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							                           DISCLAIMER

This report was prepared as an account of work sponsored by an
agency of the United States Government. Neither the United States
Government nor any agency Thereof, nor any of their employees,
makes any warranty, express or implied, or assumes any legal
liability or responsibility for the accuracy, completeness, or
usefulness of any information, apparatus, product, or process
disclosed, or represents that its use would not infringe privately
owned rights. Reference herein to any specific commercial product,
process, or service by trade name, trademark, manufacturer, or
otherwise does not necessarily constitute or imply its endorsement,
recommendation, or favoring by the United States Government or any
agency thereof. The views and opinions of authors expressed herein
do not necessarily state or reflect those of the United States
Government or any agency thereof.
                 DISCLAIMER

Portions of this document may be illegible in
electronic image products. Images are produced
from the best available original document.
                                                     FE-2346-20 (APP.)
                                                     (SSS-R-78-3442)
                                                Distribution Category UC-91




                     DON SHALE SITE
       TRACER GAS        PRESSURIZATIOl STUDY


                      E , W , PETERSON
                       P,' L', LAGUS                                    NOTICE

                                                sponsored by the United Stater Government. Netther the
                                                United Stater nor the United Stater Department or
                                                Energy, nor any o f their employees. nor any of their
                                                contractors. subcontractors, or their employees, maker
                                                any warranty. express or tmplled, or assumes any legal
                                                liability or responsibllily for the accuracy, completeness
                                                or usefulness of any information, apparatus, product or
                                                proeess dscloscd, or represenrs that its use would not

                      F i n a l Report
                3
            S        P r o j e c t No. 32021




                      OCTOBER 1977




                      Submitted to
                    Dow Chemical Co.




SYSTEMS, S C I E N C E A N D S O F T W A R E
                                 TABLE OF CONTENTS


Section                                                         Page

  1.       INTRODUCTION                                           1
  2.       RESULTS
                                                                  3
           2.1   Flow through the Antrim Formation                6
           2.2   Permeability and Porosity of the Retort         11
                 Volume
                 2.2.1   Injection Well Characteristics          12
                 2.2.2   Cross-Hole Permeabilities               13
                 2.2.3   Two-Dimensional Analyses of Retort      22
                         Region
                 2.2.4   Summary of Pzrneability and Porosity    31
                         Analysis
           2.3   Characterization of the Fracturing              32
 3.        CONCLUSIONS                                           35

  4   -.   RECOMMENDAT IONS                                      37


           APPENDIX A    -   Data Summary                        41
           APPENDIX B    -   Experimental Techniques             71
           APPENDIX C    -   Analytical Model                    79

           APPENDIX D    -   Wellbore Effects                    85




                                    ii
                       1.   INTRODUCTION

                                           3
       Systems, Science and Software (S 1 has developed tracer-
gas/pressurization techniques necessary to determine critical
media properties of undergrcund regions. .Application of this
technology is especially relevant to analysis of an oil shale
retort volume. During the period 7 July to 14 July 1977, a
series of tracer g a s pressurization experiments were undertaken
at the Dow shale site at Peck, Michigan. General objectives of
this study were to:
    0   Evaluate flow communication between boreholes open to
        both the Antrim and False Antrim layers of the retort
        volume.
    e   Determine permeability and porosity distributions within
        the retort volume.
    0   Assess qualitatively the uniformity of the fracturing
        or rubblization within the retort volume.
This report summarizes the results of the tracer gas pressur-
ization study. The system cross-hole flow communication, per-
meability and porosity distributions, and fracturing uniformity
are discussed in detail. The influence of these individual
characteristics on the total system response is also presented.
Conclusions and recommendations are made.
       A'set of appendices is also included. The first presents
graphical displays of all data, together with brief interpretive
narratives. Experimental techniques are described in the second
appendix. Descriptions of the analytical and numerical models
used for data interpretation are presented in the final two
appendices.
       Theresults given here represent our best effort to char-
acterize the Dow shale site. Conclusions presented are based
on the interpretation of the tracer gas pressurization data
only. Our knowledge of the Dow shale site is therefore some-
what limited. We recognize that the tracer gas pressurization
data taken in conjunction with additional data obtained using

                               1
other diagnostic methods may lead t o somewhat different con-
clusions as to the characteristics of the Dow s i t e .




                                                                c
                                2
                          2.   RESULTS


       The objective of the study was to determine the char-
acteristics of the retort volume, shown in Figure 1, in terms of
the tracer gas pressurization data. Experimental tests were
designed to provide answers to the following questions:
    e   Is there flow through the Antrim formation in the
        region of Well # 4 ?
        What is the dist.ribution of permeability and porosity
        throughout the retort volume?
        If the volume is fractured or rubblized, is this
        fracturing uniform or is there excessive flow channeling?
        How does the permeability and porosity of the forgation
        surrounding Well # 4 compare to that in the vicinity of
        Well # 3 ?
These questions will be specifically addressed in the following
sections.
       The tracer gas pressurization data serve as the basis
for evaluation of the Dow retort volume. Data available from
these tests include injection well measurements of air flow
rates, tracer gas concentrations and pressures. In addition,
pressures, flow rates, and tracer gas arrival times and con-
centrations are measured at the production wells. A summary
of the data obtained during the 7 July through 14 July test is
presented in Appendix A.
       The test proceeded as follows. Well # 4 had been de-
signated by Dow as the next "burn" well and was therefore the
primary subject of this investigation. Prior to pressurizing
this well, tracer gases were injected into Wells # 7 and # 3 .
The intent of this preinjection was to introduce tracer gas at
some outlying areas to provide better flow definition throughout
the system. Primary injection occurred in Well # 4 . Approximately
240,000 standard cubic feet (scf) of air were injected into


                               3
           n
     m
    c:
     11)
     3
    0
    a
     a,
0   c
    u
8
t h i s w e l l o v e r a 96 h o u r t i m e p e r i o d d u r i n g w h i c h i t s p r e s s u r e
increased t o approximately 850 psi.                     During t h e p r e s s u r i z a t i o n
p h a s e , four p u l s e s of v a r i o u s t r a c e r g a s e s were i n j e c t e d i n t o
Well # 4 .       P r e s s u r e s and tracer g a s a r r i v a l s and c o n c e n t r a t i o n s
were c o n s t a n t l y m o n i t o r e d a t t h e p r o d u c t i o n w e l l s t h r o u g h o u t
t h e d u r a t i o n of t h e t e s t .

            A d d i t i o n a l t e s t s were p e r f o r m e d , a t t h e r e q u e s t of DOW,
u s i n g Well # 3 a s t h e i n j e c t i o n w e l l i n o r d e r t o o b t a i n d e t a i l e d
i n f o r m a t i o n on t h e f o r m a t i o n p r o p e r t i e s i n t h e v i c i n i t y of t h i s
well.      A p p r o x i m a t e l y 1 1 0 , 0 0 0 scf of a i r were i n j e c t e d i n t o t h i s
w e l l o v e r a 24 h o u r t i m e p e r i o d d u r i n g w h i c h i t s pressure i n -
c r e a s e d t o a p p r o x i m a t e l y 775 p s i .    Two d i s t i n c t t r a c e r g a s p u l -
ses were i n j e c t e d i n t o Well # 3 d u r i n g t h i s t i m e .             Again, a l l
p r o d u c t i o n w e l l s were m o n i t o r e d d u r i n g t h e t e s t .

            I n p e r f o r m i n g t h e s e v a r i o u s t r a c e r tests, it w a s nec-
e s s a r y , i n o r d e r t o unambiguously i n t e r p r e t tracer g a s a r r i v a l
a n d c o n c e n t r a t i o n d a t a f r o m t h e many b o r e h o l e s , t o u s e n u m b e r s
of t r a c e r g a s e s .     The r e s u l t s d e s c r i b e d h e r e were o b t a i n e d
u s i n g s u l f u r h e x a f l u o r i d e ( S F 6 ) a n d t h e F r e o n s 13B1, C318 a n d
12B2 a s t r a c e r s .      I n a d d i t i o n , i n j e c t i o n p u l s e d u r a t i o n s and
c o n c e n t r a t i o n s were v a r i e d a s was n e c e s s a r y t o i d e n t i f y mul-
t i p l e i n j e c t i o n s of a p a r t i c u l a r t r a c e r g a s . A summary of t h e
e x p e r i m e n t a l t e c h n i q u e s is g i v e n i n A p p e n d i x B.

           Under c o n d i t i o n s w h e r e t h e r e t o r t volume i s a c t u a l l y
r u b b l i z e d , d a t a r e d u c t i o n i s accomplished u s i n g a two-dimensional
h y d r o d y n a m i c code w h i c h d e s c r i b e s t h e d i f f u s i v e f l o w of t h e
i n j e c t e d a i r p l u s t r a c e r g a s t h r o u g h o u t t h e r e t o r t volume.
T h i s h y d r o d y n a m i c m o d e l i s d e s c r i b e d i n A p p e n d i x C.    Also i n -
c l u d e d i n A p p e n d i x C a r e d e t a i l e d d e s c r i p t i o n s of m e t h o d s u s e d
t o d e t e r m i n e c r o s s - h o l e p e r m e a b i l i t i e s based o n m e a s u r e d t r a c e r
g a s i n j e c t i o n and a r r i v a l times. A m o d e l w h i c h c a n be u s e d
t o a p p r o x i m a t e f r a c t u r e d i m e n s i o n s , s h o u l d i t be deemed t h a t cross-
h o l e f l o w o c c u r s a l o n g a --- i t e number of f r a c t u r e p a t h s r a t h e r
                                            fin
t h a n t h r o u g h a permeable f o r m a t i o n , i s a l s o i n c l u d e d .

                                                  5
            B e c a u s e t h e Dow r e t o r t volume h a s a l o w p o r o s i t y , w e l l -
                                                                                                               @
bore e f f e c t s a r e s i g n i f i c a n t . The w e l l volume p l a y s a n i m p o r -
t a n t role i n i n t e r p r e t i n g p r e s s u r e , f l o w r a t e s , and tracer gas
c o n c e n t r a t i o n measurements.         The i n f l u e n c e of wellbore e f f e c t s
on i n t e r p r e t a t i o n of t h e s e d a t a a r e d i s c u s s e d i n A p p e n d i x D.
2.1         FLOW THROUGH THE A N T R I M FORMATION
            The m u l t i p l e t r a c e r g a s i n j e c t i o n t e c h n i q u e d e s c r i b e d
i n F i g u r e 2 was u s e d t o d e t e r m i n e i f f l o w o c c u r s t h r o u g h t h e
A n t r i m f o r m a t i o n i n t h e v i c i n i t y of W e l l # 4 . During p r e s s u r -
i z a t i o n of Well # 4 , a i r w a s i n j e c t e d i n t o t h e a n n u l u s r e g i o n a t
t h e wellhead.          A t r a c e r g a s was t h e n i n j e c t e d t h r o u g h t h e c a p -
i l l a r y t u b e w h i c h e x t e n d e d i n t o t h e A n t r i m t o a d e p t h of 1 2 6 5
ft.       S m a l l a m o u n t s of t r a c e r g a s ( % l o 0 s c f ) w e r e i n j e c t e d
t h r o u g h t h e c a p i l l a r y t u b e once t h e w e l l p r e s s u r e had approached
i t s maximum v a l u e of a b o u t 8 0 0 p s i .               A t these pressures the
wellbore c o n t a i n s more t h a n 1 4 0 0 scf of a i r b e t w e e n t h e e n d of
t h e c a p i l l a r y t u b e a n d t h e t o p of t h e A n t r i m f o r m a t i o n .       There-
f o r e , t h e s m a l l v o l u m e of i n j e c t e d t r a c e r c a n n o t d i s p l a c e
s u f f i c i e n t a i r i n t h e wellbore t o r e a c h t h e F a l s e A n t r i m l a y e r .
I f air i n j e c t e d i n t o W e l l # 4 travels t o t h e o u t l y i n g w e l l s
t h r o u g h t h e F a l s e A n t r i m l a y e r , t h i s a i r s h o u l d be f r e e of
tracer gas upon a r r i v a l a t t h e o u t l y i n g w e l l s .                However, if t h e
f l o w f r o m W e l l 84 o c c u r s through t h e Antrim l a y e r , tracer g a s
i n j e c t e d t h r o u g h t h e c a p i l l a r y s h o u l d be d e t e c t e d a t t h e p r o d u c -
tion wells.

           F l o w from W e l l # 4 t h r o u g h t h e A n t r i m          formation is
i l l u s t r a t e d schematically i n F i g u r e 3 .             T h e C318 i n j e c t e d
t h r o u g h t h e c a p i l l a r y a t 0330 o n 1 0 J u l y was f o u n d t o h a v e
p e n e t r a t e d t o Wells # 3 , # 6 , # 8 ,       #lo    and #12.         The 13B1 i n j e c t e d
t h r o u g h t h e c a p i l l a r y a t 0930 o n 11 J u l y was fbund o n l y a t Wells
113 a n d #12.       Two s i g n i f i c a n t c h a n g e s o c c u r r e d w i t h i n t h e s y s -
t e m b e t w e e n t h e i n i t i a l C318 i n j e c t i o n a n d t h e l a t t e r 13B1 i n j e c t i o n .
There e x i s t e d c o n s i d e r a b l e b r i n e f l o w i n t o W e l l # 6 . A t 1 7 0 0 o n


                                                  6
                                         ' . I n j e c t t r a c e r g a s 8 1 at b o t t o m
    I n j e c t a i r plus                  of retort r e g i o n ( a b o v e b r i n e l e v e l )
    tracer gas I 2                          u s i n g s m a l l diameter t u b e
                                                                                                      rface




F i g u r e 2.   Schematic i l l u s t r a t i n g m u l t i p l e tracer-gas i n j e c t i o n
                 i n t o a s i n g l e b o r e h o l e i n o r d e r t o e v a l u a t e f l o w through
0                the A n t r i m and F a l s e A n t r i m l a y e r s .



                                           7
                                                                          C318 i n j e c t e d t h r o u g h
                                                                          W e l l r(4 c a p i l l a r y b e g i n -
                                                                          n i n g 0330 o n 1 0 J u l y .
                                                              ----        13B1 i n j e c t e d t h r o u g h
                                                                          W e l l # 4 c a p i l l a r y begin-
                                                                          n i n g 0930 o n 1 J u l y1
                                                                          ( c o n f i r m a t i o n of a r r i v a l
                                                                          o f t h i s tracer a t W e l l
                                                                          1 1 2 is u n c e r t a i n ) .




                                                      Note:   T h e l i n e s shown are o n l y
                                                              intended to illcstrate t h e
                                                              cross-hole comunication
                                                              a n d are n o t i n t e n d e d t o
                                                              i l l u s t r a t e t h e p a t h traveled
                                                              by t h e g a s .




Figure 3.   Schematic i l l u s t r a t i n g cross-hole tracer gas flow o r i g i n a t i n g
            in Antrim f o r m a t i o n a t Well # 4 .
1 0 J u l y t h e c a p i l l a r y l i n e i n Well # 6 became b l o c k e d w i t h
b r i n e thereby preventing f u r t h e r tracer d e t e c t i o n a t t h i s w e l l .
A t 1 0 0 0 on 11 J u l y Well # 3 was v e n t e d to a b a c k p r e s s u r e of
8 0 p s i g f r o m i t s m a x i m u m p r e s s u r e of 3 0 0 p s i g .       Subsequent t o
v e n t i n g # 3 , t h e r e was n o a d d i t i o n a l f l o w i n t o Wells 118 o r         #lo.
Even t h o u g h p r e s s u r i z a t i o n c o n t i n u e d o n Well # 4 , t h e p r e s s u r e a t
Wells # 8 a n d # 1 0 r e m a i n e d c o n s t a n t f o r t h e d u r a t i o n of t h e t e s t .
Flow i n t o t h e s e wells a p p e a r s t o d e p e n d o n t h e pressure f i e l d i n
t h e v i c i n i t y of Well # 3 .

           Cross-hole communication through t h e Antrim f o r m a t i o n
b e t w e e n \ < e l l s # 4 a n d # 7 may e x i s t .     However, C318 w a s n o t
d e t e c t e d a t Well # 7 , p o s s i b l y b e c a u s e t h e h i g h p r e s s u r e i n t h e
r e g i o n or t h i s w e l l e f f e c t i v e l y b l o c k e d t h e f l o w .   Even a t l a t e r
t i m e s , a 13B1 a r r i v a l i s n o t a p p a r e n t , h o w e v e r , t h i s a r r i v a l may
be masked b y t h e r e s i d u a l 13B1 r e m a i n i n g from t h e p r e i n j e c t i o n
of t r a c e r i n t o Well # 7 .

           S u l f u r h e x a f l u o r i d e was i n j e c t e d w i t h t h e m a i n a i r f l o w
i n t o Well # 4 o n t w o o c c a s i o n s . Any t r a c e r i n j e c t e d a t t h e
w e l l h e a d becomes t h o r o u g h l y m i x e d w i t h a i r p r i o r t o r e a c h i n g
t h e F a l s e Antrim or Antrim l a y e r s .               S i n c e t h i s t r a c e r may l e a v e
W e l l # 4 t h r o u g h e i t h e r l a y e r , i t i s of i n t e r e s t t o compare t h e
r e s u l t i n g c r o s s - h o l e communication w i t h t h a t determined u s i n g
c a p i l l a r y i n j e c t e d tracer g a s e s which must f l o w through t h e
Antrim layer.

           T h e f i r s t SF6 i n j e c t i o n o c c u r r e d a t t h e t i m e t h e Well # 4
pressurization was initiated.                       The r e t o r t v o l u m e p r e s s u r e s were
l o w a t t h i s t i m e e x c e p t i n t h e n e a r v i c i n i t y of W e l l # 7 . T h i s
SF6 p u l s e was d e t e c t e d a s shown o n F i g u r e 4 , a t Wells # 3 , #6,
a n d #12, b u t n o t a t Wells # 8 a n d #lo. A s e c o n d SF6 i n j e c t i o n
occurred b e g i n n i n g a t 0 9 0 0 o n 11 July. T h i s p u l s e was d e t e c t e d a t
Wells # 3 , 117 a n d #12. A g a i n , d e t e c t i o n a t W e l l & 6 w a s p r o h i b -
ited b y the h i g h b r i n e l e v e l . Eote t h a t b o t h SF6 i n j e c t i o n s
o c c u r r e d when t h e W e l l # 3 p r e s s u r e w a s l o w . N e i g h e r SF6 p u l s e
was d e t e c t e d a t Wells # 8 o r #lo.

                                                   9
        8                                                                    SF6 i n j e c t e d t h r o u g h
                                                                             Well # 4 a n n u l u s b e q i n -
                                                                             i n g at 1 6 5 0 o n 9 J u l y .
                                                                    - .- --  SF6 i n j e c t e d t h r o u g h
                                                                             W e l l 1 4 annulus begin-
                                                                             n i n g a t 0 9 0 0 o n 11 J u l y .
                                                                   -- --     13B1 i n j e c t e d i n t o Well
                                                                             17 annulus beginning
                                                                             0 6 5 0 o n 9 July.
                                                                   - 0   -12B2       i n j e c t e d i n t o Well
                                                                             1 3 at 1430 o n 8 J u l y .




Figure 4.   Schematic i l l u s t r a t i n g cross-hole t r a c e r gas flow o r i g i n a t i n g
            i n e i t h e r t h e A n t r i m or False Antrim f o r m a t i o n a t Well # 4 .
!id
               SF detection at Well # 7 implies communication with
                 6
      Well # 4 . Furthermore, the absence of a noticeable C318 or
      13B1 arrival strongly implies little communication occurs through
      the Antrim between these wells. However, interpretation of the
      cross-hole communication between these wells is difficult to
      assess because of the initial high pressures at the immediate vic-
      inity of Well #7.
             The capillary tube extended into the Antrim formation only
      in Well # 4 . In most other wells, it cannot be determined
      whether tracer gas flow occurred through the Antrim or False Antrim
      layers. However, since the brine level in Well ti3 was always
      higher than the top of the Antrim, it is known that gas flow
      into Well # 3 came through the False Antrim. Obviously, the
      transition area in which the flow from Well # 4 passed from
      the Antrim into the False Antrim cannot be located from results
      of these tests, It can only be determined that initially some
      flow exits Well # 4 through the Antrim formation.
      2.2    PERMEABILITY AND POROSITY OF THE RETORT VOLUME

              Values for the retort volume permeability and porosity,
      as determined by she tracer gas pressurization tests, will be
      presented in this section. The methods of analysis used are
      described in Appendix C. First, one-dimensional results
      describing the permeability and porosity in the immediate
      vicinities of the injection wells will be given. These results
      are based on the well pressurization data. Following this,
      cross-hole permeabilities, calculated assuming flow occurs through
      discrete channels at speeds determined by measured tracer-gas
      transit times, will be presented. Next, the results of two-
      dimensional calculations describing the gas flow through the
      retort volume are given. Finally, characteristics of the retort
      volume such a s uniformity and flow channeling, will be discussed
      i n terms of the data previously presented.



                                   11
2.2.1       Injection W e l l Characteristics

           One-dimensional             axisymmetric a n a l y s e s are performed i n
order t o d e t e r m i n e t h e a v e r a g e f o r m a t i o n c h a r a c t e r i s t i c s i n t h e
i m m e d i a t e v i c i n i t y of a n i n j e c t i o n w e l l .      T h e s e r e s u l t s re-
p r e s e n t s o l u t i o n s t o E q u a t i o n ( C . 5 ) a s s u m i n g c y l i n d i r c a l sym-
metry with formation p r o p e r t i e s varying o n l y i n t h e radial
direction.              Wellbore e f f e c t s , d i s c u s s e d i n A p p e n d i x D , a r e
considered.               Numbers o f c a l c u l a t i o n s a r e p e r f o r m e d a s s u m i n g v a r -
i o u s c o m b i n a t i o n s o f p e r m e a b i l i t y a n d p o r o s i t y u n t i l o n e is
o b t a i n e d i n which t h e measured and c a l c u l a t e d p r e s s u r e s a g r e e .
V a l u e s u s e d f o r t h a t p a r t i c u l a r c a l c u l a t i o n a r e t h e n assumed
r e p r e s e n t a t i v e of t h e f o r m a t i o n .    S i n c e t h e s e r e s u l t s a r e based
on t h e e a r l y t i m e p r e s s u r i z a t i o n d a t a , f o r m a t i o n p r o p e r t i e s
so d e t e r m i n e d a r e o n l y v a l i d i n t h e immediate v i c i n i t y of t h e
injection well.

          Corresponding pressure/time h i s t o r i e s a t a d j a c e n t w e l l s
are a l s o d e t e r m i n e d d u r i n g t h e s e one-dimensional c a l c u l a t i o n s .
A l t h o u g h t h e s e h i s t o r i e s may i n some cases compare w i t h t h e
m e a s u r e d d a t a , t h e c o m p a r i s o n i s somewhat f o r t u i t o u s s i n c e
wellbore e f f e c t s c a n n o t be a d e q u a t e l y i n c l u d e d i n t h e s e a x i -
symmetric c a l c u l a t i o n s f o r w e l l s o t h e r t h a n t h e i n j e c t i o n w e l l .
The i n d i c a t e d p r e s s u r e r i s e a t t h e s e o u t l y i n g w e l l s w o u l d n o t
o c c u r i f w e l l b o r e e f f e c t s were c o n s i d e r e d s i n c e t h e f o r m a t i o n
c a n n o t t r a n s m i t t h e r e q u i r e d q u a n t i t y o f f l o w g i v e n t h e permea-
. b i l i t y shown.     The r e s u l t s d o , h o w e v e r , g i v e some i n d i c a t i o n of
t h e total formation porosity.

           A p r i m a r y o b j e c t i v e of t h e a x i s y m n i e t r i c c a l c u l a t i o n s was
t o p r o v i d e b a s i s f o r i n i t i a t i o n o f t h e more c o m p l e x t w o -
d i m e n s i o n a l a n a l y s i s . A s e c o n d a r y o b j e c t i v e was t o p r o v i d e
a comparison of t h e a v e r a g e media p r o p e r t i e s i n t h e v i c i n i t y
of Wells # 3 and # 4 s o t h a t phenomena o b s e r v e d t o o c c u r d u r i n g
" b u r n s " i n i t i a t e d a t t h e s e w e l l s c a n be a n a l y z e d i n terms of
the formation properties.


                                                12
d
6              R e s u l t s of t h e o n e - d i m e n s i o n a l . a x i s y m m e t r i c a n a l y s i s a r e
    shown i n F i g u r e s 5-7 f o r Wells # 4 , # 3 , a n d # 7 , r e s p e c t i v e l y .
    Measured a n d c a l c u l a t e d p r e s s u r e h i s t o r i e s a g r e e f o r W e l l # 4
    i f t h e formation permeability is taken a s 0.045 m i l l i d a r c i e s
    a n d i f t h e p o r o s i t y i s a s s u m e d t o be 0 . 1 f o r a r a d i u s l e s s t h a n
    1 . 7 5 f t , a n d 0.001 f o r r a d i i g r e a t e r t h a n 1 . 7 5 f t .              Since the
    wellbore d i a m e t e r i n t h e A n t r i m f o r m a t i o n i s a p p r o x i m a t e l y
    F 3/4 i n c h e s , t h e i n c r e a s e d p o r o s i t i e s o u t to t h e 1 . 7 5 f t r a d i i
    i m p l y t h e f o r m a t i o n i n m e d i a t e l y s u r r o u n d i n g t h e w e l l was f r a c -
    t u r e d or r u b b l i z e d t o some e x t e n t . C a l c u l a t e d and measured
    pressure h i s t o r i e s a g r e e f o r Well P 3 i f i t i s a s s u m e d t h a t
    k = 0 . 4 5 m i l l i d a r c i e s , w i t h ( = 0 . 3 o u t t o a r a d i u s of 3 . 9 f t
                                                   I
    a n d t h a t 4 = 0 . 0 0 3 w i t h k = 0 . 3 5 m i l l i d a r c i e s f o r a l l r a d i i lar-
    ger than this.            The l a r g e r p e r m e a b i l i t y a n d p o r o s i t y v a l u e s i n
    t h e v i c i n i t y o f Well #3 i n d i c a t e t h e f o r m a t i o n s u r r o u n d i n g t h i s
    w e l l i s much more h i g h l y f r a c t u r e d or r u b b l i z e d t h a n i s t h e
    F o r m a t i o n s u r r o u n d i n g Well t 4 .

               C a l c u l a t e d and m e a s u r e d p r e s s u r e h i s t o r i e s a g r e e f o r .
    Well # 7 a s shown i n F i g u r e 7 i f i t i s a s s u m e d t h e f o r m a t i o n
    h a s a p e r m e a b i l i t y o f 0 . 0 2 7 m i l l i d a r c i e s a n d a p o r o s i t y of 0 . 0 0 1 .
    I n t h i s c a s e , t h e r e i s n o e n h a n c e d p e r m e a b i l i t y or p o r o s i t y
    region adjacent to the w e l l .                 Well # 7 a p p e a r s t o t e r m i n a t e i n
                                 \

    virgin material.                 I t i s i n t e r e s t i n g t o note t h a t t h e W e l l # 7
    p r e s s u r e i n c r e a s e s v e r y r a p i d l y u n t i l s u c h t i m e a s i t ' becomes
    c o n s t a n t . T h i s p r e s s u r e h i s t o r y i s t y p i c a l of t h a t o b t a i n e d
    i f a i r f r a c t u r i n g of t h e m e d i a o c c u r r e d d u r i n g t h e t e s t .     Note
    also t h a t t h e maximum s y s t e m pressures o b t a i n e d a r e o n t h e
    o r d e r o f t h e local. o v e r b u r d e n pressure.

    2.2.2      Cross-Hole P e r m e a b i l i t i e s
                          _-.___I--




               T r a c c r - g a s p r e s s u r i z a t i o n t e s t s p r o v i d e a means      Of

    d i r e c t l y m e a s u r i n g t h e t i m e r e q u i r e d f o r g a s t o f l o w from a n
    injection to a production w e l l .                    Cross-hole p e r m e a b i l i t i e s d e t e r -
    m i n e d a s s u m i n g t h e f l o w o c c u r s i n c h a n n e l s s u c h a s shown i n
@


                                                      13
     900


                                                                                                                      0   0   0   0
                                           Well 1 4
           I

                                                          O,A       Measured p r e s s u r e s
                                                          - measuredt e dflow erater eisn b o s Wde lon 1 4
                                                            Calcula        pr ssu
                                                                                          t
                                                                                            a e
                                                                                                      l
     600b


       I                                              Note:   Media p r o p e r t i e s u s e d i n v i c i n i t y
                                                              of Well 14
                                                                  k = 0 . 0 4 5 mdarcy
                                                                  4 = 0 . 1 for r             1.75 f t
                                                                  @ = 0.001 f o r r > 1.75 f t
Q,


2
v)
     400L
Q,
k
a                     0
                                                                                                       A        A
                                                                                          A      A
                  0                                                                 A

     200




       01
       0                  1
           0                   10               20                        30                               40
               July 9
               1700                              Time (hours)



                 Figure 5.    Comparison of measured and calculated pressures at Well # 4
                              during pressurization of this well.
VQ
E E
               W
               r(
               s"
           Q
               Q
                    0
                    0
                    e4
      15
                                                           ,
                                            x
                                            V
                                            k
                                            m
                                           a
                                            E
                                           I--4
                                             ..
                                           N O
                                           cc
                                           00
                                            u u
                                           Y’B
                                 ..
                                 Q,
                                 u
                                 0
                                 z
     0
     0
     0
     0
     0
              a              0
0        0        O    0              0           0   0
0        0        0    0              0           0   0
00       I-       10   Lri            cr          N    -
                                                      tl
                       (brsd) aanssaid                         A
                                      16
crs   F i g u r e 8 , c a n be c a l c u l a t e d u s i n g E q u a t i o n (C.6) g i v e n i n
      Appendix C.            If t h e c r o s s - h o l e f l o w r a t e i s known, E q u a t i o n
       ( C . 7 ) c a n t h e n be u s e d t o e s t i m a t e t h e c r o s s - s e c t i o n a l a r e a
      of t h e c h a n n e l .

                  I f , as d i s c u s s e d i n t h e p r e v i o u s s e c t i o n , a n axisyinmetric
      c o n f i g u r a t i o n w i t h t h e media p r o p e r t i e s d e t e r n i n e d by t h e
      one-dimensional            c a l c u l a t i o n s i s used, t h e flow t o t h e p r o d u c t i o n
      w e l l w i l l be i n a d e q u a t e t o p r o d u c e t h e m e a s u r e d p r e s s u r e s .     TO
      account f o r t h e observed f l o w i n t o t h e production w e l l , t h e r e
      must e x i s t a c h a n n e l or r e g i o n having an enhanced permeability.
      The p e r m e a b i l i t y of t h e s e c h a n n e l s i s g i v e n i n t h i s s e c t i o n .

                  T h e s e c a l c u l a t i o n s a s s u m e a p l a n a r f l o w , t h u s t h e r e is
      n o c y l i n d r i c a l d i v e r g e n c e a s i n t h e a x i s y m m e t r i c case n o r i s
      t h e r e a n y loss t h r o u g h t h e c h a n n e l w a l l s .       As a r e s u l t ,for a
      g i v e n p e r m e a b i l i t y , t h e t r a c e r g a s t r a n s i t t i m e i s much lower
      i n t h e p l a n a r c a s e a s c o m p a r e d t o t h e a x i s y m m e t r i c case.            F o r ease
      of p r e s e n t a t i o n , t h e p e r m e a b i l i t y v a l u e s shown h e r e a s s u m e a
      t o t a l s y s t e m p o r o s i t y of 0 . 0 0 1 .    These v a l u e s a r e c o n s i s t e n t w i t h
      t h e one-dimensional             r e s u l t s , w h i c h s a t i s f y c o n s e r v a t i o n of mass
      p r i n c i p l e s . If t h e p o r o s i t y of t h e f l o w c h a n n e l d i f f e r s from
      t h i s v a l u e , t h e p e r m e a b i l i t y i s changed a c c o r d i n g l y s i n c e
      E q u a t i o n (C.6) d e f i n e s t h e r a t i o of p e r m e a b i l i t y t o p o r o s i t y
                                  b


      (i.e.   ,   k/$).
                  C r o s s - h o l e p e r m e a b i l i t i e s a r e shown o n F i g u r e s 3 a n d 4
      for tracer g a s e s i n j e c t e d through t h e W e l l # 4 c a p i l l a r y and
      annulus, respectively.                   I n g e n e r a l , t h e c r o s s - h o l e permeabilities
      a r e a l l o n t h e o r d e r of a few h u n d r e d t h s of a m i l l i d a r c y w i t h
      t h e e x c e p t i o n of t h a t b e t w e e n Wells # 4 a n d #12. G a s i n j e c t e d
      t h r o u g h t h e Well # 4 c a p i l l a r y moved toward W e l l # 1 2 a s i f t h e
      p e r m e a b i l i t y were o n e - t e n t h m i l l i d a r c y ,

                 Note t h a t t h e i n j e c t i o n t o p r o d u c t i o n w e l l t r a c e r - g a s t r a n s i t
      t i m e s d e c r e a s e ( i . e . , see A p p e n d i x A ) a s t h e s y s t e m p r e s s u r e
0
                                                        17
Figure 8 .   S u r f a c e view i l l u s t r a t i o n of f l o w c h a n n e l between i n j e c t i o n
             and p r o d u c t i o n wells.
c3   increases.          The c h a n g e s a r e c o n s i s t e n t w i t h t h a t r e q u i r e d
     for Equation ( C . 6 ) t o i n f e r p e r m e a b i l i t i e s which a r e , w i t h t h e
     e x c e p t i o n of SF f l o w from Wells # 4 t o #3, p r e s s u r e i n d e p e n d e n t .
                                6
     I n a x i s y m m e t r i c flow, a s shown i n F i g u r e s 5 a n d 9 , t h e t r a c e r
     gas t r a n s i t t i m e i n c r e a s e s s i g n i f i c a n t l y a s t h e i n j e c t i o n w e l l
     and s y s t e m p r e s s u r e i n c r e a s e .

                 R e c a l l t h a t 13B1 a n d 1 2 B 2 were i n i t i a l l y i n j e c t e d i n t o
     Wells # 7 a n d # 3 , r e s p e c t i v e l y , p r i o r t o i n i t i a t i o n of p r e s s u r i z a t i o n
     of Well # 4 .    The 13B1 a n d 1 2 B 2 were e v e n t u a l l y d e t e c t e d i n Wells
     R12 a n d 115, r e s p e c t i v e l y . T h e s e t r a c e r g a s i n j e c t i o n s o c c u r r e d
     t h r o u g h t h e a n n u l u s a n d t h e r e f o r e i t c a n n o t be d e t e r m i n e d w h e t h e r
     t h e f l o w , i n t h e c a s e of W e l l #7, i n i t i a t e d i n t h e A n t r i m o r F a l s e
     Antrim layers.             The Well # 7 t o $ 1 2 c r o s s - h o l e p e r m e a b i l i t y is
     shown i n F i g u r e 4 .         Cross-hole p e r m e a b i l i t i e s corresponding t o
     t h e 12B2 i n j e c t i o n c o u l d n o t be d e t e r m i n e d s i n c e t h e Well # 5
     c a p i l l a r y was b l o c k e d t h u s p r e v e n t i n g g a s s a m p l i n g .

                D u r i n g a s e c o n d t e s t c a r r i e d out t o a n a l y z e t h e c h a r -
     a c t e r i s t i c s of t h e r e t o r t r e g i o n i n t h e v i c i n i t y of W e l l # 3 ,
     1 2 B 2 a n d C318 were i n j e c t e d i n t o t h i s well t h r o u g h t h e a n n u l u s .
     1 2 B 2 i n j e c t i o n o e c u r r e d when t h e w e l l h e a d p r e s s u r e was 8 0
     psi.      T h i s t r a c e r g a s t r a v e l e d t o Well # 6 .         The W e l l # 3 p r e s s u r e
     was a p p r o x i m a t e l y 3 0 0 p s i g d u r i n g t h e C318 i n j e c t i o n a n d t h i s
     t r a c e r g a s t r a v e l e d t o both W e l l s # 5 a n d # 6 .            I n o r d e r to pre-
     v e n t b r i n e movement away f r o m W e l l # 3 t o w a r d Well # 4 a n d t h e
     r e m a i n d e r of t h e r e t o r t r e g i o n , p r e s s u r i z a t i o n of Well # 3 was
     c a r r i e d o u t o n l y l o n g enough t o e v a l u a t e comrnunication between
     Well # 3 a n d Wells # 5 a n d # 6 .                   T h i s was n o t s u f f i c i e n t t i m e to
     e v a l u a t e c o m m u n i c a t i o n b e t w e e n Wells # 3 a n d Wells # 8 , #9, # l o ,
     and # 1 2 . Cross-hole p e r m e a b i l i t i e s d e t e r m i n e d from t h e s e i n -
     j e c t i o n s a r e shown i n F i g u r e 1 0 . I n t h i s case g a s s a m p l e s
     were t a k e n f r o m t h e v e n t l i n e s a n d c o u l d o n l y be o b t a i n e d once
     outflow o c c u r r e d from Wells # 5 a n d # 6 . The p e r m e a b i l i t y v a l u e s
     shown t h e r e f o r e r e p r e s e n t a m i n i m u m v a l u e s i n c e t h e e x a c t t i m e
     of t r a c e r g a s a r r i v a l a t t h e s e w e l l s c o u l d n o t be d e t e r m i n e d .


                                                       19
h,
0




     July 9                                     T i m e (hours)
     1700


     F i g u r e 9.   P o s i t i o n of tracer gas f r o n t as a f u n c t i o n of t i m e d u r i n g
                      p r e s s u r i z a t i o n of Well # 4 .
c


                 8
                                                         - Well injected into
                                                           1282
                                                                13 through annulus
                                                                 beginning at 0650 on
                       .Ol md                                    13 July.
                          1     .01 md                    e---   C318 i n j e c t e d into
                                                                 Well 1 3 through annulus
                                                                 beginning at 0900 on
                                                                 13 July.




    Figure 10.   Schematic illustrating cross-hole tracer gas flow originating
                 in False Antrim formation at Well #3.
            The c r o s s - s e c t i o n a l    a r e a of t h e f l o w c h a n n e l shown i n
F i g u r e 8 may be d e t e r m i n e d a s d e s c r i b e d i n A p p e n d i x C.           If
these channels occur t h e i r porosity i s necessarily l a r g e r than
t h e a v e r a g e system p o r o s i t y of 0.001 determined from t h e one-
dimensional axisymmetric analyses.                            I t i s of i n t e r e s t t o c a l -
c u l a t e a p o s s i b l e c h a n n e l s i z e s u c h a s miry a c c o u n t f o r t h e
7 . 1 s c f m f l o w f r o m Wells # 4 t o # 3 .             I f t h e a c t u a l c h a n n e l por-
o s i t y i s t a k e n a s 0 . 0 5 t h i s i m p ] - i e s a p e r m e a b i l i t y o f 1 md a n d
a channel cross-sectional                       a r e a o f 20 f t
                                                                     2
                                                                         .
            E q u a t i o n s g i v e n i n A p p e n d i x C c a n a l s o be u s e d t o e s t i m -
ate f l o w along f r a c t u r e paths.             I f i t i s a s s u m e d t h a t Wells # 4
a n d # 3 a r e connected b y , s a y 1@ f r a c t u r e s h a v i n g a d e p t h of 1 0
f t , t h e n i t follows f r o m E q u a t i o n ( C . 8 ) t h a t t h e crack w i d t h
m u s t be a p p r o x i m a t e l y 0 . 0 0 1 c m .   Given t h i s c r a c k w i d t h t h e
W e l l # 4 t o # 3 t r a c e r g a s t r a n s i t t i m e w o u l d b e , from E q u a t i o n
 (C.9),     o n t h e o r d e r of m i n u t e s r a t h e r t h a n h o u r s a s d e t e r m i n e d
experimentally.             The a s s u m p t i o n t h a t f l o w o c c u r s t h r o u g h a
f i n i t e number o f f r a c t u r e s i s i n c o n s i s t e n t w i t h t h e e x p e r i m e n t a l
d a t a s i n c e it i n p l i e s t r a n s i t t i m e s and porosities t h a t are
s m a l l compared t o t h o s e measured.

2.2.3      -
           Two-Dimensional A n a l y s e s o f R e t o r t R e g i o n

           The r e t o r t v o l u m e r e s p o n s e t o a n i m p o s e d g a s f l o w w a s s i m -
u l a t e d u s i n g a two-dimensional               model.         D e t a i l s o f t h i s model-
i n g a r e p r e s e n t e d i n A p p e n d i x C.      The o b j e c t i v e o f t h e t w o -
dimensional a n a l y s i s w a s t o obtain f u r t h e r d e f i n i t i o n of t h e
p e r m e a b i l i t y a n d p o r o s i t y d i s t r i b u t i o n s w i t h i n t h e r e t o r t vol-
ume s o t h a t g a s f l o w t h r o u g h t h e v o l u m e c o u l d be d e f i n e d .
           I t i s a p p a r e n t from t h e r e s u l t s g i v e n i n S e c t i o n s 2 . 2 . 1          and
2.2.2     t h a t t h e r e t o r t r e g i o n c a n n o t be m o d e l e d a s a u n i f o r m v o l -
ume.      To p r o v i d e t h e measured f l o w t o p r o d u c t i o n w e l l s such
a s #3 and # 1 2 r e q u i r e s t h e e x i s t e n c e o f flow c h a n n e l s h a v i n g an




                                                    22
0
    enhanced p e r m e a b i l i t y .       A somewhat a r b i t r a r y r e p r e s e n t a t i o n of
    our e s t i m a t e s of t h e s e c h a n n e l s i s g i v e n i n F i g u r e 11, w h i c h
    shows t h e n u m e r i c a l g r i d u s e d f o r t h e t w o - d i m e n s i o n a l a n a l y s e s .

                The t w o - d i m e n s i o n a l a n a l y s e s a r e c a r r i e d o u t i n t h e same
    manner a s d e s c r i b e d f o r t h e o n e - d i m e n s i o n a l c a l c u l a t i o n s .
    A i r is forced i n t o the injection w e l l a t t h e experimentally
    determined r a t e .           N u m b e r s o f c a l c u l a t i o n s a r e p e r f o r m e d assum-
    ing v a r i o u s combinations of permeability and p o r o s i t y u n t i l one
    i s o b t a i n e d i n w h i c h t h e m e a s u r e d a n d c a l c u l a t e d pressures
     ( i . e . , t h e r e f o r e flow r a t e s ) a g r e e a t t h e p r o d u c t i o n a n d i n j e c -
    tion wells.              O n c e a g r e e m e n t i s o b t a i n e d , t h e s e v a l u e s of m a t e r -
    i a l p r o p e r t i e s a r e a s s u m e d r e p r e s e n t a t i v e of t h e f o r m a t i o r . .

               V a l u e s of p e r m e a b i l i t y a n d p o r o s i t y u s e d f o r t h e t w o -
    d i m e n s i o n a l a n a l y s e s a r e shown i n T a b l e 1.          T h e p e r m e a b i l i t y is
    a s s u m e d p r e s s u r e d e p e n d e n t i n o r d e r to b e t t e r s i m u l a t e t h e ex-
    perimental data.               R e s u l t s f r o m Run V , d e f i n e d b y T a b l e 1 a n d
    F i g u r e 11, w i l l be d i s c u s s e d i n t h e f o l l o w i n g p a r a g r a p h s .

               M e a s u r e d a n d c a l c u l a t e d p r e s s u r e h i s t o r i e s a r e shown
    i n F i g u r e 1 2 f o r yells # 7 , # 4 , a n d # 3 f o r t h e f i r s t 5 0 h o u r s of
    t h e test,       The p r e s s u r e d i s t r i b u t i o n w i t h i n t h e r e t o r t v o l u m e
    a t t h e e n d of t h i s p e r i o d i s shown i n F i g u r e 1 3 .                A h i s t o r y of
    t h e tracer g a s m o t i o n i s g i v e n i n F i g u r e 14.

               During t h e p r e s s u r i z a t i o n phase t h e W e l l #7 c a l c u l a t e d
    a n d m e a s u r e d r e s p o n s e s a g r e e c l o s e l y a s shown i n F i g u r e 12.
    Once t h e Well # 7 i n j e c t i o n i s t e r m i n a t e d t h e r e follows a r a p i d
    d e c a y i n c a l c u l a t e d p r e s s u r e t y p i c a l of t h a t o c c u r r i n g in
    any porous formation.                  However, d u r i n g t h e t e s t , when t h e i n -
    j e c t i o n stopped, t h e p r e s s u r e dropped s l i g h t l y and t h e r e a f t e r
    remained constant'.               T h i s b e h a v i o r i s . t y p i c a l of t h a t e x p e c t e d
    t o o c c u r i f t h e f o r m a t i o n were f r a c t u r e d (i.e., s e p a r a t e d a l o n g
    t h e bedding p l a n e s ) by t h e a i r i n j e c t i o n .           I n t h a t case, p r o v i d e d
@   t h e " c r a c k " p r o p a g a t i o n i s s t a b l e , o n c e t h e d r i v i n g pressure i s


                                                      23
               I
                   a
                   .-
                   L'   -
                   CC
0    0
      e
               e
CJ   ln        0
(u   4
     c
          24
                                                                                                                                                c
                                                             Table 1.

           V a l u e s of p e r m e a b i l i t y a n d p o r o s i t y u s e d i n t h e t w o - d i m e n s i o n a l
                          a n a l y s e s f o r t h e r e g i o n s shown i n F i g u r e 11.



                                                                                                                                            r




                                   1
                                                       '                                                                      I


 1"   i
      II
      I
              R e g i o n A6 8ame,as Region 13
              Q = 0.004
              k =     9 u d
                     65 u d
                                     0.001
                                          30 ud
                                          60 pd        I
                                                                0.0005
                                                               1 8 ud
                                                              180 p d
                                                                                        0.004
                                                                                         12s ud
                                                                                         1.2 ud        I
                                                                                                                0.001
                                                                                                                200 ud
                                                                                                                                   0.001
                                                                                                                                    10 ud
                                                                                                                                    75 ud


              4 = 0.004
              k - 9ud
                                   I
                                   I
                                         0.001
                                           30 ud
                                                       I        0.0005
                                                                1 8 ud
                                                                                         0.004
                                                                                         125 ud
                                                                                                                0.001
                                                                                                                100 vd       I
 S i z e of Region C0 a n d 010 i n c r e a s e d t o i n c l u d e e n t i r e d o t t e d r e g i o n shown i n F i g u r e 11.
                                                                                                                                   0.001
                                                                                                                                    10 ud




j.           NOTE:     I t W A S assumed t h a t           Q = 0 . 0 0 3 a n d k = 1 u d a r c y i n all r e g i o n s
                       of t h e g r i d shown i n F i g u r e 11 w h i c h a r e n o t d e f i n e d a b o v e . w h e r e
                       K v a l u e s a r e shown in p a r e n t h e s e s , i t was assumed t h a t                 k was
                       p r e s s u r e d e p e n d e n t . The p e r m e a b i l i t y was t a k e n c o n s t a n t , a t t h e
                       lower v a l u e , u p t o a p r e s s u r e o f SO0 psi a n d t h e n i n c r e a s e d l i n e a r l y
                                                                        a t 8 0 0 psi.
                                 PRESSURE V S T I M E




             **O   i                                            X
                                                                @
                                                                      Well 1 7
                                                                      Well 1 4
                                                                v     well 113
             6.0
                                                                --- P r ea s u ri set ai n c the ' f ofroma tti h n
                                                                         s               n             rm       o
        -
        n


        v,
                                                                    at       d               e 7
                                                                      c e n t e r l i n e of W e l l 1 3
                                                                      measured toward W e l l 1 4
                                                                                                                  e

        a
        N
        0
        4

        U
             4.0




             2.0




             0.0
                   0.0     1.0               2.0          3.0            4.0
                                               -
                                  TIME   c   IO'MIN   I




Figure 12.   Comparison of measured and c a l c u l a t e d pressure h i s t o r i e s
             at Wells # 7 , # 4 and # 3 a s determined from two-dimensional
             arralvses.
                                                                                                       c



                  20.



                  15.



                  10.



                   5.


                   0.
                                                                                         0




F i g u r e 13.    Calculated pressure d i s t r i b u t i o n w i t h i n r e t o r t volume 50
                   h o u r s a f t e r i n i t i a t i o n of Well # 7 p r e s s u r i z a t i o n .
                      20.0    I


                      15.0

                              I




                       0.0
                             0.0       5.0        10.0        15.0
                                                                 20.0                 25.0        30.0
                                                     X AXIS (IO'FT 3


          Note :      These r e s u l t s a r e i n c l u d e d f o r c o m p l e t e n e s s o n l y .
                      Because of t h e requirement to assume d i s c r e t e f l o w
                      c h a n n e l s t h e t r a c e r - g a s motion i s n o t a d e q u a t e l y r e p r e -
                      s e n t e d s i n c e t h e t r a c e r p a r t i c l e s d o n o t n e c e s s a r i l y stay
                      i n t h e c h a n n e l s . Thus, f o r example, t h e r e appeer to
                      be no t r a c e r p a r t i c l e s moving toward W e l l R12.




Figure 1 4 .   H i s t o r y of t r a c e r gas motion during the 5 0 hour period
               f o l l o w i n g i n i t i a t i o n of Well #7 p r e s s u r i z a t i o n .
G3
     s l i g h t l y relaxed, t h e t i p p r e s s u r e d r o p s and c r a c k growth stops.
     Since a i r i n t h e crack is a t very high pressure, unlike t h a t i n
     a p o r o u s m e d i a where t h e p r e s s u r e d r o p s r a p i d l y a s o n e moves
     r a d i a l l y from t h e w e l l , t h e r e i s l i t t l e p r e s s u r e d e c a y once t h e
     system i s shut-in.                I t i s of importance t o note t h a t t h e system
     shut-in pressure i s approximately equal t o t h e overburden
     pressure.

                 A c o m p a r i s o n of t h e c a l c u l a t e d a n d measured. W e l l X 4 p r e s -
     s u r e s a r e a l s o shown i n F i g u r e 1 2 .           T h e c o m p a r i s o n i s n o t a s good
     a s t h a t shown f o r W e l l # 7 , p r i m a r i l y a s a r e s u l t o f t h e l a r g e
     wellbore v o l u m e a n d c o a ' r s e z o n i n g . M a t e r i a l s p r o p e r t i e s c o u l d
     be s l i g h t l y a d j u s t e d s o t h a t t h e c u r v e s m a t c h d u r i n g t h e
     p r e s s u r i z a t i o n p h a s e , h o w e v e r , t h e e f f o r t d o e s n o t seem w a r r a n t e d .
     The mass f l o w r a t e i n t o Well # 4 i s e x a c t l y t h e e x p e r i m e n t a l f l o w
     r a t e t h u s mass i s c o n s e r v e d p r o p e r l y and t h e f i n a l p r e s s u r e i s
     approaching t h e measured p r e s s u r e .                  Therefore, t h e flow rate
     away from t h e v i c i n i t y of Well # 4 i n t o t h e r e t o r t v o l u m e is
     r e p r e s e n t a t i v e of t h a t a c t u a l l y o c c u r r i n g .

                 The p r e s s u r e b u i l d - u p a t Well # 3 i s s e e n i n F i g u r e 12 t o
     be much t o o s l o w .          Even t h e f l o w c h a n n e l a s s u m e d i n t h i s a n -
     a l y s i s i s i n a d e q u a t e and c a n n o t p r o v i d e t h e o b s e r v e d flow.
     The p r e s s u r e o u t s i d e t h e h i g h p o r o s i t y r e g i o n s u r r o u n d i n g
     W e l l # 3 , a s d e t e r m i n e d by t h i s t w o - d i m e n s i o n a l a n a l y s i s , is
     s e e n t o be r e p r e s e n t a t i v e of t h e m e a s u r e d W e l l # 3 p r e s s u r e .
     C l e a r l y , b e c a u s e of t h e l a r g e w e l l b o r e v o l u m e , p r e s s u r e s
     m e a s u r e d i n Well # 3 a r e n o t r e p r e s e n t a t i v e of t h e p r e s s u r e i n
     t h e f o r m a t i o n s u r r o u n d i n g t h i s well.

                 The t w o - d i m e n s i o n a l   a n a l y s e s were o n l y c o m p l e t e d t o a
     t i m e of 5 0 h o u r s f o l l o w i n g t h e i n i t i a l i n j e c t i o n i n t o W e l l # 7 .
      B e c a u s e o f t h e f a i l u r e of t h e m e a s u r e d W e l l s # 7 a n d # 4 , pres-
      s u r e s t o d e c a y a Z t e r c o m p l e t i o n of p r e s s u r i - z a t i o n (see F i g u r e
      1 5 ) no a d d i t i o n a l i n f o r m a t i o n c o n c e r n i n g t h e system c h a r a c t e r i s t i c s
@


                                                        29
                                                                                                       n
                                                      I       .-
        0 0         b
                                                                                                 tn
    0
        O
                  bD
                                                      -
                                                      0
                                                      Y
                                                                                                 a
                                                                                                 b,
    0                    0                            0
                b             o                       t
                                  0
    0                                 0
                D                         0
    0                                             O       Q   O
    0       '                                                           0
                D
                b
                B
                b                                                                           m
                         0
                  c      z
                         d m      t   c       O    N
                         LI                   d    d
                  b
    0                    P
                                                                                            0,
    O           b                                                                           E
                                                                                            -4
    0                                                                   0                   cl
                                                                     o
    0                                                               O
                                                                   0
        0                                                           0
        0                                                               0
                b
        0
    0
I       O     b                                                                         I
    0                   0             0       0               0     0       0       0   0
                                                                                                 a
    0                   0             0       0               0     0       0       0
                                                                                                 k
    oo                  r-            W       Y)              *     rl      (   Y   d            5
                                                                                                 tr,
                                                                                                 4
                                                                                                 E
                                                              30
Grs
      c o u l d be o b t a i n e d b y c o n t i n u i n g t h e s e r u n s t o l a t e r t i m e s .
      I f t h e a n a l y s i s were c o n t i n u e d , once t h e o u t l y i n g Wells # 6 a n d
      # l O b e g a n t o p r e s s u r i z e , t h e y would c o n t i n u e t o d o s o b e c a u s e
      of t h e d i f f u s i o n c h a r a c t e r i s t i c s r e p r e s e n t a t i v e of f l o w t h r o u g h
      a porous f o r m a t i o n e v e n i f t h e p r e s s u r e i n W e l l # 3 were r e l i e v e d .
      I t i s c o n c e i v a b l e t h a t a m o d e l of t h e r e t o r t r e g i o n c o u l d be
      d e v e l o p e d s h o w i n g s p e c i f i c c h a n n e l s t o v a r i o u s wells s u c h
      t h a t t h e p r e s s u r e r i s e o n a l l w e l l s were m o d e l e d . However,
      t h e model d e v e l o p e d i s so non-unique as t o h a v e l i t t l e v a l u e .

      2.2.4      Summarv o f P e r m c a b i l i t v a n d P o r o s i t v A n a l v s i s

                 T o s u m m a r i z e , t h e r e s u l t s of t h e p l a n a r , a x i s y m m e t r i c a n d
      two-dimensional            a n a l y s e s i n d i c a t e f r a c t u r i n g occurs or t h a t
      e x i s t i n g fractures open (i.e., separation along bedding planes
      a t h i g h p r e s s u r e s ) o n c e p r e s s u r e s r e a c h t h e n e i g h b o r h o o d of t h e
      overburden.          As a r e s u l t ,    t h e s y s t e m r e s p o n s e c a n n o t be d e s c r i b e d
      u s i n g a p o r o u s f l o w model.

                 T h e s t r o n g e s t e v i d e n c e s u p p o r t i n g t h e a b o v e p r e m i s e is
      t h e m a i n t e n a n c e of h i g h p r e s s u r e s once wells a r e s h u t - i n .        In
      addition, the f l o w rate i n t o W e l l # 3 (note the constant f l o w
      r a t e i n t o t h i s w e l l a s e v i d e n c e d by t h e c o n s t a n t p r e s s u r e r i s e
      shown i n F i g u r e 4 ) i s i n d e p e n d e n t of t h e W e l l # 3 p r e s s u r e .           This
      i n d i c a t e s t h a t t h e pressure i n t h e f o r m a t i o n surrounding t h i s
      w e l l i s , even a t e a r l y t i m e s , a t l e a s t 300 p s i . T h i s would
      o c c u r o n l y i f t h e c r a c k s o r f r a c t u r e s were b e i n g f o r c e d o p e n a t
      t h e h i g h p r e s s u r e s . T r a c e r g a s t r a n s i t t i m e s a r e a l s o s e e n to
      e i t h e r s l i g h t l y i n c r e a s e or r e m a i n t h e same o n c e t h e s y s t e m
      p r e s s u r e becomes e l e v a t e d .      I n a uniformly porous media, t h e s e
      t r a n s i t t i m e s would d e c r e a s e a s t h e s y s t e m p r e s s u r e i n c r e a s e d .

                 Fiow c h a n n e l i n g i s a l s o s t r o n g l y i n d i c a t e d cxperimen-
      t a l l y by t h e p o r t i o n o f t h e f l o w w h i c h a r r i v e s a t W e l l # 3 a n d
      #12, a n d a n a l y t i c a l l y b y t h e r e s u l t s of t h e t w o - d i m e n s i o n a l
0
                                                       31
analyses.           Based o n s o l i d a n g l e a r g u m e n t s , t h e s e w e l l s s h o u l d
r e c e i v e less t h a n 2 p e r c e n t and 0.3 p e r c e n t o f t h e t o t a l f l o w
i f t h e s y s t e m were u n i f o r m , w h e r e a s t h e y r e c e i v e 1 8 p e r c e n t
and 4 p e r c e n t , r e s p e c t i v e l y .
2.3         CHARACTERIZATION OF THE FRACTURING
            The u n i f o r m i t y o f t h e m b b l i z a t i o n , f r a c t u r i n g , or bed-
d i n g p l a n e s e p a r a t i o n can be d e t e r m i n e d from t r a c e r g a s c o n c e n -
t r a t i o n measurements a t t h e p r o d u c t i o n w e l l s .               I f t h e formation
i s u n i f o r m t o t h e e x t e n t t h a t a l l g a s f l o w i n g from t h e i n j e c t i o n
w e l l to a production w e l l t r a v e l s along geometrically iden-
t i c a l f i v w p a t h s t h e n g a s motion occurs a s s l u g f l o w .            In that
case, t h e t r a c e r g a s p u l s e w i d t h a n d c o n c e n t r a t i o n m e a s u r e d a t
the production w e l l is i d e n t i c a l t o t h a t occurring a t t h e in-
jection well.            I f t h e i n j e c t i o n t o p r o d u c t i o n well f l o w p a t h s
are not uniform, then t h e first t r a c e r gas a r r i v a l s a t t h e
p r o d u c t i o n w e l l s w i l l be o f l o w c o n c e n t r a t i o n , a n d t h e t i m e re-
quired for t h e concentration t o i n c r e a s e t o t h e i n j e c t i o n level
will be l o n g c o m p a r e d t o t h e i n j e c t i o n p u l s e l e n g t h .
            I n t e r p r e t a t i o n of t r a c e r g a s C o n c e n t r a t i o n m e a s u r e m e n t s
made i n t h e p r o d u c t i o n w e l l s i s c o m p l i c a t e d by t h e l a r g e w e l l -
bore v o l u m e a n d l o w s y s t e m p o r o s i t y .         E x p e c t e d maximum p r o d u c t i o n
w e l l t r a c e r g a s c o n c e n t r a t i o n s c a n be e s t i m a t e d u s i n g A p p e n d i x
D.    The u n i f o r m i t y of t h e c r o s s - h o l e f l o w p a t h s c a n be q u a l i -
t a t i v e l y e v a l u a t e d b y c o m p a r i s o r , of t h e m e a s u r e d c o n c e n t r a t i o n s
and r i s e t i m e s w i t h t h o s e e s t i m a t e d a s s u m i n g no d i s p e r s i o n .

            The r a t i o s g i v e n by t h e maximum d e t e c t e d p r o d u c t i o n w e l l
t r a c e r g a s c o n c e n t r a t i o n s d i v i d e d b y t h e maximum e x p e c t e d
c o n c e n t r a t i o n s , determined a c c o r d i n g t o t h e f o r m u l i g i v e n i n
A p p e n d i x D , a r e shown i n p a r e n t h e s i s i n F i g u r e s 3 a n d 4 .

            T h e tracer g a s i n j e c t i o n p u l s e l e n g t h ( u s u a l l y approx-
i m a t e l y 3 - 4 h o u r s ) a n d the time r e q u i r e d f o r t h e maximum c o n c e n -
t r a t i o n I.cvels t o o c c u r i n t h e p r o d u c t i o n w e l l s c a n be s e e n i n
                                                                                                                   @
                                                   32
G   t h e d a t a summary g i v e n i n A p p e n d i x A .           D a t a shown i n F i g u r e s 3
    and 4 a r e f o r t r a c e r g a s e s i n j e c t e d i n t o W e l l # 4 . T h e r e i s i n s u f -
    f i c i e n t d a t a t o make a c c u r a t e i n t e r p r e t a t i o n s from t r a c e r g a s
    i n j e c t i o n s i n W e l l s f13 a n d # 7 .

               Gas f l o w from Well # 4 t o # 3 i s e s s e n t i a l l y s l u g f l o w .
    The r a t i o o f m e a s u r e d t o a n t i c i p a t e d maxiinum c o n c e n t r a t i o n i s
    shown t o be 0 . 3 f o r t h e C318, 13B1 a n d s e c o n d SF6 p u l s e s .
    A s shown      in F i g u r e A . 2 of A p p e n d i x A , t h e r i s e t i m e , m e a s u r e d
    f r o m t h e t i m e of t h e f i r s t a r r i v a l of t h e t r a c e r t o t h e t i m e a t
    w h i c h t h e p e a k c o n c e n t r a t i o n i s o b t a i n e d , i s o n t h e same o r d e r
    as the injection pulse t i m e .                  One e x c e p t i o n t o t h e s l u g f l o w is
    t h e f i r s i SF6 a r r i v a l o c c u r r i n g a t l o w p r e s s u r e .  I t i s much
    more d i s p e r s i v e , a s i n d i c a t e d b o t h by i t s lower peak r e l a t i v e
    c o n c e n t r a t i o n a n d by t h e f a c t a p p r o x i m a t e l y 30 h o u r s o c c u r r e d
    b e t w e e n t h e t i m e o f f i r s t a r r i v a l a n d t h e a t t a i n m e n t of t h e
    peak c o n c e n t r a t i o n .

                Tracer g a s i n j e c t e d t h r o u g h t h e Well # 4 c a p i l l a r y was
    d e t e c t e d a t Wells # 8 a n d #10 a t low c o n c e n t r a t i o n s .             T h e detec-
    t i o n t i m e was s h o r t ( a p p r o x i m a t e l y 1 0 h o u r s a n d 3 h o u r s a t
    Wells # 8 a n d # l o , r e s p e c t i v e l y ) s i n c e f l o w i n t o t h e s e w e l l s
    s t o p p e d o n c e Well if3 w a s v e n t e d .        The p e a k c o n c e n t r a t i o n s w h i c h
    may h a v e eventually occurred at t h e s e wells i s therefore i n -
    determinant.              However, d u r i n g t h e m e a s u r e m e n t t h e c o n c e n t r a t i o n
    l e v e l s i n c r e a s e d v e r y s l o w l y if a t a l l . T h e l o w i n i t i a l c o n -
    c e n t r a t i o n l e v e l s t o g e t h e r w i t h t h e s l o w i n c r e a s e i n concen-
    t r a t i o n i n d i c a t e f l o w c h a n n e l s from K e l l # 4 t o Wells # 8 a n d #10
    are h i g h l y n o n - u n i f o r m .
                For t h e f i r s t 8 0 t o 1 0 0 h o u r s of t h e t e s t (see F i g u r e s 3
    a n d 4 and A . 1 7 )      g a s f l o w i n t o W e l l #12 i s predominantly t h a t
    o r i g i n a l l y i n j e c t e d i n t o W e l l # 7 a s i n d i c a t e d by t h e h i g h 1 3 B l
    concentration.             A t later t i m e s         (100 h o u r s ) t h e s e c o n d SF6 p u l s e
    i n j e c t e d i r . t o \ J e l l 114 b e g i n s t o a r r i v e a t Well # 1 2 .      AS




                                                      33
i n d i c a t e d by t h e c o n c e n t r a t i o n l e v e l a n d a p p a r e n t r i s e t i m e ,
t h i s flow i s approaching s l u g f l o w .

            T h e r e was i n s u f f i c i e n t d a t a t o e v a l u a t e t h e u n i f o r m i t y
of t h e f o r m a t i o n b e t w e e n W e l l # 3 a n d Wells # 5 a n d # 6 . The l a c k
of d a t a r e s u l t s p r i m a r i l y from t h e f a c t t h a t t h e c a p i l l a r y t u b e s
o n W e l l s # 5 a n d # 6 were p l u g g e d or c l o s e d , t h u s d a t a c o u l d n o t
be o b t a i n e d f r o m t h e s e w e l l s w h i l e t h e y were s h u t - i n .         When
Well # 3 was p r e s s u r i z e d , b o t h Wells # S a n d # 6 were r e g u l a t e d
a t 4 0 p s i g . Once p r e s s u r e s i n t h e s e w e l l s e x c e e d e d t h i s v a l u e
o u t f l o w occurred a n d s a m p l e s were o b t a i n e d f r o m t h e f l o w i n g g a s .
The t i m e a t w h i c h t r a c e r g a s f i r s t e n t e r e d t h e s e w e l l s c a n n o t
be a c c u r a t e l y d e t e r m i n e d .   However, a s shown i n F i g u r e s A . 6 a n d
A.8    once t h e outflow had been established, the C318                                 (C318 and
12B2) l e v e l s a t Wells # 5 ( # 6 ) were on t h e o r d e r of t h e i r i n -
j e c t i o n concentrations. T h i s evidence strongly suggests slug
f l o w o c c u r s b e t w e e n Wells # 3 a n d Wells # 5 a n d # 6 .




                                                 34
                                       3,   CONCLUSIONS


           An e x t e n s i v e a m o u n t of d a t a w a s o b t a i n e d f r o m t h e D o w
s h a l e s i t e during t h e tracer g a s p r e s s u r i z a t i o n study.                 From
t h i s d a t a , a number o f s i g n i f i c a n t c o n c l u s i o n s c a n be d e t e r m i n e d .
T h e s e a r e p r e s e n t e d below.


       0   The s y s t e m i s n o n - u n i f o r m .    F l o w from W e l l # 4 t o t h e
           o t h e r w e l l s o c c u r s p r i m a r i l y t h r o u g h v a r i o u s f l o w chan-
           nels.       T h e s e c h a n n e l s o p e n when t h e w e l l h e a d p r e s s u r e
           approaches t h e overburden pressure and appear closed a t
           lower p r e s s u r e s . C o n s e q u e n t l y , t h e s y s t e m i s p r e s s u r e
           s e n s i t i v e and t h e f l o w i s enhanced a t e l e v a t e d system
           pressures. Flow t o o u t l y i n g w e l l s , s u c h a s f18 a n d #lo,
           o c c u r o n l y when Well # 3 w a s a t a n e l e v a t e d p r e s s u r e .

           When t h e s y s t e m a p p r o a c h e d s t e a d y s t a t e , a s i n d i c a t e d
           b y a n absence of p r e s s u r e c h a n g e s , t h e p r o d a c t i o n
           r a t e was a b o u t 1 / 3 t h e i n j e c t i o n r a t e , The a d d i t i o n a l
           i n j e c t e d g a s m u s t be c o n t a i n e d i n e v e r - i n c r e a s i n g p o r -
           t i o n s of t h e r e t o r t v o l u m e .     B e c a u s e of t h e low s y s t e m
           p e r m e a b i l i t i e s t h i s flow p r o b a b l y c a n n o t be t a p p e d , e v e n
           w i t h i n t r o d u c t i o n of a d d i t i o n a l p r o d u c t i o n wells.

       0   M u l t i p l e t r a c e r g a s i n j e c t i o n i n t o Well # 4 a t v a r i o u s
           d e p t h s d e m o n s t r a t e d c o n c l u s i v e l y t h a t f l o w d o e s occur
           t h r o u g h t h e A n t r i m f o r m a t i o n i n t h e v i c i n i t y o f Well
           #4.     I t c a n n o t be d e t e r m i n e d t o w h a t d i s t a n c e t h i s f l o w
           c o n t i n u e s t o p a s s t h r o u g h t h e Antrim l a y e r .

       a T h e p e r m e a b i l i t y a n d p o r o s i t y f o u n d i n t h e v i c i n i t y of
           Well # 4 was k         2,   0.045 m i l l i d a r c y and @ = 0 . 1 for a
           radius          <1.75 f t a n d % 0 . 0 0 1 f o r r a d i i g r e a t e r t h a n 1 . 7 5
           f t . T h i s may be c o m p a r e d t o Well # 3 v a l u e s of k               0.45
                                                                                               Q


           m i l l i d a r c y w i t h @ = 0 . 3 f o r o u t t o a r a d i u s of 3 . 9 f t



                                                35
                                                                                           A



    and    $ = 0.003    w i t h k = 0.35   m i l l i d a r c i e s for a l l
    r a d i i larger than this.    In effect, the permeability i n
    t h e r e g i o n o f W e l l # 3 i s a n o r d e r of m a g n i t u d e l a r g e r
                                                                   I

    t h a n t h a t f o u n d i n t h e v i c i n i t y of W e l l # 4 .    In addi-
    t i o n , t h e volume p e r f t of w e l l l e n g t h o f t h e h i g h
    permeability, high p o r o s i t y region surrounding W e l l # 3
    i s 5 times l a r g e r t h a n t h a t s u r r o u n d i n g W e l l # 4 .
Q   The major f l o w f r o m W e l l # 4 i s t o w a r d Well 13, w h i c h i n
    t u r n c o m m u n i c a t e s r e a d i l y w i t h Wells # S a n d # 6 .   This
    f l o w occurs as a slug flow.                Decreasingly smaller por-
    t i o n s o f t h e f l o w go t o Wells #12, # 8 , a n d #lo.                Flow
    t o Well # 1 2 may o c c u r a s a s l u g f l o w , h o w e v e r , f l o w t o
    Wells # 8 a n d # l o i s d i s p e r s i v e .




                                       36
                                  4.     RECOMMENDATIONS


            A number of r e c o m m e n d a t i o n s a r e d i s c u s s e d i n t h e follow-
ing paragraphs.    F i r s t s u g g e s t i o n s a r e g i v e n which would l e a d
t o improvements i n t h e t r a c e r g a s p r e s s u r i z a t i o n t e s t r e s u l t s .
F o l l o w i n g t h i s some comments a r e i n c l u d e d c o n c e r n i n g t h e
m o d e l i n g a n d d e s i g n of p o s s i b l e f u t u r e i n - s i t u   r e t o r t volumes.
F i n a l l y , comments a r e p r o v i d e d r e l a t i n g t o d e v e l o p i n g a r e t o r t
v o l u m e so t h a t i t may p e r f o r m t o d e s i g n o b j e c t i v e s . Many o f t h e
                                                                                                   3
t h o u g h t s p r e s e n t e d w e r e b r o u g h t t o l i g h t d u r i n g t h e j o i n t S /Dow
e f f o r t t o c h a r a c t e r i z e t h e e x i s t i n g r e t o r t volume u s i n g t r a c e r -
gas p r e s s u r i z a t i o n techniques.             I n t h a t s e n s e , many of t h e i d e a s
P u t f o r t h a r e n o t u n i q u e t o S3, b u t a r e i n c l u d e d h e r e f o r
completeness.

           Many c h a r a c t e r i s t i c s of t h e e x i s t i n g r e t o r t r e g i o n were
determined during t h e tracer-gas p r e s s u r i z a t i o n tests reported
here.       However, t e c h n i q u e s c a n be e m p l o y e d o n f u t u r e t e s t s t o
e n s u r e b o t h t h a t better d a t a i s o b t a i n e d and t h a t t h e s e d a t a .
focus on answering specific q u e s t i o n s r e l a t i n g t o t h e retort
volume p e r f o r m a n c e .         A number of s t r i c t l y t e c h n i c a l problems s h o u l d
be a d d r e s s e d .      I f p o s s i b l e , i n f u t u r e t e s t s a l l h o l e s s h o u l d be
c a s e d down t o a n d p e r h a p s e v e n a f e w f e e t i n t o t h e A n t r i m forma-
t i o n . T h i s w o u l d e n s u r e t h a t a n y a n d all f l o w c h a r a c t e r i s t i c s
w e r e b e i n g measured i n t h e Antrim and n o t i n t h e False Antrim o r
some o t h e r z o n e .         I t may a l s o p r e c l u d e a major s o u r c e of g r o u n d
water leakage i n t o t h e formation. Correspondingly, t h e h o l e s
should terminate w i t h i n t h e Antrim r e g i o n , i f possible.                            Several
d o w n h o l e m e a s u r e m e n t s t a k e n d u r i n g t h i s t e s t were compromised
b e c a u s e of b r i n e a c c u m u l a t i o n .      Problems w h i c h w i l l a r i s e d u r i n g
t h e r e t o r t i n g process i f b r i n e i s p r e s e n t a r e o b v i o u s .           It i s
t h e r e f o r e recommended t h a t f u t u r e i . n - s i t u r e t o r t v o l u m e s h a v e
d o w n h o l e pumps p e r m a n e n t l y i n s t a l l e d a n d operated i n a l l w e l l s




                                                  37
                                                                                               A




where brine accumulation is a problem. In future tests, as done
with this test, it is recommended that the specific objectives for
the tracer gas analyses be well-defined before testing commences.
To aid in this definition, it is recommended that preliminary pres-
sure test data, specifically related to the tracer gas test, be
obtained before initiation of the tracer gas tests. These tests
would utilize compressed air only. This would greatly improve the
tracer gas test design and data interpretation. Applying the usual
hindsight to the tests reported here, two changes are apparent which
could possibly have been determined with preliminary pressure
testing. First and foremost, additional shut-in pressure decay
data is required. Secondly, initial tracer gas injection into
Wells P 7 and t 3 should h a v e t a k e n p l a c e a f t e r t h e f i r s t a r r i v a l
of f l o w from Well 8 4 .

       The required porosity and permeability distributions
needed for successfully retorting the Dow shale site are, from
a technology standpoint, unknown at this time. We are of the
opinion that significantly more fracturing than was in evidence
in the retort (especially around Well # 4 ) would lead to considerably
easier burning of the in-situ kerogen. Because the required
degree of rubblization is unknown, it is recommended that a
combined theoretical-experimental effort be undertaken in which
the question of required porosity and permeabilities necessary
for successful retorting be addressed. A first step in the
theoretical aspects of this program may be to develop a theoretical
model describing the in-situ burning and recovery processes.
Natural building blocks for such a model could be models pre-
viously developed by S3 to describe porous media flow and com-
bustion as related to coal gasification. T h e s e analyses could
be integrated to provide a model describing in-situ retorting.
Development of a theoretical model together with the experimental




                                          38
@   work would eventually lead to characterizing media requirements
    necessary for successful in-situ oil retorting.
            In conjunction with model development, it is also re-
    commended that efforts be made to rubblize future retort volumes
    a s required to provide the necessary porosity and permeability
    distributions. In this sense it is recommended that the explo-
    sive requirements and placements such as downhole pre-hydrofrac-
    turing, etc., be developed and designed so that required system
    characteristics can be obtained. It is also recommended that
    pressure tests, and possibly tracer gas tests, be conducted
    as required during the fracturing program in order to ensure that
                                                              3
    the desire6 rubblization is being accomplished. Again, S has
    extensive experience in characterizing explosively fractcred
    media of this type. These analytical methoc7,s may be used to
    provide a theoretical prediction of the extent of fracturing and
    the distribution of porosity. Again, attainment of suitable per-
    meabilities and porosities are necessary ingredients for devel-
    opment of a successful in-situ retort.




                                39
                                           APPENDIX A

                                         DATA SUMMARY


           A summary of t h e             test d a t a is included i n t h i s appendix.
Table A . l o u t l i n e s t h e t e s t s c h e d u l e a n d d e f i n e s t h e s e q u e n c e
of a l l c r i t i c a l o p e r a t i o n s . F i g u r e A . l i s a s c h e m a t i c of t h e
well l a y o u t s h o w i n g t h e w e l l n u m b e r s w h i c h w i l l be r e f e r r e d t o
in l a t e r s e c t i o n s of t h e a p p e n d i x a n d t h r o u g h o u t t h e r e p o r t .
T a b l e A . 2 p r o v i d e s a h i s t o r y of t h e s y s t e m b r i n e l e v e l s m e a s u r e d
d u r i n g t h e t e s t p e r i o d . F o l l o w i n g t h i s , t h e r e s p o n s e of e a c h
individual w e l l is discussed i n d e t a i l , Included i n t h e dis-
c u s s i o n i s a summary of s i g n i f i c a n t e v e n t s o c c u r r i n g a t t h i s
w e l l , t o g e t h e r w i t h a r e c o r d of t h e p r e s s u r e h i s t o r y a n d t r a c e r
gas c o n c e n t r a t i o n h i s t o r i e s a s measured i n t h e w e l l .




                                                 41
                                                    Table A . l
                                        Summary of T e s t P r o g r a m

  Date
                       AiiI-nj e c t i on                                                 Remarks
                                                                                          ---
--- u l y l
 (J           Time
   07         7000                                                        All wells shut in at this time.
   08         14 30                         l Z B ? into Well 43          Well 4 3 fillet with 12B2 at concen-
                                            (through capil l c r y        tration of -10-5.     Tracer in2ecteC into
                                            at w b i e n t pressure)      this w e l l prior to pressurization Of
                                                                          Well 4 4 in order to observe flow from
                                                                          Well t3.
   08         1630                          lZB2 injection completed
   08         2200                          Brine purr.pe3 Iran           2293 gallons obtained f r o = Well (3.
                                            Uells (3 and bS               Kone from 45.
   09         0640    On at 47
   09         0650                          1381 into annulus at          13Bl tracer < a s injected into region
                                            well 1 7 at -10-6             surrounding Hell 1 7 . Hovenent of
                                            concentration                 this tracer vi11 be observed during
                                                                          pressurization test from b4.
   09         0850                          1 3 B 1 injection completed
   09         0945    Off st (7                                           No f l w into formation at t h f r t b e ,
                                                                          air flou continued.
   09         1030    On at b7
   09         1630    Off at ( 7                                          1381 tracer gar should be in formation
                                                                          at thir time.
   09         1650    On at 1 4                                           P r h . A r y test program initiated.
   09         1650                          dF into annulus at            b r 6 I s mixed with injection air i n
                                            WePl 1 4 at concentra-        annulur.
                                            tion of -10-7
   09         1930                          SF6 injection completed
   10         0330                          C318 into capillary at        End of capillary is 1265 ft depth.
                                            Well 1 4 at concentration     C318 will enter forration only i f
                                            of -10-6 (if mixed v i t h    there is f l o w through Antrim.
                                            air r t r e a m )
   10         0600                          C318 injection completed
   11         0900                          SF into annulus at            Repeat earlier test to observe system
                                            wet1 1 4 at concentration     response at operating prersure
                                            of %io-7
   11         0930                          1381 into capillary at        Repeat earlier tent to observe s y s t a
                                            Well 4 4 at concentration     response at operating pressure
                                            of %10-6
   11         1000    Initiate vent o n                                   Well (3 outflow at B O psig back pressure.
                      Well (3 per Lm
                                   h                                      (Prevent Well 83 pressure becoming l a r g e
                      requeat                                             enough to displace brine to other n l l r ) .
   11         1300                          SFg an8 13Bl injections
                                            completed
   13         0430    Vent terminated                                     Prepare system for pressurization fram
                      o n Well 4 3                                        Well 43.
   13         0650    Off at 0 4                                          Test froa Well ( 4 completed.
   13         0650    On at 4 3                                           Determine communication from 13 to
                                                                          4 5 And ( 6 per Dov requert.
   13         0650                          l ? B Z injection into
                                            ar.nuIus At %io-6
                                            concentration
   13         0700                                                        Uellr ( 5 and 16 vented t o and regulated
                                                                          at 40 psig. Cas from ( 5 saturated w i t h
                                                                          12B2 (sample obtained at 0600). Noter
                                                                          Capillaries o n both ( 5 and (6 plugged.
  13          0850                          1 ? R 2 completed
   13         0900                          C318 injectlon into           Observe system response at higher prer-
                                            annulus at %io-6              sure and use g a r not found in Hell 8 5 .
                                            concent ration
   13         1200                          C 3 1 8 injection completed
   14         0700    off at e3                                           Test completed.




                                                    42
     \
         .
43
                            Table A . 2
            History of B r i n e L e v e l in Wells




                                                      Quantity
Well     Brine              Date                      Removed
Number   Level              Examined                 -a l l o n s )
                                                     (G               Remarks

3        1176f              6/2 8                     3876
                            7/3                       1097
                            7/7                        137
                            7/8                       2293
                            7/11                         9
                            7/13                      1703

4        1315               6/24
         1316               7/5
         1312               7/16

5        1311*              7/10                        129

6        1098               6/26                                      Air L i f t e d
         1138               7/5
         1167               7/15

7        1320               6/26
         1339               7/5
         1330               7/15

8        1295               7/4
         1283               7/6                                       L e v e l dropped
         1323               7/14                                      40' during test
                                                                      period.

10        1347              7/5
          1330              7/6
         '1315              7/15

12       1327               7/5                                       Level increased
         1210               7/14                                      117 ' during
                                                                      test period




            +REDA pumps l o c a t e d i n t h e s e w e l l s .




                                                                                          n




                               44
                            FG2SPONSE O F WELL 43
                       (See F i g u r e s A . 2 t h r o u g h A . 4 )



Summary:
       0     SFg a r r i v e d a t 5 3 a t l o w c o n c e n t r a t i o n s 1 4 h o u r s
             after injection a t #4.                   The f l o w p a t h c o u l d be
             e i t h e r t h r o u g h t h e A n t r i m or F a l s e A n t r i m l a y e r s .

       .If t h e r e i s n o d i s p e r s i o n , w h i c h r e s u l t s p r i m a r i l y
         from v a r i a t i o n s i n f l o w c h a n n e l d i m e n s i o n s , t h e n
         t h e t r a c e r gas concentrations should reach t h e i r
         maximum l e v e l s of 3 x 10-8, 2 x 10-7, 3 x 10-7 a n d
         4 x 10-8 for t h e SF^, c 3 1 8 , 1 3 B 1 a n d SF^ a r r i v a l s ,
         r e s p e c t i v e l y . T h e s e p e a k v a l u e s s h o u l d be o b t a i n e d
         w i t h i n 1 6 0 , 1 5 0 , 2 4 5 a n d 2 l n m i n u t e s (i.e.! t h e
         i n j e c t i o n p u l s e d u r a t i o n ) of t h e i r r e s p e c t i v e f i r s t
         arrivals.

       0     T h e i n i t i a l SF a r r i v a l o c c u r s a f t e r 14 h o u r s .
             I n i t i a l c o n c e n t r a t i o n s a r e low, t h e r i s e t i m e i s
             l o n g ( > 3 0 h o u r s ) a n d t h e p e a k c o n c e n t r a t i o n i s low.
             A l l t h e s e f a c t o r s i n d i c a t e l a r g e dispersion.

       e C 3 1 8 a r r i v e d a t P 3 , w i t h l i t t l e d i s p e r s i o n , 28 h o u r s
         a f t e r i n j e c t i o n through c a p i l l a r y tube a t #4.
         I n i t i a l l y , t h e C 3 1 8 f l o w m u s t be t h r o u g h t h e A n t r i m
         f o r m a t i o n ( s e e F i g u r e -2      ,
                                                      t h e v o l u m e of t r a c e r g a s
             i n j e c t e d t h r o u g h c a p i l l a r y i s s o s m a l l t h a t it
             c a n n o t f i l l t h e w e l l v o l u m e up t o t h e F a l s e A n t r i m ,
             t h u s t h e flow i n t o t h e f o r m a t i o n m u s t o c c u r t h r o u g h
             the Antrim).

           @ T e s t r e p e a t e d w i t h s y s t e m a t h i g h e r p r e s s u r e by
            i n j e c t i o n of 1 3 B 1 i n t o c a p i l l a r y a t # 4 .       Transit
            t i m e through Antrim reduced t o 1 0 hours.                           Dispersion
             of t r a c e r g a s was a g a i n s m a l l .

       eSF           injection i n t o annulus repeated w i t h system a t
             h i t h e r p r e s s u r e . A 1 0 h o u r t r a n s i t t i m e was o b s e r v e d .
             Under t h e s e c o n d i t i o n s , t h e r e was l i t t l e d i s p e r s i o n
             Of   the S F g .
             The a p p a r e n t p e r m e a b i l i t y a n d p o r o s i t y v a l u e s f o r t h e
             f o r m a t i o n i n t h e v i c i n i t y of \+e11 8 3 a r e shown i n
             Figure 6.




                                             45
                                                                       n
Conclusions :
       0   There is flow through Antrim formation a t l e a s t in
           vicinity of 8 4 .
           F l o w rate between 6 4 and 113 increases and dispersion
           decreases as system pressure is increased.
       e Immediate vicinity of 8 3 is highly fractured a n d has
         a porosity r a n g i n g up to QO.3.  T h e apparent perme-
         ability of r e g i o n surrounding 113 is % 0 . 4 md.




                                                                       A




                               46
c

                     (i)                             (ii)         ("1                                            13Bl
                                                      I            I                                             C318




        4
    c
    2Ja
    L
    2a
                                                                                              mm
                                                                                  I'

                                                                              0
                                                                                                   Gas injection at Well 14
                                                                                          (i)      sF6 injection at annulus
                                                                                         (ii)      SF6 injection at annulus
                                                                                        liii)      C318 injection at capillary
                                                                                         (iv)      1381 injection at capillary
                                        m m                                               (VI      Time at which sF6 reaches Antrim
                                      . .           t:/+lo4                             ( v i ) 4 3 venting from 320 psig t o
                                  * B   B                 hours                                 80 p i g . After this period,
             10-lC                                                                                 t 3 regulated at 8 0 psig.
                             -8
                              2                4
                                            hours

                     c   1   4    4
                      hours
                                        1             I                  I        A A     I                 1             I
                                        20           40                  50              80                100           120          140
                  July 9                                                Time (hours)
                  1700




            Figure A . 2 .            History of t r a c e r g a s c o n c e n t r a t i o n s m e a s u r e d a t Well # 3
                                      d u r i n g p r e s s u r i z a t i o n of Well # 4 .
        400                                                                       x Annulus p r e s s u r e


                                                            Note:   Reda pump down h o l e ,
                                                                    t h e r e f o r e , no p r e s s u r e
                                                                    i n d i c a t e d on t u b e .

        30C
4
cn




        20c




           01            I         I          1             1                 I                     i         I
              0         20        40         60             80               100                   120        IO
              July 9                          T i m e (hours)
              1700



     Figure A . 3 .    Pressure   history of Well # 3 during pressurization of Well # 4 .
 0
     0
     0
         0
         0
          0
           0
            0
                0
                0
                        0
                                    0
                                        0
                                             0
                                                   0
                                                        0
                                                                 0
I         I         I           I            I           1         ’    -   0   -       i
0         0         0           0            0           0         0        0       I
0         0         o       +   0            0           0         0        0
0)        e         W           v1           w           0         cy       4
                                        (67sd) a r n s s a z d
                                        49
                                                                         A




                              RESPONSE OF WELL # 4
                                (See Figure A . 5 )




         Summary :
     -
              0   The apparent permeability and porosity values for
                  the formation in the vicinity of Well # 4 are shown
                  in Figure 5.
     i




         Conclusions :
             0    The region surrounding # 4 has a significantly lower
                  permeability and porosity compared to that observed
                  in the region surrounding Well #3.




..




                                                                         A




                                        50
                                                                  .
                                                                 rl
                                                                 rl
                                                                 P
    0                                                            tn
                                                                 -4
    0                                                            c
                                                                 U
    0                                                            vc
                                                                 0
    0                                                            c
                                                                 0
                                                                 -4
    0                                                            u
                                                                 a
     0                                                           N
                                                                 -4
                                                                 k
     0                                                           3
                                                                 v)
     0                                                           v)
                                                                 al
                                                                 k
     0                                                           a
                                                                 tn
    0                                                            c
                                                                 4
    0                                                            k
                                                                 1
                                                                 a
    0
    0
    0 w
    0"
         r(
    0:s
    0
    0
    0
    0
     0
        0
              0
                                0                                 .
                                        O       O
0   0             0    0   0        0       0       0   0    0
0   0             0    0
m   m             fi   *   0
                           VI
                                    0
                                    0
                                            0
                                            0
                                                    0
                                                    N
                                                        0
                                                        r(
                            51
                             RESPONSE OF W L L # S
                          (See F i g u r e s A . 6 and A.7)



Summary:
            F a i l u r e of c a p i l l a r y t u b e to r e m a i n o p e n r e s u l t e d
            i n n o d a t a u n t i l p r e s s u r i z a t i o n of 6 3 i n d u c e d flow
            into Y5.
       .Well         / 5 w z s v e n t e d p r i o r to p r e s s u r i z a t i o n of 8 3 .
            A t t h i s t i m e , a i r i n d5 c o n t a i n e d 12B2 a t t h e
            c o n c e n t r a t i o n i n j e c t e d i n t o # 3 a t 1430 o n J u l y 8.
            T h i s a i r c o n t a i n e d no o t h e r t r a c e r g a s e s .

       e C318 i n j e c t e d i n t o 8 3 a r r i v e d a t 4 5 w i t h l i t t l e
         d i s p e r s i o n i n less t h a n 1 0 hours.

            12B2 i n j e c t e d i n t o 113 when # 3 was a t a v e r y l o w
            pressure was not d e t e c t e d a t /!.(No      explanation.)

       O L ~ cWn c e n t r a t i o n s of 13B1 a n d SF6 o r i g i n a l l y
              o
            i n j e c t e d i n 114 d i d a r r i v e a t 8 5 .


Conclusion:

        0   I n i t i a l l y , c o m m u n i c a t i o n o c c u r s b e t w e e n Wells 4 3
            and b 5 a s if           k ; .01 mdarcy.
                                            0



            NOTE:                        !
                          T h e Well b p r e s s u r e w a s r e g u l a t e d at 4 0 - 5 0 p s i g .
            About 1 0 h o u r s following p r e s s u r i z a t i o n of W e l l 8 3 ,
            t h e r e was s u f f i c i e n t flow t o well 8 5 t o c a u s e t h i s
            well t o b e g i n v e n t i n g . A i r flowing from Well 1 5
            c o n t a i n e d t r a c e r g a s e s i n t h e a m o u n t s shown i n
            F i g u r e A.6.        The p e r m e a b i l i t y w a s c a l c u l a t e d based
            o n the 1 0 h o u r t r a n s i t t i m e using E q u a t i o n (C.6)
             ( w i t h 0 = 0,001) a n d t h e r e f o r e r e p r e s e n t s a lower
            limit.




                                        52
c                                                                                                                                                        c

                               1381
                           A   C318
                           m   SF6                                                                                       *   4
                                                                                                                             ..




                                                                                                             G a s samples
                                                                                                                                       -4
                   b
                                       Capillary l i n e blocked
                                                                                                             obtained
                                       Could n o t o b t a i n gas sample
                                                                                                         1   from v e n t lin'e
                                                                                                             (regulated a t
                                                                                                             4 0 - 5 0 psig)

                          ( i ) l r i r a n d l2B2 i n j e c t i o n i n i t i a t e d a t W e l l 1 3
                                 ( 2 h o u r p u l s e of 1 2 8 2 )
                        ( i i ) C318 i n j e c t i o n i n i t i a t e d a t W e l l 1 3
                                                                                                                 0

                                                                                                                             0
                                                                                                                                   ..
                                                                                                                                 0 .




                                                                                                                                            * '



                                 ( 3 h o u r p u l s e o f C318)
                       ( i i i ) I n i t i a t i o n of o u t f l o w f r o m W e l l 1 5
                        (iv) W e l l 1 5 v e n t e d t o a r e g u l a t e d b a c k p r e s s u r e
                                o f 50 p s i g .     Gas samples t a k e n d u r i n g v e n t
                                were s a t u r a t e d w i t h 12R2 o r i g i n a l l y i n j e c t e d
                                i n t o 83. S a m p l e c o n t a i n e d no o t h e r t r a c e r gases.



                                                                                                             e

                                                                                                                     m

           10-l1                        1                   1                    I                  1                    I
                                       20                  40                   60                80                 100                          I 10
                July 9                                                Time (hours)
                1700




    Figure A . 6 .         History of tracer concentration measured at Well # 5
                           during pressurization of Well #3.
                                              !




       4 00       x Annulus p r e s s u r e



                       Note:    Leak on Reda pump fitting
                                may be c a u s e of f a i l u r e
                                to p r e s s u r i z e




       loo




          C                     I                 1             I            1    I
                               20                 40           60            80   100   0

              July 9                                    Time ( h o u r s )
              1700



Figure A . 7 .         Pressure h i s t o r y of Well # 5 .

                                                                                            Q
                            RESPOXSE OF WELL 1 6
                         (See F i g u r e s A. 8 and A . 9 )


Summary :

        0   SF6 a n d C318 a r r i v e d a t # 6 a t h i g h c o n c e n t r a t i o n s
            ( t h u s i n d i c a t i n g l i t t l e d i s p e r s i o n ) even prior t o
            n o t i c e a b l e pressure a r r i v a l .          These t r a c e r g a s e s
            had b e e n i n j e c t e d a t 8 4 .          T r a c e r a r r i v a l i n 86
            s u b s t a n t i a l l y p r e c e d e d t h a t i n 113.

        e Once pressure i n c r e a s e d i n $6, t h e c a p i l l a r y t u b e
            a p p a r e n t l y f i l l e d w i t h b r i n e so t h a t f u r t h e r g a s
            samples c o u l d not be o b t a i n e d .

        ~ K h e n e l l R6 v e n t e d , p r i o r t o p r e s s u r i z a t i o n f r o m
                  W
          # 3 , t r a c e a m o u n t s of SF6 were f o u n d , h o w e v e r , t h e r e
          w a s no 12B2 i n t h i s w e l l .

        0 1 2 B 2 a n d C318 i n j e c t e d i n t o 1 3 a r r i v e d a t 6 5 w i t h
           l i t t l e d i s p e r s i o n i n less t h a n 1 0 h o u r s . T h e 12B2,
           i n j e c t e d i n t o Well t 3 when wells f 3 , d 5 and 6 6 were
          at l o w pressure a p p e a r s t o have p r e f e r e n t i a l l y
          t r a v e l l e d t o W e l l 116.

        e w e 1 1 86 r a p i d l y f i l l e d w i t h b r i n e f o l l o w i n g pres-
          s u r i z a t i o n 'of 1 3 .

Conclusions:

        @ T h e e a r l y a r r i v a l of C318 a n d SFg i n a6 i n d i c a t e s
         f l o w t r a v e l s from 1 4 t o # 6 t o E3 a n d t h e n t o # 5 .
         S i m i l a r l y , 12B2 o r i g i n a l l y i n j e c t e d i n t o P 3 w a s
         f o u n d i n 4 5 , b u t not in 86. C o m m u n i c a t i o n b e t w e e n
         4'4 a n d 86 s t o p p e d once t h e p r e s s u r e in W e l l # 3 h a d
         reached ~ 2 0 0       psig.
        @ I n i t i a l l y , c o m m u n i c a t i o n occurs b e t w e e n Wells # 3 a n d
         $6 a s i f k 2 0.01 m d a r c y ( c a l c u l a t e d a s d e s c r i b e d
         for Well # 5 ) * T h e a i r flow d e g e n e r a t e s w i t h t i m e as
         a p p a r e n t l y b r i n e i s p u s h e d t o w a r d #6. T h e r a p i d
         i n c r e a s e i n t u b e pressure shown i n F i g u r e A . 9 r-cslulted
         from b r i n e f i l l i n g the t u b e .



                                        55
                                       SF6                              t t
                                    4 12B2




    A
         10"
                                                                      '7
    b
    .A
    a
C




                                                                                  '   88:               1
                                                Capillary line blocked.               I.   ,'.
                                                Could not obtain gas                                        Gas samples
                                                sample                                                      obtained from
                                                                                                            vent line (regu-
                                                                        I,                                  lated at 40-50
                                                                              0                    rn       Psi91
                                                                              0
                                                                                                 510    m
                        (i) Air and 12B2 injection initiated at Well 13
                -           (2 hour pulse of 1282)
                       (ii) C318 injection initiated at Well 13 (3 hour pulse of C318)
                      (iii) 'Initiation of outflow from Well 1 5
                      (iv) Well t 5 vented to a regulated back pressure of ~ 5 psig.
                                                                               0
                           Gas sample taken during vent contained a trace Of SF6, but
                           n o other tracer gasee.
         lo-l:
                              I           I            I            1           1
               0             20
               July 9                            Time (hour81
               1700



         F i g u r e A.8.   H i s t o r y of tracer c o n c e n t r a t i o n measured a t Well # 6 .
c                                                                                       c



           400                    x   Annulus p r e s s u r e
                                  0   Tube p r e s s u r e




     h


     .


     v
      P
      d
      v)
      a
      P)
      Ll
      3
      v)

      9
      Lc
     0.
           300




           200
                                                                          f
                                                                              I
           100




             0
                            20           40                  60    80   100        -
                                                                                  l 0
                 July 9                             Time (bourn)
                 1700




    Figure A.9.           Pressure history of Well # 6 .
                        RESPONSE O F WELL # 7
                 (See Figures A . 1 0 through A . 1 2 )

Summary :
          @The l o n g duration 13B1 pulse results from the
           injection of 13B1 in Well 117 at 0 6 5 0 on July 9.
           This tracer gas was initially forced into the
           formation around 8 7 and is now returning as a
           result of pressurization of 8 4 .
      -   eThe later SF6 arrival at 8 7 corresponds to a
           formation permeability of %Lo. 01 mdarcy* (calculated
           according to Equation !C.6)). The long time required
           for the pulse to reach a maximum concentration indi-
           cates much dispersion.
          o C 3 1 8 injected at 8 4 did not reach # 7 .
          .The apparent permeability and porosity values
            for the formation in the vicinity of Well 8 7
            are shown in Figure 7     .
Conclusions:
          .There is no measureable flow between R4 and # 7
            through kntrim formation.
          .The apparent permeability and porosity in immediate
            vicinity of Well 8 7 is 0.03 mdarcy and 0.001,
            respectively.




 It is assumed that SF6 detected at Well ill corresponds to the
 first injection of SFg in W e l l # 4 . If it results from the
 second SF6 injection, then k Q 0 . 0 4 mdarcy. This would a l s o
 imply there is no communication between 8 4 and through the
 Antrim since no C 3 1 8 was detected at 1 7 .




                                58
                              (il                                      (ii)
                                                                        1         (VI
                                                                                    I                     Gas i n j e c t i o n a t W e l l 1 4
                                                                                                  ( i ) SF6 i n j e c t i o n a t a n n u l u s
                                                                                                ( i i ) SF6 i n j e c t i o n a t a n n u l u s
                                                                                               ( i i i ) C318 i n j e c t i o n a t c a p i l l a r y
                                                                                                ( i v ) 1381 i n j e c t i o n a t c a p i l l a r y
                                                                                                    (VI   T i m e a t w h i c h SF6
                                                                                                                             injection
                                                                                                          (ii) reaches antrim.
             L


                                            ,    .   I   '



                                             4.

                                                     : e
ul       L
W       AJL
         co,
         @a
         u
         cu)
         o a      .
         v.m      '




         L k                                13B1
         U4-J     .   ,.*<
         u
                                                                                                                             . I

                                         Note :
                                           1. Well 17 w a s p r e s s u r i z e d for                                eaB'
                                                                                                                    m  .
                                               14 h o u r s prior to a i r i n j e c t i o n
                 10-1
                                                         at 14.
                                                                                                                  90,
                                            2.           1 3 8 1 was i n j e c t e d i n t o   Well 117
                                                         d u r i n g f i r s t 2 h o u r s of
                                                         p r e e s u r i za t i o n .

                                                                                                            m m
                 10-1                        I                           I                     1                     1                   I
                                            20                         40                      60                  till               100               I !O
                             Ju'ly 9                                            Time ( h o u r s )
                             1700



     F i g u r e A.lO.              H i s t o r y of t r a c e r g a s c o n c e n t r a t i o n s m e a s u r e d a t W e l l #7
                                    d u r i n g p r e s s u r i z a t i o n of W e l l # 4 .
     u-l
     0
      u-l
       0
60
      9 oc
                           0 ooo O C P 0
                                           0 0 0 0
      700               0

                      00
      600

                                                         0 Measured   pressures

      500
                    0

      400




      300
                  0

      200



      100     3


                                  I                  I                     I
        OJuly 9                   10                20                    30
             0640
                                            T i m e (hours)



Figure A . 1 2 .        Pressure measured at Well # 7 during pressurization of this
                        well.

                                                                                      I
                       RESPONSE OF WELLS C8 AND # l o
                     (See F i g u r e s A . 1 3 t h r o u g h A.16)


Summary:
       8    Flow occurs t o Wells 48 a n d dl0 when Well # 3 has
            a n e l e v a t e d p r e s s u r e . T h e C318 a r r i v a l t i m e s cor-
            r e s p o n d t o a p e r m e a b i l i t y of 0 . 0 4 m d a r c y .     It
            s h o u l d be n o t e d t h a t t h i s i s a f i r s t a r r i v a l
            a t a 1 o w . c o n c e n t r a t i o n . The R a v e r a g e " p e r m e a b i l i t y
            f o r t h e b u l k f l o w may be f a c t o r s o f t e n l e s s t h a n
            t h i s value.
       0    The l o w c o n c e n t r a t i o n of C318 i n d i c a t e c o n s i d e r a b l e
            d i s p e r s i o n o c c u r s b e t w e e n i n j e c t i o n a t Well 114 a n d
            d e t e c t i o n a t Wells t 8 a n d 410.                 (If slug flow
            o c c u r r e d w i t h n o d i s p e r s i o n , t h e C318 c o n c e n t r a t i o n s
            a t Wells # 8 a n d $10 s h o u l d r e a c h a m a x i m u m l e v e l of
            a b o u t 1 x 10-7 w i t h i n 3 h o u r s a f t e r t h e f i r s t d e t e c t i o n . )

        0   Flow t o 118 a n d F10 i n i t i a l l y s t a r t s t h r o u g h A n t r i m
            formation around 84.

       0    Absence of SF6 a t t h e s e w e l l s i n d i c a t e s f l o w p a t h s
            were n o t o p e n when S F 6 i n j e c t e d ( s y s t e m p r e s s u r e
            was l o w d u r i n g SF6 i n j e c t i o n ) .


Conclusion :

       Q    Flow o c c u r s f r o m # 4 t h r o u g h A n t r i m f o r m a t i o n t o
            # 8 a n d 810 so l o n g a s W e l l 8 3 is a t a n e l e v a t e d
            pressure.




                                            62
                     lo-6
                                 (i)

                                       (ii)


                     10”
                                       1                                         AC318

                                                                                ( i ) SF6 injection into
                c
                 &
                rl
                                                                                       1 4 annulus
            cm
            0                                                                  ( i i ) C318 injection into
                                                                                        #4 capillary
                                                                              ( i i i ) Well 1 3 venting from
                                                                                        320 p s i g t o 8 0 p s i g .
                                                                                        After t h i s period, 1 3
                                                        A                 d             regulated at 8 0 p s i g .

                                                                  _. -
                                                            A
                                                                 * *-    .f




                                                   *-   .
                                                        -       .I---




                                                                        rii7
                     1O’ll
                             0                20                        40             60                80             100
                             July 9                                     Time (hours)
                             1700




63   F i g u r e A . 13.          History of t r a c e r gas c o n c e n t r a t i o n s m e a s u r e d at
                                  Well # E l .
                                                            63
           4
                                                                     X



                                                                             I
                                           0


  -
  0,
  4
           3

  m
  a
  Y


  0,
  &


  :
  &    2
  a




           1                      I   Annulus p r e s s u r e
                                  0   Tube p r e s s u r e




               '                                         I       i       I
                        20            40                60      EO   100'        10
               July 9                           Time (hours)
               1700




F i g u r e A.14.       P r e s s u r e history of Well #8.

                                               64
                          I                           (i I SF6 injection into
                                                             1 4 annulus
                                                    (ii] C318 injection into
            k                                                1 4 capillary
            4
        c a                                        ( i i i ) Well 1 3 venting from
        0
        -4  4J                                               320 psig t o 80 psig.
        U k
        Q I Q                                                After t h i s period, 1 3
        ka                                                   regulated a t 80 psig.
        U
        C k
        001
        oa
        c
        om
        om                              b A
            D,
        m
        4 k
        0101
            o
        alk
        v u
        4
        kr,
        ek
            m
            a
            CI




                 July 9
                 1700                         Time (hours)




br3   Figure A. 15.       H i s t o r y of t r a c e r gas concentrations m e a s u r e d at
                          Well #lo.
                                              65
    50


                                       /                      0   0   0   0   0   -
                                                                                  b



    40




                                                    X


                                                                      X




                                              X   Annulus pressure
                                              o   Tube pressure


    10




     0
         0                                                                            20
         July 9                              Time (hours)
         1700




Figure A.16.      P r e s s u r e h i s t o r y of W e l l   #lo.

                                        66
                              RESPONSE OF WELL 1 9



Summary:

         e Well # 9 developed a p r e s s u r e , b u t air samples
           taken from t h e w e l l contained n o evidence of
           tracer g a s e s . T h e v a l v e o n t h e compressed air
           inlet w a s f o u n d to leak. T h e w e l l was vented
           ( 0 7 0 0 o n 1 2 July) and t h e air line r e m o v e d .
           S u b s e < u e n t l y , t h e p r e s s u r e on \;ell 8 9 remained
            con s t a n t .

Conc l u s ions :
         e Subsequent t o 0700             o n 12 J u l y , t h e r e w a s no
            c o m m u n i c a t i o n w i t h Well t 9 .

            E a r l i e r communication w i t h W e l l %9 c o u l d
            n o t be d e t e r m i n e d s i n c e # 9 w a s b e i n g
            p r e s s u r i z e d from t h e s u r f a c e .




                                     67
                           RESPONSE OF WELL #12
                       (See F i g u r e s A . 1 7 a n d A . 1 8 )


Summary:
       . T h e r a p i d 13B1 a r r i v a l a t 1112 occurs a t a t i m e
          e x p e c t e d i f t h e 87 t o 1112 p e r m e a b i l i t y w e r e
                   m
          ~ 0 . 1 darcy.
       . F l o w from t 4 t o C12 o r i g i n a t i n g t h r o u g h t h e A n t r i m
          f o r m a t i o n ( e v i d e n c e d by t h e s h a r p C318 a r r i v a l ,
          t h e s u g g e s t i v e s e c o n d 13B1 a r r i v a l ) o c c u r s
          a t a t i m e corresponding t o a permeability
          of ~ 0 . 1m d a r c y .

       .Flow     a t l o w p r e s s u r e s through t h e F a l s e Antrim
           o r some other p a t h d i f f e r e n t from t h a t followed
           by t h e C318 ( e v i d e n c e d b y t h e f a c t t h e f i r s t
           SF6 p e a k a r r i v e d 28 h o u r s a f t e r t h e C318) was
           much slower t h a n t h a t o r i g i n a t i n g t h r o u g h t h e
           Antrim.

       .The        low c o n c e n t r a t i o n s of C318 a n d SFg c o m p a r e d
           t o t h a t of t h e 13B1 i n d i c a t e m o s t f l o w into               .
           Well e12 i s 13B1 o r i g i n a l l y i n j e c t e d i n t o W e l l 87.
           (If a l l g a s e n t e r i n g W e l l # 1 2 c o n t a i n e d
           t r a c e r a t t h e i n j e c t i o n c o n c e n t r a t i o n , t h e C318
           a n d S F g c o n c e n t r a t i o n s i n W e l l # 1 2 w o u l d be
           e x p e c t e d t o o b t a i n a peak of 7 x 10-7 a n d
           7 x 10-8, r e s p e c t i v e l y . )


Conclusions :

        ~ C o m r n u n i c a t i o n b e t w e e n 117 a n d 8 1 2 c o r r e s p o n d s t o
          a p e r m e a b i l i t y of ~ 0 . 1 d a r c y .
                                                    m

       .Flow o r i g i n a t i n g t h r o u g h A n t r i m f o r m a t i o n from # 4
         t o 8 1 2 i s much f a s t e r a t t h e h i g h e r pressures t h a n
         is t h e f l o w a t l o w p r e s s u r e s w h i c h possibly w e n t
         t h r o u g h t h e False A n t r i m f o r m a t i o n .




                                  68
                                                     'i" (7
                                                                                Gas injection at Well 1 4
                                                                                 (i)     SF6 injection at annulus
                          (iii)                                                 (ii)  sF6 injection at annulus
                                                             (iv)

         1o - ~                                       I                        (iii)
                                                                                (iv)
                                                                                      C318 injection at capillary
                                                                                      13B1 injection at capillary
                                                                                ( v ) Time at 'which SF6 reaches
                                                                                      antrim
                                                                                   ' e     . _.

                                                     .. .       .* *.     --              e        -   **.   .       .   4




                                         6           A                                            '%
                                                                                               a. , '
                                             4   4

                                                                                               m
                  -                                                                      --•

                                13Bl
                           A    c318
                                SF6
          0l-
         1-'          Note:
                        1. Well 17 w a s p r e s s u r i z e d for
                            14 hours prior to air injection
                            at 1 4 .                                 0,
                        2. 13B1 w a s injected into Well ( 7
                            during first 2 hours of                a
                            pressurization.                               -'


                                   I                     I              -dA!                       I             I




6d   Figure A . 1 7 .          H i s t o r y of t r a c e r g a s c o n c e n t r a t i o n s measured at
                               Well #12.

                                                          69
   400   -



   300
                  Note:       Lack of s u b s t a n t i a l C 3 1 8
                              f o l l o w e d by l a t e r i n p u t
                              of SF6



                  0   Tube p r e s s u r e
                  x   P.nnulus p r e s s u r e




                                                                       Note:   Pressure d i d not increase
                                                                               a t Well ( 1 2 u n t i l 16 hour
                                                                               a6 a r e s u l t of v a l v e
                                                                               leaking.         P r e s s u r e began
                                                                               to i n c r e a s e a s soon a s
                                                                               leak f i x e d .


         0               20                   40                 60            80                  100                  120
         July 9                                          Time (hours)
         1700




Figure A.18.           Pressure history of Well #12.


                                                 70
crs                                               APPENDIX B
                                      EXPERIMENTAL TECHNIQUES


                 The a c t u a l i m p l e m e n t a t i o n o f t h e e x p e r i m e n t a l p r o g r a m i n
      t h e f i e l d was p r e d i c a t e d on d e t e r m i n i n g t h e d e g r e e a n d e x t e n t
      of c o m m u n i c a t i o n b e t w e e n t h e v a r i o u s b o r e h o l e s a t t h e Dow T e s t
      Site.        I n o r d e r t o h a v e a r e a s o n a b l e c h a n c e a t success f o u r d i s -
      t i n c t t r a c e r g a s e s were u t i l i z e d :       s u l f u r h e x a f l u o r i d e (SF6) a n d
      t h e F r e o n s 13B1, C-318, a n d 12B2. W h a s t e n t o p o i n t o u t t h a t
                                                                     e
      the use of d i s t i n c t t r a c e r gases is a necessity i n undertaking a
      c h a r a c t e r i z a t i o n program u t i l i z i r . ; m u l t i p l e b o r e h o l e i n j e c t i o n ,
      s i n c e i t i s iiilpossible t o u n a m b i g u o u s l y i n t e r p r e t t r a c e r g a s
      a r r i v a l and c o n c e n t r a t i o n d a t a from m u l t i p l e b o r e h o l e s u s i n g o n l y
      a single tracer gas.

                  Due t o t h e a n t i c i p a t e d e x t r e m e l y h i g h i n j e c t i o n p r e s s u r e s ,
      and t h e f a c t t h a t a l l proposed tracer g a s e s l i q u e f y a t s u b s t a n t i a l l y
      lower p r e s s u r e s , t h e v a r i o u s t r a c e r g a s e s were c o m m e r c i a l l y d i l u t e d
      10,OOO:l i n n i t r o g e n a n d t h e n c o m p r e s s e d t o 6 , 0 0 0 p s i by t h e
      Linde Corporation.                  I n t h i s m a n n e r , a q u a n t i t y of t r a c e r g a s w a s
      a v a i l a b l e a t s u f f i c i e n t p r e s s u r e t o overcome any r e a s o n a b l e
      injection pressure expected at t h e Dow Test S i t e .

                 T r a c e r g a s flow r a t e s a n d t h e r e f o r e i n j e c t i o n c o n c e n t r a -
      t i o n s were a d j u s t e d u s i n g a v a r i a b l e o r i f i c e m e t e r i n g v a l v e
      which had been p r e v i o u s l y c a l i b r a t e d .       With t h i s t e c h n i q u e t h e
      t r a c e r g a s c o u l d be d i l u t e d t o t h e d e s i r e d c o n c e n t r a t i o n l e v e l s
      i n t h e c o m p r e s s e d a i r stream. A s a n a d d i t i o n a l d a t u m , t h e t o t a l
      tracer g a s f l o w was d e t e r m i n e d b a s e d o n t h e p r e s s u r e d r o p of t h e
      Compressed g a s c y l i n d e r .

                 P r e s s u r e a n d t r a c e r g a s h i s t o r i e s were m o n i t o r e d a t a l l
      wells.        I n g e n e r a l , pressures were r e a d on Dow-provided p r e s s u r e
(-,   g a u g e s c o n n e c t e d t o c a p p e d m a n i f o l d s e x t e n d i n g i n t o e a c h of t h e



                                                         71
                                                                                                                 A




 boreholes.          I n addition, polypropylene tubing extended i n t o m o s t
 of t h e b o r e h o l e s down t o t h e l e v e l of t h e A n t r i m f o r m a t i o n .            Since
 a l l t h e b o r e h o l e s were e x p e c t e d t o be p r e s s u r i z e d , w e u t i l i z e d
 t h e s e downhole c a p i l l a r i e s i n c o n j u n c t i o n w i t h s a i n p l i n g b a g s
 (i.e., l a r g e b a l l o o n s ) t o d r a w s a m p l e s f r o m d o w n h o l e w i t h o u t t h e
 u s e of a s o p h i s t i c a t e d s a m p l i n g pump. T h i s t e c h n i q u e , of u s i n g
 downhole p r e s s u r e t o f i l l t h e s a m p l e b a g s , w a s c o n s i d e r a b l y
 s i m p l e r t h a n o t h e r a v a i l a b l e methods.

             I n p r a c t i c e , a sample bag w a s p l a c e d on t h e v a l v e d c a p i l l a r y
                                                                                                        I
 l i n e . S i n c e t h e b o r e h o l e was p r e s s u r i z e d , s a m p l e s c o u l d be ob-
 t a i n e d by o p e n i n g t h e v a l v e . O n e o r more b a l l o o n s were u s e d , as
 r e q u i r e d t o c l e a r t h e c a p i l l a r y l i n e of t h e p r e v i o u s s a m p l e , t o
e n s u r e t h e m a j o r p o r t i o n of t h e c o n t a i n e d g a s w a s from t h e w e l l -
b o r e . A i r s a m p l e s w e r e t h e n drawn f r o m t h e b a l l o o n s u s i n g d i s -
p o s a b l e Nalgene s y r i n g e s .      The g a s w i t h i n t h e s y r i n g e w a s t h e n
i n j e c t e d i n t o t h e chromatograph and a n a l y z e d . A l l a n a l y s e s w e r e
                                   3
accomplished u s i n g a n S t r a c e r gas monitor. T h i s i n s t r u m e n t
is described i n the next section.
            S y r i n g e S a m p l e s were o b t a i n e d f r o m t h e area i m m e d i a t e l y
 s u r r o u n d i n g t h e i n j e c t i o n and o u t l y i n g sampling m a n i f o l d s a t
p e r i o d i c i n t e r v a l s t o i n s u r e t h e r e w a s no tracer g a s l e a k a g e
fron? e i t h e r t h e a b o v e - g r o u n d p i p i n g o r from c r a c k s e x t e n d i n g t o
t h e formation.           The m e a s u r e m e n t i n t e r v a l w a s i n i t i a l l y o n t h e
 o r d e r of e v e r y t w o h o u r s , d e c r e a s i n g u l t i m a t e l y t o o n c e a d a y
,during t h e f i n a l phases of t h e experiment. No l e a k s w e r e
detected.

            T h r o u g h o u t t h e c o u r s e of t h e e x p e r i m e n t p o r t a b l e hand-
h e l d d i c t a t i o n - t y p e r e c o r d e r s were u t i l i z e d b y a l l f i e l d p e r -
s o n n e l t o make r e a l t i m e f i e l d n o t e s .      I n t h i s manner a l l
o b s e r v a t i o n s a n d occurrences were c a p t u r e d a s t h e y a c t u a l l y
h a p p e n e d . P r e v i o u s e x p e r i e n c e h a s shown t h a t i n a p r o g r a m of
t h i s magnitude, it i s v e r y u n l i k e l y t h a t p e r s o n n e l i n v o l v e d w i l l
remember m i n o r d e t a i l s some number of d a y s a f t e r t h e y o c c u r .
Monitoring Instrumentation
       The S3 tracer gas monitor is an electron capture gas
chromatograph shown schematically in Figure B.l. The electron
capture gas chromatograph utilizes the high electron affinity
of gases with halogen group elements to provide a measurable
signal. A sample to be analyzed is injected into the instrument
by means of a disposable syringe. Injection is through a rubber
septum located on the sample port. This septum prevents spur-
ious contaminants from diffusing into the chromatograph and
producing anomalous signals.
       The heart of the instrument is the column. It sepzretes
the various gaseous components cf a sample by selectively slow-
ing down some gases relative to others. The column can be
thought of as a device to elute the distinct components in a
gas sample in a definite order.
       When monitoring SF6 p l u s selected Freons, experience
has shown that a column (stationary phase) consisting of one
of the Porapaks provides excellent separation. This separ-
ation is illustrated in Figure B . 2 f o r the tracer gases used
in tests repeated here. Porapak is a porous polymer composed of
ethylvinylbenzene cross-linked with divinylbenzene to form a
uniform structure of distinct pore size. The columns and
detector are generally operated at elevated temperatures to
increase detector sensitivity to tracer peaks and to allow a
complete measurement to be performed in a relatively short time.
Care must be exercised in the choice of operating temperature
since the relative arrival time (elution time) is a function of
Porapak type as temperature and chemical species (see Figure
B.3).  Incorrect operating temperature could provide erroneous
or confusing data output due to peak arrival overlap.




                             73
4
4




    Figure B . l .   Schematic drawing af e l e c t r o n capture gas chromatograph.
                                      Time
Figure B . 2 .   C h r o m a t o g r a p h response showing separation of v a r i o u s
                 t r a c e r g a s e s o n aOonc meter P o r a p a k Q c o l u m n . Column
                 t e m p e r a t u r e = 1 0 0 C; C a r r i e r f l o w r a t e = 5 0 cc/min.

                                        75
       1




cc
 m
 Q,
 +,
 3
 c
-4
 E
 Y



 Q)
  E
 .PI
 4J
  c
  0
 .ri
 JJ
  7
 d
 'W




           0.2   :
                 10
                         I     I
                               20
                                      I        i   I
                                                   40
                                                          1   I

                                                              60
                                                                   I   T
                                                                       80 100
                             T e m p e r a t u r e ("C)

Figure B . 3 .        Elution time as a function of temperature for
                      selected tracers on a o n e meter Porapak Q column.       @

                                          76
6rs
            The detector portion of the chromatograph consists of a
      tritiated titanium foil encased within an electrically con-
      ductive housing. Specific pulse-generator circuitry energizes the
      detector, initiating a flow of electrons from the tritium foil.
      A collector wand within the detector receives the electrons and
      establishes a current flow which is amplified through an
      electrometer circuit. Should an "electron-capturing gas"
      (such as SF6 or one of the Freons) flow through the stream of
      electrons, the current is decreased in proportion to the con-
      centration of the gas.




                                  77
n
crs                              APPENDIX C
                             ANALYTICAL MODEL


                The tracer gas pressurization technique may be used to
      determine many characteristics of an in situ retort region.
                                              -   c   _   _




      Methods of analyzing data for a homogeneous porous formation,
      a F x o u s formation with channeling, or a fractured formation
      are discussed in this Appendix.
      Porous Flow
             When the system responds as IC it were a porous media,
      a two-dimc-nsional finite element time-dependent diffusion code
      isused in a iterative manner to aid in determining permeabilities
      and porDsities. Specifically, a set of material properties
      is selected. A calculation is then made using this set of
      material properties and the known injection rates. Calculated
      pressures and tracer gas arrival times are then compared with
      the experimentally measured pressures and tracer arrivals.
      Various distributions of permeability and porosity are selected
      until the calculated and measured results agree.
             In a uniformly rubblized material, the calculated and
      measured tracer g a s arrival times agree provided the calculated
      and measured pressure and flow rate histories agree. Further-
      more, tracer gas concentrations measured at sampling locations are
      essentially equivalent to the injection concentration. Early
      tracer gas arrivals at low concentration levels imply non-
      uniformities within the formation. For example, a portion of
      the tracer gas may rapidly flow through a fracture to the samp-
      ling region. Under such conditions, the initially measured
      tracer gas concentration at the sampling region is much lower
      than the concentration at the injection region and the time required
      to reach the maximum concentration is long compared to the injec-
6d    tion pulse duration.


                                     79
           This a n a l y s i s d e s c r i b e s flow through a l o c a l l y uniform
media. I f t h e f o r m a t i o n i s l a c e d w i t h n u m b e r s o f f r a c t u r e s or
flow c h a n n e l s , t h i s s h o u l d be a p p a r e n t b y t h e f a i l u r e of
t h e a n a l y s i s t o simulate t h e observed response.

           If t h e r e t o r t r e g i o n i s r u b b l i z e d s o t h a t g a s c a n s l o w l y
d i f f u s e from t h e i n j e c t i o n w e l l t o t h e p r o d u c t i o n w e l l s , t h i s
f l o w may be m o d e l e d u s i n g t h e t w o - d i m e n s i o n a l h y d r o d y n a m i c
c o d e . T h i s code d e s c r i b e s s i m p l e Darcy f l o w .         Thus, t h e
area a v e r a g e f l u i d v e l o c i t y 6 is p r o p o r t i o n a l t o t h e g r a d -
i e n t pressure, p, giving

        - = - - kv p
        q
                   IJ

w h e r e k a n d p a r e t h e p e r m e a b i l i t y a n d f l u i d v i s c o s i t y , re-
spectively.             The c o r r e s p o n d i n g f l u i d p a r t i c l e v e l o c i t y ( i . e . ,
tracer p a r t i c l e v e l o c i t y ) i s j u s t




where 9 i s t h e porosity.                   Note t h a t k a n d 41 may be f u n c t i o n s
of b o t h p o s i t i o n a n d p r e s s u r e .       C o m b i n i n g E q u a t i o n ((2.2) w i t h
t h e mass c o n s e r v a t i o n e q u a t i o n a n d e q u a t i o n of s t a t e




         p = cpy                                                                                 (C.4)



where p , y , and c r e p r e s e n t d e n s i t y , r a t i o o f s p e c i f i c h e a t s a n d
a c o n s t a n t , r e s p e c t i v e l y , y i e l d t h e d e f i n i n g e q u a t i o n for
compressible f l o w i n the porous m e d i a .




                                                 80
    T h e terms o n t h e f a r r i g h t hand s i d e o f E q u a t i o n (C.4) a n d (C.6)
    r e p r e s e n t a s o u r c e w i t h i n t h e m e d i a ( i . e . , a n i n j e c t i o n well).
    n o l u t i o n s t o E q u a t i o n (C.5)     a r e a v a i l a b l e i n b o t h one- and two-
    d i m e n s i o n s ( e i t h e r a x i s y m m e t r i c or C a r t e s i a n ) b y u s i n g a f i n i t e
    element numerical code.                    I n t h e r e t o r t r e g i o n , i t i s assumed
    t h e f l o w i s i s o t h e r m a l , t h u s y = 1.

                Some comments a r e n e c e s s a r y c o n c e r n i n g t h e a n a l y s e s u s e d
    t o i n t e r p r e t r e s u l t s of t h i s e x p e r i m e n t . T o o b t a i n e c o n o m i c a l
    c o m p u t e r c o s t s , it i s n e c e s s a r y t o h a v e t h e z o n e s i z e r e l a t i v e l y
    large.       The s m a l l e s t z o n e s ( s e e F i g u r e 11) i n t h e r e g i o n s of
    Wells ct3, & 4 , #7, a n d P6 were t h e r e f o r e t a k e n a s 3 f t x 3 f t ,
    w h i c h i s much l a r g e r t h a n t h e wellbore d i m e n s i o n s .              To simulate
    w e l l b o r e e f f e c t s , t h e p o r o s i t y of t h e s h a d e d z o n e s , r e p r e s e n t -
    i n g t h e w e l l s , w a s i n c r e a s e d t o c o n s i d e r t h e t o t a l v o l u m e of t h e
    wellbore p l u s t h e p o r o s i t y of t h e m a t e r i a l .    S i n c e t h e calcu-
    l a t i o n is two-dimensional and t h e r e f o r e m u s t be of constant
    t h i c k n e s s , some a d j u s t m e n t s m u s t be made i n t h e a n a l y s i s t o
    account for v a r i a t i o n s i n brine l e v e l t h r o u g h o u t t h e r e t o r t
    region.  Experimental evidence i n d i c a t e s t h a t except i n t h e
    r e g i o n of Wells # l 2 a n d # 6 , t h e b r i n e l e v e l s d i d not s i g n i -
    f i c a n t l y change throughout t h e test.                    The measured g a s f l o w
    w a s t h e r e f o r e p r e d o m i n a n t l y t h r o u g h tgose r e g i o n s of t h e s y s t e m
    w h i c h were f r e e of b r i n e .         I n t h e r e g i o n of t h e i n j e c t i o n W e l l
    # 4 , t h e d e p t h of t h i s b r i n e f r e e r e g i o n i s a b o u t 1 5 2 f t .            This
    d i s t a n c e was t h e n t a k e n a s t h e t h i c k n e s s of t h e s y s t e m .          In
    t h e r e g i o n of Well # 3 , t h e b r i n e free d e p t h i s a b o u t 36 f t .
    F o r c a l c u l a t i o n p u r p o s e s t h e m e d i a p r o p e r t i e s i n t h e r e g i o n of
d
6
                                                    81
a well such as 113 would be adjusted so that this 36 ft section
is simulated by a 150 ft section. The total porosity in the
region of Well # 3 is conserved, but spread over the 150 ft section.
Correspondingly the permeability used in the numerical model was
taken as the actual permeability reduced by the ratio of the real
depth of the brine free region at Well # 3 divided by the depth
used in the analysis. Properties in regions surrounding the
other wells were changed in a similar manner to account for var-
iations in brine depth.
Channel Flow
       Equation ( C . 5 ) can be solved assuming flow occurs in
one direction only (1-D plane flow). This solution can be
used to estimate the s o u r c e to production well permeability
corresponding to an observed tracer gas transit time through
a flow channel such as illustrated in Figure 8. The resulting
permeability to porosity ratio is given by

           4pL2
            3T

where T is the tracer gas transit time and where L is the dis-
                                                         .
tance between the injection and production wells (denoted by
subscripts I and P,* respectively)   .
                                    The mass flow rate (w)
through th.is channel is given by
                 PI’   -    2
                           Pp
                                                             (C.7)


Since the flow rate can usually be inferred from the well
pressurization data, Equation (C.7) can be used to determine
the cross-sectional area (A) of the channel.
Fracture Flow
       Flow along a fracture can also be modeled by assuming
the flow occurs between two parallel flat plates. If the             69
                                82
CIS
      cross-sectional             a r e a of t h e f l o w i s t a k e n a s t h a t a r e a b e t w e e n
      t h e f r a c t u r e p l a n e s , t h e n t h e m a s s flow a n d c o r r e s p o n d i n g v e l -
      o c i t y a r e g i v e n by*

                           2  - (PI -
                              Hb3
                                p
                                                      PPI
                    w = F r;- L                               e




                          -
                        1 b2
                    v = - v (PI-PP )
                        3
                                                                                                           (C.9)

      v h e r e b i s t h e d i s t a n c e between t h e f r a c t u r e p l a n e s                 (i.e.8

      w i d t h of t h e c r a c k ) a n d H i s t h e d r a c k d e p t h m e a s u r e d i n a d i r e c t i o n
      normal t o t h e f l o w v e l o c i t y .            G i v e n measured t r a n s i t t i m e s a n d
      flow r a t e s , t h e c o r r e s p o n d i n g c r a c k d e p t h a n d w i d t h may be i n -
      f e r r e d f r o m E q u a t i o n s (C.8) a n d & . 9 j , i f it i s a s s u m e d t h a t a l l
      f l o w occurs through t h e s e fractures.




      *
          S c h l i c h t i n g , H., B o u n d a r y L a y e r T h e o r y , M c G r a w H i l l ,    1960.




                                                         83
cps                                               APPENDIX D

                                           WELLBORE EFFECTS


                 Wellbore e f f e c t s m u s t be c o n s i d e r e d when i n t e r p r e t i n g
      d a t a t a k e n d u r i n g t h e t r a c e r g a s p r e s s u r i z a t i o n t e s t s of t h e D o w
      i n s i t u retort region.
      7-                                       T h e s e e f f e c t s are v e r y i m p o r t a n t b e c a u s e
      t h e w e l l volume i s l a r g e c o m p a r e d t o t h e v o i d v o l u m e i n t h e
      A n t r i m i n t h e n e a r r e g i o n of t h e w e l l .        The w e l l v o l u m e m u s t
      be c o n s i d e r e d i n a n y i n t e r p r e t a t i o n s of m e a s u r e m e n t s of pres-
      s u r e , t r a c e r g a s c o n c e n t r a t i o n , tracer g a s a r r i v a l t i m e and
      f l o w rate i n t o a production w e l l .

                  The w e l l a c t s a s a l a r g e r e s e r v o i r f o r i n c o m i n g f l o w .
      S i n c e t h e incoming f l o w rates are small, i t t a k e s a c o n s i d e r -
      able t i m e f o r t h e w e l l p r e s s u r e t o i n c r e a s e . As a r e s u l t ,
      t h e w e l l p r e s s u r e may be s i g n i f i c a n t l y lower t h a n t h e p r e s s u r e
      i n t h e formation immediately surrounding t h e w e l l .                              This is
      p a r t i c u l a r l y t r u e i f t h e f l o w i n t o t h e w e l l i s moving t h r o u g h
      f r a c t u r e s r a t h e r t h a n through a uniformly porous media.                          The
      n e t e f f e c t i s t h a t t h e w e l l p r e s s u r e w i l l be much lower t h a n t h e
      p r e s s u r e i n t h e s G r r o u n d i n g media.       T h e s e w e l l p r e s s u r e s pro-
      v i d e a t l e a s t a lower bound f o r t h e p r e s s u r e i n t h e s u r r o u n d i n g
      media, b u t g i v e no i n d i c a t i o n w h a t t h e a c t u a l p r e s s u r e level
      may be.

                  I n o r d e r t o q u a l i t a t i v e l y e v a l u a t e t h e u n i f o r m i t y of
      t h e l o c a l i z e d f r a c t u r e s , i t i s n e c e s s a r y t o know t h e t r a c e r
      c o n c e n t r a t i o n i n t h e gas a r r i v i n g a t t h e p r o d u c t i o n w e l l s .
      C o n c e n t r a t i o n m e a s u r e m e n t s are c o n f u s e d by t h e l a r g e p r o d u c t i o n
      w e l l volume.       I n o r d e r t o i n t e r p r e t t h e measured tracer g a s
      concentrations it is necessary to determine t h e concentration
      w h i c h would e x i s t i n t h e p r o d u c t i o n w e l l i f a l l i n c o m i n g g a s
      c o n t a i n e d tracer a t t h e i n j e c t i o n c o n c e n t r a t i o n . Measurements




                                                       a5
t a k e n f r o m c a p i l l a r y samples w i l l h a v e t r a c e r g a s c o n c e n t r a t i o n s
e q u a l t o t h a t i n t h e a i r l e a v i n g r e g i o n A shown i n F i g u r e D.l.
The r e l a t i o n s h i p b e t w e e n t h e c o n c e n t r a t i o n of t r a c e r i n t h e a i r
l e a v i n g r e g i o n A t o t h a t i n t h e a i r a r r i v i n g i n r e g i o n A is




                        vO       + J (GI - GL)          dt
                                    0

where


                   -
           .
           C

           W       -
                             tracer g a s concentration
                             f l o w r a t e (scfm)

           vO
                   -         v o l u m e of g a s c o n t a i n e d i n r e g i o n " A " shown
                             i n F i g u r e D.l a t t i m e of f i r s t a r r i v a l of
                             t r a c e r (scf)
           t       -         t irne

a n d w h e r e t h e s u b s c r i p t s a r e g i v e n by
           I       -            f l o w i n t o r e g i o n "A"
           L       -            f l o w l e a v i n g r e g i o n "A"
           0       -         i n i t i a l c o n d i t i o n s e x i s t i n g i n r e g i o n "A".

I n w r i t i n g Equation ( D . l ) ,       i t i s assumed t h a t t h e g a s i n r e g i o n "A"
i s c o m p l e t e l y m i x e d s o t h a t t h e t r a c e r g a s c o n c e n t r a t i o n is
uniform throughout.                     I f , as i n t h i s case,      t h e f l o w rates are
t a k e n a s c o n s t a n t w i t h respect t o t i m e and i f it i s assumed
t h a t CI i s c o n s t a n t , t h e n t h e s o l u t i o n of E q u a t i o n (D.l) is
j u s t g i v e n by


         c(t) =        CI   -     (CI    -   co)   { r+yqT-\      1
                                                                                _.
                                                                                              (D.2)

                                                                  vo




                                                   86
@
             .
             wI




             .
             wI

             wL




    Figure D.1.
                  =


                  =
                      -
                      '
                          I
                              -I--




                                                     False A n t r i m



                                                        Antrim




                      A i r flow i n t o p r o d u c t i o n well f r o m a n t r i m or
                      false a n t r i m region

                      A i r flow i n t o cased p o r t i o n of well




                  Model u s e d f o r e v a l u a t i o n of t r a c e r conc
                  i n air entering p r o d u c t i o n w e l l .

                                         87
Equation ( D . 3 ) i s v a l i d i n t h e s i t u a t i o n where t h e p r o d u c t i o n
w e l l i s o p e n so t h e r e e x i s t s n o n e t f l o w i n t o or o u t of r e g i o n
A.    These e q u a t i o n s i n d i c a t e t h e e x p e c t e d tracer g a s c o n c e n t r a -
t i o n s m e a s u r e d a t t h e c a p i l l a r y t u b e i n t h e case w h e r e t h e r e is
no d i s p e r s i o n w i t h i n t h e s y s t e m .
           T h e r e e x i s t s a t i m e d e l a y b e t w e e n t h e moment a t r a c e r
gas f i r s t e n t e r s a p r o d u c t i o n w e l l and t h e t i m e i t i s d e t e c t e d
a t t h e c a p i l l a r y tube. If t h e t r a c e r gas uniformly e n t e r s t h e
p r o d u c t i o n w e l l t h i s t i m e p e r i o d i s u s u a l l y small (i.e., cO.5
h o u r f o r W e l l # 3 ) . However, i f t h e t r a c e r g a s were t o e n t e r
t h e production w e l l a t t h e t o p of t h e b r i n e l e v e l only, t h e
t i m e p e r i o d b e t w e e n i t s f i r s t arrLl/..al a n d i t s d e t e c t i o n c o u l d
be s i g n i f i c a n t . The a r r i v a l to d e t e c t i o n t i m e p e r i o d i s j u s t
t h a t t i m e r e q u i r e d for t h e i n c o m i n g flow to d i s p l a c e all t h e
g a s b e t w e e n t h e t o p of t h e b r i n e a n d t h e bottom o f t h e c a p i l l a r y
tube.        T h i s t i m e i s d e f i n e d by

                V
            t = -C

where

           vc
                    -        t h e v o l u m e ( s c f ) of g a s i n t h e w e l l b o r e b e t w e e n
                             t h e b r i n e and c a p i l l a r y a t t h e t i m e tracer is
                             first detected a t t h e capillary.

           W e l l # 3 , b e k a u s e of i t s l a r g e volume a n d r e l a t i v e l y h i g h
t e s t p r e s s u r e s , p r o v i d e s a good e x a m p l e f o r e x a m i n i n g t h e s e
e f f e c t s . The maximum p o s s i b l e t r a n s i t t i m e s r e q u i r e d f o r g a s
i n j e c t e d i n t o t h i s w e l l , a t t h e t o p of t h e b r i n e l e v e l , t o
reach t h e c a p i l l a r y tube are 5.5,               7 . 7 , 3 . 6 and 5 . 2 hours for t h e
a r r i v a l of t h e f i r s t S F 6 , C318, 13B1 a n d s e c o n d SF6 p u l s e s ,
respectively.            T h e s e t i m e s c a n n o t be c o n s i s t e n t l y i n t e r p r e t e d
i n terms o f t h e m e a s u r e d c r o s s - h o l e f l o w i n t e r v a l s .        I t was
t h e r e f o r e assumed t h e f l o w e n t e r e d t h e w e l l u n i f o r m l y a n d t h a t
measured t i m e i n t e r v a l s r e p r e s e n t t h e t i m e r e q u i r e d f o r t h e
tracer g a s t o f l o w from t h e i n j e c t i o n w e l l t o t h e p r o d u c t i o n w e 1


                                                 88
           When t h e p r o d u c t i o n w e l l is s h u t - i n ,   the pressure t i m e
h i s t o r y c a n be u s e d t o d e t e r m i n e e i t h e r t h e f l o w i n t o t h e w e l l ,
o u t o f t h e w e l l , or if t h e f l a w i s known, t h e a c t u a l w e l l v o l -
ume.     Assuming i s o t h e r m a l c o n d i t i o n s , t h e r e l a t i o n b e t w e e n t h e
w e l l in-flow or out-flow and t h e c o r r e s p o n d i n g p r e s s u r e change
is g i v e n i n E q u a t i o n ( D . 5 )
                   B
                   '     dP                                                                  (D.5 )
            w = p        dt
where P i s t h e w e l l p r e s s u r e

						
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