Page 308 - Fundamentals of Reservoir Engineering
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REAL GAS FLOW: GAS WELL TESTING                              244


                                               p    - from material balance
                                               Z

                                               p

                                             k = 1


                                              1
                                                  p
                                             µ  =  ( )
                                                 µ
                                              1
                                             Z  = Z( )p
                                                                   1/ 2
                                     2  1422 Qµ k Z T    r  3
                                                 k

                             p k wf  =   p −          ln  e  −  +  S
                                            kh      
  r w  4
                                                                                                p k -1
                                                                                  k          p +  wf
                                                                                 µ      = µ     2
                                                     k = 1
                                               k                k = k +  1
                                                                                              p +  p k -1
                                                                                 Z k    =  Z      wf
                                         k  > 1                                                  2

                                 -                                  +
                                     p k wf  − p k wf -1  −  TOL            k = k +  1


                            accept p wf


                                                                    2
                     Fig. 8.2   Iterative calculation of p wf  using the p  formulation of the radial,
                                semi-steady state inflow equation, (8.5)

                     The limits of integration are between a base pressure p b and the pressure of interest p.
                     The value of the base pressure is arbitrary since in using the transformation only
                     differences in pseudo pressures are considered i.e.

                                             p  pdp      p wf  pdp   p  pdp
                             () mp
                           mp −     (  wf  ) = 2     −  2       =  2
                                             p b  µ Z    p b  µ Z    p wf  µ Z

                     As will be seen presently, it is possible, and indeed advantageous, to express all flow
                                                                                    2
                     equations in terms of these pseudo pressures rather than in the p  formulation of
                     Russell and Goodrich. However, conceptually it is more difficult and generally
                                                                  2
                     engineers feel more comfortable dealing with p  rather than an integral transformation.
                     Therefore, it is worthwhile, at this stage, to examine the ease with which these
                     functions can be generated and used.
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