Page 257 - Characterization and Properties of Petroleum Fractions - M.R. Riazi
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                                           June 22, 2007
  AT029-06
                        AT029-Manual-v7.cls
            AT029-Manual
                                                        20:46
                                               6. THERMODYNAMIC RELATIONS FOR PROPERTY ESTIMATIONS 237
            For practical applications the above equation is converted
            into dimensionless form in terms of parameters Z defined by  Solution—By substituting the Maxwell’s relation of Eq. (6.15)
                                                                  into Eq. (6.30) we get
            Eq. (5.15). Differentiating Z with respect to T at constant P,         ∂ H            ∂V
            from Eq. (5.15) we get                               (6.40)                 = V − T
                                                                                  ∂P  T         ∂T  P
                       ∂ Z     P   ∂V     PV     1

            (6.34)          =           +      −                  differentiating this equation with respect to T at constant P
                       ∂T      RT  ∂T      R    T 2               gives
                           P           P
                                                                                                               2
            Dividing both sides of Eq. (6.33) by RT and combining with      ∂   ∂ H        ∂V       ∂V       ∂ V
                                                                                       =        −        + T
            Eq. (6.34) gives                                                ∂T  ∂P         ∂T       ∂T        ∂T 2
                                                                                    T  P      P        P          P
                                                                                              ∂ V
                                                                                               2
                    H − H ig     P     ∂ Z     dP                 (6.41)               =−T    ∂T 2
            (6.35)         =−T               (at constant T )                                     P
                      RT            ∂T  P  P
                                0                                 From mathematical identity we have
                                                                                ∂    ∂ H          ∂    ∂ H
            It can be easily seen that for an ideal gas where Z = 1,  (6.42)              =
                                                 ig
            Eq. (6.35) gives the expected result of H − H = 0. Similarly      ∂T   ∂P  T  P  ∂P  ∂T  P  T
            for any equation of state the residual enthalpy can be calcu-  Using definition of C P through Eq. (6.20) and combining the
            lated. Using definitions of T r and P r by Eq. (5.100), the above  above two equations we get
            equation may be written as
                                                                                                2
                                                                                               ∂ V
                                                                 (6.43)            ∂C P  =−T     2
                   H − H ig       P r   ∂ Z     dP r                               ∂P  T       ∂T  P
            (6.36)        =−T  r 2            (at constant T )
                     RT c           ∂T r  P r  P r                Upon integration from P = 0 to the desired pressure of P at
                                0                                 constant T we get
            where the term in the left-hand side and all parameters in the              P         2
                                                                                   ig
            RHS of the above equation are in dimensionless forms. Once  (6.44)  C P − C =  −T  ∂ V 2  dP
                                                                                   P
            the residual enthalpy is calculated, real gas enthalpy can be             P=0      ∂T  P  T
            determined as follows:
                                                                  Once C ig  is known, C P can be determined at T and P of in-
                                        H − H                     terest from an EOS, PVT data, or generalized corresponding
                                             ig                         P
                                ig
            (6.37)        H = H + RT c
                                          RT c                    states correlations.
              In general, absolute values of enthalpy are of little interest
            and normally the difference between enthalpies in two differ-  6.1.4 Fugacity and Fugacity Coefficient
            ent conditions is useful. Absolute enthalpy has meaning only  for Pure Components
            with respect to a reference state when the value of enthalpy  Another important auxiliary function that is defined for cal-
            is assigned as zero. For example, tabulated values of enthalpy  culation of thermodynamic properties, especially Gibbs free
            in steam tables are with respect to the reference state of satu-  energy, is called fugacity and it is shown by f . This parameter
            rated liquid water at 0 C [1]. As the choice of reference state  is particularly useful in calculation of mixture properties and
                              ◦
            changes so do the values of absolute enthalpy; however, this  formulation of phase equilibrium problems. Fugacity is a pa-
            change in the reference state does not affect change in en-  rameter similar to pressure, which indicates deviation from
            thalpy of systems from one state to another.          ideal gas behavior. It is defined to calculate properties of real
              A relation similar to Eq. (6.33) can be derived in terms of  gases and it may be defined in the following form:
            volume where the gas behavior becomes as an ideal gas as

            V →∞:                                                (6.45)              lim  f  = 1
                                                                                     P→0  P
                                       ∂P                         With this definition fugacity of an ideal gas is the same as
                                 V

                         ig
            (6.38)  (H − H ) T,V =  T       − P dV + PV − RT
                                       ∂T  V                      its pressure. One main application of fugacity is to calculate
                                                                  Gibbs free energy. Application of Eq. (6.8) at constant T to an
                               V→∞
            Similar relation for the entropy departure is         ideal gas gives
                                                                                       ig
                                                                 (6.46)             dG = RTdln P
                                         ∂P     R
                                   V
                           ig
            (6.39)    (S − S ) T,V =        −    dV               For a real fluid a similar relation can be written in terms of
                                        ∂T    V
                                           V                      fugacity
                                 V→∞
                                                                 (6.47)              dG = RTdln f
            Once H is known, U can be calculated from Eq. (6.1). Sim-
            ilarly all other thermodynamic properties can be calculated  where for an ideal gas f  ig  = P. Subtracting Eq. (6.46) from
            from basic relations and definitions.                  (6.47), the residual Gibbs energy, G , can be determined
                                                                                                 R
                                                                  through fugacity:
            Example 6.1—Derive a relation for calculation of C P from          G R   G − G ig   f
            PVT relation of a real fluid at T and P.              (6.48)           =        = ln   = ln φ
                                                                               RT     RT        P
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