The Effects of Temperature and Pressure on … · THE EFFECTS OF TEMPERATURE AND PRESSURE ON...
Transcript of The Effects of Temperature and Pressure on … · THE EFFECTS OF TEMPERATURE AND PRESSURE ON...
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Stanford Geothermal Program I n t e r d i s c i p l i n a r y Research
i n Engineering and Ear th Sciences Stanford Univers i ty Stanford , C a l i f o r n i a
THE EFFECTS OF TEMPERATURE AND PRESSURE O N
ABSOLUTE PERMEABILITY OF SANDSTONES
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by Muhammadu Aruna
A p r i l 1 9 7 6
This r e s ea r ch was c a r r i e d out under Research Grant GI- 34925
by t h e National Science Foundation
ACKNOWLEDGEMENT -
T h e a u t h o r would l i k e t o express h i s s i n c e r e apprec i - I
a t i o n t o h i s a d v i s e r , D r . Henry J. Ramey, Jr., for h i s i n- I
s t r u c t i o n and guidance throughout t h e r e s e a r c h work.
made it p o s s i b l e f o r t h e a u t h o r t o come t o S tanfo rd U n i v e r s i l y
and complete h i s g radua te s t u d i e s s u c c e s s f u l l y .
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The a s s i s t a n c e and p r a c t i c a l sugges t ions from t h e
f a c u l t y of t h e Department of Petroleum Engineering, p a r t i c u -
l a r l y from Dr. W . E . Brigham and D r . S u l l i v a n S . Marsden, 1 are g r a t e f u l l y acknowledged. The coopera t ion I enjoyed from
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t h e department secretaries, e s p e c i a l l y from A l i c e Mansouria4, I w i l l n o t be f o r g o t t e n . I
Many thanks are due t o m y f r i e n d s , p a r t i c u l a r l y Rorio
A r i h a r a , H. K . Chen, and Paul Atkinson, f o r t h e i r h e l p f u l
comments and Timely h e l p through the days of exper imenta l w&k.
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C r e d i t f o r m d i f i c a t i o n of t h e a p p a r a t u s b u i l t by Wei4
braadt and Cass6 i s due Jon Grim, t h e Petroleum Engineering1
Dezs-tnent mach in i s t .
F i n a l l y , Dr. F. Ca.ss6 reviewed t h i s manuscript and ma& I
E?-- : ? s l p f u l sugg3st ions ' . ~
?>lis w s ~ k was fund.ed under Nat ional Science Foundatiovl
pm= _- ' 7 - . 3L . . - r - G I- 3 4 9 2 5 . I
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This r e p o r t was prepared o r i g i n a l l y as a
d i s s e r t a t i o n sub,mitted to t h e Department of
Petroleum Engineering and the Committee on the
Graduate D iv i s i on of S tanford Un ive r s i t y i n
p a r t i a l f u l f i l l m e n t o f the requirements f o r t he
degree of Doctor of Philosophy.
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ABSTUCT
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The s t a n d a r d procedurle f o r de t e rmin ing t h e p e r m e a b i l i t y
of porous media acco rd ing t:o API Code Mo. 2 7 i s based on t h e I
fundamental assumption that : , as long as v i s c o u s f l o w p r e v a i l s , I '
t h e a b s o l u t e p e r m e a b i l i t y of a porous medium i s a p r o p e r t y of
t h e medium, and i s independlent of t h e f l u i d used i n i t s deter-11
mina t ion , s l i p e f f ec t be ing t aken i n t o accoun t i n t h e case of
gas f l o w . Abso lu t e p e r m e a b i l i t y h a s , t h e r e f o r e , been t r a d i t i o d -
a l l y measured a t room c o n d i t i o n s , w i th t h e assumpt ion t h a t it I
changes o n l y w i t h overburden p r e s s u r e and n o t w i t h t e m p e r a t u r e +
R e s u l t s o b t a i n e d a t room tempera ture may t h e n be used t o p r e -
d i c t performance a t r e s e r v o i r c o n d i t i o n s a f te r c o r r e c t i o n f o r
r e d u c t i o n by stress e f fec t s .
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Although t h i s assumption i s t r u e for m o s t f l u i d s , re-
s u l t s of r e c e n t a b s o l u t e pe rmeab i l i t y measurements of water
f low through porous media a t h igh t empera tu re s and h i g h
overburden p r e s s u r e s d i f f e r from room c o n d i t i o n v a l u e s .
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N o t
only was t h e a b s o l u t e p e r m e a b i l i t y t o water a t h i g h c o n f i n i n g
p r e s s u r e lower t h a n t h a t to1 o t h e r f l u i d s used a t room tempera-
t u r e , b u t also, t h e r e was a s i g n i f i c a n t p e r m e a b i l i t y r e d u c t i o n ~l
a t e l e v a t e d t e m p e r a t u r e s .
An e x i s t i n g permeaneter w a s modified t o e n a b l e f l o w of I I d i f f e r e n t f l u i d s t h rough s e p a r a t e flow l i n e s .
water, a wh i t e m i n e r a l o i l , n i t r o p e n and 2- octanol were the
D i s t i l l e d
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f l u i d s used, and t es t s were c a r r i e d o u t on n a t u r a l conso l i-
d a t e d sands tones and unconso l ida ted s i l i c a sand.
With t h e excep t ion of w a t e r , t h e a b s o l u t e p e r m e a b i l i t i e s
of t h e cores t o o t h e r f l u i d s showed l i t t l e o r no t empera tu re
dependence.
t e m p e r a t u r e i n c r e a s e w a s a t t r i b u t e d t o i n t e r a c t i o n between
The r e d u c t i o n i n p e r m e a b i l i t y t o w a t e r wi th 1 1
water and s i l i ca .
systems o r i n thermal r ecove ry p r o c e s s e s which c a u s e l a r g e
changes i n format ion t empera tu re s , t h e effect of t e m p e r a t u r e s l
on absolute p e r m e a b i l i t y should be cons ide red i n e n g i n e e r i n g
c a l c u l a t i o n s . I
I n t h e case of water f l o w t h rough geothermd
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TASLE OF CONTENTS - Page
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ACKNOWLEDGEMENT . . . . . . . . . . . . . . . . . . . i v
ABSTRACT, . . . . . . . . . . . . . . . . . . . . . . . V
TABLE OF CONTENTS . . . . . . . . . . . . . . . . . . v i i
L I S T OF TABLES. . . . . . . . . . . . . . . . . . . . X
L I S T OF FIGURES . . . . . . . . . . . . . . . . . . . x i
CFAPTERS
1. INTRODUCTION. . . . . . . . . . . . . . . . 1
2. FLOW I N POROUS YEDIA. . . . . . . . . . . . 4
2 . 1 Darcy 's Law. . . . . . . . . . . . . . 4
2 . 2 Darcy's Law for Gas Flow . . . . . . . 5 '
2.3 S l i p Phenomena i n G a s F low . . . . . . 6 1 ;
2 . 4 Visco- Inert ial Flow. . . . . . . . . . 7
3.
4.
LITERATURE. . . . . . . . . . . . . . . . . 9
EXPERIMENTAL EQUIPMENT. . . . . . . . . . . 15 1
4 . 1 General D e s c r i p t i o n . . . . . . 1 5
4 . 2 C o r e Holder. . . . . . . . . . . . . . 1 8 ~
4 . 3 A i r B a t h and Temperature Control . . . 1 8 ' 4 . 4 Liquid and Gas Sources . . . . . . . . 20
4 . 5 Liq,uid Pumps . . . . . . . . . . . . . 2 1
4 . 6 Hydraulic Hand Puny. . . . . . . . . . 2 1
4 . 7 Heat Exchangers. . . . . . . . . . . . 21
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Table of Conten ts , con t inued
4.8 Backpressure Valve . . . . . 4.9 Flow Rate Measuring Devices.
4 .9- 1 Liquid F l o w
4.9- 2 Gas F l o w
4- 10 Pressure Recording Devices . PROCEDURE . . . . . . . . . . . . 5.
6 .
5.1
5.2
5 . 3
Core P r e p a r a t i o n . . . . . . 5 . 1 - 1 Conso l ida t ed Mass i l lon Sand-
s t o n e s
5.1- 2 Unconsol idated O t t a w a Sand
E s t a b l i s h i n g Run Cond i t i ons . . Measurements and C a l c u l a t i o n s .
5 . 3- 1 Liquid F l o w
5.3- 2 Gas Flow
ANALYSIS OF RESULTS AND DISCUSSION.
6 . 1
6 .2
6.3
6.4
6.5
Water Flow . . . . . . . . . . . 6 . 1- 1 Conso l ida t ed Sandstones
6.1- 2 Unconsol ida ted Sand
G a s Flow . . . . . . . . . . . 6 . 2- 1 Conso l ida t ed Sandstones
6.2- 2 Unconsol ida ted Sand
O i l Flow . . . . . . . . . 2-Octanol Flow . . . . . . Discuss ion . . . . . . . .
7 . C ONC LU S I O N S AND R.EC OIWENDAT I O N S
8 . REFERENCES. . . . . . . . . . .
.
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Table of C o n t e n t s , c o n t i n u e d Page
9. APPENDICES. . . . . . . 70
9 . 1 L i s t of T a b u l a t e d Data . - . . . . . 71
9 . 2 C o r e Data. . . . . . . . . . . 9 0
9 .3 D e r i v a t i o n s of E q u a t i o n s . . . . . 9 4
9 . 4 L i s t of Manufacturers . . . . . . . . 9 9
1 0 . NOMENCLATURE. ,, . . . . . . . . . 102
v i i i
Table
'LI'ST OF TABLES - I I
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D e n s i t y and V i s c o s i t y of Water vs .
V i s c o s i t y of Ni t rogen vs. Temperature . . . 73
1 Temperature . . . . . . . . . . . . . . . . . 72
! I V i s c o s i t y of Chevron . O i l No. 3 vs. Temperature . . . . . . . . . . . . . . . . . 7 4
. . . . D e n s i t y of 2-Octanol vs. Temperature. 75 I
V i s c o s i t y of 2-Octanol v s . Temperature. . . . 7 6 ,
F l o w D a t a f o r Mass i l lon Sandstone Core N o . Water Flow. 77
F low D a t a for Mass i l lon Sandstone Core N o . Water Flow. 78
Flow D a t a for Mass i l lon Sandstone Core No. Water Flow. 80
Flow Data for Mass i l lon Sandstone Core N o .
2, . . . . . . . . . . . . . . . . . 1 1 3 , . . . . . . . . . . . . . . . . . 1 4, . . . . . . . . . . . . . . . . . i I 5,
N i t r o g e n Flow . . . . . . . . . . . . . . . . 8 1 I
F l ow D a t a for Mass i l lon Sandstone Core N o . 6 , N i t rogen Flow . . . . . . . . . . . . . . . . 8 2
Flow Data for P?assi l lon Sandstone Core N o . 1 0 , O i l Flow. . . . . . . . . . . . . . . . . 8 4
Flow Data for Mass i l lon Sandstone Core N o . I 11, O i l Flow. . . . . . . . . . . . . . . . . 85 I
Flow Data f o r Unconsol idated O t t a w a S i l i c a I Sand Core N o . 1 4 , Water Flow. . . . . . . . . 86
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Flow Data f o r Unconsol idated O t t a w a S i l i c a Sand Core No. 1 5 , Water Flow. . . . . . . . . 87
F low Data for Unconsolidated O t t a w a S i l i c a Sand Core N o . 1 6 , Nitrogen Flow and Water F l o w . . . . . . . . . . . . . . . . . . . . . 88
Flow Data for Unconsolidated O t t a w a S i l i ca Sand Core No. 1 7 , 2-Octanol Flow. 89
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LIST OF FIGUP,ZS -
F i g u r e Page -
1 Photograph of Apparatus . . . . . . . . . . . 16
2 Details of Assembly i n t h e A i r Bath . . . . . 16
3 Schematic Diagra.m of Apparatus . . . . . . . . 1 7
4 Schematic Diagram of t h e Core Holder . . . . . 19
5 Dens i ty of Water1 vs . Temperature of 2 0 0 p s i g 31
6 Water V i s c o s i t y vs . Temperature a t 2 0 0 p s i g . 3 2
7 Dens i ty vs . Temperature for Chevron White Oil No. 3 a t 14.7 p s i . . . . . . . . . . . 33
8 V i s c o s i t y v s . Temperature for Chevron White O i l N o . 3 . . . . . . . . . . . . . . . . . 34
9 Dens i ty of 2-Octanol vs . Temperature a t 1 4 . 7 p s i . . . . . . . . . . . . . . . . . . . . . 35
1 0 V i s c o s i t y of 2-Octanol vs . Temperature. . . . 36 ~
11 V i s c o s i t y of Ni t rogen vs . Temperature . . . 39
1 2 Water P e r m e a b i l i t y vs. Temperature , Mass i l lon Sandstone Core No. 2 . . . . . . . . . . . . 42
13 Water Pe rmeab i l i t y v s . Temperature , Mass i l lon Sandstone Core No. 3 . . . . . . . . . . . . 44
1 4 Water Pe rmeab i l i t y v s . Temperature a t a Cons tan t Conf in ing P r e s s u r e of 3000 p s i g , Mass i l lon Sandstone Core No. 3 . . . . . . . . 45
1 5 Water Pe rmeab i l i t y vs. Temperature , Mass i l lon Sandstone Core No. 4 . . . . . . . . . . . . . 4 6
1 6 Water Pe rmeab i l i t y v s . Temperature , Unconsoli- d a t e d O t t a w a S i l i c a Sand Core N o . 1 4 . . . . . 47
1 7 Water Perrr-eahil i ty vs . Temperature , O t t a w a S i l i c a Sand Core No. 1 5 . . . . . . . . . . 4 9
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F i g u r e
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L i s t df €Figures, c o n t i n u e d
Apparent P e r m e a b i l i t y vs . X e c i p r o c a l Mean P r e s s u r e a t S e v e r a l Tempera tures for M a s s i l l o n Core No. 5. . . . . . . . . . . Modif ied V i s c o- I n e r t i a l Graph, M a s s i l l o n C o r e N o . 5 w i t h Ni t rogen Flow . . . . . . . .
Page
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Apparen t P e r m e a b i l i t y vs. I i e c i p r o c a l Mean P r e s s u r e a t S e v e r a l Temperatures for M a s s i l l o n S a n d s t o n e Core N o . 6 , Conf in ing P r e s s u r e = 1 0 0 0 p s i g . . . . . . . . . . . . . . . . . . 53
Apparen t P e r m e a b i l i t y v s . R e c i p r o c a l Mean P r e s s u r e a t S e v e r a l Temperatures for Mas- s i l l o n Sands tone Core 110. 6 , C o n f i n i n g Pres- s u r e . 3000 p s i g . . . . . . . . . . . . . . . . 5 4
Apparen t P e r m e a b i l i t y vs. R e c i p r o c a l Mean P r e s s u r e a t S e v e r a l Temperatures for M a s s i l l o n S a n d s t o n e Core No. 6 , Conf in ing P r e s s u r e = 4 0 0 0 p s i g . . . . . . . . . . . . . . . . . . 5 5
Apparen t P e r m e a b i l i t y vs . R e c i p r o c a l Mean P r e s s u r e a t S e v e r a l Temperatures for O t t a w a S i l i c a Sand Core No. 1 6 , Conf in ing P r e s s u r e = 2000 p s i g . . . . . . . . . . . . . . . . . . 57
O i l P e r a e a b i l i t y 'vs . TeEpera ture for M a s s i l l o n Core So. 10 . . . . . . . . . . . . . . . . . 59
O i l P s r n e a b i l i t y vs. Temperature for M a s s i l l o n CcFe KO. 11 . . . . . . . . . . . . . . . . . 60
2 - O c ~ z n o l P e r m e a b i l i t y vs. Tempera ture f o r Uncc r - so i ida t ed O t t a w a S i l i c a Sand Core N o . 1 7 6 1
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1,. L?VIiODUCTION
A l o n g he ld conc lus ion t h a t t h e a b s o l u t e p e r m e a b i l i t y
of a porous medium i s a c o n s t a n t de t e rmined only by t h e
s t r u c t u r e of t h e medium i n q u e s t i o n i s t he s u b j e c t of t h i s
s t u d y .
m e a b i l i t y of porous media have shown t h a t t h e a b s o l u t e , ~
p e r m e a b i l i t y t o water f o r c e r t a i n s a n d s t o n e c o r e s v a r i e s w i t +
t h e l e v e l of con f in ing p r e s s u r e as w e l l as w i t h tempera ture .
For w a t e r f low, pe rmeab i l i t y r e d u c t i o n s of up t o 6 0 % were
observed when t empera tu re was i n c r e a s e d from 7OoF t o 30OoF.
This important d i s c o v e r y m y have s i g n i f i c a n t r a m i f i -
Experiments des igned t o measure t h e a b s o l u t e per-
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1 c a t i o n s i n many o i l r ecove ry by thermal p roces ses .
j e c t i o n of h o t water and steam i n t o o i l r e s e r v o i r s , under-
ground combustion, i n j e c t i o n of f l u i d s i n t o w e l l s , t h e pro-
d u c t i o n of geothermal energy , and t h e d i s p o s a l o f atomic
The i n- 1
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waste p r o d u c t s i n porous fo rma t ions a l l c a u s e changes
f o r m a t i o n t empera tu re s .
I n r e s e r v o i r e n g i n e e r i n g , a b s o l u t e pe rmeab i l i t y
b a s i c parameter which h a s o f t e n been measured a t room
i n I
i s a
con- ~1
d i t i o n s , w i t h t h e i m p l i c i t assumption t h a t on ly c o n f i n i n g
p r e s s u r e affected t h e r e s u l t .
known r e a c t i o n s between water and c l a y s . 1
f o r e , a s i n g l e va lue of a b s o l u t e p e r m e a b i l i t y throughout a
r a n g e of r e s e r v o i r t empera tu re s has been used in r e s e r v o i r
e n g i n e e r i n g c a l c u l a t i o n s .
t (Of c o u r s e w e i gno re t h e w e 1 4
H i t h e r t o , t h e r e-
Weinbrandtl ' found foir water f l o w , t h a t t h e a b s o l u t e
pe rmeab i l i t y of c o n f i n e d , f i r e d sands tone cores w a s s t r o n g l y
temperature dependent . Casse v e r i f i e d t h e Weinbrandt r e s u l t .
I n r a i s i n g t h e t empera tu re l e v e l of a f i r e d c o n s o l i d a t e d
sandstone core under a c o n f i n i n g p r e s s u r e of 2 0 0 0 p s i from
room tempera ture t o 3OO0F, h e observed a r e d u c t i o n i n a b s o l u t e
pe rmeab i l i t y of as much as 65%. With mine ra l o i l flow, or
i n e r t gas f low, he found t h a t t empera tu re had no a p p r e c i a b l e
e f f e c t on a b s o l u t e permeabilt i t y .
t h a t i n h i s w a t e r f low exper iments th rough s y n t h e t i c cement-
conso l ida t ed sand cores, he d i d n o t observe t empera tu re
effects on a b s o l u t e p e r m e a b i l i t y .
con f in ing p r e s s u r e s .
2
Recent ly , Ar iha ra2 r e p o r t e d
However, h e a p p l i e d l o w
C a s s g l sugges t ed t h a t c lay- water i n t e r a c t i o n caused t he
pe rmeab i l i t y r e d u c t i o n he observed. However, Greenberg, e t al.
i n 1 9 6 8 r e p o r t e d d a t a on t he p e r m e a b i l i t i e s t o water o f core
samples a r t i f i c i a l l y c o n s o l i d a t e d w i t h pheno l i c r e s i n o r by
s i n t e r i n g . The g e n e r a l t r e n d showed s l i g h t t o moderate de-
creases i n p e r m e a b i l i t y w i t h i n c r e a s i n g tempera ture .
f i n i n g p r e s s u r e w a s a p p l i e d to the core.
observed changes t o m i c r o - s t r u c t u r a l re- arrangements i n t h e
m a t r i x geometry of t h e sampl-es which had a rough and i r r e g u l a r
s u r f a c e . They observed no changes i n p e r m e a b i l i t i e s f o r
N o con-
They a t t r i b u t e d the
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samples wi th r e l a t i v e l y smooth s u r f a c e s .
The purpose of t h i s work w a s (1) t o v e r i f y t h e r e s u l t s
of p rev ious s t u d i e s , ( 2 ) t o ex tend t h e p rev ious work t o o t h e r
i systems, and ( 3 ) t o i n v e s t i g a t e t h e r ea son fo r t empera tu re
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effects on a b s o l u t e pe rmeab i l i ty .
c l u e as t o what a c t u a l l y caused t h e p e r m e a b i l i t y t o d e c r e a s e
w i t h i n c r e a s i n g t e m p e r a t u r e , it was dec ided t o u s e c l a y- f r e e
rocks and o t h e r p o l a r l . iqu ids , such as 2- octanol .
I n o r d e r t o p r o v i d e a
2. FLOW IN POROUS WDIA
7 I n 1856 , as a r e s u l t of expe r imen ta l s t u d i e s on t h e f l o
of water through unconso l ida t ed sand f i l t e r beds , Henry Darcy k
formulated a flow l a w which now b e a r s h i s name. T h i s l a w hag
been extended t o d e s c r i b e ,
of o t h e r f l u i d s , i n c l u d i n g
conso l ida t ed r o c k s and 0 t h
2 . 1 Darcy's' L a w
w i th some l i m i t a t i o n s , t h e movemeqt
t w o or more immiscible f l u i d s , i n
r porous media.
Darcy's law, f o r t h e h o r i z o n t a l , v i s cous f l o w o f a f l u i d
i n a l i n e a r medium, s ta tes t h a t t h e flow v e l o c i t y of a homo-
geneous f l u i d i s p r o p o r t i o n a l t o t h e p r e s s u r e g r a d i e n t , and
i n v e r s e l y p r o p o r t i o n a l t o t h e f l u i d v i s c o s i t y , or:
(2-
where v i s t h e v e l o c i t y i : n cm/sec, a_ i s t h e f l o w ra te i n cc/
sec, p i s t h e f l u i d v i s c o s i t y i n c p , dp /ds i s t h e p r e s s u r e
g r a d i e n t i n a t m / c m , t a k e n i n t h e f i r e c t i o n of f l o w , and k
i s t h e rock p e r m e a b i l i t y , d a r c i e s .
m e a b i l i t y i s one i n which a f l u i d of one c e n t i p o i s e v i s c o s i t j
w i l l move a t a v e l o c i t y of one c e n t i m e t e r p e r second under a
p r e s s u r e g r a d i e n t of one a tmosphere p e r cen t ime te r .
A rock of one darcy pe r-
Darcy's l a w a p p l i e s o n l y i n t h e r e g i o n of l aminar f l o w .
For " t u r b u l e n t " or non-laminar f lows which occu r a t h i g h e r
v e l o c i t i e s , t h e p r e s s u r e g r a d i e n t i n c r e a s e s a t a g r e a t e r r a t e
t h a n does t h e flow r a t e .
- 4 -
A c o r r e l a t i o n produced by Fancher , L e w i s , and Barnes 5
may be used t o e s t i v a t e t h e r e p i o n of v i s c o u s flow f o r a
porous medium.
media when a modi f ied Reynolds' number
I n g e n e r a l , 9 a r c y ' s l a w is v a l i d f o r porous
vd P R e = - IJ
i s less t h a n one.
t h e f l u i d v i s c o s i t y , and d i s t h e d i ame te r of the ave rage
g r a i n s ize .
v i s v e l o c i t y , p is f l u i d d e n s i t y , 1.1 i s
A r e c e n t s t u d y by Geertsma' showed t h a t t h e ave rage
g r a i n s i z e s h o u l d be r ep l aced by a 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 t o p r o v i d e a b e t t e r c o r r e l a t i o n .
The r equ i r emen t t h a t t h e p e r m e a b i l i t y be determined
for c o n d i t i o n s of v i scous flow i s b e s t s a t i s f i e d 7 by o b t a i n i h g
d a t a a t s e v e r a l flow rat:es and g raph ine f l o w ra te v e r s u s prtels-
s u r e drop fo r l i q u i d and f o r gas by p l o t t i n g the p roduc t of ~
* where p1 , mean f l o w r a t e and pore p r e s s u r e v e r s u s p1 2 - p2 i s t h e upst ream p r e s s u r e and p2 i s the downstream p r e s s u r e .
For c o n d i t i o n s of v i scous flow, t h e d a t a shou ld p l o t a s t r a i g h t
l i n e , p a s s i n g th rough t h e o r i g i n . Turbulence i s i n d i c a t e d I
by c u r v a t u r e of t h e p l o t t e d p o i n t s .
2 . 2 Darcy 's Law f o r G a s Flow
I n t h e case of f low of gases , t h e f l o w ra te i s no t
c o n s t a n t , b u t i n c r e a s e s w i t h t h e p r e s s u r e d rop , a c c o r d i n g t o I
Boyle 's l a w . T h e i n t e g r a t e d form of Darcy 's l a w which des- I
c r i b e s h o r i z o n t a l l inear . pas flow, under s t e a d y s t a t e , i s o -
thermal c o n d i t i o n s i s : i
- 5-
( 2 - 3 )
2 . 3 S l i p Phenomena i n G a s Flow
Kundt and Warburg* f i i ~ s t showed t h a t a l a y e r of gas
nex t t o a s o l i d s u r f a c e m!y have a f i n i t e v e l o c i t y w i t h
r e s p e c t t o t h e w a l l .
g ive a g r e a t e r ra te t h a n would be computed from P o i s e u i l l e ' s
l a w .
w a l l . T h i s " s l i p "
phenomena i s dependent upon t h e mean free p a t h of t h e gas
molecules ; t h e r e f o r e , gas pe rmeab i l i t y should b e a f u n c t i o n
of t h e factors c o n t r o l l i n g t h e mean f ree p a t h . These factors
are p r e s s u r e , t e m p e r a t u r e , and t h e n a t u r e of t h e gas i t s e l f .
When t h e mean f r e e p a t h s ar*e small, e.g. , a t h i g h p r e s s u r e s ,
t h e p e r m e a b i l i t y t o gas should be expected t o approach t ha t
I n case o f c a p i l l a r y f l o w , t h i s would
I n ef fec t , t h e g a s stream l l s l i p s " w i t h r e s p e c t t o t h e
Th i s i s n o t t h e case fo r l i q u i d f l o w .
t o l i q u i d s . T h i s i d e a w a s supported by t h e Klinkenburg 9
s tudy .
Based upon a t h e o r e t i c a l a n a l y s i s of t h e s l i p phenomenon
i n c i r c u l a r c a p i l l a r i e s , arid assuming a n ana logous b e h a v i o r
i n a porous medium, Klinkenberg' developed the r e l a t i o n s h i p
between t h e p e r m e a b i l i t y of a porous medium t o g a s and t o a
n o n r e a c t i v e l i q u i d as follows:
(2-411
I I.
2
J
J
J
J
4
J
J
J
..J
.J
where ka i s t h e apparent: o r observed p e r m e a b i l i t y t o g a s , k
i s t h e a b s o l u t e pe rmeab i l i t y t o gas a t h i g h p r e s s u r e s (p re-
sumed e q u a l t o t h e a b s o l u t e p e r m e a b i l i t y t o a s i n g l e l i q u i d
phase) , X i s the mean fr5ee p a t h of t h e g a s m l e c u l e s , r is -
t h e r a d i u s of a capi l lax-y (assumed t o be c o n s t a n t ) , and c
i s a p r o p o r t i o n a l i t y f a c t o r . The mean f r ee p a t h can be
expressed as:
where d i s a c o l l i s i o n diameter, n i s t h e c o n c e n t r a t i o n of
molecu les p e r u n i t volume, N i s Avogadro's N u m b e r , p, i s the
mean p r e s s u r e , T i s a b s o l u t e t empera tu re , and R i s t h e un i - ~
v e r s a 1 gas c o n s t a n t . F ~ o m Ea_. 2- 5, Eq. 2-4 becomes:
b k = k(l+- 4c'T ) = k(l+-) 2 m r N d pm
a Pm
c.
where b is r e f e r r e d t o as t h e Kl inkenberg factor , and is
u s u a l l y t a k e n as a c o n s t a n t f o r a g iven gas and a given
c porous medium. From Eq . 2- 6, t h e Kl inkenberg factor appear\$
d i r e c t l y p r o p o r t i o n a l t o t empera ture .
2 . 4 V i s c o- I n e r t i a l Flow - Darcy ' s l a w and t h e preced inp e q u a t i o n s are v a l i d when
c o n d i t i o n s of v i scous f low p r e v a i l . A t h i g h flow rates, f L b w
has been shown t o be desc r ibed by a q u a d r a t i c equa t ion . Su
an e q u a t i o n was proposed by Forchheimer'' and modif ied by
C o r n e l l and K a t z l l as fo l lows :
-7-
Dranchuk and Kolada12 have shown how t o d e l i n e a t e t h e visco-
i n e r t i a l f low r e g i o n from flow measurements, and how t o
determine t h e a b s o l u t e p e r m e a b i l i t y of a r o c k c o r e (see
Appendix 9 . 3 ) .
The v i s c o - i n e r t i a l f l o w d e s c r i b e d by Eq . 2-7 is some-
The d e p a r t u r e from t imes r e f e r r e d t o as "tur lbulent" flow.
laminar f low d e s c r i b e d by Eq. 2-7 i s n o t caused by physical
f a c t o r s which (cause t u r b u l e n t flow i n p i p e . T h i s phenomenon I
i s u s u a l l y r e f e r r e d t o as "non-Darcy," " i n e r t i a l , " or "visco-r
i n e r t i a l " f low. We s h a l l use t h e l a t t e r term. I
I
J
J
J
J
J
J
Y
-8-
I
.J
..
3. LITE-WTURE
I n 1 9 3 7 , Muskat4 s t a t e d t h a t t h e a b s o l u t e p e r m e a b i l i t y
of a porous medium "is t h u s a c o n s t a n t determined o n l y by
t h e s t r u c t u r e of t h e medium i n q u e s t i o n and i s e n t i r e l y i n d e t
pendent of t h e n a t u r e o f t h e f l u i d . " Also , t h e s t a n d a r d p r a t
cedure f o r de te rmin ing t h e p e r m e a b i l i t y of porous medium
according t o API Code No. 2 7 1 5 ( f i r s t e d i t i o n , October 1935)
w a s based on t h e fundamental assumption t h a t as long as t h e
ra te of flow w a s p r o p o r t i o n a l t o t h e p r e s s u r e g r a d i e n t , t h e I
p e r m e a b i l i t y c o n s t a n t of a porous medium w a s a p r o p e r t y of
t h e medium and w a s independent o f t h e f l u i d used i n i t s detdLmi-
n a t i o n .
~
... A major s t u d y by Klinkenberg appeared i n 1 9 4 1 . Klinkefi-
9 b e r g performed l i q u i d p e r m e a b i l i t y measurements on J e n a
f i l t e r s i n o r d e r t o a v o i d c l a y s w e l l i n g o r e r o s i o n . The
were not conf ined n o r w e r e v a r i a t i o n s i n t e m p e r a t u r e studiedl.
From h i s a n a l y s i s o f gas, f low through t h e same c o r e s , he t h e p e -
f o r e suppor ted t h e n o t i o n t h a t t h e p e r m e a b i l i t y c o n s t a n t of
a porous medium w a s a p r o p e r t y of t h e medium, and w a s indepen-
d e n t of t h e f l u i d used. I n a d d i t i o n , he w a s t h e f i r s t pe r sdn ~
t o e x p l a i n s l i p phenomena.
I n 1 9 4 3 , Grunberg and Nissan13 s t u d i e d t h e e f f e c t of
f low of aqueous s o l u t i o n s th rough l imes tone and sands tone
c o r e s ove r a r a n g e of t e m p e r a t u r e s . Four s o l u t i o n s w e r e t e s t e d :
-9-
(1) d i s t i l l e d water, (2) a 2 % n-amyl a l c o h o l s o l u t i o n , and
( 3 ) two sodium c h l o r i d e s o l u t i o n s ( 0 . 9 6 0 and 0.614N).
cho ice of t h e s e s o l u t i o n s was made so as t o obse rve t h e i n-
f l u e n c e o f s u r f a c e forces on t h e f l o w of l i q u i d s t h rough
porous media.
The
The core tempera tures were v a r i e d from 6OC I
t o 3OoC. 1
Pe rmeab i 1. it y d ecr e a:; e d w i t h i n c re as i ng temper a t u r e f o r 1 1
a l l of t h e four, aqueous s o l u t i o n s .
p e r m e a b i l i t y t e m p e r a t u r e curves wi th approximate ly t h e same
s l o p e . The slope of t h e graphs o f p e r m e a b i l i t y v s . tempera-
t u r e w a s 0 .8 mcV0C. Thus:
A l l f o u r gave l i n e a r
1
k = if - 0.8(t,OC) ( 3-1
I
As ~
where a i s a characteristic c o n s t a n t o f t he l i q u i d used.
t h e f l u i d v i s c o s i t y w a s cons idered p r o p e r l y i n c a l c u l a t i n g I
p e r m e a b i l i t y , t:hey concluded t h a t v i s c o s i t y w a s n o t t h e on ly 1 p r o p e r t y i n f l u e n c i n g f low.
2 I
I n a d d i t i o n , a log- log graph of
k/k , vs.(-) lJ gave a s t r a i g h t l i n e . kl i s a base p e r m e a b i l i t y ; 1 Pa
1.1 i s f l u i d v i s c o s i t y , p i s f l u i d d e n s i t y , and Q i s s u r f a c e
t e n s i o n .
1
A c o n c l u s i o n reached w a s t h a t the e f f e c t i v e c r o s s- s e c t i t
under v i s c o u s flow was d i f f e r e n t f o r d i f f e r e n t l i q u i d s due t i d i f f e r e n c e s i n s u r f a c e energy, and t h u s d i f f e r e n c e s i n t h e
t h i c k n e s s of adsorbed l a y e r s .
I n 1 9 4 6 , Calhoun and Yus te r " p r e s e n t e d r e s u l t s of flow
through a r t i f i c i a l porous bod ie s , some made of p y r e x g l a s s
and o t h e r s of f'used q u a r t z . I No c o n f i n i n g p r e s s u r e was a p p l i e
-10-
c.
L
They d i s a g r e e d w i t h Grunberg's and Ni s san ' s r e s u l t s and con-
firmed Kl inkenbe rg ' s r e s u l t s .
Calhoun and Yuster found that water gave a s l i g h t l y
lower va lue for pe rmeab i l i t y t h a n benzene. A s u s p i c i o n of
a n e l e c t r o - k i n e t i c e f fec t w a s r u l e d o u t because a d d i t i o n of
a t race of H C 1 or C a C 1 2 t o t h e water caused no appa ren t i n-
crease i n p e r m e a b i l i t y .
b i l i t y as low as t h a t of water, and, w i t h this hydrocarbon
l i q u i d a n e l e c t r o - k i n e t i c e f fec t should have been a b s e n t .
Calhoun and Y u s t e r were unable t o g i v e an e x p l a n a t i o n of
t h i s anomaly. They were t h e f i r s t t o obse rve a dependency od Kl inkenberg ' s fac tor , b on t empera tu re . 1
Furthermore, naphtha gave a permea-
I n t r y i n g t o correlate Klinkenberg b v a l u e s a t d i f f e r e n t
t e m p e r a t u r e s , Calhoun and Yus te r assumed t h a t e q u a l mean fred
c.
c. I
p a t h s would o c c u r a t equ iva l en t molecu la r c o n c e n t r a t i o n s a t ,
d i f f e r e n t t e m p e r a t u r e s , A gas a t p r e s s u r e p1 and T1 should ~
.
.
c
have t h e same molecu la r c o n c e n t r a t i o n as t h e same g a s a t a P:1 p2 I p r e s s u r e pz and T2, i f ~1 were e q u a l t o T. Therefore, e q u i j
2 v a l e n t p e r m e a b i l i t y v a l u e s should e x i s t f o r the same g a s , whcin
two d i f f e r e n t t empera tu re s were used, a t a mean p r e s s u r e p,
and t e m p e r a t u r e T1, and a t mean p r e s s u r e p (-1 a t a temperad
t u r e of Tz. T h i s c o r r e L a t i o n a t d i f f e r e n t t e m p e r a t u r e s w a s ' n o t i nc luded i n e i t h e r Kl inkenberg ' s or Grunberg and Nissan'B
T1 T2
p r e s e n t a t i o n . 18
I n t h e l a t e 1960s, Greenberg, e t a1.,3 and Weinbrandt
a g a i n observed a p e r m e a b i l i t y dependency on t empera tu re levea .
Greenberg, e t a l . , d i d not r e s t r a i n t h e i r cores and observed i I
-11-
16 o n l y small t empera ture e f fec ts . Weinbrandt , i n h i s e x p e r i-
ments on t h e e f fec t of t empera tu re on r e l a t i v e and a b s o l u t e
p e r m e a b i l i t y of sands tones , s u b j e c t e d h i s cores t o 2000 p s i
c o n f i n i n g p r e s s u r e . H e a l so f i r ed t h e cores a t 94OoF p r i o r
t o use t o o x i d i z e o r g a n i c matter i n t h e cores and t o d e a c t i - ' I
v a t e t h e c l a y s . H i s exper iments f o r Boise sands tone core
samples a t room t empera tu re and a t 175OF showed t h a t w i t h a n
i n c r e a s e i n t empera ture : (1) t h e i r r e d u c i b l e water saturatiofa
i n c r e a s e d ; ( 2 ) t h e r e s i d u a l o i l s a t u r a t i o n decreased ; ( 3 )
t h e r e l a t i v e p e r m e a b i l i t y t o w a t e r a t f lood- out i n c r e a s e d ; (
t h e r e l a t i v e perrneabi1it:y t o o i l i n c r e a s e d ; ( 5 ) t h e r e l a t i v e
p e r m e a b i l i t y iqatio, kw/ko, d e c r e a s e d ; and ( 6 ) t h e a b s o l u t e
p e r m e a b i l i t y to water dec reased . Casse v e r i f i e d the Wein-
b r a n d t f i n d i n g s and s u b s t a n t i a l l y extended t h e work.
.1 I
The ef fec t of mechanical stresses on t h e p e r m e a b i l i t y
of r o c k s has heen s t u d i e d by s e v e r a l i n v e s t i g a t o r s . I n 196711 I I
Wilhelmi and Somerton17 i n v e s t i g a t e d t h e e f f e c t of overburdefl 1
p r e s s u r e on rock p e r m e a b i l i t y .
by F a t t and Davis 1 8 i n 1!352, and r e p o r t e d t h a t p e r m e a b i l i t y ' They confirmed ea r l i e r work
a t 1 5 , 0 0 0 p s i c o n f i n i n g p r e s s u r e cou ld be 2 5 t o 6 0 % smaller
t h a n t h e p e r m e a b i l i t y a t a z e r o c o n f i n i n g p r e s s u r e , dependin PP I t
on t h e t y p e of rocks s t u d i e d . G e n e r a l l y speaking, t h e h i g h e l
t h e p e r m e a b i l i t y , t h e h i g h e r t h e pe rcen tage o f r e d u c t i o n .
About 6 0 % of t h e t o t a l r e d u c t i o n occu r red du r ing t h e f i r s t ~
3000 p s i c o n f i n i n g p r e s s u r e .
In 1963!, G r a y , --- e t a1 ,
I
I a l so measured t h e e f f e c t of 19
overburden p r e s s u r e on p e r m e a b i l i t y . P e r n e a b i l i t y r e d u c t i o n
was shown t o be a f u n c t i o n of t h e r a t i o of r a d i a l t o a x i a l
- 12-
J
J
J
J
J
J
J
J
J
J
J
stress, wi th t h e maximum r e d u c t i o n o c c u r r i n g under a uniform
stress, i . e . , when t h e a x i a l stress is e q u a l t o t he r a d i a l
stress.
c o n d i t i o n s of uniform s t ~ e s s .
The p r e s e n t work r e p o r t e d h e r e w a s accompanied undeth
Zoback and Bye r l ee (1975aI2' showed t h a t due t o t h e
presence of compres s ib l e matr ix material i n a r e l a t i v e l y
incompress ib le g r a n u l a r framework, t h e p e r m e a b i l i t y o f sand-
s t o n e i s n o t s imply a f u n c t i o n of e f f e c t i v e stress, b u t i s
h i g h l y s e n s i t i v e t o changes i n po re p r e s s u r e .
~
The ef fec t of t h e r m a l stresses on r o c k p r o p e r t i e s and
t h e effect of overburden p r e s s u r e on p o r o s i t y have a l s o been
of p a r t i c u l a r i n t e r e s t .
Somerton, e t al . ,* 'L h e a t e d a number of s a n d s t o n e s t o
about 150OOF under b o t h a tmospher ic and s i m u l a t e d r e s e r v o i r
p r e s s u r e s . P e r m e a b i l i t y w a s measured a t room tempera tu re
u s ing a s t a n d a r d a i r perimeameter, b e f o r e and a f te r h e a t i n g I
t h e samples. No p e r m e a b i l i t y changes were r e p o r t e d i n t he
range of 75-350°F. A t t empera tu re s w e l l above 5OO0F, t h e y
showed that permanent s t i r u c t u r a l damage and decompos i t ion ofi 1
rock minerals o c c u r r e d due t o thermal stresses.
Wyble22, working om t h e effect o f a p p l i e d p r e s s u r e on
sands tone ' s p r o p e r t i e s , observed asympto t ic d e c r e a s e s i n con-
d u c t i v i t y , p o r o s i t y , and p e r m e a b i l i t y o v e r a 0 p s i t o 3,500
p s i range . A t 2 0 0 0 p s i c o n f i n i n g p r e s s u r e , about a 1 0 % reduc-
t i o n i n p o r o s i t y w a s obslerved, and beyond t h i s , t he p o r o s i t y
va lue remained e s s e n t i a l l y c o n s t a n t .
-13-
I n summry , many s t u d i e s i n d i c a t e t h e l i k e l i h o o d of
a b s o l u t e p e r m e a b i l i t y of r o c k s be ing a f u n c t i o n of tenpera-
t u r e beyond the ef fec ts caused by a change i n the v i s c o s i t y
of the f l u i d .
i n d i c a t e d an effect o f major importance for r e s t r a i n e d c o r e s 4
I
The r e c e n t works of Weinbrandt’‘ and Cass6 1 1
N o obvious e x p l a n a t i o n e x i s t e d .
s t u d y w a s a v e r i f i c a t i o n of and s t u d y of poss ib le e x p l a n a t i o o s
of these effects . 1
The main purpose of t h i s I
I
-14-
i
I.
c.
4. EXPERIMENTAL EQUIPMENT
The e x p e r i m e n t a l eciuipment used w a s s i m i l a r t o t h a t .. -
desc r ibed p r e v i o u s l y by Cass6’ and Weinbrandt 1 6 . f i c a t i o n s were made i n t h e appara tus , however.
of t h e a p p a r a t u s f o l l o w s .
4 . 1 Genera l D e s c r i p t i o h
Some modi- 1
A d e s c r i p t i o n
I
Fig . 1 i s a photogriaph of t h e l a b o r a t o r y , and F i g .
2 p r e s e n t s t h e d e t a i l s of t h e a i r ba th assembly. A schemat ic
diagram o f t h e a p p a r a t u s i s shown i n Fig. 3 . T h e flow l i n e s ,
h e a t exchangers , and f i t t i n g s were c o n s t r u c t e d o f 316 s t a i n l e
s tee l material.
Three p a r a l l e l flow l i n e s were c o n s t r u c t e d for- gas ,
6S
o i l , water, or 2- oc tano l i n j e c t i o n . For each exper iment , the1
d e s i r e d f l o w l i n e w a s connected t o t h e c o r e ; a new c o r e be ing
used f o r each exper iment . Liquid flow w a s s u p p l i e d by a pul-
s a t i n g pump, and gas f l o w w a s supp l i ed from h i g h p r e s s u r e
c y l i n d e r s and d e l i v e r e d t‘hrough p r e c i s i o n p r e s s u r e r e g u l a t o r s .
Liquid f low r a t e th:rough t h e c o r e w a s measured by
a weighing b a l a n c e .
gas flow r a t e w a s measured e i t h e r by t h e use of a bubble f i l m 1
flowmeter o r by a Wet T e s t Meter.
a t t h e i n l e t f a c e of t h e c o r e , and t empera tu re w a s r eco rded
con t inuous ly d u r i n g t h e r u n s . The core h o l d e r assembly was
p laced i n an air b a t h t h a t maintained r u n t e m p e r a t u r e . Mea-
surements of u p s t r e a m p r e s s u r e and p r e s s u r e drop across t h e
Depe:nding upon t h e l e v e l of f low ra te ,
A thermocouple w a s p laced
-15-
I I I
c o r e were accomplished by the use of p r e s s u r e t r a n s d u c e r s
connected t o p r e s s u r e i n d i c a t o r s and r e c o r d e r s .
The d e s i r e d c o n f i n i n g p r e s s u r e l e v e l was a t t a i n e d
by us ing a h y d r a u l i c hand pump. Chevron No. 15 heavy O i l
was used as a c o n f i n i n g f l u i d and a "Viton A" r u b b e r s l e e v e ,
l / S " t h i c k , s e p a r a t e d t h i s f l u i d from t h e core. I
A d e s c r i p t i o n of the major components of t h e a p p a r a t u s
follows.
4 .2 Core H o l d e r - - -_
Fig . 4 s 'hows the d e t a i l s of t h e c o r e h o l d e r which
i s a Hassler r u b b e r sleeve t y p e . The r o c k specimen t o be
s t u d i e d i s h e l d i n a "Viton A" rubbe r s l e e v e , 1/8" t h i ck ,
between an ups t ream p l u g , which i s immobile, and a downstrean
p lug which moves h o r i z o n t a l l y and a d j u s t s t o t h e core l e n g t h .
The upstream p2ug h a s two p r e s s u r e t a p s A and D , one tap B
f o r i n l e t f l o w : , and a thermocouple w e l l C .
E i t h e r l i q u i d o r gas p r e s s u r e can be a p p l i e d t o
t h e Viton s l e e v e , b u t thrloughout t h e s e exper iments , Chevron
White O i l No. 1.5 w a s used . Both a x i a l and r a d i a l c o n f i n i n g
p r e s s u r e s are a.pplied s imu l t aneous ly t o the core because the
downstream plug, i s mobile and s u b j e c t t o t h e c o n f i n i n g p r e s-
s u r e . A p e r f o r a t e d aluminum t u b e i s f i t t e d around t h e core
r u b b e r s l e e v e t o p r e v e n t l a t e ra l deformat ion of c o r e d u r i n g
load ing .
1 . 9 4 6 i n . OD by 3 .0 i n . long.
4 . 3 A i r Bath and Temperature Con t ro l
The s l e e v e w a s i~ t h i c k c y l i n d e r 1 . 2 2 5 i n . I D by
I
An a i r b a t h w i t h a working space of 2 4 c u b i c f ee t
housed t h e core h o l d e r assemblv. Four kilowatts of power may -18-
J
J
.d
be a p p l i e d t o t h e h e a t i n g elements by an A P I model 4010
power pack and a n API model. 2 2 8 t empera ture c o n t r o l l e r . The
thermocouple t h a t c o n t r o l s t h e ou tpu t of the heater c o n t r o l l e r
can be p laced a t any l o c a t i o n i n s i d e t h e oven, bu t t h e most
e f f i c i e n t h e a t i n g c y c l e w a s found t o r e s u l t when t h e thermo-
couple s e n s o r w a s f a s t ened t i g h t l y t o t h e core h o l d e r . A f a n
provided adequa te a i r c i r c u l a t i o n and the a i r b a t h w a s equipped'
~
I I
with a l i g h t and a window. ~
Temperature was monitored by a 24- point thermocouple I
r e c o r d e r wi th i ron- cons tan t an thermocouples . Two thermocouple$'
were a c t u a l l y used. One thermocouple measured t h e t empera ture I
of t h e c o r e , and t h e o t h e r measured t h e a i r b a t h temperature .
The a i r b a t h t empera ture reached t h e d e s i r e d t e s t tempera ture
i n about 1- 1 / 2 hou r s , but a.t least a n o t h e r four hour s were
r e q u i r e d f o r t h e rock specimen t o r each t h e t e s t temperature .
4 .4 L iqu id and Gas' Sources - A d e a e r a t e d l i q u i d was s t o r e d i n a 4000 cc c a p a c i t y
vacuum f l a s k . A Lapp "Microflo" P u l s a f e e d e r pump w a s used
t o pump t h e l i q u i d through t h e core . The pump h a s a d i a l
i n d i c a t o r , c a l i b r a t e d i n 1 0 0 0 increments which enab led f i n e
ad jus tmen t s i n f low r a t e t o be made.
w e r e used: w a t e r , o i l , and 2- octanol .
Three t y p e s o f l i q u i d s
Gas flow through t h e samples w a s s u p p l i e d from high
p r e s s u r e c y l i n d e r s , and reg,ula ted by a two- s tage a d j u s t-
able r e g u l a t o r equipped wi th a r e l i e f va lve . The i n i t i a l
c y l i n d e r p r e s s u r e w a s 2 5 0 0 p s i , and d e l i v e r y p r e s s u r e s ranged
from 5 p s i t o a maximum o f 4 0 0 p s i .
- 20 -
c
4 . 5 Liquid Pumps
The pumps w e r e a Lapp "Microflo" P u l s a f e e d e r t ype w i t h
a d i a l i n d i c a t o r c a l i b r a t e d i n 1 0 0 0 increments .
created l a r g e p r e s s u r e p u l s a t i o n s when d e l i v e r i n g a t h igh
Both pumps I
I
pres su re s . Accumulators, i n s e r t e d a long t h e f low l i n e s , I
e l im ina t ed t h e s e p u l s a t i o n s . A s t eady f low cou ld b e e s t ab-
l i s h e d and c o n s t a n t p r e s s u r e s maintained a t bo th ends of the
co re .
4 .6 Hydrau l ic Yand P u r 2
An Enerpac hvdraul-ic hand pump wi th a r ange of 0 t o
1 0 , 0 0 0 p s i provided adjustment o f t h e c o n f i n i n g p r e s s u r e .
The pump w a s connected to t h e c o r e h o l d e r and Chevron White
Mineral O i l No, 1 5 was used t o o b t a i n t h e d e s i r e d c o n f i n i n g
p re s su re .
4.7 Heat Exchangers
To ma in t a in t h e t empera ture of t h e f lowing f l u i d con-
s t a n t d u r i n g a r u n , large r e s e r v o i r s were i n s t a l l e d on each1
f low l i n e i n s i d e t h e oven be fo re t h e c o r e h o l d e r . Cold flu1
e n t e r e d a t t h e bottom of t h e r e s e r v o i r . Because of t h e larj
I
s i z e of t h e r e s e r v o i r arid t h e s m a l l f low rates that were
used w i th l i q u i d f low, ho t f l u i d l e f t from the t o p . The
tempera ture o f t h e l i q u i d s l e a v i n g t h e r e s e r v o i r and e n t e r i d g
I
I t h e c o r e w a s measured and found t o remain c o n s t a n t a t t h e 1
d e s i r e d test t empera ture du r ing t h e e n t i r e r u n . I I
The gas r e s e r v o i r i n s i d e t h e oven w a s f i l l e d wi th s t a i n - I
less s t e e l wool. Th i s improved h e a t exchange and enabled
t h e gas t o r e a c h t h e t e s t t empera ture b e f o r e e n t e r i n g t h e cbre .
-21-
The e f f l u e n t f r o m the c o r e and t h e a i r b a t h was cooled
p r i o r t o f l o w r a te de te rmina t ion . This w a s accomplished by
l e t t i n g t h e e f f l u e n t flow through a c o i l immersed i n a con-
s t a n t room tempera ture water b a t h .
4 .8 Backpressure Valve
~
Backpressure was r e g u l a t e d by means of a f i n e meter ing
n e e d l e va lve . This v a l v e , i n a d d i t i o n t o be ing used t o c h a n g e / I I
t h e f l o w r a t e , se rved t o main ta in a s u f f i c i e n t l y h igh p r e s s u r e I
i n t h e system t o keep t h e o p e r a t i n g l i q u i d i n the l i q u i d I
s ta te .
mean pore p r e s s u r e could be mainta ined. Mainta in ing a con-
s t a n t mean pore p r e s s u r e l e v e l w a s impor tan t because exper i-
By a d j u s t i n g t h e va lve and t h e pump r a t e , a c o n s t a n t i
, mental work by Zoback*' showed t h a t a change i n mean pore
p r e s s u r e could affect a b s o l u t e p e r m e a b i l i t y t o an even g r e a t e r
e x t e n t t h a n d i d a change i n c o n f i n i n g p r e s s u r e . A c o n s t a n t
mean pore p r e s s u r e of 2 0 0 ps i w a s ma in ta ined fo r a l l l i q u i d
r u n s .
,
l i
4.9 Flow Rate Measuring Devices
4 .9- 1 Liquid F low: A t s t e a d y s t a t e , t h e mass f l o w ra te
w a s c o n s t a n t throughout t h e system. The mass f l o w ra te w a s
measured by weighing small volumes of t h e e f f l u e n t l i q u i d by
a n a n a l y t i c a l ba lance over a known p e r i o d of trime. Repeated
measurement pe rmi t t ed checking d e t e r m i n a t i o n of s t e a d y s t a t e .
T h e vo lumet r i c flow ra te w i t h i n t h e core was determined as
t h e ratio of t h e mass flow ]?ate t o t h e d e n s i t y of t h e l i q u i d
a t r u n t empera tu re and mean p r e s s u r e . The flow ra te could
- 2 2-
L
be changed by a d j u s t i n g t h e pump ra te and /o r by a d j u s t i n g
t h e need le valve.
4.9-2 Gas Flow: Gas p r e s s u r e w a s r e g u l a t e d upstream
by a two-stage p r e s s u r e r e g u l a t o r and g a s flow w a s r e g u l a t e
downstream by means of a need le v a l v e . T h e cho ice of t he
a p p r o p r i a t e flowmeter w a s made a c c o r d i n g t o t h e l e v e l of f l
i . e . , laminar flow (low r a t e ) , or v i s c o - i n e r t i a l f low ( h i g h
r a t e ) . A bubble f i l m f lowmeter w a s used for a l l l aminar f l
measurements and a Wet T e s t Meter was used f o r v isco- iner t :
f l o w measurements. A s t o p watch, g radua ted i n d i v i s i o n s of
0 .2 second, w a s used as a t i m i n g d e v i c e .
I
I The bubble f i l m f lowmeter w a s t h e m o s t a c c u r a t e of th$/
two d e v i c e s , and was used t o check t he Wet T e s t Meter a t lod
flow rates . The bubble f i l m flowmeter w a s made as follows. I
The v e r t i c a l p a r t of a Y-shaped t u b e i s plunged j u s t up t o
t h e t h r o a t i n a soap so l .u t ion (see F ig . 1). The g a s f l o w
t o be metered e n t e r s through one of t h e branches and bubble$'
i n t o t h e other branch arid t h e n up i n t o t h e v e r t i c a l b u r e t t e
The flow ra te i s ob ta ined by measuring the t i m e it t a k e s f o
a bubble t o t r a v e r s e a known volume i n t he b u r e t t e . T h i s
method e s s e n t i a l l y provj-ded f l o w r a t e measurements a t room
c o n d i t i o n s because t h e p r e s s u r e r e q u i r e d t o d i s p l a c e t h e
bubbles was always less t h a n 0 . 0 1 p s i .
4 . 1 0 P r e s s u r e Recording Devices
1
I
Upstream p r e s s u r e and p r e s s u r e d r o p a c r o s s t h e c o r e I
w e r e measured w i t h a Pace Model KP15 d i f f e r e n t i a l p r e s s u r e
- 2 3 -
t r a n s d u c e r and a Pace '-%del C D 2 5 t r a n s d u c e r i n d i c a t o r . The
a p p r o p r i a t e p l a t e (1 p s i , 5 p s i , 25 p s i , 1 0 0 p s i , o r 500 p s i )
w a s used f o r t h e working range of pressure o r p r e s s u r e d rop .
An e l e c t r o n i c two-pen mult i- range r e c o r d e r , "Chesse l l ,I' was
connec ted t o t h e i n d i c a t o r and p rov ided a permanent r ecord
of t h e p r e s s u r e .
c a l i b r a t e t h e p r e s s u r e r e c o r d i n g d e v i c e s .
A Barne t t Dead Weight Tes te r w a s used t o I l i
J
J
J
J
.J
'i
-
- 2 4 -
L
5. PROCEDURE
Core samples t o be s tud i ed were h e l d , complete ly sat&-
a t e d wi th t h e d e s i r e d l i q u i d , i n a Hassler, r u b b e r s l e e v e
type c o r e h o l d e r , i n an a i r ba th .
ba th and t h a t o f t h e core were t hen brought t o t h e d e s i r e d
l e v e l . Flow w a s e s t a b l i s h e d , and a f te r r e a c h i n g a s teady-
s t a t e c o n d i t i o n , t h e necessa ry p r e s s u r e measurements and f l b w
rates were measured.
e f f e c t o f t empera tu re on f l u i d v i s c o s i t y and d e n s i t y , abso-
l u t e p e r m e a b i l i t y o f t h e core w a s computed a t run t empera t
The l i q u i d s used were water, Chevron White O i l N o . 3 , and 2
The t empera tu re of t h e a i r
I
With t h e necessa ry c o r r e c t i o n s f o r thlh I
o c t ano l . Ni t rogen was t h e gas used. I
5 . 1 Core P r e p a r a t i o n
I
The t w o t y p e s of ‘rocks used i n t h i s s t u d y were conso l I
da ted Mass i l l on Sandstones , and unconso l ida ted O t t a w a S i l i c h
Sand.
i .e . , exper iments N o . 2 and No. 1 4 , t h e cores were f i r e d f o r
a t least 1 2 hou r s i n a 5OO0C fu rnace so as t o o x i d i z e any
o rgan ic matter presef i t .
With t h e excep t ion of t h e f i r s t run w i t h each t y p e ,
5 .1- 1 Consc l ida t ed Massi l lon Sandstones : The c o r e s
were c u t wi th a one-inch diameter diamond d r i l l , trimmed on
a l a t h e , e x t r a c t e d i n a Dean S t a r k t ype a p p a r a t u s , and ign iyed
i n a 5OO0C fu rnace .
i n Ref. 1.
F u l l d e t a i l s o f t h e p r o c e s s are given
- 2 5-
2
A f t e r i g n i t i o n , thle c o r e s were s a t u r a t e d under vacuum
w i t h t h e d e s i r e d f lowing l i q u i d . The d i f f e r e n c e i n weight
a t 1 0 0 % l i q u i d s a t u r a t i o n and a t o t a l l y d r y c o n d i t i o n w a s J
used t o c a l c u l a t e t h e c o r e p o r o s i t y .
For n i t r o g e n f low, t h e a i r - s a t u r a t e d c o r e w a s mounted I I
i n t h e core h o l d e r and f l u s h e d w i t h s e v e r a l pore volumes of
n i t r o g e n . I
i
I
Details of t h e p h y s i c a l and m i n e r a l o g i c a l p r o p e r t i e s 1 ~
i I
Unconsolidated O t t a w a Sand: The sand was s i e v e d 1 j
periment No. 1 4 , t h e sand t h a t passed through s i e v e N o .
of t h e s e c o r e s appear i n Appendix 9 . 2 .
5.1-2
and s e p a r a t e d i n t o uniforbmly graded s i z e s . For one run, ex-
35 J
b u t r e t a i n e d i n s i e v e No. 4 5 w a s used. Fo r all t h e o t h e r
r u n s , the sand s i z e t h a t passed through s i e v e No. 8 0 b u t was ,
d
r e t a i n e d i n s i e v e No. 1 0 0 w a s used. This g i v e s average sand I
I !
' 1
g r a i n s i z e s of 0.385 mm and 0.156 rrun r e s p e c t i v e l y .
sand w a s i g n i t e d a t 50OoC.
The
4
The c o r e load ing and assembly programwas as follows:
T h e upstream p lug was i n s e r t e d i n t o t h e rubber s l e e v e and
t i g h t l y t i e d t o it w i t h 20 gage s t a i n l e s s s tee l w i r e . With 1 1 the assembly h e l d v e r t i c a l l y u p r i g h t , a No. 400 s t a i n l e s s I
4
s t e e l mesh, one inch i n d i a m e t e r , w a s s e a t e d on t h e upstream
I I
Y p l u g , and t h e sand w a s poured i n t o t h e s l e e v e slowly. When
t h e sand was about 2 inches h i g h i n t h e s l e e v e , ano the r
s imilar mesh w a s p laced on t o p of sand pack and t h e down-
stream p lug was in t roduced and a l s o f a s t e n e d i n t h e same
manner. The assembly w a s t h e n p laced i n the core h o l d e r and
I ~
3
-26-
u
aga in we l l compacted and t i g5 t ened wi th t h e h e l p of a v i ce .
The f i n a l o v e r a l l measurtenent o f t h e co re h o l d e r w a s used t o
calculate t h e a c t u a l l e n g t h of t h e co re i n p l a c e .
of t h e c o r e w a s t h e same as t h a t of t h e end p l u g s (1- inch
d i ame te r ) .
The diameter
With t h e core h o l d e r placed i n t h e a i r b a t h and con-
nected t o t h e flow l i n e , t h e c o r e and t h e f low l i n e were
complete ly evacuated and, while under vacuun?, f low w a s s t a rdkd
so as t o comple te ly s a t u r a t e t h e core and f i l l the l i n e s w i t l
t h e l i q u i d . 1 I
The d e t a i l s of t h e p h y s i c a l and m i n e r a l o g i c a l p r o p e r t i e s
of t h e s e c o r e s a l s o appear i n Appendix 9 .2 .
5 .2 E s t a b l i s h i n g Run Condi t ions
With t h e core i n t h e c o r e h o l d e r , the e n t i r e asserrbly
w a s p laced i n a c r a d l e i n t h e a i r ba th and a l l necessa ry
connec t ions w e r e made t o t h e flow l i n e s , p r e s s u r e t a p s , and
c o r e t empera tu re probe.
Conf in ing p r e s s u r e w a s t hen a p p l i e d s lowly by pumping
Chevron White O i l N o . 1 5 around t h e c o r e s l e e v e , care being
t a k e n t o d i s p l a c e a l l t h e a i r i n t h i s l i n e by opening t h e
c o r e end of t h e l i n e dur ing t h e i n i t i a l s t a g e of pumping.
A d e c r e a s i n g c o n f i n i n g p r e s s u r e wi th t i m e u s u a l l y i n d i c a t e d
leakage o f t h e c o n f i n i n g f l u i d i n t o t h e c o r e and flow sys tem,
To avoid l e a k a g e , a 2 0 gage s t a i n l e s s s tee l w i r e w a s always
t i e d around t h e rubbe r s l e e v e between t h e end p l u g s and t h e
1
rock b e f o r e assembly.
A i r t h a t might have been t rapped i n t h e c o r e and t h e
flow system w a s removed by connect ing a vacuum pump t o -27-
t h e ou t f l ow end of t h e s y s t e m , and app ly ing vacuum f o r a t
l e a s t f i v e hou r s . Before t h e vacuum pump w a s d i sconnec ted ,
f low w a s s t a r ted so t h a t t h e whole sys tem w a s complete ly
f i l l e d w i t h t h e l i q u i d t o be used.
The assembled system w a s t h e n hea t ed t o t h e desired ~
r u n t empera tu re a f t e r takfing room c o n d i t i o n measurements. I
The a i r b a t h t empera ture I?eached t h e desired t e s t tempera ture
i n about 1-1/2 hour s , but a t l eas t a n o t h e r f o u r hours were
i
r e q u i r e d for t h e rock specimen t o r each t h e t e s t temperature .
During t empera tu re changes
t he rma l expansion or contr3act i on depending upon whether h e a t i d g
t h e c o n f i n i n g f l u i d underwent
or c o o l i n g . Repeated manual ad jus tments were made t o keep l
t h e overburden p r e s s u r e w i t h i n t h e d e s i r e d l e v e l .
When e q u i l i b r i u m temperature was r eached , f l u i d flow
w a s s t a r t e d and cont inued f o r about a n hour b e f o r e measure-
ments w e r e t a k e n . I
Repeated measurement:s of t empera tu re , p r e s s u r e s and I
I
flow rate w e r e made a t r e g u l a r t i m e i n t e r v a l s . Steady s ta te
w a s assumed when no change w a s observed i n t h e r ead ings and
t h e s t e a d y v a l u e s were recorded. A l l f l o w ra te measurements ~
were t a k e n a t room conditi .ons.
5 .3 Measurements and C a l ~ c u l a t i o n s ! I
5.3- 1 Liqu id Flow: Three k inds of l i q u i d s were used
i n t h i s work: d i s t i l l e d w a t e r , m i n e r a l o i l , and a l coho l . i
I Tap w a t e r w a s d i s t i l l e d i n a Barnstead s t a i n l e s s s t ee l
s t i l l . The o i l used w a s Chevron White Minera l O i l No. 3 ,
and w a s commercial ly a v a i l a b l e . The p h y s i c a l p r o p e r t i e s of 1 I
J
J
J
4
- 2 8-
t h e o i l v a r i e d s l i g h t l y from one c o n t a i n e r t o ano the r .
a l c o h o l used w a s 2- octanol ( P r a c t i c a l ) . Before u s e , each
l i q u i d w a s d e a e r a t e d under a vacuum of about 0.3 p s i a and
f i It e r e d .
The
To keep the f l u i d i n t h e l i q u i d state a t h i g h tempera+
t u r e s , t h e e x i t f lowing p r e s s u r e was k e p t c o n s t a n t at 2 0 0
p s i f o r a l l r u n s .
dampen pump p r e s s u r e p u l s a t i o n s and also he lped t o keep t h e
f lowing p r e s s u r e from changing d r a s t i c a l l y when t h e flow wag
s t a r t e d or stopped.
An accumula tor , charged t o 200 p s i , h e l p e p
Darcy's l a w f o r v i s c o u s f l o w i n a h o r i z o n t a l and l i n e a r I I i porous medium is : I
where q i s i n cc/sec, k is i n d a r c i e s , 1.1 i n cp , A is i n c m 2 l i and i n a tdcm.
Eq. 5- 1 can be expressed as:
Lvw k = - 14700 a- PAP
where k i s i n m d , Ap i s i n p s i , w i n gm/sec, p i n gm/cc, and! I
t h e o t h e r u n i t s and symbols are as d e f i n e d p r e v i o u s l y .
equa t ion was used i n all c a l c u l a t i o n s .
T h i a
I n a d d i t i o n t o u s i n g Qefs. 5 and 6 t o estimate t h e
r e g i o n of v i scous flow w l h e r e p o s s i b l e , c o n d i t i o n s of viscousl ~
f l o w were a l so determined by o b t a i n i n g da ta a t s e v e r a l f l o w ,
r a t e s a t each t e m p e r a t u r e l e v e l and graphing f l o w ra te , q,
- 2 9-
versus p r e s s u r e d rop , p . F o r c o n d i t i o n s of v i s c o u s flow,
t h e d a t a should f a l l on a s t r a i g h t l i n e , p a s s i n g through t he
o r i g i n .
ward c u r v a t u r e of t h e p l o t t e d p o i n t s f r o m the s t r a i g h t l i n e .
The onse t of non--Darcy f l o w was i n d i c a t e d by a down-
It i s necessa ry t o know the v i s c o s i t y and d e n s i t y of
each l i q u i d a t each working t empera tu re l e v e l . Water d e n s i t y '
and v i s c o s i t y v e r s u s t e m p e r a t u r e were found i n t h e Steam i
T a b l e s z 3 and are p r e s e n t e d i n F i g s . 5 and 6 , and i n Table 1, 1
Appendix 9 .1 .
A c a p i l l a r y t u b e v i scomete r w a s c o n s t r u c t e d t o measure
o i l and a l c o h o l (2-octanol.) v i s c o s i t i e s v e r s u s t empera tu re
a t t h e working p r e s s u r e l e v e l of 200 p s i . The procedure f o r
t h e s e measurements i s pres ,ented i n d e t a i l i n Appendix 9.3.
1 1
The r e s u l t s of t h e s e measurements checked v e r y c l o s e l y w i t h I !
t h e d a t a supp l i ed by t h e manufac tu re r s and t h o s e found i n
Iief. 39. The d e n s i t y of a l c o h o l a t v a r i o u s t empera tu res w a s
measured wi th a Bingham t y p e pycnometer.
o i l was measured a t 6OoF and t he tables i n R e f . 2 4 were used
t o estimate t h e d e n s i t i e s a t h i g h e r t empera tu res . R e s u l t s
The d e n s i t y of t h e ' 1 ~
,
are shown i n F i g s . 7 th rough 1 0 , and Tab les 3 through 5 i n I Appendix 9 .1 .
-30-
0
0
110 01 9 0,8 017 016
5
4
013
01 2
011 I I I I
?do I
60 100 150 200 250 TEMPERATURE, O F
'=i~. F. !!ater l l i s c o s i t y v s . T e m D e r a t u r e a t 2 9 0 n s i g
- 3 2 -
O1 85
OI84
0183
O1 82
O1 81
0.80
o1 79
OI78
\
0
0
\ \
0
100 150 200 lEMPERATURE, O F
250 300
F i g . 7. 9ensityvs.Temperature for Chevron White O i l ‘*e. 3 - 3 3 -
w a 5- a n I-
w c3 L
w v)
u v)
0 ' 0
W
>
a a I-
a cn 2 0 Q:
I V
- z 0
0 0 0 o m L n r f M N 4
o m x ) I \ c o m a- M 4
S3XOlS IlN33 All S O X I r\ 3 I l V W 3 N I ]
6.k
F ~ F . 8 . Viscosity vs. Temperature for Chevron White O i l No. 3 -34-
c 0 \
0 \
\ 0 \ 0
'\ 0
50 100 150 200 250 300 TEMPERATURE, O F
Fip. 9 . q e n s i t y of 2-nctanol vs . TemDerature a t 1 4 . 7 psi.
-35-
10 9 8 7 6
5
4
3
2
0
0
5
0
\
4 I I I 4 I I
300 1 i I
50 100 150 200 250 TEMPERATURE, O F
Fi.p. 10. l ’ i scos i tv of 2 - k t a n o l vs. Temerature at 1 4 . 7 n s i
-36-
5.3-2 Gas Flow: Gas w a s supp l i ed from h igh p r e s s u r e
c y l i n d e r s , and flow r a t e cou ld be r e g u l a t e d upstream of t h e
c o r e by a two- stage a d j u s t a b l e r e g u l a t o r equipped wi th a re-
l i e f va lve , and downstretsm. hy means of a needle valve. Most
experiments involved larrhar flow i n o r d e r t o o b t a i n a b s o l u t e
pe rmeab i l i t y and t h e Kliiikenberg s l i p f a c t o r . One visco-
i n e r t i a l run w a s made. I
I n a d d i t i o n t o measuring p re s su re d rop , Ap, a s e p a r a t e I
I
1
t r a n s d u c e r w a s used t o measure the upstream p r e s s u r e , pl .
From t h e s e va lues , t h e mean p res su re pm =
I
AP p1 - 7 was corn-
pu ted , and t h e d i f f e r e n c e (p12-p22) w a s c a l c u l a t e d as 2pmAp.
Low flow ra tes w e r e measured w i t h a bubble f i l m t ype
flowmeter and a Wet T e s t Yeter w a s used f o r h igh flow rate
measurements. Atmospheric p r e s s u r e and room temperature
were a l s o recorded t o pe:rmit c o r r e c t i o n s t o f lowing condi-
t ions . I
The i n t e g r a t e d form o f Darcy's l a w which desc r ibed
s t eady h o r i z o n t a l l i n e a r gas flow under i s o t h e r m a l c o n d i t i o n $
is: I
where :
= gas f low r a t e a t room c o n d i t i o n s , cc/sec 9,
k = a b s o l u t e p e r m e a b i l i t y , d a r c i e s
A = c r o s s s e c t i o n a l area of porous medium, c m
L = l eng th of porous medium, c m
2
= room t e m p e r a t u r e , OK Ta -37-
T = f l o w i n g t empera tu re , OK
= room p r e s s u r e , a t m . abs . Pa Ap = p r e s s u r e drop across porous Fedium, atrr..
pm = mean p r e s s u r e w i t h i n porous medium, a t r . abs.
v = g a s v i s c o s i t y a t T and pm, c p
z = mean gas c o m p r e s s i b i l i t y fac tor
I -
Ni t rogen w a s t r e a t e d as an i d e a l g a s and t a k e n as 1
because of t h e l o w working p r e s s u r e range .
s i d e of Eq. 5-3 w a s d iv ided by 1 4 , 7 0 0 because , i n t h e l a b o r a
t o r y , p r e s s u r e s were measured i n p s i and p e r m e a b i l i t i e s calc - l a t e d i n m i l l i d a r c i e s . Thus:
The r i g h t hand
7 " -L1J. Qa P aT AAPPmTa
k, md =: 1 4 , 7 0 0
Gas v i s c o s i t y ve r sus t empera tu re i s g iven by Suther lanQ's 25 formula .
For n i t r o g e n , N 2 :
-4 1 . 5 1.3.85(10 I T - - - VN2 102+T
where T i s i n 0 K and V is i n cp. Nitrogen v i s c o s i t y v e r s u s , I
t empera tu re a t atm0spheri.c p r e s s u r e i s p r e s e n t e d on F i g . 11 1
and i n Table 2, Appendix 9 . 1 . No s i g n i f i c a n t i n c r e a s e i n
n i t r o g e n v i s c o s i t y occurs from a tmospher ic p r e s s u r e t o the I
o p e r a t i n g l e v e l s , 2 0 0 ps i . , used i n t h i s s tudy . I
I I E q s . 5-4 and 5-6 were used i n gas f l o w c a l c u l a t i o n s
for v i s c o u s f l o w . See Appendices, s e c t i o n 9.3-2, f o r a n a l y s i s
- 3 8 -
Lo CN 0 - 0
cv CN 0 - 0
0 N 0
0 -
d 3 ‘AlIS03SII\
00 t-l 0 - 0
CD 4 0 - 0
0 0 M
0 L n cu
0 0 (v
0 I n 4
0 L n
- 39-
of v i s c o - i n e r t i a l flow. A l i n e a r graph of (p12-p22), ( p s i a ) 2 , where p1 i s upstream p r e s s u r e ( p s i a ) , p2 i s downstream pres-
s u r e ( p s i a ) , ve r sus g a s flow r a t e , g, (cc/sec) , w a s used t o
determine c o n d i t i o n s for v i s c o u s flow.
-40-
6 . ANALYSIS O'F P,ESULTS AND DISCUSSION
The fo l lowing p r e s e n t s t h e r e s u l t s found f o r t h e
ef fect of tempera ture l e v e l and c o n f i n i n g p r e s s u r e on s i n g l e *
phase f l o w i n sands tones . Conf in ing p r e s s u r e had t h e e f fec t
of r e d u c i n g t h e a b s o l u t e p e r m e a b i l i t y o f sands tones f o r a l l
t y p e s of f l u i d s used. S l i p factor f o r gas flow w a s found t o
be t empera tu re dependent as p r e d i c t e d by theory . A change
( d e c r e a s e ) i n a b s o l u t e p e r n e a b i l i t y w i t h tempera ture increasles
w a s observed only i n t h e case o f water flow.
6 . 1 Water Flow
Both conso l ida ted and unconso l ida ted sands tones were
used i n t h i s s tudy.
6 . 1- 1 Consolidated Sandstones : The f i r s t experiment
was c a r r i e d o u t w i t h a core t h a t was h e a t e d t o 3OO0C for 3
h r s and allowed t o cool o v e r n i g h t b e f o r e use. F i g . 1 2 pre-
s e n t s t he r e s u l t . The rock w a s f i r s t h e l d a t 1 0 0 0 p s i con- I
f i n i n g p r e s s u r e , and t h e a b s o l u t e p e r m e a b i l i t y was recorded
w i t h t empera tu re i n c r e a s i n g t o 30OoF. The rock was t h e n ,
al lowed t o cool t o room t e m p e r a t u r e . Confining p r e s s u r e
w a s i n c r e a s e d t o 2 0 0 0 p s i and t h e p r o c e s s o f h e a t i n g and
measurement r epea ted .
p o r t e d h e r e i n i s ra.ted a t 5 0 0 0 p s i a t 35OoF s a f e l y , but a
maxinum of 4 0 0 0 p s i and 3OO0F w a s used.
I
The core h o l d e r used i n t h e work re-
-41-
~ ~~ ~ ~~
~
It can be seen from t h e graph t h a t a t each l e v e l o f
c
..
conf in ing p r e s s u r e , t h e a b s o l u t e p e r m e a b i l i t y t o water de-
creased a t an approximate rate of -1.0 nd/OF.
The nex t series of experiments w e r e performed on cores
f i r e d a t 5OO0C i n o r d e r to i n v e s t i g a t e h y s t e r e s i s and r e p r o-
d u c i b i l i t y of r e s u l t s . The r e s u l t s are shown on F i g s . 1 3 ,
1 4 , and 15 . A l l showed a decrease of a b s o l u t e p e r m e a b i l i t y
t o water w i t h t e m p e r a t u r e i n c r e a s e , b u t t h e s l o p e dec reased
wi th i n c r e a s i n g t empera tu re .
t o - 1.6 & / O F w a s observed.
An average s l o p e of - 1 .3 rnd/OF
The r e s u l t s a l s o show tha t t he
tempera ture effect w a s e s s e n t i a l l y r e v e r s i b l e (see Fig . 1 3 ) .
The f irst c o o l i n g c y c l e for t h e Mass i l lon Sandstone Nol
3 (Fig . 14) a t 3000 p s i g c o n f i n i n g p r e s s u r e i n d i c a t e d h y s t e r d -
s is . On t h e f i rs t c o o l i n g c y c l e , t h e pern-!eability i n c r e a s e d ~
w i t h r e s p e c t t o t h e f i r s t : h e a t i n g c y c l e .
a g a i n , r e s u l t s fo l lowed t:he f i r s t c o o l i n g r u n , i n d i c a t i n g telr-
p e r a t u r e r e v e r s i b i l i t y arid good r e p r o d u c i b i l i t y . No r e a s o n
for t h e i n c r e a s e i n p e r m a b i l i t y a f te r t h e first h e a t i n g r u n
w a s found.
On h e a t i n g and cool/ing
I
6.1-2 Unconsol ida ted Sand: The f i rs t experiment i n t h q s
series w a s r u n w i t h unconso l ida ted O t t a w a S i l i c a Sand of ,
average g r a i n s i z e of 0 .385 mm, This core w a s n o t s u b j e c t e d ~
t o h e a t t r e a t m e n t and was loaded as o u t l i n e d i n t h e procedur 3 , s e c t i o n 5 . Data were not: ob ta ined f o r the c o o l i n g c y c l e s .
The r e s u l t s a re shown i n F ig . 1 6 . Confining p r e s s u r e s of 500i,
1 0 0 0 , and 1500 p s i g were used. Absolute p e r m e a b i l i t y t o watw 1
- 43-
c(
v) CL
0 0 cv II
z
E 4
Gi
I 1 I I I
0 0 u3
0 0 Ln
0 0 a-
0 0 M
0 0 w
0 In M
0 0 M
0 In cv
0 0 cv
0 In 4
0 0 4
0 Ln 0 0
h ic,
’. M
4 r l 44
‘A11 1 I IfW3Wt13d - 4 6 -
v) n m 00
O M 0 - c v o II II
E W t r r e n - Z o n
a z v )
0 0 0
%
cv N
0 c3 0 00' 11
0 0 0
% a- ll
0 0 0
0 1
%
- 4 7 -
0 0
0 In M
0 0 M
0 L n cv
0 0 cv
0 In ll
0 0 11
0 Ln
0 0 0
decreased w i t h a n i n c r e a s e i n c o n f i n i n g p r e s s u r e .
of change was - 0.5 rnd/OF a t a11 l e v e l s of c o n f i n i n g p r e s s u r e c
As t h e a b s o l u t e p e r m e a b i l i t y of t h i s core w a s very h igh ,
2 2 , 0 0 0 md a t 500 p s i g co:nf in ing p r e s s u r e , t h e average sand
g r a i n s i z e was reduced for t h e nex t exper iment .
f o r methods of c o n t r o l o f p e r m e a b i l i t y and p o r o s i t y of syn-
t h e t i c sands .
6 .2 Gas F l o w
"he rate
( 1 1
See Ref. 26 1
1
1 Gas f low experiments were conducted a t t h r e e d i f f e r e n t 1
Abso- t e m p e r a t u r e l e v e l s and a range of c o n f i n i n g p r e s s u r e s .
l u t e p e r m e a b i l i t i e s were measured w i t h n i t r o g e n flow under
c o n d i t i o n s of v iscous flow and graphed as a f u n c t i o n of the
r e c i p r o c a l mean p r e s s u r e on a c o n v e n t i o n a l Klinkenberg graph.
One run w a s conducted i n t h e v i s c o - i n e r t i a l flow reg ion for
a c o n s o l i d a t e d sands tone .
gas flow d a t a are given i n Table 9 and i n Appendix ( s e c t i o n
9 . 3- 2 ) .
t e m p e r a t u r e s but for t h e same c o n f i n i n g p r e s s u r e , e x t r a p o l a t e d
t o t h e same i n f i n i t e p r e s s u r e v a l u e .
g raphs are, however, p robably n o t t r u e Klinkenberg s l i p coef-
I 1 1 Details of t h e a n a l y s i s of t h i s 1
I n a l l c a s e s , t h e a b s o l u t e p e r m e a b i l i t i e s a t d i f f e r e a t
I ! The s l o p e s o f t h e s e
f i c i e n t s . i
combina t ion of both s l i p and mean p o r e p r e s s u r e- c o n f i n i n g p r e s *
s u r e stress e f f e c t s on p e r m e a b i l i t y . Although t h e c o n f i n i n g
p r e s s u r e was h e l d c o n s t a n t a t 1000. psi o r more, t h e pore p res-
s u r e changed from n e a r l y a tmospher i c t o s e v e r a l hundred p s i
for each ser ies of r u n s .
w a s n o t a major o b j e c t i v e of t h i s s t u d y .
t i o n from t h e s e graphs is t h a t t e m p e r a t u r e has no apparen t effect
on a b s o l u t e pe rmeab i l i ty to gas.
The high s l o p e s are a r e s u l t of t h e e f f e c t s of a
I I
' I 3 e t e r m i n a t i o n of s l i p c o e f f i c i e n t s
The va luab le informadl
Figs . 18 and 19, r e s p e c t i v e l y . On Fig. 1 8 , t h e Klinkenberg
s l i p f a c t o r s a t 6 8 , 1 5 0 , and 25OoF are 2 . 2 6 4 , 3.587, and 4.351
p s i , r e s p e c t i v e l y .
s l i p f a c t o r depends upon temperature. T h e apparent permea- I
b i l i t i e s a t d i f f e r e n t temperatures and p r e s s u r e s ex t rapo la ted
This shows t h a t t h e apparent Klinkenberg
t o t h e same va lue of 9 6 0 md and agree reasonably w i th t h e v i s c
i n e r t i a l a n a l y s i s value of 932 md shown on Fig. 1 9 . The turbud
l e n c e factor 8 , which may be obtained from Fig . 1 9 , was 1 . 7 x 7 10 ft-l, and i s i n agree,ment with a c o r r e l a t i o n proposed i n
R e f . 2 7 .
i n t h e s e r u n s .
The conf in ing p ressure was he ld c o n s t a n t at 1 0 0 0 p s i 1
Another se r ies o f experiments w a s conducted on Massillon i
! I
1 1
Sandstone Core N o . 6 a t room, 15OoF, and 25OoF tempera ture
l e v e l s and a t conf in ing p ressures of LOOO, 3000, and 4000 psig . !
Resu l t s are shown on Figs, , 20- 22, and are similar t o those of 1 1
Fig. 18. Absolute permeabi l i ty decreased w i t h an i n c r e a s e i n , conf in ing p r e s s u r e ; and at: t h e same l e v e l of conf in ing pressurq
t h e apparen t p e r m e a b i l i t i e s ex t rapo la ted t o t h e same i n f i n i t e
p r e s s u r e va lue apparent s l i p f a c t o r s a t room and 15OoF tempera-i
I
t u r e l e v e l s w e r e e s s e n t i a l l y t h e same for a l l l e v e l s o f con-
ni.trop,cn flow a n d wstcr flow for t h c consol i d c i t e d
c o r e s w e r e d i f f e r e n t . Pe rmeab i l i t i e s t o water a t
perature ranged between 550 rrd and 450 md f o r a l l -50-
6 . 2 - 1 Consolidatetl Sandstones: The r e s u l t s of t h e
first run i n t h e viscous and v i s c o- i n e r t i a l f low reg ions on
I Massi l lon Consolidated Sandstone Core Yo. 5 are shown on
f i n i n g p r e s s u r e , but higher a t 2 5OoF tempera ture . I
The v a l u e s of a b s o l u t e p e r m e a b i l i t i e s ob t a ined w i t h I
sandstone
room t e m -
of t h e
I
~
u, 0 0 Ln N
II I-
L L L L 0 0 0 0 0 L n c D I+
II II
t- I-
\
U
v) a 0 0 0 4
II w p: 3 v) v) w p:
(3 z z L z 0 u
n
U
U
0 0
0 0 cn
(7W ‘AlIlI€fW3W~3d lN3tlWddb -51-
% I 3 L
0 LI 3
0 4 Ln cv ca
n - 0
-
I
E Ln
0 - a
3 W E 3
Ef
0 - u
@ a , P ' S I 0 *o
a 0 0 E a
M 0
- w u w cr:
0 0 m
Q 0 co
0 0 h
-53-
LL
0 Ln 1
0
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a
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conf in ing p r e s s u r e l e v e l s , whi le a b s o l u t e p e r m e a b i l i t i e s t o
n i t r o g e n were cons ide rab l ly h i g h e r and ranged from 9 6 0 md t o
800 md fo r t h e same c o n d i t i o n s .
omena caus ing t h e permea .b i l i ty r e d u c t i o n w i t h water f l o w a t
d This s u g g e s t s tha t t h e phen-
room t empera tu re may also be r e s p o n s i b l e for the p e r m e a b i l i t y
r e d u c t i o n a t h i g h t e m p e r a t u r e s . The Mass i l l on Sandstone has 4
a low c l a y c o n t e n t , and had been f i r e d at 50OoC. i
6.2- 2 Unconsol ida ted Sand: Fig . 23 shows r e s u l t s ob-
t a i n e d wi th f i r e d s i l i c a sand.
w a s a p p l i e d , and t h e t empera tu re l e v e l s used were 68OF, 150af,
and 25OoF. The r e s u l t s were s imilar t o t h o s e for t h e consol,!-
da t ed sands tones . 4
A 2000 p s i g c o n f i n i n g p r e s s u r e J i
I
P e r m e a b i l i t y t o water w a s a l s o measured f o r t h i s core.'
While t h e e x t r a p o l a t e d a b s o l u t e p e r r e a b i l i t y t o n i t r o g e n w a s /
4,260 md, t h e p e r m e a b i l i t y t o water was o n l y 2 , 1 2 7 md a t roq
tempera ture .
6 . 3 O i l F low
J
1" ~
.J
~
Because of t h e d i f f e r e n c e between t h e r e s u l t s o b t a i n e d
a t e l e v a t e d t e m p e r a t u r e s w i th water f l o w and gas f l o w , s i m i l g r
exper iments w e r e r u n w i t h ano the r f l u i d . Chevron White O i l ~
J
No. 3 w a s chosen for i t s h i g h e r v i s c o s i t y and i t s non- polar
c h a r a c t e r i s t i c s
v i s c o s i t y p o l a r f l u i d and may i n t e r a c t w i t h t h e r o c k s u r f a c e l
Experiments (see 3.ef. 1) had a l r eady been c a r r i e d o u t w i t h
j
as opposed t o water, which i s an i n t e r m e d i d t e
d
Chevron White O i l No. 1 5 , which i s very v i scous . A s i n water
f l o w or gas f low expe r imen t s , t h e combined ef fec t of temperait I
I 4
t u r e and overburden p r e s s u r e was i n v e s t i g a t e d . ~
-56-
Figs . 2 4 and 25 show t h e r e s u l t s wi th o i l f low for
c o r e s No. 1 0 and 11. O i l flow w a s cofiducted on ly on con-
s o l i d a t e d sands tones .
a f f e c t e d by c o n f i n i n g p r e s s u r e , as expec ted , b u t t h e r e w a s
on ly a s l i g h t d e c r e a s e i n a b s o l u t e p e r m e a b i l i t y t o o i l w i t h
tempera ture i n c r e a s e . H y s t e r e s i s e f f ec t s i n c o o l i n g c y c l e s
were more pronounced a t high c o n f i n i n g p r e s s u r e s of 3000 p s i
and 4 0 0 0 p s i .
Absolu te p e r m e a b i l i t y t o o i l w a s
Pe rmeab i l i t y l e v e l s a t room tempera tu re a g r e e c l o s e l y 1 I
with t h o s e o b t a i n e d w i t h n i t r o g e n flow.
rock- o i l i n t e r a c t i o n i s b e l i e v e d t o be r e s p o n s i b l e for the
d i f f e r e n c e between water and o i l p e r m e a b i l i t i e s . T h i s sug- 1 g e s t s a d e f i n i t e i n t e r a c t i o n between water and sands tone , I
The absence of
i I
conso l ida t ed o r unconso l ida t ed . I
6 . 4 2-Octanol Flow I
I n view of t h e results w i t h water, it appeared
u s e f u l t o run s i m i l a r expe r imen t s wi th a n o t h e r polar l i q u i d .
2- octanol a l c o h o l w a s chosen.
Experiments were conducted w i t h commercial g rade 2-
o c t a n o l , and t h e r e s u l t s are p re sen ted i n F ig . 2 6 . The un-
I conso l ida t ed O t t a w a S i l i c a Sandcore used was f i r ed a t 50OoC.
The average sand g r a i n s i z e w a s 0 . 1 5 6 mm. The c o n f i n i n g
p r e s s u r e a f f e c t e d t h e a b s o l u t e p e r m e a b i l i t y as expec t ed , b u t ~
t empera ture appeared t o c a u s e a. small i n c r e a s e i n a b s o l u t e
pe rmeab i l i t y . I n a d d i t i o n , t h e r e w a s a permanent r e d u c t i o n
i n a b s o l u t e p e r n e a b i l i t y o n each c o o l i n g c y c l e .
a re d rama t i c when compared t o t h e water d a t a on F igs . 1 6 and,117.
I
i
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These r e s u l d s
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-61-
I ,
I -
The s l i g h t i n c r e a s e i n p e r m e a b i l i t y t o o c t a n o l w i t h tempera-
t u r e i n c r e a s e f o r bo th h e a t i n g and c o o l i n g r u n s emphasizes
t h e impor tance of t h e dec rease i n k with t e m p e r a t u r e i n c r e a s e 3
for water. Recent d i s c u s s i o n s between Ramey and Dreher (Yara-
thon O i l C o . , Denver) r e v e a l e d t h a t o c t a n o l o f t e n behaves more
d l i k e an o i l t h a n a n aqueous w e t t i n g phase i n s ands tones .
r e t r o s p e c t , it might have been b e t t e r t o h a v e selected b o -
p r o p y l a l c o h o l (IPA) as t h e second p o l a r s u b s t a n c e . It i s
recommended t h a t IPA be cons idered f o r f u t u r e s t u d i e s .
I n
J
6 . 5 D i s c u s s i o n
J I
have been one r ea son for t l h e effect of t e m p e r a t u r e l e v e l upon I 1 Cass6’ concluded t h a t c lay- water i n t e r a c t i o n s may
i I ~
a b s o l u t e p e r m e a b i l i t y t o w a t e r f o r s a n d s t o n e s h e observed.
G r i m 3 ’ 31 p r e s e n t e d a comprehensive rev iew of the mechanism
involved i n c lay- water i n t e r a c t i o n s . Because t h e r o c k s used J
i n t h i s work w e r e t o t a l l y or n e a r l y c l a y- f r e e , c lay- water ~
1 i n t e r a c t i o n i s cons ide red r e s p o n s i b l e f o r o n l y a minor role
i n the phenomenon observed i n t h i s s tudy . .d
It i s almost c e r t a i n t h a t water-cilica i n t e r a c t i o n s
a re r e s p o n s i b l e f o r t h e mafior e f fec ts obse rved w i t h w a t e r . I n ! 13
I Glass F i l t e r s of low p e r m e a b i l i t y ( 1 6 0 rrd a t room t e m p e r a t u r e ) ’ \ I
a d d i t i o n t o the r e s u l t s of t h i s s t u d y , Grunberg and Nissan
used aqueous s o l u t i o n s ( i n c l u d i n g Amyl Alcohol) w i t h J ena
and found a l i n e a r dec rease i n a b s o l u t e p e r n e a b i l i t y wi th an 1
3
J
i n c r e a s e i n t e m p e r a t u r e . 3 2 F l u i d f l o w mechanisms o f t e n fit t w o c a t e g o r i e s :
3
(1) mechanisms which are e s s e n t i a l l y mechanical i n n a t u r e , t h e 1 1
- 62-
f l o w depending on t h e bulk p r o p e r t i e s of t h e f l u i d s concerned
..
!-
and upon the mechanical f o r c e s e x e r t e d upon the f l u i d b o d i e s ;
and ( 2 mechanisms which are e s s e n t i a l l y m o l e c u l a r i n char&-
t e r , t h e f l o w depending l a r g e l y on t h e motion of t h e i n d i v i d u a l
molecules, t h e moleculair, weight , t h e c o l l i s i o n cross-section,
t h e mean f ree p a t h , r o c k- f l u i d a t t r a c t i v e forces, etc., ra tder
than upon t h e d e n s i t y , p r e s s u r e v i s c o s i t y , e t c . , of t h e f l u i d
i n bulk .
of t h e e f fec t of t empera tu re upon water f l o w i n s ands tones
under p r e s s u r e .
The l a t t e r mechanisms may be dominant i n t h e case
S u r f a c e a t t r a c t i v e forces between s i l i c a and water
molecules may be l a r g e enough t o l e a d t o chemi- sorp t ion . I n
such a case, t h e a d s o r b a t e molecules become p r a c t i c a l l y a
p a r t o f t h e solid s u r f a c e and, compared with o the r rnolecules
i n the l i q u i d , such chemfi-sorbed molecu les may be l a r g e l y
immobilized. The e f f e c t i v e c r o s s- s e c t i o n under v i s c o u s f l o w I
could t h e n be d i f f e r e n t f o r water from t h e o t h e r f l u i d s test&.
I n c r e a s e s i n t e m p e r a t ~ r e ~ ~ seem t o i n c r e a s e t h i s e f f e c t from
t h e r e s u l t s of t h i s s t u d y . An exhaus t ive l i t e r a t u r e su rvey
i n d i c a t e d no known phenomna capable of e x p l a i n i n g t h e magni-
t u d e of t h e ef fects observed i n t h i s s tudy .
t h a t a major, and h e r e t o f o r e unsuspected a t t r a c t i o n between
water and s i l i c a h a s been d i scovered . It is p o s s i b l e t h a t
t h i s a t t r a c t i o n i s e s s e n t i a l l y r e s p o n s i b l e for t h e l a r g e
tempera ture e f fec t s on p r a c t i c a l i r r e d u c i b l e water s a t u r a t i o n
and r e l a t i v e p e r m e a b i l i t i e s 34916,35, and on c a p i l l a r y p r e s -
s u r e s 36-38 and r e s i s t i v i t y p rev ious ly r e p o r t e d .
It is b e l i e v e d 1
- 6 3-
If a s t r o n g a t t r a c t i o n between water and s i l i c a i s _.
t h e major t e m p e r a t u r e e f f ec t , s e v e r a l new exper iments w i t h
g a s- o i l flow i n sands tones w i l l show no t e m p e r a t u r e e f fec t , I
~
whi le gas- water f l o w i n sands tone w i l l depend on t empera tu re .
I n a d d i t i o n , exper iments of any s o r t i n l i m e s t o n e s shou ld
no t depend s t r o n g l y on t e n p e r a t w e .
- 64 -
J
v,
J
J
d
J
J
J
J
J
J
i
7. CONCLUSI3NS AND RECOY!!!TYIkTIONS
Experimental r e s u l t s i n d i c a t e t h a t t h e a b s o l u t e per-
meabi l i ty t o water f o r conf ined sands tones i s s t r o n g l y t e m -
p e r a t u r e dependent. The a b s o l u t e p e r m e a b i l i t y of s a n d s t o n e s
t o o t h e r f l u i d s ( n i t r o g e n , mine ra l o i l , o c t a n o l ) i s e i t h e r ,
una f fec ted o r on ly s l i g h t l y a f f e c t e d by t e m p e r a t u r e l e v e l .
Temperature increase has t h e e f f e c t of d e c r e a s i n g t h e abso-
l u t e p e r m e a b i l i t y t o w a t e r f o r sands tones remarkably.
Temperature change h a s l i t t l e o r no effect on t h e abeo-
l u t e p e r m e a b i l i t y o f s a n d s t o n e s t o n i t r o g e n , m i n e r a l oil, qr
o c t a n o l . I n t h e case o f water f l O t 7 , p e r m e a b i l i t y r e d u c t i o h s
o f up t o 60% were o b s e w e d o v e r a t empera tu re r a n g e of 70-$OO0F. ~
Regardless of t h e t y p e of f lowing f l u i d , t h e l e v e l of
c o n f i n i n g p r e s s u r e a f f e c t e d a b s o l u t e p e r m e a b i l i t y i n the s@ne
manner , i .e . , p e r m e a b i l i t y decreased wi th i n c r e a s i n g confizhing
p r e s s u r e . For water f:Low exper iments , i n c r e a s i n g t h e c o n f i n i n g
p r e s s u r e had t h e a d d i t i o n a l effect of i n t e n s i f y i n g t h e tembera-
t u r e dependence o f a b s o l u t e p e r m e a b i l i t y i n many cases (but
n o t a l l ) .
I n t h e l i g h t of t h e r e s u l t s o b t a i n e d , it seems t h a t wn-
suspec ted f l u i d - s o l i d s u r f a c e a t t r a c t i v e f o r c e s between w a t e r
molecules and s i l i ca were l a r g e l y r e s p o n s i b l e for t h e m a j o r
e f f e c t s observed. The f o l l o w i n g recomnendations a p p e a r
,
p e r t i n e n t .
-65 -
J' - 66 -
It i s recornended t h a t t h e r e s u l t s o b t a i n e d by G r u n - 13 b e r g and Ni s san be rechecked for t h e same aaueous s c l u t i o n s
and for c o n f i n e d porous media. It i s also recornended t h a t
exper iments b e r e p e a t e d f o r h i g h e r t e m p e r a t u r e s and conf inin ,g
p r e s s u r e s .
J
S i n c e o c t a n o l behaves more l i k e an o i l t h a n a n aq-ueous J
w e t t i n g phase i n s ands tones , it i s recommended that i sop ropy l
alcohol b e used as the second polar s u b s t a n c e for f u t u r e
s t u d i e s .
t h e d e c r e a s e i n water pe rmeab i l i t y w i t h i n c r e a s i n p temperatqhe
is due t o t h e p o l a r i t y o f water.
R e s u l t s from such s t u d i e s may h e l p t o e x p l a i n whether A
d I
I f a s t r o n g a t t r a c t i o n between w a t e r and s i l i c a causes '
t h e t e m p e r a t u r e e f f ec t , experiments des igned t o i so la te watap
a n d / o r s i l i ca w i l l be e n l i g h t e n i n g . Exper iments w i t h water I f l o w i n l i m e s t o n e s should no t depend s t r o n F l y on tempera tura
I n a d d i t i o n , exper iments wi th g a s- o i l f l o w i n s ands tones may
show no t e m p e r a t u r e e f f ec t whi le gas-water f l o w i n sandstond
w i l l depend on t empera tu re .
J
i
J
J
-66-
8 . REFERENCES
1.
2 .
3.
4.
5.
6 .
7.
8.
9 .
10.
11.
1 2 .
Cassg , F. J . : "The Effect of Temperature and Confining P re s su re on F l u i d Flow P r o p e r t i e s of Consol ida ted Xocks ," Ph.D. D i s s e r t a t i o n , S t a n f o r d U n i v e r s i t y ( 1 9 7 4 ) .
A r i h a r a , N . : "A Stud17 of Non- Isothermal S i n g l e and Two- Phase Flow th rough Consol ida ted Sandstones ,!' Ph.D. D i s - s e r t a t i o n , S t an fo rd U n i v e r s i t y ( 1 9 7 4 ) .
Greenberg, D .B . , Cresap, R.S:, and Malone, T.A.: " I n t r i n - s i c Pe rmeab i l i t y of Hydro log ica l Porous Mediums: V a r i a t i o n wi th Temperature," Water Resources Research (Aug. 19681, - 4 , No. 4, 7 9 1 .
Muskat, M. : Flow of Homogeneous F l u i d s through Porous Media, M c G r a w - H i l l Book Company, I n c . , 1937, C h . 11.
Fancher , G.H. ? L e w i s , J . A . , and Barnes , K.: "Some Physi- , ca l C h a r a c t e r i s t i c s of O i l Sands,"Ind. Eng. C h e m . , 2 5 : 1 1 3 9 ( 1 9 3 3 ) .
Geertma, J. : " Est imat ing t h e C o e f f i c i e n t of t h e I n e r t i a l ' Res i s t ance i n F l u i d Flow th rough Porous Media," SOC. Pe t . Eng. Jou r . ( O c t . 1 9 7 4 1 , 465.
- -
Amyx, J . W . , Bass, D.M., Jr., and Whiting, R.L.: Pet roleul Rese rvo i r Engineer in ,&, M c G r a w - H i l l Book Company, Inc . , ' 1 9 6 0 , Ch . . 2
Kundt, A . , and Warbu:rg, E. : Pogpendorf ' s Ann. Phys ik , pp 155, 337, 525.
Klinkenberg , L. J . : "'The P e r m e a b i l i t y of Porous Media t o Liquids and Gases," D r i l l . and Prod. P rac . , API (19411, 200 .
Forchheimer, P.: "Hydraulik," Le ipz ig a n d . B e r l i n , C h . 1s S e c t i o n s 1 1 6- 1 1 8 , Druck and Ver l ag von B.G. Teubner ( 1 9 1 4 ) .
C o r n e l l , D . , and Katz, D.L. : "Flow of Gases through Consol ida ted Porous Media," Ind . Eng. Chem. (19531, Vol. 4 5 , p . 2145.
Dranchuk, P.H., and Kolada, L . J . : " I n t e r p r e t a t i o n of Steady L i n e a r V i s c o- I n e r t i a l Gas F ~ O W Data," Jour . ' Can. P e t . Tech. ( 1 9 6 8 1 , -. 7 , No. 1, p. 36.
- 6 7 -
13.
14.
1 5 .
1 6 .
1 7 .
18.
1 9 .
2 0 .
2 1 .
2 2 .
23.
24 .
25.
2 6 .
i
J
J
J
kJ
d
J
4
J
.J
I
.J
Grunberg, L . , and Nissan, A . H . : "The Permeabi l i tv of Porous S o l i d s t o Gases and Liquids ," Jou r . of . I n k . of P e t . (19531, 2 9 , No. 2 3 6 , p . 1 9 3 . - - Calhoun, J . C . , Jr . , and Yus te r , S.T.: "A Study of t h e Flow of Homogeneous F l u i d s th rouph I d e a l Porous Media," D r i l l and 'Pro'd. Prac., API ( 1 9 4 6 1 , 335.
API RP 2 7 : "Recommended P r a c t i c e for Determining Permea- b i l i t y of Porous Media," Am. P e t . I n s t . (Aug. 1956).
Weinbrandt , R.M. : "The Effect of Temperature on Relat ive P e r m e a b i l i t y , " Ph .D. D i s s e r t a t i o n , S t a n f o r d U n i v e r s i t y (1972).
W i l h e l m i , B . , and Somerton, W.H.: "Simul taneous Measure- ment of Po re and Elas t ic P r o p e r t i e s of Rocks under T r i - ax i a l S t r e s s Cond i t i ons , " SOC. P e t . Eng. J o u r . (Sep t . 1 9 6 7 1 , - 240, 283.
w i t h Overburden Pressure," Trans . , AIME (1952) , - 3 1 9 5 329.
F a t t , I. , and Davis , : D . H . : "Reduction in P e r m e a b i l i t y I I
Gray, D.H. , F a t t , I:, and Bergamini, G. : "The Effect of I
I S t r e s s on P e r m e a b i l i t y of Sandstone Cores," SOC. Pe t . Eng. Jour . ( J u n e 1 9 6 3 ) , 9 5 .
Zoback, M . D . , and Byeiqlee, J . D . : " P e r m e a b i l i t y and Ef- f e c t i v e S t r e s s , " A m e r . Assoc. P e t . Geol. B u l l . , 59 (1) (1975a1, 1 5 4 .
Somerton, W.H. , Mehta,, M.M. , and Dean, G.W. : "Thermal A l t e r a t i o n of Sandstones ," J. P e t . Tech. (May 19651, 589.
Wyble, D.O.: "Effect of Applied P r e s s u r e on t h e Conduc-
i 1
t i v i t y , P o r o s i t y , and Pe rmeab i l i t y of Sands tones ," Trans . , AIME (19581. 213. 430.
Meyer, C.A. , McClintock, R.B. , S i l v e s t r i , G . J . , and Spencer , R . C . , Jr.: 19167 ASME S t eam Tab le s , Am, SOC. I
Mech. Engrs . , 2nd e d . , New York, N . Y . , 1968.
ASTM-IP-Petroleum Measurement T a b l e s , ASTM, P h i l a d e l p h i a I
(19521 . P e r r y , J . H. : Chemical Engineer ' s Handbook, M c G r a w - H i l l Book Company, Inc . (19691, pp. 23- 10.
Larman, H . J . : " V a r i a t i o n s i n P e r m e a b i l i t y and P o r o s i t y of S y n t h e t i c O i l Rese rvo i r Rock--!<ethods of Control," SOC. of P e t . Eng. J o u r . (Dec. 19651, 329.
I
-6 8-
2 7 .
2 8 .
29.
30.
31.
32,
33.
34.
35.
36.
37.
38.
39 .
Katz, D . L . , and C o a t s , K . H . : Underground S t o r a g e of F l u i d s , U l r i c h s Books, Inc . , Ann Arbor, Michigan c19 6 8 ) . Jones , S .C . : "A Rapid , Accurate Unsteady- State Kl inken- berg Permeameter," SOC. P e t . Eng. J o u r . ( O c t . 1 9 7 2 1 , 483.
Sax, N. I. : Dangerdus P r o p e r t i e s of I n d u s t r i a l Materials , Reinhold P u b l i s h i n g Corpora t ion (1963) . G r i m , R.E. : Mineralogy, M c G r a w - H i l l Book Company, I n c
G r i m , R.E. : Clay Mineralogy, M c G r a w - H i l l Book Company, Inc . (1968) .
Flood, E .A. : " I n f l u e n c e o f Su r face Fo rces o n F l o w of F l u i d s t h rough C a p i l l a r y Systems ,I' Highway Research Board, Spec. Rep. N o . 40 (19581,
Bar te l l , F . E . , Thomas, T .L . , and Fu, Y.: "Thermdynam$cs of Adsorpt ion from S o l u t i o n , i v . Temperature Dependenae of Adsorp t ion ," J o u r . - of Phys. Chem. (19511, - 5 5 , 1 4 5 6 ,
Poston, S . W . , Ysrael, S. , Hossain , A.K.M.S. , Montgomery, E.F. , 111, and Rarney, H.F. , Jr.: "The Effec t of Tempeva- t u r e on I r r e d u c i b l e Water S a t u r a t i o n and R e l a t i v e Permed- b i l i t y of Unconsol-idated Sands," SOC. of P e t . Eng. Joqr. ( June 1 9 7 0 1 , 1 7 1 .
Weinbrandt, R.M., Casse, F , J . , and Ramey, H . J . , Jr.: , "The Effect of Temperature on R e l a t i v e and Abso lu t e ' Permeab i l i t y of Sands tones ," SOC. of P e t . Eng. J o u r . ( O c t . 1 9 7 5 1 , 376.
S innokro t , A.A. , Ramey, Hi; J., Jr, , and Marsden, S.S , , ~ Jr, : "Effect of Temperature Level upon C a p i l l a r y P r e s s u r e ' Curves," SOC. o f P e t . Eng. Jou r . (March 19711, 13 .
Okandan, E . , Marsden, S .S., Jr. , and Ramey, H.J., Jr. E " C a p i l l a r y P r e s s u ~ e and Contact Angle Measurements at Eleva ted Temperatures , I 1 presen ted a t AIChE Meet ing, FLlsa, Oklahoma, March 1:2, 1 9 7 4 .
Sanya l , S .K . , Ramey, H . J . , J r . , and Marsden, S . S . , Jri. : "The Ef f ec t of Teinperature on C a p i l l a r y P r e s s u r e Propkr- t i e s of Rocks," S:PWLA 1 4 t h Annual Logging Symposium (May 1973) .
Na t iona l Research Counci l of U. S .A. : " I n t e r n a t i o n a l Cr i t ica l Tables of Numerical Data, P h y s i c s , Chemis t ry and Technology," 'Vol. I-1111, 1 9 3 3 ,
-69-
Table 1. Dens i ty and Vi . scos i ty of Water vs. Temperature
(from Steam
P r e s s u r e = 2 0 0 p s i g
Temperature . ' OF
6 0
1 0 0
1 5 0
2 0 0
250
3 0 0
350
Dens i ty gm/cc
0.9990
0.9931
0.9803
0 . 9 6 3 2
0 .9423
0.9180
0.8904
V i s c o s i t y cp
1.100
0.679
0 .426
0 .300
0.228
0 .183
0 .152
J
r'
J
J
4
J
4
4
3
4
-72 -
c Table 2. V i s c o s i t y of Nitrogen vs. Temperature
I
Pr-essure = 14.7 p s i a
Temperature Temperature Viscosity OF ' OK c p
60 288.7 0.01739
100
150
200
2 50
300
310.9
338.7
366.5
394.3
0.01839
0.01959
0.02074
0.02185 I
422.0 0.02291
OK = T(°F)-32 + 273.16 1.8
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0
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0 .
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0
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0 9
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0
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v) I 0 rl X b a hl + ri U 0 t-i ri v) 0
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VlD.413 0 0 0 0 0 0
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Table 5.
Temp. OF
66
100
150
200
250
300
Viscosity of 2-Octanol vs. Temperature
“T cpTsec ps1-cc
0.05112
0.05117
0.05124
0.05131
0.05138
0.05144
Pressure = 200 psig
A P
p s i
1.50
1.25
1.00
1.00
0.75
0.75
Q cc/sec
0.00725
0.01266
0.02222
0.04000
0.04494
0.0625
where aT. = .05113 1+2.67~10-~ (T-7O0F‘I]
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0 0 0 0 0 0 0 0 0 0 0 0 0 o o o o o o o c o o o o o 0 0 0 0 0 0 0 0 0 0 0 0 0 f f j f f f 3 f j f f f f
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m N N m m m N N m m N m N . . . . . . . . . . . . .
d o m o l - l F o m m ~ m w m m m m m o m m m a d m o a 3 f m N d 3 N m d d f N m r - i
0 0 0 0 0 0 0 0 0 0 0 0 0 . . . . . . . . . . . . .
m o w r l l n m a 3 a o o o d o m m l n N m f a , m f m N a l - 4 Nddr lC9C'Jddd2tmC'4N
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f c n L o r . 0 c o 0 m 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 o m c n m o c n o m o o o o o o o o o o o o o o o . . . . . . . . . . . . . . . . . . . e . . . f o m m f m f m f f ~ ~ f f f f f f f f f f f
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0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 d d r l r l 4 d m o m C Q o m
f w c n L n W ( r 1 0 03 m 3 c n m c o m c n c V C l m c n o m = l - c o b c o b c D m = t - m c n m O m b m b O o m b P J m o 0 0 0 d 0 0 0 0 0 d 0 0
0 0 0 0 0 0 0 0 0 0 0 0 . . . . . . . . . . . .
o o o o o o r l o o o o o 0 0 0 0 0 0 0 0 0 0 0 0
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9.2- 1-3 D e s c r i p t i o n : The Mass i l lon sands tone i s found
i n Holmes County, Ohio, and h a s been e x t e n s i v e l y q u a r r i e d
for a v a r i e t y of purposes . The s t o n e is medium-to-coarse .J
gra ined and i s composed m s t l y of q u a r t z g r a i n s , which are
subangular t o subrounded i n shape. The cementing materials
are i r o n o x i d e , c l a y m i n e r a l s , and secondary s i l ica . d'
Tests made for t h e Briar Hill Stone Company show t h a t
t h e s t o n e h a s a n a b s o r p t i o n of water of approximate ly 6 % b y
weight .
5000 p s i being abou t ave rage .
.J
The c r u s h i n g s t r e n g t h r a n g e s from 4000 t o 6000 p s i ,
The s t o n e weighs 135 pounds
p e r c u b i c foot . The average p e r m e a b i l i t y of t h e samples J
used i n t h i s s t u d y w a s 8 0 0 md, and t h e average p o r o s i t y about
2 2 % .
9 .2- 2 Uncons 'ol idated O t t a w a S i l i c a
9 . 2- 2- 1 P h y s i c a l P r o p e r t i e s
Core No. 1 4 1 5 1 6 1 7 1
Length, c m 5 .696 5.590 5.657 5 .894 J
Cross- Sec t iona l Area, c m 5 .067 5.067 5.067 5 . 0 6 7
mesh 1 mesh) m e s h ) mesh) Average Grain S i z e , mm ( 3 5- 4 5 (80- 100 (80- 100 (80- 100
3
9 .2 .2- 2 M i n e r a l o g i c a l Composition
S i l i c o n d i o x i d e ( S i O , )
Aluminum ox ide (A1203) I r o n oxide ( F e 2 0 3 )
T i tan ium d i o x i d e ( T i 0 2 ) Calcium oxide ( C a O )
Magnesium oxide (MgO)
Loss on I g n i t i o n (LO11
Weight %
99.806 0.047
0 .019
0.018 <o. 01 <0,01
0.09
3
4
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J
9.2- 2- 3 Desc r ip t ion : The O t t a w a sand used i n
t h i s s t u d y i s t h e No. 1 7 s i l i c a g rade and i s commercial ly
a v a i l a b l e from t h e O t t a w a D i v i s i o n , P a r k e r I n d u s t r i a l and
Foundry Supply , Rurlingame, C a l i f o r n i a . It i s more t h a n 9 9 %
weight q u a r t z and t h e g r a i n s are f a i r l y w e l l rounded. The
d i s t r i b u t i o n of g r a i n s i z e s i s as fo l lows:
U.S. Sieve N o .
40
50
7 0
1 0 0
1 4 0
2 0 0
2 7 0
Opening, !li l l imeter
0.420
0 .297
0 .210
0 . 1 4 9
0.105
0 .074
0 . 0 5 3
P e r c e n t Weight Re ta ined
8 . 1
44.5
28 .8
12 .7
4.4
1.1
0.2
The sand w a s s i e v e d and o n l y un i formly s i z e d g r a i n s w e m
used t o p r e p a r e a core f o r t h i s s tudy .
- 93 -
9 .3- 1 C a p i l l a r y Tube Viscometer: Because l i q u i d v i s -
c o s i t y d a t a ob ta ined from s u p p l i e r s are ave rage p roduc t q u a n t i -
t i e s and t h o s e from c o n v e n t i o n a l r e f e r e n c e s were n o t given at
high working t e m p e r a t u r e s , it was n e c e s s a r y t o de t e rmine v i s -
c o s i t y ve r sus t e m p e r a t u r e a t o p e r a t i n g pressures.
A c a p i l l a r y t ube v i scome te r , whose o v e r a l l l e n g t h w a s
62.875 inches and whose i n t e r n a l d i ame te r was 0.033 i n c h e s ,
w a s c o n s t r u c t e d f rom a 316
c o e f f i c i e n t of t h e r m a l expans ion w a s 8 .9 x
s t a i n l e s s s t e e l tube . The l i n e a r
in/in-OF.
The laminar f low o f l i q u i d s th rough c i r c u l a r c o n d u i t s
obeys P o i s e u i l l e ' s l a w :
4 rr Ap ' = 8pR
where q = f l o w r a t e , cc/sec; r = i n s i d e r a d i u s , cm; Ap =
p r e s s u r e drop , dynes/cm 2 ; ?J = l i q u i d v i s c o s i t y , p o i s e s , 2 =
l e n g t h of c a p i l l a r y , c m .
For r and R i n i n c h e s , Ap i n p s i , and i n cp u n i t s , Eq.
9- 1 becones:
and
4 7 r A 2 RP
q = 4 . 4 3 7 x 1 0
?J = 0 . 5 2 3 0 !& 9
( 9 - 2 )
(9-3)
Knowing t h e a c t u a l v a l u e of v i s c o s i t y a t 7OoF, and f r o m
measurements of p and q , t h e m u l t i p l y i n g c o n s t a n t w a s found
t o be 0.5113. The re fo re :
= 0 . 0 5 1 1 3 % ( 9 - 4 ) '70
-95-
J p, Ap (l+--) b
T h e r e f o r e , a graph of Y = Dm vs . x a (1+- b 1 ; & Pa 9, prn
shou ld y i e l d a s t r a i g h t l i n e of s lope rj and i n t e r c e p t E 1 , a
d
provided t h a t t h e va lue of b is known.
J
J
3
J
J
J
J
J
Eq . 9-10 was t h e working equa t ion for t h i s a p p a r a t u s .
The r e s u l t s a g r e e c l o s e l y w i t h t h o s e found i n t h e I n t e r n a t i o n a l
C r i t i c a l Tab le s . 3 9
9 . 3 - 2 V i s c o - I n e r t i a l Flow of G a s : The q u a d r a t i c equatbh
as proposed by Forchheimer and modified by C o r n e l l and Katz
(see re f s . 1 0 and 11) i s :
(9-11) 2 -8 = avq + BPq
for t h e case of v i s c o - i n e r t i a l flow o f gas . For v i s c o u s flea,
t h e q u a d r a t i c t e r m o f 9- 1 1 i s small enough t o be n e g l e c t e d ,
and a h a s t o be t h e r e c i p r o c a l o f p e r m e a b i l i t y , i . e . , Q = l / k .
The i n t e g r a t e d form of E q . 9- 1 1 f o r h o r i z o n t a l l i n e a r
flow i n t h e absence of s l i p p a g e i s :
1 b ' When t h e r e i s gas s l i p p a g e , a becomes
_I k (l+:) and s i m p l i f y i n g , b
Pm k(l+-
Replac ing a by
or Y = E + fix
- 97 -
A t t e m p e r a t u r e s , T , o t h e r t h a n room t e m p e r a t u r e , t h e
l e n g t h of t h e t u b e i s :
and
o r
rT 4 = r 7 0 ‘[l + B ( ~ - 7 0 1 1 ~
Because B , t h e l i n e a r c o e f f i c i e n t of t h e r m a l expans ion , i s
small, Eq. 9-7 can be approximated as:
4 4
‘T ‘70 ’T - = - r70 6 + 3 B ( T - 7 0 1 7
For t h e a p p a r a t u s :
= 0,05113 l l + 2 . 6 7 x (T-70)3 UT Q
There fo re , t h e v i s c o s i t y a t any t empera tu re is :
Where : aT = 0.05113ll t 2 . 6 7 x 10’’ ( T - 7 0 1 1
(9 -5 )
(9-6)
( 9 - 7 )
(9-9)
(9 -10)
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LIST OF YANUFACTURERS
The fo l lowing i s a l i s t of t h e v a r i o u s p i e c e s of equip-
ment or s u p p l i e s t h a t were used i n t h i s work, t o g e t h e r w i t h
t h e corresponding names of manufac ture rs and /o r s u p p l i e r s
from whom t h e y were a c q u i r e d .
Chevron White Minera l O i l N o . 3 - Van Waters E Rogers, I n c . San Franc isco .
P re s su re Transducers - Dynasciences Corp. , Model KP 1 5 , c/o Gaco Inst rument S a l e s , 655 Castro S t r e e t , S u i t e 2 , Mountain V i e w , C a . , 9 4 0 4 0 ( 9 6 1 - 2 2 2 2 ) .
B a r n e t t I n d u s t r i a l Dead Weight Tester - c/o Gaco Ins t rumen t Sales, 655 C a s t r o S t r e e t , S u i t e 2 , Mountain V i e w , C a . , 94040 ( 9 6 1 - 2 2 2 2 ) .
P r e s s u r e I n d i c a t o r - Pace Node1 CD 25, c / o Gaco Ins t rumen t Sales, 655 Castro S t r e e t , S u i t e 2 , Mountain V i e w , C a . , 9 4 0 4 0 ( 9 6 1 - 2 2 2 2 ) .
P r e s su re Regu la to r - Volumet r ics , Model VRC- 400 , 1 0 2 5 Arbor Vitae S t r e e t , Inglewood, C a . , 90301 ( 2 1 3 ) 6 4 1- 3 7 4 7 , o r c /o Gaco Ins t rument S a l e s , 6 5 5 Castro S t r e e t , S u i t e 2 , Foun ta in V i e w , C a . , 94040 ( 9 6 1 - 2 2 2 2 ) .
High P re s su re Regu la to r - Model 4-580, Matheson Gas P r o d u c t s , Newark, C a . (793-2559).
Va r i ab l e R a t e O i l Pump - Model PC, Whitey Tool E D i e Company, 3 6 7 9 Landregan Emvl., Oakland, C a , (653-51001, loan from USBM.
Hydraul ic Hand Pump - Enerpac, Model P-39, Pau l Monroc Hydrau l i c s , I nc . , 1 5 7 0 G i l b r e t h Road, Burlinganre, C a . , 9 4 0 1 0 (697-2950).
Constant R a t e Pump - Hand-made e q u i v a l e n t t o Ruska 2 2 0 0 series. Uses Viton 0 r i n g w i t h machined t e f l o n back -up . r ing .
Accumulators ( G r e e r o l a t o r ) , Model No. 20- 30 TMR-S-% WS, Hy- d r a u l i c C o n t r o l s , I nc . , 1330 6th S t . , Emervvi l l e , C a . , 94608 ( 6 5 8- 8 3 0 0 ) .
Recording Po ten t iome te r (for t empera tu re ) 3- Model Speedo Max v, Leeds E Northrup, 1 0 9 5 Market S t . , S a n Francisco, C a , (349-6656).
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Thermocouples - I r o n- C o n s t a n t a n , Conax, c /o I n s t r u m e n t Lab- o r a t o r y , 6 4 4 Emerson S t . , P a l o A l t o , C a . , 94303 (328-1040) .
Temperature C o n t r o l l e r - API Model 228 with 4010 Power P a c k , A P I I n s t r u m e n t s , 2339 Charleston Rd . , Mountain V i e w , Ca., 94040 (964-0512) .
L a b o r a t o r y F lowra tor K i t - Model No. 10A3565ALK2, F i s h e r E P o r t e r C o . , 1 3 4 1 North Main S t . , Walnut Creek, C a . , 94596 (933-8880) .
Core S l e e v e - V i t o n A t u b i n g , \?‘est American Rubber Co., 750 North Main S t . , Orange , Ca., 92668 (714-532-3355)-
0 !ings - Viton A w i t h t e f l o n back- up r i n g s , ABSCOA I n d u s- t r i e s , 880 B u r l i n g a m e Ave . , Redwood C i t y , C a . (369-4897) OR 1 0 7 1 W. Arbor Vitae S t . , Znglewood, C a . , (213- 7764561).
T u b i n - T u b e s a l e s , 500 Sansome S t . , S a n F r a n c i s c o , Ca. d l 9 1 9 ) .
F i t t i n g s E Valves - Van Dyke E F i t t i n g C o . , 5525 M a r s h a l St., O a k l a n d , C a . (658-1700) .
Gas Analyzer - Gas Master, Laboratory Model, GOW-MAC Ins t r tk - ment C o . , 1 0 0 Kings F.d., Mad i son , N . J . 07940 (201-377-34501 o r Appl ied Ins t rument C o . , 1 9 9 1s t S t r e e t , Los A l t o s (941-592k3).
Recording P o t e n t i o m e t e r ( f o r p r e s s u r e ) - Two pen m u l t i - r a n g e recorder , L e e d s and N o r t h r u p , BD-9, P.O. Box 634 , B e l m n t , C a . (593-8392) .
Alundum Core - N o r t o n Co., I C D , 2555 L a y a f e t t e S t . , S a n t a Clara, C a . 95050 (234-7710) .
Lapp P u l s a f e e d e r Pump - Model LS-20, 316SS, 1 / 6 hp, 94 Natoma S t . , S a n F r a n c i s c o , Ca. 94105 (391-7650) .
O t t a w a S i l i c a , No. 1 7 S i l i c a , P a r k e r I n d u s t r i a l and Foundry S u p p l y , 1 8 8 1 R o l l i n g Rd. , Burlingame, C a . , 94010 (697-8865) .
Massillon S a n d s t o n e - The Briar H i l l S t o n e C o . , Glenrnont , Ohio, 44628 (216-2764011) .
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10. NOMENCLATURE
E n g l i s h
A = area, c m 2
k = p e r m e a b i l i t y , md
L = l e n g t h of core , c m
p = p r e s s u r e , p s i
q = flow r a t e , cc/sec
w = flow r a t e , gm/sec
T = t e m p e r a t u r e , 0 K or OF
r = r a d i u s , c m
v = flow v e l o c i t y , cm/sec
G r e e k
p = d e n s i t y , gm/cc
u = v i s c o s i t y , c p
4 = p o r o s i t y , f r a c t i o n
A = i n c r e m e n t
Subscr i D t s
a = a t m o s p h e r i c c o n d i t i o n
c = c o r e or c o n f i n i n g
m = mean v a l u e
T = t e m p e r a t u r e
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