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6.8.  LIQUID-GAS  FLOW  IN  PIPELINES  111

             one is obtained as follows. Begin with                 Although  the  key  equations  are  transcendental,  they  are
                                                                 readily  solvable  with  hand  calculators,  particularly  those  with
                                                                 root-solving provisions. Several charts to ease the solutions before
                                                         (6.78)   the  age of  calculators have  been  devised: M.B.  Powley, Can. J.
                                                                 Chem.  Eng.,  241-245  (Dec.  1958); C.E.  Lapple,  reproduced  in
                                                         (6.79)   Perry’s Chemical Engineers’ Handbook,  McGraw-Hill, New  York,
                                                                 1973,  p.  5.27;  0. Levenspiel,  reproduced  in  Peny’s  Chemical
                                                                 Engineers’  Handbook,  McGraw-Hill, New  York,  1984,  p.  5.31;
             from which
                                                                 Hougen, Watson, and Ragatz, Themodyiurmics, Wiley, New York,
                                                                 1959, pp. 710-711.
                                                         (6.80)     In all compressible fluid pressure drop calculations it is usually
                                                                 justifiable to evaluate the friction factor at the inlet conditions and
                                                                 to  assume  it  constant.  The  variation  because  of  the  effect  of
             and the integral is                                 temperature  change on the  viscosity  and  hence  on the  Reynolds
                                                                 number, at the usual high Reynolds numbers, is rarely appreciable.
                                                          (6.81)
                                                                 NONlDEAL GASES
             Also
                                                                 Without the assumption of gas ideality, Eq. (6.71) is
                                 dV
                 VdP  = d(PV) - (PV) 7                    (6.82)

             Substitutions into Eq. (6.71) result in
                                                                 ‘In the isothermal case, any appropriate PVT equation of state may
                                                                 be  used  to  eliminate  either  P  or  V  from  this  equation  and  thus
                 d(PV) - PV-  + - VdV +-  fG2  dL = 0.   (6.83)   permit integration.  Since most of  the useful equations of  state are
                          dV  G2
                              gc      2gcD                       pressure-explicit, it is simpler to eliminate P. Take the example of
                                                                 one of  the  simplest of  the  non-ideal  equations,  that  of  van  der
             Further  substitutions from Eqs.  (6.80)  and  (6.81) and multiplying   Waals
             through by 2kgc,lG2V2 result in
                                                                        RT
                                       dV
                 2--  dV   [  ;; -I- (k - l)Vi] p + (k - 1) - - dL = 0.   p=---   a                          (6.91)
                                                dv  kf
                       -- ZkgPV
                                                   +
                                                                       V-b  V2’
                  V         I                    V  D
                                                         (6.84)   of which the differential is
             Integrating from VI to V2 and L = 0 to L gives
                                                                    dp=  -~ RT  + ”> dV.
                                                                        (  (V-b)’   V3
                                                                 Substituting into Eq. (6.90),
                                                          (6.85)
             or                                                                                              (6.93)

                                                                 Although  integration  is  possible  in closed form,  it  may  be  more
                                                                 convenient  to  perform  the  integration  numerically.  With  more
                                                                 accurate  and  necessarily  more  complicated  equations  of  state,
                                                                 numerical integration will be mandatory. Example 6.13 empioys the
             In terms of  the inlet Mach number,                 van der Waals equation of steam, although this is not a particularly
                                                                 suitable one; the results show a substantial difference between the
                                          ~
                                     ~
                 MI = u   l     /  = GVl/aT/M,,  ~        (6.87)   ideal and the nonideal pressure drops.  At the inlet condition, the
                                                                 compressibility factor of  steam is I = PV/RT = 0.88,  a substantial
              the result becomes                                 deviation from ideality.

                                                                 6.8. LIQUID-GAS  FLOW  IN PIPELINES
              When everything else  is  specified,  Eqs.  (6.86)  or  (6.88) may  be   In flow of  mixtures of the two phases in pipelines, the liquid tends
              solved for the exit specific volume V,.  Then Pz may be found from   to wet  the  wall  and the  gas  to  concentrate  in the  center  of the
              Eq. (6.81) or in the rearrangement                 channel,  but  various  degrees  of  dispersion of  each  phase  in  the
                                                                 other may exist, depending on operating conditions, particularly the
                                                          (6.89)   individual flow  rates.  The  main  patterns  of  flow  that  have  been
                                                                 recognized are indicated on Figures 6.7(a) and (b).  The ranges of
                                                                 conditions over which individual patterns exist are represented on
              from which the outlet temperature likewise may be found.   maps like those  of  Figures 6.7(c) and  (d).  Since the  concept of  a
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