Page 41 - Petroleum Production Engineering, A Computer-Assisted Approach
P. 41

Guo, Boyun / Computer Assited Petroleum Production Engg 0750682701_chap03 Final Proof page 31 3.1.2007 8:30pm Compositor Name: SJoearun




                                                                                RESERVOIR DELIVERABILITY  3/31
                       The real gas pseudo-pressure can be readily determined  The flow time required for the pressure funnel to reach the
                       with the spreadsheet program PseudoPressure.xls.  circular boundary can be expressed as
                                                                         fm o c t r 2
                                                                 t pss ¼ 1,200  e  :                 (3:7)
                       3.2.2 Steady-State Flow                             k
                       ‘‘Steady-state flow’’ is defined as a flow regime where the  Because the p e in Eq. (3.6) is not known at any given time,
                       pressure at any point in the reservoir remains constant  the following expression using the average reservoir pres-
                       over time. This flow condition prevails when the pressure
                       funnel shown in Fig. 3.1 has propagated to a constant-  sure is more useful:
                                                                           p
                       pressure boundary. The constant-pressure boundary can  q ¼  kh(  p   p wf )    ,  (3:8)

                       be an aquifer or a water injection well. A sketch of the  3
                                                                    141:2B o m o ln  r e    þ S
                       reservoir model is shown in Fig. 3.2, where p e represents  r w  4
                       the pressure at the constant-pressure boundary. Assuming  where p ¯ is the average reservoir pressure in psia. Deriv-
                       single-phase flow, the following theoretical relation can be  ations of Eqs. (3.6) and (3.8) are left to readers for exer-
                       derived from Darcy’s law for an oil reservoir under the  cises.
                       steady-state flow condition due to a circular constant-  If the no-flow boundaries delineate a drainage area of
                       pressure boundary at distance r e from wellbore:  noncircular shape, the following equation should be used
                                                                 for analysis of pseudo–steady-state flow:
                             kh(p e   p wf )
                                                                           p
                       q ¼                ,                 (3:5)  q ¼   kh(  p   p wf )    ,        (3:9)

                          141:2B o m o ln  r e  þ S                         1   4A
                                    r w                                      ln
                                                                    141:2B o m o 2  gC A r 2 þ S
                                                                                 w
                       where ‘‘ln’’ denotes 2.718-based natural logarithm log e .  where
                       Derivation of Eq. (3.5) is left to readers for an exercise.
                                                                    A ¼ drainage area, ft 2
                                                                    g ¼ 1:78 ¼ Euler’s constant
                       3.2.3 Pseudo–Steady-State Flow              C A ¼ drainage area shape factor, 31.6 for a circular
                       ‘‘Pseudo–steady-state’’ flow is defined as a flow regime  boundary.
                       where the pressure at any point in the reservoir declines
                       at the same constant rate over time. This flow condition  The value of the shape factor C A can be found from
                       prevails after the pressure funnel shown in Fig. 3.1 has  Fig. 3.4.
                       propagated to all no-flow boundaries. A no-flow bound-  For a gas well located at the center of a circular drainage
                       ary can be a sealing fault, pinch-out of pay zone, or  area, the pseudo–steady-state solution is
                       boundaries of drainage areas of production wells. A sketch  kh[m(  p)   m(p wf )]
                                                                            p
                                                                 q g ¼                   ,           (3:10)
                       of the reservoir model is shown in Fig. 3.3, where p e  1,424T ln  r e  3
                       represents the pressure at the no-flow boundary at time  r w    þ S þ Dq g
                                                                               4
                       t 4 . Assuming single-phase flow, the following theoretical  where
                       relation can be derived from Darcy’s law for an oil reser-  D ¼ non-Darcy flow coefficient, d/Mscf.
                       voir under pseudo–steady-state flow condition due to a
                       circular no-flow boundary at distance r e from wellbore:
                                                                 3.2.4 Horizontal Well
                               kh(p e   p wf )                   The transient flow, steady-state flow, and pseudo–steady-
                       q ¼                  :               (3:6)  state flow can also exist in reservoirs penetrated by horizon-
                                       1
                          141:2B o m o ln  r e    þ S
                                    r w  2                       tal wells. Different mathematical models are available from
                                            h           p
                                                p e
                                                              p wf
                                              r e                          r
                                                                 r w

                                       Figure 3.2 A sketch of a reservoir with a constant-pressure boundary.
                                                p i
                                                      t 1
                                                     t 2
                                            h       t 3
                                                   t 4     p
                                                p e
                                                              p wf
                                                                           r
                                              r e
                                                                r w
                                           Figure 3.3 A sketch of a reservoir with no-flow boundaries.
   36   37   38   39   40   41   42   43   44   45   46