![]()
Correlation Between Gas
Molecular Weight, Heating Value and Sonic Speed Under Variable Compositions of
Natural Gas
by
Dr.
L. Burstein, Dr. D. Ingman and Dr. Y. Michlin
[Published in ISA Transactions 38 (1999), 347-359]
Abstract
A simulation study of
likely uncertainties in molecular weight and heating value of the gas
mixture as predicted from measured or calculated sonic speed. The sonic
speed, molecular weight and heating value of natural gas were studied as a
function of random fluctuation of the gas fractions. A method of sonic
speed prediction was developed and used for over 50,000 computer-simulated
variants of component concentrations in four- and five-component mixtures.
Comparison of the obtained and the reference data on binary
(methane-ethane) and multicomponent (Gulf Coast) gas mixtures under
standard pressure and moderate temperatures indicates predictability of
sonic speed on the basis of the binary virial coefficients, sonic speeds
and heat capacities of the pure components. The results for two natural
gas mixtures - with and without nonflammable components - are reported.
Bivariate distribution - and covariance elliptic zone plots are presented
for three pairs of dependences of practical interest: molecular weight -
sonic speed, heating value - sonic speed and heating value - molecular
weight. The correlation coefficients, covariance, and regression equations
are given for each pair of variance and mixture.
Keywords Sonic Speed; Molecular Weight; Heating Value; Composition
Fluctuations; Natural Gas; Uncertainties; Statistical Analysis
1. Introduction
Sonic speed is widely used for improving the
accuracy of gas meters, measurement of molecular weight, in BTU-analyzers, etc.
The correlation between the molecular weight of natural gas and speed of sonic
waves is utilized in modern flowmeter apparatus (e.g. VGN868 by Panametrics or
GFS700 by Krohne) and are the subject of various inventions - e.g. US Patent No
5645071. A correlation is also known between molecular weight and gas heating
value, so that the sequence "sonic speed - molecular weight - heating
value" (see e.g. US patent No 4246773), or the direct correlation between
sonic speed and gas heating value, can be used for heating value estimation. In
that case significant uncertainty can arise due to the presence of a
nonflammable component. To a lesser extent in the case of molecular weight
determinations - and to a large extent in the case of heating value
determination - uncertainty in the gas composition leads to errors in the
determined values. This is also true for engineering calculations of these
values based on the thermodynamic properties of gas mixtures. The most accurate
values can be obtained or measured in the case of strict determination of the
gas component concentration or by comparison with reference sample (in the case
of measuring). Here we intend to study the influence of possible fluctuations
of the component concentrations in natural gas on the "molecular weight -
sonic speed" and "heating value - sonic speed" correlations with
a view to applying sonic speed testing directly to the molecular weight and
heating value measurement omitting the additional definition of gas content.
In view of the infinite diversity of gas mixtures, various
attempts are made to predict their thermal and caloric properties on the basis
of pure component data. Equations of state are widely used for this purpose -
E. A. Mason[1], J. Hirshfelder et al. [2]. In the region of moderate pressures
and temperatures the virial equation is adopted:
p =
rRT(1+
), (1)
where p, r and T are
gas pressure, density and
temperature respectively, R is the universal gas constant, B - the virial
coefficient and n its number so
that 2B - is the second virial, 3B - the third virial and
so on; in the case of a gas mixture
nB =
, . (2)
where x - component concentration; i, j and l the
component numbers.
The virial coefficients of pure components -
,
, ... - are readily available for most technical gases,
in particularly for the hydrocarbon gases - CRC Handbook [3]. By contrast, the
cross virial coefficients
,
, ... - have been less studied and are determined as combinations
of the virial coefficients of the pure gases, or of their intermolecular
constants, using the dependence of the virial coefficient on the intermolecular
potential of interaction [2]. Further, using Eq.(1), the differential equations
of thermodynamics and ideal gas functions, the density r, enthalpy I, heat capacities cp
and cv , and entropy s of gas mixtures are calculated.
The same approach may be used for determining the
thermodynamic sonic speed
c2
=
, (4)
or
c2
= k
, (5)
where k is the ratio of the heat capacities cp
and cv .
Under the ideal gas approach
= M R T, where M is the molecular weight; thus c2 = M k R T. Thus it would appear
to be possible to use the sonic speed measurements/calculations for determining
the molecular weight of pure gases and their mixtures - L. C. Lynaworth [4]. In this case
besides the uncertainty due to idealization of the gas, further uncertainty is
introduced by fluctuation of the composition. In reality it must be borne in
mind that a gas mixture may have the same molecular weight but different sonic
speeds owing to different gas component concentrations and conversely the same
sonic speed may occur at different molecular weights for the same reason. Table 1 shows that the mole fraction
concentration of secondary fractions may change by a whole order of magnitude
at constant molecular weight or at constant sonic speed. Uncertainties in M or c for such cases remain
unevaluated to date.
Table
1. Example of Molar Concentration Fluctuations:
Five
Component Gas Including a Nonflammable
Fraction
|
Methane |
Ethane |
Propane |
Butane |
Nitrogen |
|
|
Molecular weight 17.26±0.02 kmol/kg |
|
||
|
0.912 |
0.014 |
0.001 |
0.004 |
0.069 |
|
0.912 |
0.031 |
0.001 |
0.003 |
0.052 |
|
0.914 |
0.029 |
0.001 |
0.004 |
0.053 |
|
0.925 |
0.044 |
0.010 |
0.002 |
0.018 |
|
0.925 |
0.031 |
0.013 |
0.001 |
0.029 |
|
0.926 |
0.036 |
0.010 |
0.003 |
0.025 |
|
0.930 |
0.039 |
0.010 |
0.005 |
0.016 |
|
0.933 |
0.016 |
0.018 |
0.003 |
0.030 |
|
0.934 |
0.048 |
0.012 |
0.004 |
0.001 |
|
0.934 |
0.033 |
0.018 |
0.002 |
0.012 |
|
0.935 |
0.036 |
0.014 |
0.004 |
0.011 |
|
0.935 |
0.038 |
0.014 |
0.004 |
0.009 |
|
|
Sonic speed 438±2 m/s |
|
|
|
|
0.907 |
0.027 |
0.002 |
0.001 |
0.063 |
|
0.920 |
0.043 |
0.007 |
0.002 |
0.028 |
|
0.921 |
0.038 |
0.007 |
0.003 |
0.031 |
|
0.922 |
0.038 |
0.008 |
0.003 |
0.029 |
|
0.922 |
0.033 |
0.008 |
0.003 |
0.034 |
|
0.923 |
0.034 |
0.011 |
0.001 |
0.030 |
|
0.923 |
0.031 |
0.006 |
0.005 |
0.035 |
|
0.924 |
0.026 |
0.010 |
0.003 |
0.037 |
|
0.926 |
0.039 |
0.010 |
0.003 |
0.022 |
|
0.927 |
0.034 |
0.009 |
0.004 |
0.026 |
|
0.931 |
0.031 |
0.016 |
0.002 |
0.021 |
|
0.939 |
0.036 |
0.016 |
0.005 |
0.004 |
It was established that the heating value H of
natural gases for light hydrocarbons is an almost linear function of the
molecular weight, though this fact is of no practical use, as the presence of
nonflammable components in the gas mixture reduces the real heating value and
exaggerates the measured/calculated value at the same time.
So the object of this research is prediction of the
sonic speed, molecular weight and heating value of natural gas mixtures on the basis
of those and other thermodynamic data of the pure components, for a large
number of random molar concentrations; determination of the correlation between
the obtained values; statistical analysis of the results.
2. Multicomponent Gas Mixture Model in Approach to
Sonic speed.
Here we use the classical approach, in which
the thermodynamic properties of a real mixture are constituted from those of
the pure components with corrections for the ideal gas mixture approach. Such a
concept was used by L. M. Burshtein [5] for the equation of state of a gas
mixture, and can be extended to the sonic speed in it.
From Eq.(4)
=
. (6)
For m-component mixtures of constant composition,
the derivative in (6) can be determined from the equation of state (1) and the
virial coefficient equation (2).
(7)
Under normal conditions we can only use the second
virial coefficient, which for m=2 (binary mixture, x2 = 1 - x1)
equals
2B = 2B1 x12 + 2B2
x22 + 2 2B12
x1 x2 = 2B1 x1 + 2B2
x2 + (2 2B12
- 2B1 - 2B2) x1 x2
. (8)
Here and further on we use the notations
.
Taking into account that
-
= rRT(2B1 - 2B2) we obtain
=
x1 +
x2 +
x1 x2 , (9)
where
= (2 2B12
- 2B1 - 2B2)/( 2B1
- 2B2).
Thus Eq.(9) comprises the pure component values
, the correction
-
and the coefficient A representing a
combination of the second virial coefficients.
Extending the described operations to the
m-component case we have
=
xi +
xi xj , (10)
where
= (2 2Bij
- 2Bi - 2Bj)/( 2Bi
- 2Bj) .
Repeating this type of transformation with the
third, fourth and higher virial coefficients we obtain the heat capacities
ratio
. (11)
and the sonic
speed in an m - component gas mixture is
c =
. (12)
where
,
,
are given in the
Appendix.
In the case of an ideal gas mixture
=0 , and for
the ideal gas capacity ratio k = ki = Const , eq.(12) reduces to
.
For natural gases under normal conditions it
suffices to use eqs.(11,12) with the coefficients
, which include only the second virials. The cross
coefficients
and
can be found
from the rule (see ASTM Standard [6]):
![]()
(13)
Thus for the second residual virial
coefficients we have
or
in the case of a pressure-series equation of state ; now, as
an example, the equation of
is obtained as
, (14)
where B must have the same sign for different fractions;
in the case of negative B we can use its absolute value with a negative sign of
the square root. The relationship for calculating the virial coefficient for a
pure gas can be found from the equation
, (15)
where To = 298.15 and the
coefficients ai are given in the CRC Handbook[3].
Applicability of the model was checked on the B. A.
Younglove et al. [7] sonic speed data for binary methane-ethane gas mixtures
and multicomponent Gulf Coast gas, which consists of flammable and nonflammable
components. We use the data for 0.1013 MPa in the temperature range 250...400
K. As can be seen from Tables 2 and 3 the model gives more accurate values of
sonic speed throughout the data range; the one-sided uncertainty in c is not
worse than ±1.4 percent, which falls
within the inaccuracy limits of pure gas speed (dw up to 2%) , and heat
capacities (dcp above 3%)
data. For a multicomponent gas the inaccuracies are significantly smaller than
in the case of a binary mixture.
Table
2. Calculated and Measured Values of Sonic Speed , m/s. Methane - Ethane
Gas
Mixture at Standard Pressure
|
T, K |
Data [7] |
Ideal Mixture |
Deviation % |
Eqs.(28,29) |
Deviation % |
|
250 |
362 |
373.8 |
3.3 |
369.9 |
2.2 |
|
275 |
375 |
390.9 |
4.2 |
386.0 |
2.9 |
|
300 |
392 |
406.9 |
3.8 |
402.1 |
2.6 |
|
325 |
406 |
421.8 |
3.9 |
416.7 |
2.6 |
|
350 |
420 |
435.9 |
3.8 |
430.6 |
2.5 |
Table
3. Calculated and Measured Values of Sonic Speed, m/s. Multicomponent
Mixture
(Gulf Coast) at Standard Pressure
|
T, K |
Data [7] |
Ideal Mixture |
Deviation % |
Eqs.(28,29) |
Deviation % |
|
275 |
422 |
428 |
1.4 |
414 |
1.9 |
|
300 |
437 |
445 |
1.8 |
445 |
1.8 |
|
325 |
455 |
461 |
1.3 |
451 |
0.9 |
|
350 |
470 |
477 |
1.5 |
468 |
0.4 |
3. Modeling of Component Fluctuations in Natural Gas
The composition of natural gases fluctuates
according to both the number of components and their concentrations. In Table 4
the mean values of component concentrations in natural gas for the average
composition of 120 natural gases based on GRI (report 82/0037) and MTI1 data. As can be seen, methane, ethane and a certain mount of
nitrogen are always present in natural gases. The actual concentrations of
these and other components vary over a wide range, in particular for small
components.
|
|
|
|
|
|
Table
4. Average
Composition of Natural Gases*, mole % |
|||
|
Component |
Mean
Value |
Deviation |
Min.
Value |
|
Methane |
93.0 |
5.5 |
80.0 |
|
Ethane |
3.0 |
2.6 |
0.4 |
|
Propane |
1.0 |
1.4 |
0.0 |
|
Butanes |
0.5 |
1.0 |
0.0 |
|
Pentanes |
0.1 |
0.3 |
0.0 |
|
Hexane |
0.1 |
0.1 |
0.0 |
|
Nitrogen |
1.5 |
2.9 |
0.1 |
|
Carbon
Dioxide |
0.5 |
0.5 |
0.0 |
*based on GRI
and MTI-data.
It is natural to suggest that the molar
concentration is a random value, which fluctuates within certain limits. As a
result, the molecular weight of a specific natural gas may be the same while
the molar concentrations of the fractions differ. In that case the measured
sonic speed also differs and we observe a number of molecular weights instead
of the single true value. Obviously, a series of molecular weight values can
correspond to a single value of sonic speed as a result of accidental variation
of the gas component concentrations. Sonic speed calculations for the large
possible number of component concentrations have to be carried out to estimate
the inaccuracy in molecular weight or sonic speed determination due to the
random fluctuations of the molar concentration.
Such a procedure was created under the following
premises:
· the gas mixture has not less
than four flammable components, with methane as basic component;
· the concentrations of m-1
components vary as a random value normally distributed with given dispersion s; the
concentration of the last component varies between 1 and the sum of all
the others.
· zero concentrations and
those less than 0.05% are disregarded.
· if the sum of the concentrations
exceeded unity, these variants were not included in the calculations.
The MathCAD rnorm-function was used to
generate random normally distributed values of concentrations of the pure gas
components.
The molecular weight of the gas mixture
, (16)
the sonic speed - as per Eq.(12), and the gas
heating value
, (17)
were calculated from the generated values of xi.
As the gas heating value of the nonflammable
component is zero, the value for the gas mixture determined by sonic speed
measurements is erroneous both in terms of the concentrations and of the
presence of such contamination. The suggested method permits determination of
the relationship between these errors and indicates when the accuracy in
determining the heating value is sufficient.
4. Results and Discussion
The heat capacity ratio, sonic speed, molecular
weight, and gas heating value were obtained by Eqs.(11,12,16,17) using CRC data
[3] for the virial coefficients, S. S. Chen et al. [8], J. Chao et al.[9], and
R. T. Jakobson et al.[10] data for the ideal gas function and tables of J. Chao
et al. [10], R. T. Jacobson et al.[11] for methane, ethane, propane, butane,
and nitrogen. The mean values of the components were taken from Table 1, the
dispersions of these values were 0.017, 0.008, 0.004 and 0.001 for methane,
ethane, propane, and butane respectively.
The results of the M, c, H - calculations and
obtained statistical characteristics for four- and five-component gases are
presented in Figs.1 through 8 and in Table 5.
The dependences between the molecular weight and
sonic speed (Fig.1), between the gas heating value and sonic speed (Fig.2), and
between the gas heating value and molecular weight (Fig.3) were found from
46110 computer-simulated random concentrations for the four-component and 48970
computer-simulated random concentrations for the five-component gas.

Figure
1. Molecular Weight Versus Sonic Speed for Two Natural Gases Mixtures:
1- Methane + Ethane + Propane + Butanes;
2- Methane + Ethane + Propane + Butanes + Nitrogen.

Figure
2. Heating Value Versus Sonic speed for Two Natural Gas Mixtures:
1-
Methane + Ethane + Propane + Butanes;
2 -
Methane + Ethane + Propane + Butanes + Nitrogen

Figure
3. Heating Value Versus Molecular Weight for Two Natural Gas Mixtures:
1 -
Methane + Ethane + Propane + Butanes;
2 -
Methane + Ethane + Propane + Butanes + Nitrogen
As we can see from Fig.1, the changes in the molecular
weight of the gases through random fluctuation of the fraction concentrations
amounted to 20% at sonic speed fluctuation above only 3.5%. It is interesting
that with the added nonflammable nitrogen fraction (five-component gas), the
maximal molecular weight fluctuation range is half that for the same rate of
variation of the sonic speed. The accuracy of M evaluation by sonic speed
measurement or calculation is more than double in this case. The maximum
inaccuracy in molecular weight by sonic speed data is above 1.3% at sonic speed
uncertainty not more than 0.1%.
Figs.2, 3 illustrate the dependence between heating
value, sonic speed and molecular weight for four- and five-component gases.
Though the nitrogen fraction strongly influences the results, even in this
case, as it can be seen we have an interval of speeds or weights where owing to
the concentration fluctuations, the inaccuracies exceed those due to addition
of the nonflammable component.
From Fig.2,3 it follows that with an added
nonflammable component the natural gas heating value is reduced up to 30%
through variation of the gas contents; the uncertainty of the gas heating value
is about ± 2.5% for gas with
inflammable components only. Moreover, there is the probability of correct
determination of the heating value from the c data, as the range of cross-data
involves almost 20% of all possible component concentrations of the four- and
five-component mixtures .As for the H data, although the inaccuracy increases
in the presence of the nonflammable component, cross data exist here as well,
with equal heating values for both mixtures, with and without the nonflammable
component. In other words, the error in heating value or molecular weight
determined from sonic speed data, due to ignorance of the number of gas
components, may be negligible over a sufficiently wide range, unlike the error
due to concentration disturbances. The concrete values of their errors, the
bivariate distribution of variables, the covariance areas and the regression
equations are discussed further on.
Figs.4,5 show bivariate bar and surface histograms
for four (Figs.4A, 5A) and five (Figs.4B, 5B) - component gas mixtures, with
the molecular weight as X, and the sonic speed and heating value as Y.

(A)

(B)
Figure
4. Bivariate Sonic Speed-Molecular Weights Distributions
A) Methane-Ethane-Propane and Butanes Mixture;
B) Methane-Ethane-Propane- Butanes and Nitrogen Mixture.
(A)

(B)
Figure
5. Bivariate Gas Heating-Molecular Weight Distributions.
A) Methane-Ethane-Propane and Butanes Mixture;
B) Methane-Ethane-Propane- Butanes and Nitrogen Mixture
Figs.6 through 8 present the covariance 68% -, 95% -
areas and 100% - point population for the M,c - , H,c -, and H,M - pairs of
variables. Points lying in the 68% and 95% zones were screened from the values
calculated in accordance with the covariance (error) ellipse equation [12] of
the bivariate normal distribution:
, (18)
where X is c or M and Y is M or H in our
cases, s is the standard deviation, mX and mY are the means of the
frequency distributions,
is the correlation
coefficient.

A)
B)
Figure
6. Molecular Weight - Sonic Speed Covariance Ellipses for
Four
- Component (A) and Five - Component (B) Mixtures.
1- All point population
2- 95% points area
3- 68% points area

A)
B)
Figure
7. Heating Value - Sonic Speed Covariance Ellipses for
Four
- Component (A) and Five - Component (B) Mixtures.
1- All point population
2- 95% points area
3- 68% points area

A)
B)
Figure
8. Heating Value - Molecular Weight Covariance Ellipses for:
Four
- Component (A) and Five - Component (B) Mixtures.
1- All point population
2- 95% points area
3- 68% points area
Figs.6,7 can be used for determining the uncertainty
in the molecular weight or heating value from measured data of sonic speed. For
this we must draw a perpendicular from the point of the measured value of c up
to say the circumference of the 95% ellipse, which gives us the limits of error
caused by gas composition fluctuations. For example, for a measured value of
c=435±0.4m/s, from Fig.6A (flammable components only) we obtain the molecular
weight limits 17.7...18.2 or 17.95±0.25 kg/kmol and
from Fig.6B (nonflammable component present) 17.6...17.8 or 17.7±0.1
kg/kmol. This
example shows also that a nonflammable component reduces the uncertainty in the
molecular weight by more than half.
The same tendency appears in the case of the heating
value as well. For example, for aforesaid value of c, from Fig.7A (flammable
components only) we obtain the heating value limits 1040...1120
or 1080±40
BTU/ft3 and from Fig.7B (nonflammable
component present) 960...990 or 975±15 BTU/ft3. As a
nonflammable component is present in more than 120 natural gases (Table 2),
even more accurate determination of the molecular weight or heating value from
the sonic speed measurements or calculations can be expected than for gases
with flammable components only.
All the above justifies also determination of the
heating value and its error from molecular weight data - in this case Fig.8
must be used. With the regression equation as a sort of calibration curve, and
using the covariance ellipse with the appropriate statistical parameters, we
can obtain the limits of error for every concrete case. Thus, in Table 5 the
regression equations and some statistical characteristics of four (upper line),
and five (lower line) component gas mixtures are presented for three pairs of
dependences - molecular weight/sonic speed, heating value/sonic speed, and
heating value/molecular weight.
|
Table 5. Four - and Five - Component (lower line)
Gas Mixture Statistical Characteristics |
|||
|
Pair of |
M, kg/kmol - c,
m/s |
H, Btu/ft3
- c, m/s |
H, Btu/ft3
- M, kg/kmol |
|
Variables |
|
|
|
|
Correlation |
-0.99 |
-0.95 |
0.97 |
|
Coefficient |
-0.95 |
0.74 |
-0.57 |
|
Covariance |
-1.63 |
-86.97 |
23.42 |
|
|
-0.37 |
-2.19 |
28.01 |
|
Regression |
M=131.246-0.261
c |
H=7130-13.906 c |
H=119.887+53.919
M |
|
Equation |
M=59.542-0.096
c |
H=-2188+7.216 c |
H=23.115-0.005824
M |
|
Mean |
18.10 |
1096 |
1096 |
|
Value |
17.26 |
1004 |
1004 |
|
Standard |
0.096 |
12.09 |
9.63 |
|
Error |
0.062 |
13.16 |
0.16 |
The correlation coefficients are 0.99 and 0.95 for the
gas mixture without- and with the nonflammable component respectively, showing
good reliability for the weight - sound measurements. Thus the given regression
M(c) equations can be used in practice. The standard error in the molecular
weight (found from sonic speed data) is here only ±0.3% for the five - component as against ±0.5% for the four - component gas mixture.
The heating value can be determined more precisely
from molecular weight data than from sonic speed (see Table 5). In this case
the standard error in H is only about 0.02% for the five - component mixture.
5. Conclusion
Our calculations estimate that the proposed method
for obtaining the sonic speed of a gas mixture on the basis of pure component
data with correction for the interaction of heterogeneous atoms of the gas
components gives an uncertainty about ±1.4% in the case of selected
variations of natural gas.
The used simulation method of random concentration
fluctuation enables one to obtain the standard error in the molecular weight,
sonic speed and heating values.
The uncertainty range in determining the molecular
weight and heating value appears reduced on addition of a nonflammable
component.
6. Acknowledgments
The authors are indebted to Select
Corporation (9300 Wilshire Blvd., Suite 600 Beverly Hills, CA 90212, U.S.A) for
encouraging this research.
7. References
1. E. A. Mason. The Virial
Equation of State. Oxford, Pergamon Press, 1969, 297p.
2. J. Hirshfelder, C. Curtiss,
R. Bird. Molecular Theory of Gases and Liquids. University of Wisconsin. N.Y.,
L. 1954.
3. CRC Handbook of Chemistry
and Physics. A Ready Reference Book of Chemical and Physical Data. 78th
Edition, 1997, pp.6-23 - 6-42.
4. L. C. Lynaworth. Ultrasonic
Gas Flowmeters. Measurements & Control. Vol.29, No.5, Oct. 1995, pp.92-101.
5. L. M. Burshtein. The
Equation of State of a Gas Mixture for Gas-Analysis calculations. Measurement
Techniques. Plenum Publishing Corporation, Vol.18, No.12, Dec.1975,
pp.1818-1812.
6. ASTM Standard. D3588 -- 91
Standard Practices for Calculating Heat Value, Compressibility Factor, and
Relative Density (Specific Gravity) of Gaseous Fuels.
7. B. A. Younglove,
N.V.Frederick. Sonic speed Measurements on Gas Mixtures of Natural Gas
Components Using a Cylindrical Resonator. Int. Journal of Thermophysics. Vol.
11, No 5, Dec. 1990, pp.897-910.
8. S. S. Chen, R.C.Wilhoit, B.
J. Zwolinski. Ideal Gas Thermodynamic Properties and Isomerization of n-Butane
and Isobutane. J. Phys. Chem. Ref.
Data, Vol. 4, No 4, 1975, pp.859-867.
9. J. Chao, R.C.Wilhoit, B. J.
Zwolinski. Ideal Gas Thermodynamic Properties of Ethane and Propane. J. Phys.
Chem. Ref. Data, Vol.2, No 2,1973, pp. 427-436.
10.R. T. Jacobson, R. B.
Stewart. Thermodynamic Properties of Nitrogen from the Freezing Line to 2000 K
at pressures to 1000 Mpa. J.Phys. Chem. Ref. Data, Vol.15, No 2, 1986, pp.
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Purves. Statistics. 3rd Edition, 1997, New York.
Appendix
Sonic
Speed for Multicomponent Gas Mixture through the Complete Virial Equation
At moderate and higher pressures the third and
higher virial coefficients have to be taken into account. In that case we must
execute with every virial coefficient of mixture the same conversion as it was
done for the second virial. So for the third virial for instance we have
3Bmix = 3B1
x1 + 3B2 x2 + (3 3B112
- 2 3B1 - 3B2) x1 x2
+ [(3B1 + 3B2) - 3(3B112
- 3B122)] x1 x22 . (A1)
Taking into account the fourth and higher
virials we obtain
=
xi +
. (A2)
Here xi >
xj and
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,
(A3)
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,
...,

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,
and
we shall call the residual
virial coefficients.
Dropping the terms with higher degrees of xi
and xj (as the residual virials and their products with the higher
degrees of molar concentration are very small) we obtain
=
xi +
. (A4)
In this equation the mixture heat capacity ratio is
still undetermined. Thus the capacities cp and cv have to
be rewritten in terms of those of the pure components. From the differential
relation
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(A5)
we have
=
- T
dp , (A6)
where
- the heat capacity of the ideal gas and v = 1/r.
Using the
virial equation of state expanded in a pressure series:
v =
( 1 +
) (A7)
in which
,
, ... , we have
(A8)
and
-
RT
. (A9)
Using now the
relation nB for the mixture and the equation
=
+ RTp
. (A10)
with
=
i -
j , we obtain for the m
component mixture
, (A11)
where
And
as
so by analogy
with the derivation of c we obtain
. (A13)
For the heat
capacity at constant volume
=
+ T
dv (A14)
using
equation of state (1) we can obtain
(A15)
or
. (A16)
with
. (A17)
Thus the heat
capacity ratio for the gas mixture has the form
. (A18)
From eq.(A2),
the sonic speed in an m-component gas mixture is
c =
. (A19)
So far eqs. (A1, A7, A11, A15) were constructed on the
basis of the virial equations of state without any simplifications, as they are
rigorous throughout the range of applicability of the virial equation.
The author apologizes for possible mistakes in mathematical expressions
and other absurdities caused by MSWord which was used for
creation this html file from original document
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