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         348 CHARACTERIZATION AND PROPERTIES OF PETROLEUM FRACTIONS
                                                              Slattery and Bird [38] developed a generalized chart in terms
                                                              of (PD)/(PD) versus T r and P r . The chart is in graphical form
                                                                         ◦
                                                              and is based on a very few data on self-diffusion coefficient
                                                    ∞
                                                   D BA       of simple gases, which were available six decades ago. Later
                                                              Takahashi [39] proposed a similar and identical chart but us-
               L
             D AB                                             ing more data on self- as well as some binary-diffusion coef-
                                                              ficients. Obviously these methods cannot be used with com-
                                                              puter tools and use of the charts is inconvenient to obtain
                                                              an accurate value of diffusion coefficient. However, Slattery–
                 ∞
                D AB                                          Bird chart has been included in the API-TDB [5].
                                                                Sigmund [40] measured and reported binary diffusion co-
                                                              efficient of dense gases for C 1 ,C 2 ,C 3 , n-C 4 , and N 2 for the
                                                              pressure range of 200–2500 psia (14–170 bars), temperature
                                                                                      ◦
                                                                            ◦
                   0                              1           range of 38–105 C (100–220 F) and mole fraction range of
                                  X A
                                                              0.1–0.9 for methane. Sample of Sigmund’s dataset for some
                                                              binary systems are given in Table 8.9. Sigmund also reported
               FIG. 8.6—Dependency of liquid diffusion coeffi-
             cients with composition.                         experimental data on the density of mixtures and based on
                                                              the original work of Dawson et al. [41] correlated reduced
                                                              density–diffusivity product (ρD AB ) to the reduced density in
         systems:                                             a polynomial form as follows:
                                    ∞L
                     L
        (8.64)      D AB  = (1 − x A ) × D AB     + x A D ∞L     (ρD AB)  = 0.99589 + 0.096016ρ r − 0.22035ρ + 0.032874ρ 3


                                                                                                   2
                                             BA
                                                               (ρD AB) ◦                           r          r
                         ∞L
                ∞L
         where D AB  and D BA  are diffusivities at infinite dilutions
         and are known from experiments or may be calculated from  (8.65)
                                                L
         Eq. (8.60) or (8.61). For nonideal systems D AB  calculated  where (ρD AB) is a value of (ρD AB ) at low pressure for an
                                                                          ◦
         from Eq. (8.64) must be multiplied by factor α AB defined in  ideal gas and should be calculated from Eq. (8.57). For devel-
         Eq. (8.63). This is demonstrated in Fig. 8.6 in which the binary  oping this correlation, Sigmund used liquid diffusivity data
         diffusion coefficient of ideal systems is shown by a dotted line  for binary systems of C 1 –n-C n (n varied from 6 to 16) in ad-
         while the actual diffusivity of nonideal solutions is shown by a  dition to diffusivity data of dense gases. The main advantage
         solid line. Riazi and Daubert [37] showed that corresponding  of this equation is that it can be used for both gases and liq-
         state approach can also be used to correlate diffusion coeffi-  uids and for this reason reservoir engineers usually use this
         cient of liquids and developed a generalized chart for reduced  method for calculation of diffusion coefficients of reservoir
         diffusivity (D r = D/D C ), in a form similar to Eq. (8.21), for cal-  fluids under reservoir conditions. However, the main disad-
         culation of liquid diffusivity at low pressures.     vantage of this method is its sensitivity to reduced density for
                                                              liquid systems where reduced density approaches 3. This is
                                                                                                ◦
         8.3.3 Diffusivity of Gases and Liquids at High       shown in Fig. 8.7 in which (ρD AB)/(ρD AB) is plotted versus ρ r
         Pressures                                            according to Eq. (8.65). For gases where ρ r < 1, reduced dif-
                                                                                 ◦
                                                              fusivity (ρD AB)/(ρD AB) is about unity; however, for liquids
         Pressure has significant effect on diffusivity of gases while it  where ρ r > 2.5 the curve is nearly vertical and small error
         has lesser effect on liquid diffusivity. At very high pressures  in ρ would result in a much larger error in diffusivity calcu-
         diffusion coefficients of gases approach those of liquids. For  lation. For this reason, this equation generally gives higher
         calculation of diffusion coefficients of gases at high pressures,  errors for calculation of diffusion coefficient of liquids even
                                     TABLE 8.9—Diffusion coefficient of gases at high pressures [40].
                                                                                                2
                                                                                          5
                        No.    Component A  Component B     x A      T,K      P, bar    10 D AB ,cm /s
                         1      Methane      Propane      0.896      311       14.0        883
                         2      Methane      Propane      0.472      311      137.9         22.5
                         3      Methane      Propane      0.091      311      206.8         16.9
                         4      Methane      Propane      0.886      344       13.9       1196
                         5      Methane      Propane      0.15       344      206.8         21.6
                         6      Methane      Propane      0.9        378       13.7       1267
                         7      Methane      Propane      0.116      378      168.9         36.5
                         8      Methane      n-Butane     0.946      311      137.2         55.79
                         9      Methane      n-Butane     0.973      344       13.8       1017
                        10      Methane      n-Butane     0.971      344      172.4         62.99
                        11      Methane      n-Butane     0.126      344      135.4         16.34
                        12      Methane      n-Butane     0.973      378       13.8       1275
                        13      Methane      n-Butane     0.124      378      135.1         26.82
                        14      Methane      Nitrogen     0.5        313       14.1       1870
                        15      Methane      Nitrogen     0.5        313      137.9        164
                        16      Methane      Nitrogen     0.5        366      137.8        232






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