired = (0.955)(32.6) = 31.133
Aas-fired = (0.955)(59.1) = 56.411
Mas-fired = 4.500
Check Sum = 99.971
Heating valueas-fired = (0.955)(4918) = 4697 Btu/lbm

Similarly, the as-fired ultimate analysis is 32% C, 1.15% H2, 4.87% O2, 0.57% N2,
0.48% S, 56.44% ash, and 4.5% moisture, with a checksum of 100.01.
_____________________________________________________________________

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As a solid fuel, coal may be burned in a number of ways. Starting with the smallest
of installations, coal may be burned in a furnace, in chunk form on a stationary or
moving grate. Air is usually supplied from below with combustion gases passing
upward and ash falling through a stationary grate or dropping off the end of a moving
grate into an ash pit. A wide variety of solid fuels can be burned in this way.
Though all furnaces were onced fired manually, today many are fired by or with the
assistance of mechanical devices called stokers. Figure 3.3 shows a spreader stoker,
which scatters coal in a uniform pattern in the furnace, the finer particles burning in
suspension in the rising combustion air stream while the heavier particles drop to the
grate as they burn. The particles that reach the grate burn rapidly in a thin layer, and the
remaining ash drops off the end into the ash pit. This type of combustion system has
been in use for over fifty years for hot water heating and steam generation.
In large installations, coal is crushed to a particular size, and sometimes pulverized
to powder immediately before firing, to provide greater surface exposure to the

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oxidizer and to ensure rapid removal of combustion gases. Because of the wide
variation in the characteristics of coals, specialized types of combustion systems
tailored to a specific coal or range of coal characteristics are used.

Natural Gas

Natural gas is a mixture of hydrocarbons and nitrogen, with other gases appearing in
small quantities. Table 3.4 shows the composition of samples of natural gases found in
several regions of the United States. For these samples, it is seen that the gases contain
83-94% methane (CH4), 0-16% ethane (C2H6), 0.5-8.4% nitrogen and small quantities
of other components, by volume. The ultimate analysis shows that the gases contain
about 65-75% carbon, 20-24% hydrogen, 0.75-13% nitrogen, and small amounts of
oxygen and sulfur in some cases. The higher heating values are in the neighborhood of
1000 Btu/ft3 on a volume basis and 22,000 Btu/lbm on a mass basis. In regions where it
is abundant, natural gas is frequently the fuel of choice because of its low sulfur and ash
content and ease of use.

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EXAMPLE 3.4

Determine the molecular weight and stoichiometric mole and mass air-fuel ratios for the
Oklahoma gas mole composition given in Table 3.4.

Solution
Equation (3.2),

CH4 + 2O2 + 2(3.76)N2 Y CO2 + 2H2O + 2(3.76)N2 (3.2)

shows that there are 2 + 2(3.76) = 9.52 moles of air required for complete combustion
of each mole of methane. Similarly for ethane, the stoichiometric reaction equation is:

C2H6 + 3.5O2 + (3.5)(3.76)N2 Y 2CO2 + 3H2O + 13.16N2

where 2 carbon and 6 hydrogen atoms in ethane require 2 CO2 molecules and 3 H2O
molecules, respectively, in the products. There are then 7 oxygen atoms in the
products, which implies 3.5 oxygen molecules in the reactants. This in turn dictates the
presence of (3.5)(3.76) = 13.16 nitrogen molecules in both the reactants and products.
The reaction equation then indicates that 3.5(1 + 3.76) = 16.66 moles of air are
required for complete combustion of one mole of ethane.
In Table 3.5, the molecular weight of the gas mixture, 18.169, is found in the
fourth column by summing the products of the mole fractions of the fuel components
and the component molecular weights. This is analogous to the earlier determination of
the average air molecular weight from the nitrogen and oxygen mixture mole fractions.
The products of the mole fractions of fuel components and the moles of air
required per mole of fuel component (as determined earlier and tabulated in the fifth
column of Table 3.5) then yield the moles of air required for each combustible per mole
of fuel (in the sixth column). Summing these, the number of moles of air required per
mole of fuel yields the stoichiometric mole air-fuel ratio, 9.114.
The stoichiometric mass A/F is then given by the mole A/F times the ratio of air
molecular weight to fuel molecular weight: (9.114)(28.9)/18.169 = 14.5.

Table 3.5 Calculations for Example 3.4
i Mi xi xiMi Moles air per Moles air per mole fuel
mole i

Methane 16 0.841 13.456 9.52 (0.841)(9.52) = 7.998

Ethane 30 0.067 2.010 16.66 (0.067)(16.66) = 1.116

CO2 44 0.008 0.351 0.0

Nitrogen 28 0.084 2.352 0.0

Totals 1.000 18.169 moles air /mole fuel = 9.114

105

Liquid Fuels

Liquid fuels are primarily derived from crude oil through cracking and fractional
distillation. Cracking is a process by which long-chain hydrocarbons are broken up into
smaller molecules. Fractional distillation separates high-boiling-point hydrocarbons
from those with lower boiling points. Liquid fuels satisfy a wide range of combustion
requirements and are particularly attractive for transportation applications because of
their compactness and fluidity. Table 3.6 gives representative analyses of some of these
liquid fuels. Compositions of liquid and solid fuels, unlike gaseous fuels, are usually
stated as mass fractions.

3.4 Combustion Reactions and Analysis

Mechanism of Combustion

Details of the mechanics of combustion depend to a great extent on the fuel and the
nature of the combustion system. They are sometimes not well understood and are
largely beyond the scope of this book. There are, however, certain fundamentals that
are useful in dealing with combustion systems.
The chemical reaction equations presented here do not portray the actual
mechanism of combustion; they merely indicate the initial and final chemical
compositions of a reaction. In most cases the reactions involve a sequence of steps,
leading from the reactants to the products, the nature of which depends on the
temperature, pressure, and other conditions of combustion. Fuel molecules, for
instance, may undergo thermal cracking, producing more numerous and smaller fuel
molecules and perhaps breaking the molecules down completely into carbon and
hydrogen atoms before oxidation is completed.
In the case of solid fuels, combustion may be governed by the rate at which
oxidizer diffuses from the surrounding gases to the surface and by the release of
combustible gases near the surface. Combustion of solids may be enhanced by
increasing the fuel surface area exposed to the oxidizer by reducing fuel particle size.

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The following simple model illustrates the effect.

Example 3.5 is, of course, an idealized example. In reality, the reacting surface area of
solid fuels is usually much larger than the spherical surface area implied by their size.
We have seen that, for combustion to occur, molecules of oxidizer must affiliate
with fuel molecules, an action enhanced by the three T’s of combustion: turbulence,
time, and temperature. Chemical reactions take place more rapidly at high temperatures
but nevertheless require finite time for completion. It is therefore important that burners
be long enough to retain the fuel-air mixture for a sufficiently long time so that
combustion is completed before the mixture leaves. Turbulence, or mixing, enhances
the opportunities for contact of oxidizer and fuel molecules and removal of products of
combustion.
A flame propagates at a given speed through a flammable mixture. It will
propagate upstream in a flow of a combustible mixture if its flame speed exceeds the
flow velocity. If a fixed flame front is to exist at a fixed location in a duct flow in which
the velocity of the combustion gas stream exceeds the propagation speed, some form of
flame stabilization is required. Otherwise the flame front is swept downstream and
flameout occurs. Stabilization may be achieved by using fixed flameholders (partial

107

flow obstructions that create local regions of separated flow in their bases where the
flame speed is greater than the local flow velocity) or by directing a portion of the flow
upstream to provide a low-speed region where stable combustion may occur.
Each combination of oxidizer and fuel has been seen to have a particular
stoichiometric oxidizer-fuel ratio for which the fuel is completely burned with a
minimum of oxidizer. It has also been pointed out that it is usually desirable to operate
burners at greater than the theoretical air-fuel ratio to assure complete combustion of
the fuel and that this is sometimes referred to as a lean mixture. Occasionally it may be
desirable to have incomplete combustion, perhaps to produce a stream of products in
which carbon monoxide exists or to assure that all the oxidizer in the mixture is
consumed. In that case a burner is operated at less than the stoichiometric air-fuel ratio
with what is called a rich mixture.
There are limits to the range of air-fuel ratios for which combustion will occur
called limits of flammability. Here the density of the mixture is important. The limits of
flammability around the stoichiometric A/F are reduced at low densities. If combustion
is to occur reliably in mixtures at low densities, it is necessary to closely control the
air-fuel ratio.

Combustion Analysis of Solid Fuels

In the determination of the air-fuel ratio and flue gas composition for the combustion of
solid fuels, it is important to account for the ash and moisture in the fuel in the as-fired
condition. In the following analyses, all of the elements of the reactants in the fuel and
oxidizer are assumed to be present in the flue gas products except for the ash, which is
assumed to fall as a solid or flow as molten slag to the furnace bottom. Nitrogen and
oxygen are present in many solid fuels and should be accounted for in predicting the
flue gas composition. While both carbon monoxide and oxygen may be present in
combustion products at the same time because of imperfect mixing of combustibles and
oxygen in some instances, we will assume for prediction of the flue gas composition
that perfect mixing occurs such that no carbon monoxide is present when excess air is
supplied.

EXAMPLE 3.6

A coal with a dry, ash-free composition of 0.87 C, 0.09 H2, 0.02 S, and 0.02 O2 is
burned with 25% excess air. The as-fired ash and moisture contents are 6% and 4%,
respectively.
(a) What are the stoichiometric and actual air-fuel ratios?
(b) What is the flue gas composition?

Solution
(a) Before performing combustion calculations, it is necessary to convert coal
composition data to an as-fired basis. The ratio of as-fired to dry, ash-free

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mfj = (kg j / kg fg) = (kg j / kg coal) / (kg fg / kg coal)

115

(Note: The reference conditions of the 1985 JANAF Thermochemical tables used differ
slightly from those of preceding editions.) Heats of formation are usually determined
based on statistical thermodynamics and spectroscopic measurements.
By definition, heats of formation are zero for all elements in the standard state.
Hence, from the steady-flow First Law of Thermodynamics, the heat transferred in a
formation reaction of a compound created from elements in the standard state is the
heat of formation for the compound, as in the hydrogen-to-water example just
mentioned.

Heat Transfer in a Chemically Reacting Flow

Consider now the combustion problem in which fuel and oxidizer flow into a control
volume and combustion products flow out. The steady-flow First Law of Thermo-
dynamics applied to the control volume may be written as

Q = Hp – Hr + Ws [Btu | kJ] (3.7)

where Q is heat flow into the control volume, Ws is the shaft work delivered by the
control volume, and the enthalpies, H, include chemical as well as thermal energy. The
subscripts r and p refer to the reactants entering and products leaving the control
volume, respectively. The enthalpy Hp is the sum of the enthalpies of all product
streams leaving the control volume. A similar statement applies to Hr for the entering
reactant streams.

116

The individual enthalpies may each be written as the product of the number of
moles of the component in the reaction equation and its respective enthalpy per mole of
the component. For example, for k products:

Hp = n1h1 + n2h2 +...+ nkhk [Btu | kJ] (3.8)

where the n’s are the stoichiometric coefficients of the chemical equation for the
combustion reaction, and the enthalpies are on a per-mole bases.

EXAMPLE 3.9

Write an equation for the enthalpy of the products of complete combustion of octane in
oxygen.

Solution The balanced equation for the complete combustion of octane is

C8H18 + 12.5O2 Y 8CO2 + 9H2O

The mole coefficients, 8 and 9, of the products are stoichiometric coefficients that yield

Hp = 8h(CO2) + 9h(H2O) [Btu | kJ]

per mole of octane consumed.
___________________________________________________________________

The enthalpy of any component of the reactants or products may be written as the
sum of (1) its enthalpy of formation at the standard temperature, To, and standard
pressure, and (2) its enthalpy difference between the actual state and the standard state
of the components. Thus, for each component:

h(T) = hf (To) + [h(T) – h(To)] [Btu /mole | kJ /mole] (3.9)

where it is assumed that the sensible gas enthalpy difference is independent of pressure.
Sensible enthalpies (those that depend on temperature but do not involve reactions or
phase change) relative to the standard reference state are given in Appendix D.
Thus, returning to the formation reaction for the combustion of hydrogen in
oxygen at the standard state to produce water, as discussed in the preceding section,
we see that the steady-flow First Law of Thermodynamics becomes

Q = (1)hf, H2O – (1)hf, H2 – (0.5)hf, O2 = –103,996 – 0 – 0 = – 103,996 Btu/lb-mole

with water in the vapor phase as the product of combustion of one mole of H2. Here
the sensible enthalpy differences are zero, because both the products and the reactants
are at the standard state. Note that because the stoichiometric coefficients of both

117

hydrogen and water are the same in this reaction, the resulting heat transfer may be
interpreted as either per mole of water formed or per mole of hydrogen consumed.
If, instead, liquid water is the combustion product, the heat transfer is given by

Q = – 122,885 – 0 – 0 = – 122,885 Btu/lb-mole

of H2O. The difference between the two cases, 18,919 Btu/lb-mole H2O, is equivalent
to 18,935/18 = 1,051.9 Btu/lbm of water, the enthalpy of vaporization of water. This
result compares with the enthalpy or latent heat of vaporization of water at 77°F,
1050.1 Btu/lbm, given in the steam tables.
With either liquid or gaseous water as the product, the heat transfer term for the
control volume is negative, indicating, in accordance with the usual sign convention,
that the heat flows from the control volume to the surroundings. The two calculations
above illustrate the fact that the heat transfer in a formation reaction at the standard
state is the heat of formation of the compound created.

EXAMPLE 3.10

What is the enthalpy of water vapor at 1800°R and 1 bar? What is the heat transfer in
the formation reaction of water from hydrogen and oxygen if the products are at
1800°R and the reactants are (a) at the standard state, and (b) at 900°R?

Solution
The heat of formation of water vapor at the standard state of 298.15K. (536.7°R)
and one bar is – 103,966 Btu/lb-mole. The enthalpy of water vapor at 1800°R is the
sum of the heat of formation at the standard state and the sensible enthalpy difference
of water vapor between 536.7°R and 1800°R. Thus:

Hp = – 103,966 + 11,185 = – 92,781 Btu/lb-mole of water.

(a) In this case, the reactants, oxygen and hydrogen, have zero enthalpies because they
are in the standard state and, as elements, their heats of formation are zero. Thus the
heat transferred is – 92,781 Btu/lb-mole, or 5154.5 Btu/lbm of water.

(b) For reactants at 900°R , Appendix D gives hH2(900) – hH2(536.7) = 2530 Btu/mole
of H2 and hO2(900) – hO2(536.7) = 2617 Btu/mole of O2. The enthalpy of the reactants
is then Hr = (1.0)(2530) + (0.5)(2617) = 3838.5 Btu/lb-mole H2O. The heat transferred
is then:

Q = Hp – Hr = – 92,781 – 3,838.5 = – 96,619.5 Btu/lb-mole of water,
or
Q = – 96,619.5 / 18 = – 5,367.8 Btu/lbm of water.

118

Thus more heat must be transferred from the control volume to form water vapor at
1800°R if the reactants are at 900°R than if they are in the 536.7°R standard state.

Combustion Flame Temperature

In many combustion problems, the reactants enter the combustor near room tempera-
ture and products emerge at an elevated temperature. The temperature of the products
flowing from the control volume depends on the energy released in the combustion
reaction and heat gain or loss through the boundary of the control volume. The
resulting combustion product temperature is sometimes called the flame temperature.

EXAMPLE 3.11

Methane and stoichiometric air enter a combustor at the standard state. Using a spread-
sheet, calculate the heat transfer as a function of the exit (flame) temperature of the
products of complete combustion. Assume the water in the products remains a vapor.

Solution
The reaction equation for complete combustion of methane in air is:

CH4 + 2O2 + (2)3.76N2 Y CO2 + 2H2O + 7.52N2

The enthalpy of the products at temperature T and of the reactants at the standard state
is

Hp = (1)hf, CO2 + (1)[hCO2 (T) – hCO2 (537)] + (2)hf, H2O
+ (2)[hH2O (T) – hH2O (537)] + (7.52)[hN2 (T) – hN2 (537)]

Hr = hf, CH4 = – 32,189.6 Btu/lb-mole

of methane, where the heats of formation of elemental nitrogen and oxygen are zero
and the heat of formation of water is for the vapor phase. Writing the enthalpy
differences as )h’s and applying the steady-flow First Law of Thermodynamics, we get

Q = Hp – Hr = – 169,184 + )hCO2(T) + (2)(– 103,966)
+ (2) )hH2O(T) + 7.52 )hN2(T) – (– 32,189.6)

= – 344,926.4 + )hCO2(T) + (2))hH2O(T) + 7.52 )hN2 Btu/lb-mole

of methane. This function is tabulated in the spreadsheet in Table 3.10 and plotted in
Figure 3.4 using values of enthalpies at the temperature T from the the JANAF tables.
Negative values of Q indicate that heat must be rejected from the control volume to
maintain product effluent temperature below about 4200°R. Beyond 4200°R, the CO2,

119

N2, and H2O outflow carries more energy than is released in the control volume by
chemical reaction; hence, heat must flow into the control volume to achieve the
resulting high exit temperatures. Thus the final flame temperature clearly depends on
the chemical composition of the flow and on the consequent control volume heat
transfer.
____________________________________________________________________

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Heat of Combustion and Heating Value

The heat of combustion, or enthalpy of combustion, of a fuel is defined as the energy
transferred during a steady-flow process in which the fuel is completely burned and
where the products are returned to the temperature and pressure of the reactants. It will
be seen that the enthalpy of combustion evaluated at the standard state may be deter-
mined from the heats of formation. The heat of combustion of hydrogen has, in fact,
been determined in a preceding section that examined the formation reaction for water.
The negative of the enthalpy of combustion of a fuel burned in air is usually
referred to as the heating value of the fuel. When water in the combustion products is
condensed, the heat of vaporization of the water adds to the chemical energy released,
and the resulting heating value is called the higher heating value, HHV. Recall also
that the heating value obtained when the product water stays a vapor is called the lower
heating value, LHV. The difference between HHV and LHV has been illustrated in the
previous section for the formation reaction of water resulting from the combustion of
hydrogen.
For methane, note also that the heat of combustion, and thus the magnitude of the
lower heating value, appears in the value of Q in the top row of table 3.10, since there
the combustion products are at the reference temperature.

EXAMPLE 3.12

Illinois no. 6 raw coal has the following dry mass composition: 61.6% C, 4.2% H2,
9.7% O2, 1.3% N2, 4.6% S, and 18.5% ash. Using heats of formation, determine the
higher and lower heating values, in kJ / kg, of the as-fired coal with 10% moisture, and
compare them with the heating value in Table 3.3.

Solution
To adjust the composition for 10% moisture, the factor 1 – A – M becomes 1 – 0
– 0.1 = 0.9. The resulting moist coal composition is given in the following table.
It was seen earlier that the heat of reaction of hydrogen in its standard state, and
thus its heat of combustion, is the heat of formation of its product of combustion. The
reaction equation

H2 + 0.5O2 Y H2O

shows that one mole of hydrogen produces one mole of water. Thus, from Table 3.9,
the heat of formation of steam, – 241,826 kJ per kg-mole of water formed or per kg-
mole of hydrogen burned, is also the heat of combustion of hydrogen in the standard
state. Thus the hydrogen contributes 241,826/2 kJ per kg of hydrogen in the coal. The
total energy released by the hydrogen in the coal is then 241,826/2 times the mass
fraction of hydrogen in the coal, as shown in the following table. Similar arguments
may be made for hydrogen with product water in the liquid phase and the carbon and
sulfur components of the coal.

121

Element i Dry mfi Wet mfi Heat of Combustion kJ/kg coal

H2:

For LHV 0.042 0.0378 (241,826)(0.0378)/2 = 4,570.5 (v)

For HHV (285,830)(0.0378)/2 5402.2 (l)

C 0.616 0.5544 (393,522)(0.5544)/12 = 18,180.7

O2 0.097 0.0873

N2 0.013 0.0117

S 0.046 0.0414 (296,842)(0.0414)/32 = 384.0

Ash 0.185 0.1665

H2O _____ 0.1000

0.999 0.9991 23,135.2 (v)

23,966.9 (l)

Thus the lower and higher heating values of the coal are 23,135.2 and 23,966.9 kJ/kg,
respectively. Table 3.3 lists a heating value of dry Illinois no. 6 raw coal of 11,345
Btu/lbm. The corresponding heating value for the wet coal is (0.9)(11,345) = 10,210.5
Btu/lbm. This corresponds to (10,210.5)/(0.43) = 23,745 kJ/kg.
____________________________________________________________________

Adiabatic Flame Temperature

The results of Example 3.11, tabulated in Figure 3.10, show that for a given air-fuel
mixture there is a unique product temperature for which the control volume is
adiabatic. This temperature is known as the adiabatic flame temperature. It can be
determined as in Example 3.11, or it may be calculated from the steady-flow First Law
of Thermodynamics by setting Q = 0. The resulting First Law equation for the adiabatic
flame temperature, designated T*, becomes:

Hp (T*) = Hr (T r) [Btu | kJ] (3.10)

where the reactants are at the temperature Tr . The enthalpy terms depend on the
individual enthalpies of the components as functions of temperature. Thus a trial-and-
error solution is required using data on heat of formation from Table 3.9 and the
enthalpy tables in Appendix D. Given a known Tr , the adiabatic flame temperature may
also be obtained as the intercept (Q = 0) on a graph of Q versus temperature, T, such as
Figure 3.4.
Adiabatic Flame Temperature for Solid Fuels

122

As a final example, we will determine the combustion products, heat of combustion,
and adiabatic flame temperature for a solid fuel specified by its ultimate analysis. The
solution is presented in a spreadsheet in which enthalpies are tabulated as a function of
temperature for the relevant chemical components as given in the JANAF tables.

124

The number of moles of excess O2 in the flue gas per pound of coal may also be
obtained from the excess air-fuel ratio:

[(A/F)actual – (A/F)theor ](0.233)/32 = (8.288 – 6.375)(0.233)/32 = 0.0139

The number of moles of flue gas nitrogen is also given by

[(A/F)actual ](1 – 0.233)/28 + d = 8.288(0.767)/28 + 0.000357 = 0.227

With the actual balanced reaction equation known, the mole coefficients may then be
used to write an equation for the enthalpy of the products per unit mass of coal.
Because all the reactants are assumed to be elements at the reference temperature, the
enthalpy of the reactants is zero. By setting Q = Hp = 0, we can solve this First Law
equation for the adiabatic flame temperature by trial and error. However, with a
spreadsheet, it is convenient to calculate the heat transfer at each temperature-enthalpy
data point and determine the adiabatic flame temperature by inspection and, if
additional precision is required, by explicit interpolation. The heat transfer equation is
shown on the spreadsheet, and the values of the flue gas mole coefficients and heats of
formation are shown above the appropriate JANAF enthalpies to which they relate.

It is seen that the adiabatic flame temperature for combustion with 30% excess air
is about 2110K, or 3800°R. Note also that the heat of combustion of the coal, 8506.7
Btu/lbm of coal, may be read from the spreadsheet at the JANAF table reference
temperature. This is possible because the heat of reaction is independent of the amount
of excess air employed in the reaction.
_____________________________________________________________________

The spreadsheet for Example 3.13 is easily modified to compute and plot the
composition of the flue gas as a function of the percentage of excess air. Figure 3.5
shows that the mole fractions of excess oxygen and of nitrogen increase while the
fractions of other products decrease. Excess oxygen measured from a flue gas sample
is commonly used as a measure of excess air in adjusting the air-fuel ratio of
combustion systems.

3.6 Molecular Vibration, Dissociation, and Ionization

The temperature of a gas is a measure of the random translational kinetic energy of
molecules. The simple kinetic theory of the heat capacity of a gas predicts heat
capacities that are independent of temperature and determined by the number of
degrees of freedom of the molecules. The kinetic theory is usually regarded as
applicable at low pressures and moderate and high temperatures, conditions at which
collisions between molecules are rare.

125

For monatomic gases, kinetic theory predicts an internal energy per atom of

u = 3kT/2

and an enthalpy of

h = u + pv = 3kT/2 + kT = 5kT/2

Here k, the Boltzmann constant, is the ideal-gas constant per molecule, which can be
calculated from the universal gas constant, ú, and Avogadro’s number of molecules
per mole. Thus

k = ú/No = 8.32/(6.025 × 1023) = 1.38 × 10 -23 J/K

From their definitions, Equations (1.14) and (1.15), this leads to cv = 3k/2 and cp = 5k/2
per atom and to a heat capacity ratio of k = cp /cv = 5/3 = 1.667.
The concept of equipartition of energy assumes that the energy of a particle is
equally divided among its various degrees of freedom. Each mode of energy storage of
a molecule is assigned an energy kT/2. The theory then represents the internal energy
as nkT/2, the enthalpy as (n + 2)kT/2, and the heat capacity ratio as k = (n + 2)/n,
where n is the number of modes of energy storage, or degrees of freedom, of the
molecule. For atoms with three translational and no rotational degrees of freedom,
n = 3 (an atom is presumed to be a point and to have no rotational kinetic energy

126

because it has zero radius); and these relations reduce to the findings described in the
preceding paragraph.
The simple kinetic theory suggests that a diatomic molecule has five degrees of
freedom: three degrees of translational freedom and two modes having significant
rotational kinetic energy. For this case we obtain u = 5kT/2, h = 7kT/2, and
k = 7/5 = 1.4, in agreement with experiment for oxygen and nitrogen at moderate
temperatures and densities.
At higher temperatures, diatomic molecules start to vibrate, adding additional
degrees of freedom that reduce the heat capacity ratio k below 1.4. As the temperature
increases and the collisions between molecules become more vigorous, molecules not
only vibrate but they start to be torn apart, each forming separate atoms, the process
known as dissociation. The energy required to break the bonds between atoms in
molecules is called the dissociation energy. At low temperatures, few molecules have
sufficient kinetic energy to provide the energy needed to cause dissociation by collision.
At higher temperatures, when more molecules have energies exceeding the dissociation
energy, the chemical equilibrium shifts to a composition in which there are more atoms
and fewer molecules in the gas. This trend continues as temperature increases.
At still higher temperatures, when particle kinetic energies exceed the ionization
energy of the gas, outer electrons are separated from atoms, forming positively charged
ions, in a process known as the ionization. Particles lose kinetic energy when causing
dissociation and ionization. This lost energy is then not reflected in the temperature.
Thus, when vibration, dissociation, and ionization occur, the internal energy and
enthalpy increase more rapidly than the temperature. Then the simple linear relations
just given for u and T are no longer correct. Stated another way, the temperature of a
gas rises less rapidly with heat addition when it is at temperature levels where
significant vibration, dissociation, or ionization take place. The phenomenon may be
thought of as analogous to phase change, in which enthalpy increases with heat addition
while temperature does not.
As a result of these phenomena, high flame temperatures determined with ideal gas
enthalpies may be overestimated. At temperatures exceeding 2000K (3600°R), flame
temperature calculations based on the JANAF gas enthalpies may start to become
inaccurate. At these temperature levels, dissociation (and at still higher temperatures,
ionization) starts to influence the composition of the gases and hence their
thermodynamic properties. The progression of dissociation and ionization with
temperature is shown for air at sea level density in Figure 3.6. It is seen that, at this
density, little dissociation of nitrogen occurs below about 6000 K. but that oxygen
starts to dissociate significantly above 3000 K.. At lower densities, the onset of
dissociation occurs at progressively lower temperatures. In Figure 3.6, the number of
particles per initial atom of air may be obtained by multiplying the ordinates by 1.993.
Usually, dissociation does not seriously influence combustion calculations when the
oxidizer is air, but the high combustion temperatures resulting from use of pure oxygen
may be significantly influenced by dissociation. The reader is referred to advanced
thermodynamics, physical chemistry, and advanced engineering texts for methods of
predicting the effects of dissociation and ionization.

127

Bibliography and References

1. Anon, Steam, Its Generation and Use, 39th ed. New York,: Babcock and Wilcox,
1978.

2. Singer, Joseph G. (Ed.), Combustion / Fossil Power Systems. Windsor, Conn.:
Combustion Engineering Inc., 1981.

3. Anon., Classification of Coals by Rank, Standard D-388. Philadelphia: American
Society for Testing Materials, Section 5, Volume 05.05, 1983.

4. Chase, M. W. Jr., et.al., JANAF Thermochemical Tables, 3rd ed., J. Phys. Chem.
Ref. Data 14, Supplement No. 1, 1985.

5. Van Wylen, Gordon J., and Sonntag, Richard E., Fundamentals of Classical
Thermodynamics. New York: Wiley, 1986.

128

6. El-Wakil, M. M., Powerplant Technology. New York: McGraw-Hill, 1984.

7. Campbell, Ashley S., Thermodynamic Analysis of Combustion Engines. New York:
Wiley, 1979.

8. Culp, Archie W., Principles of Energy Conversion. New York: McGraw-Hill, 1979.

9. Wood, Bernard D., Applications of Thermodynamics. Reading, Mass.: Addison-
Wesley, 1982.

10. Lefebvre, Arthur H., Gas Turbine Combustion, New York: McGraw-Hill, 1983.

11. Baumeister, Theodore, and Marks, Lionel S. (Eds.), Standard Handbook for
Mechanical Engineers, 7th ed. New York: McGraw-Hill, 1967.

12. Sorenson, Harry A., Energy Conversion Systems. New York: Wiley, 1983.

13. Hill, Phillip G., Power Generation. Cambridge, Mass.: MIT Press, 1977.

14. Anon., Coal Quality Information Book, CS-5421, Interim Report. Palo Alto:
Electric Power Research Institute, December 1987.

15. Moeckel, W. E., and Weston, Kenneth C., “Composition and Thermodynamic
Properties of Air in Chemical Equilibrium,” NACA TN 4265, April 1958.

EXERCISES

3.1 Determine the mass fractions of a mixture of six grams of carbon, three grams of
sulfur, and one gram of sodium chloride.

3.2 Determine the mole fractions of a gas consisting of a mole of oxygen, eight moles
of nitrogen, a mole of CO, and two moles of CO2. Determine also the mass fractions.
What is the average molecular weight of the gas?

3.3 Write the balanced reaction equation for the complete combustion of sulfur in
oxygen. What are the mass and mole fractions of oxygen in the reactants?

3.4 Write the balanced reaction equation for the complete combustion of carbon in
oxygen. What are the mass and mole fractions of oxygen in the reactants?

3.5 Write the balanced reaction equation for the complete combustion of carbon in air.
What are the mass and mole fractions of fuel, air, oxygen, and nitrogen in the reactants?

129

3.6 Write the balanced reaction equation for the complete combustion of ethane, C2H6,
in air. What are the mass and mole fractions of fuel, air, oxygen, and nitrogen in the
reactants? What are the mass and mole fractions of carbon dioxide and water vapor in
the combustion products?

3.7 Write the balanced reaction equation for the complete combustion of propane,
C3H8,, in air. What are the mass and mole fractions of fuel, air, oxygen, and nitrogen in
the reactants? What are the mass and mole fractions of carbon dioxide and water vapor
in the combustion products. What are the mass and mole air-fuel ratios?

3.8 Write the balanced reaction equation for the complete combustion of C8H18 in air.
What are the mass and mole fractions of fuel, air, oxygen, and nitrogen in the reactants?
What are the mass and mole fractions of carbon dioxide and water vapor in the
combustion products? What are the mass and mole air-fuel ratios?

3.9 Gasoline, sometimes represented as C8H18, is burned in 25% excess air mass. What
are the mass and mole stoichiometric and actual air-fuel ratios? Determine the mass
and mole fractions of the combustion products.

3.10 Determine the lower and higher heating values of methane using the JANAF table
of heats the formation.

3.11 Determine the as-fired stoichiometric and actual air-fuel ratios for Greene,
Pennsylvania raw coal (Table 3.3) with 5% moisture and the mass and mole flue gas
compositions for combustion with 20% excess air.

3.12 Compare the stoichiometric and actual air-fuel ratios and the mole flue gas
composition for combustion with 20% excess air for the following raw and clean
(process #1) coals (Table 3.3): (a) Freestone, Texas, big brown lignite; (b) Indiana,
Pennsylvania, Freeport (upper); (c) British Columbia, Hat Creek (A zone); (d) Perry,
Illinois no. 6; (e) Muhlenberg, Kentucky no. 9; (f) Nicholas, West Virginia, Kittanning;
(g) Belmont, Ohio, Pittsburgh; (h) Big Horn, Montana, Robinson; (i) Greene,
Pennsylvania, Sewickley; (j) Kanawha, West Virginia, Stockton-Lewiston; (k) Belmont,
Ohio, Waynesburg.

3.13 If Union, Kentucky no. 11 raw coal has 10% moisture, as mined, determine the as-
mined proximate and ultimate analyses for this coal.

3.14 If Big Horn, Montana, Robinson raw coal has 15% moisture, as-mined, what are
its as-mined proximate and ultimate analyses?

3.15 Determine the ultimate analyses of the raw coals listed in Exercise 3.12 (a-e)
assuming 10% as-mined moisture.

130

3.16 Write the balanced chemical equation for the combustion of methane in
stoichiometric air. Use the table of heats of formation to determine the heats of
reaction of methane (in Btu/lbm and Btu/lb-mole), with products and reactants all at the
standard state and product water as liquid. What are the values if the product water is
vapor? Would the heat of reaction be different if the combustion were in pure oxygen?
Compare your results with tabulated heating values for methane.

3.17 Solve Exercise 3.16 in SI units: kJ/gm-mole and kJ/kg.

3.18 Calculate the heating values, in Btu/lbm and Btu/lb-mole, for the complete
combustion of hydrogen, with product water in liquid and in vapor phases. Compare
with tabulated heating values. Repeat the calculations in SI units.

3.19 Determine the heat transferred when ethane is burned (a) in stoichiometric air, and
(b) in 100% excess air. In both cases the reactants are in the standard state and
products at 1000K. Use a heat of formation of –36,420 Btu/lb-mole.

3.20 What is the adiabatic flame temperature for the combustion of ethane in air,
ignoring dissociation? Use a heat of formation of –36,420 Btu/lb-mole of ethane.

3.21 Compare the adiabatic flame temperatures for the stoichiometric combustion of
hydrogen in air and in pure oxygen, ignoring dissociation.

3.22 Determine the adiabatic flame temperature for the stoichiometric combustion in
air of Illinois no. 6 coal after the clean #2 process. Determine also its heat of
combustion, and compare with the tabulated value.

3.23* Develop a spreadsheet that determines the air-fuel ratio for coal characterized by
a dry ultimate analysis, such as given in Table 3.3. Apply it to several of the coals in
the table, as assigned by your instructor.

3.24* Develop a spreadsheet that determines the air-fuel ratio for a coal characterized
by a dry ultimate analysis, such as given in Table 3.3, and a given moisture content.
Apply it to a coal in the table and several different moisture contents, as assigned by
your instructor.

3.25* Develop a spreadsheet that determines the mass and mole, wet and dry flue gas
compositions for a coal characterized by a dry ultimate analysis, such as given in Table
3.3, and a given percentage of excess air. Apply it to several coals in the table for 20%
and 40% excess air.

______________________
*Exercise numbers with an asterisk involve computer usage.

131

3.26* Develop a spreadsheet that determines the average molecular weight, and the
mass and mole, wet and dry flue gas compositions for a coal characterized by a dry
ultimate analysis, such as given in Table 3.3, a given percentage of excess air, and a
given moisture content. Apply it to a coal in the table for 10% moisture and 10% and
20% excess air.

3.27* Develop a spreadsheet that determines the theoretical air-fuel ratio for a gas
characterized by any combination of the components of Table 3.4. Apply it to the
gases in the table, as assigned by your instructor.

3.28* Develop a spreadsheet that determines the average molecular weight, and the
mass and mole, wet and dry flue gas compositions for a gas characterized by any
combination of the components of Table 3.4 and a given percentage of excess air.
Apply it to several the gases in the table for 20% excess air.

3.29 What are the theoretical and actual air-fuel ratios and the wet and dry mole flue
gas compositions for 20% excess air for the Oklahoma natural gas in Table 3.4?

3.30 What are the theoretical and actual air-fuel ratios and the wet and dry mole flue
gas compositions for 15% excess air for the Ohio natural gas in Table 3.4?

3.31 An adiabatic gas turbine combustor burns methane at 77°F with air at 400°F. The
combustion products emerge from the combustion chamber at 3200°F. What is the air-
fuel ratio? What is the equivalent external heat transferred per lbm of air to produce this
temperature rise, assuming a mean heat capacity of 0.24 Btu/lbm-R?

3.32 An adiabatic gas turbine combustor burns methane at 25°C with air at 250°C. The
combustion products emerge from the combustion chamber at 2000K. What is the air-
fuel ratio? What is the equivalent external heat transferred per kilogram of air to
produce this temperature rise, assuming a mean heat capacity of 1.005 kJ/kg-K?

3.33 An adiabatic combustor burns methane with 400% excess air. Both air and
methane are initially at 298K. What is the exit temperature?

3.34 An adiabatic combustor burns methane with 500% theoretical air. Both air and
methane are initially at 77°F. What is the flame temperature?

3.35 An adiabatic combustor burns methane in 100% excess oxygen. Both fuel and
oxidizer enter at the JANAF tables reference temperature. What is the flame
temperature?

3.36 Calculate and tabulate the higher and lower heating values of methane, in kJ/kg-
mole and in kJ/kg.

132

3.37 Determine the theoretical air-fuel ratio and the air-fuel ratio for 20% excess air
for Muhlenberg, Kentucky, raw coal with 10% moisture.

3.38 Determine the air-fuel ratio and wet and dry flue gas mole and mass fractions for
dry Muhlenberg, Kentucky no. 9 raw coal with 20% excess air.

3.39 Solve Exercise 3.38 for the coal having 10% moisture in the as-fired condition.

3.40 Solve Exercise 3.38 for 40% excess air.

3.41* Set up a spreadsheet to solve Exercises 3.38–3.40 where it is necessary to
change only one parameter for each of the latter cases.

3.42 Using the compound composition data of Table 3.4, calculate the ultimate
(elemental) analysis, and compare with the tabular results for the following natural
gases: (a) Pennsylvania, (b) Southern California, (c) Ohio, (d) Louisiana, (e) Oklahoma.

3.43* Develop an interactive computer program to solicit and receive ultimate analysis
data for an arbitrary coal, arbitrary as-fired ash and moisture fractions, an excess air
percentage, and output the appropriate air-fuel ratio and mass and mole, wet and dry
flue gas compositions.

3.44* Develop an interactive computer program to solicit and receive ultimate analysis
data for an arbitrary coal, arbitrary as-fired ash and moisture fractions, and Orsat CO,
CO2, and O2 data. The program should determine the actual operating air-fuel ratio.

3.45* Apply the spreadsheet of Example 3.13 to determine the adiabatic flame
temperature, heat of combustion, and wet flue gas composition for stoichiometric
combustion of the liquid fuels in Table 3.6.

3.46* Develop a well-organized spreadsheet in which the user may enter a coal
ultimate analysis for C, H, O, N, and S; dry flue gas mole compositions for CO, CO2,
and 02; and as-fired moisture and ash mass fractions to determine theoretical and actual
air-fuel ratios and percentage of excess air.

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