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o ID
-aj IITRI Project No. D6059
Semi-Annual Technical Report
EFFECT OF SPECIMEN SIZE ON CONFINED COMPRESSION TESTING OF ROCK CORES
for
Bureau of Mines Twin Cities, Minnesota
July 1971
Roproducod by
NATIONAL TECHNICAL INFORMATION SERVICE
Spnrmtiold Va 22151
IITRI Project No. D6059
Semi-Annual Technical Report
EFFECT OF SPECIMEN SIZE ON CONFINED COMPRESSION TESTING OF ROCK CORES
for
Bureau of Mines Twin Cities, Minnesota
July 1971
D D C lnp^rn ffl
C
IIT RESEARCH INSTITUTE Technology Center
Chicago, Illinois 60616
IITRI Project No. D6059
Semi-Annual Technical Report
EFFECT OF SPECIMEN SIZE ON CONFINED
COMPRESSION TESTING OF ROCK CORES
by
Peter Jay Huck Madan M. Singh
Monitored by
Bureau of Mines U. S. Department of the Interior
Twin Cities, Minnesota
Sponsored by
Advanced Research Projects Agency Washington, D.C.
July 1971
>D D C^
SEP tZ 1971
ESEITU'El c
The views and conclusions contained in this document are those of the authors and should not be interpreted as necessarily representing the official policies, either expressed or implied of the Advanced Research Projects Agency, Bureau of Mines, or the U. S. Government.
" Dir-TRIEUTION STATEMENT A f __._ i— <' ?'
Approved hr public releotM}
FOREWORD
This is the semi-ar.nual report on IIT Research Institute
(IITRI) Project No. D6059, entitled, "Effect of Specimen Size
on Confined Compressicn Testing of Rock Cores" co ;=ring the
work period 29 December 1970 to 15 July 1971. This program is
being performed under Contract No. H02100Ö9 with the Bureau
of Mines of the U. S. Department of the Interior, with Mr. Egons
R. Podnieks of the Twin Cities Mining Research Center acting
as technical monitor. The program is being spenscred by the
Advanced Research Projects Agency of the U. S. Department of
Defense under ARPA order no. 1579, Amendment 2.
The project is being conducted jr.der the direct s ;per
vision of Dr. Madan M. Singh, who is tcrvlng as pcrgram manager,
Mr. Peter J. Huck is project engineer. Othsr TITRI staff
members contributing to the overall research effort include
Drs. R. H. Cornish and A. Semmelink; and Messrs. L, A, Finlaysc
P. A. Hettich, E. J„ Smithy J. Vosatka a-d A Wa^r iz -
Respettf-'.l s r-nr.ltted
IIT RESEARCH INSTIT' TE
Madan M. Si->- M.» v r Soil a-d Re. K Mi : .A U I
APPROVED:
HO»* R. H. Cornish Director of Research Mechanics of Materials Di rltic:
MMS/bk
IIT RESEARCH INSTITUTE
i
IITRI PROJECT NO. D6059
Semi-Annual Technical Report
(Covering the Period 29 December 1970 to 31 July 1970)
Sponsored by
Advanced Research Projects Agency
ARPA Order No.;
Program Code Number;
Contract No.;
Title of Work;
Name of Contractor;
Effective Date of Contract;
Contract Expiration Date;
Amount of Contract;
Principal Investigator and Phone No.;
Project Engineer and Phone No.;
ARPA 1579, Amendment 2
1F10
H0210009
Effect of Specimen Size on Confined Compression Testing of Rock Cores
IIT Research Institute 10 West 35th Street Chicago, Illinois 60616
29 December 1970
29 January 1972
$75,791
Madan M. Singh AC312/225-9630 Ext 4784, 4785
Peter J. Huck AC312/225-9630 Ext 4735
Experimental Apparatus
Four sizes of rock cores are to be Investigated In this
program. Each core size was tested In a different pressure
cell. The specimen dimensions and pertinent pressure chamber
specifications are listed below:
IIT RESEARCH INSTITUTE
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Specimen Dia.(in.)
Specimen Length(in.)
Chamber I.D.(in.)
Chamber Pressure Rating(ksi)
Maximum Rated Axial Load(lb.)
2.06 4 4.0 30 375,000
3.65 7 6.5 30 995,000
12 24 14.7 20 3,400,000
32 or 36 60 48.3 20 axial 10 confining
36,500,000
To date only two (2) 2-in. diameter specimens have been subjected
to triaxial pressure. The other cores have already been prepared
and gaged. The apparatus for the tests has also been set up.
The test data should become available in the near future.
Prior to testing the rock cores triaxially, the
cylindrical specimens were tested acoustically to map out any
major variations in acoustic velocity through them.
Triaxial Cells
Each triaxial cell consists of a thick-walled pressure
chamber with a honed interior in which a floating piston moves.
A typical arrangement is depicted in Figure 1. The triaxial
cell for the 2-in. dia. specimens carries a spherical seat
between the piston and the specimen. Because of size restrictions,
spherical seats are not used in the larger specimens. Instead,
all pistons are provided with special high compliance seal rings
that allow the pistons to rotate to conform to the rock specimens.
A capping platen covers the top of the core, with a chamber closure
above it to hold the assembly in place. The strain gage leads
from the rock core and are led through this closure to the data
acquisition system. The confining pressure is introduced around
the jacketed core, while the axial load is applied by pumping
oil below the sliding piston. This scheme for applying axial
pressure eliminates the need for a large separate loading machine,
and can withstand fairly high loads, depending on pressure cell
design.
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Chamber Closure with Instrumentation Lead- Out
Confining Pressure Region
Test Specimen
Sliding Piston with Loading Blocks
Axial Pressure Region
FIG. 1 TYPICAL TRIAXIAL CELL SCHEMATIC
The axial stress In the rock depends upon the ratio
of the rock and piston areas and the difference in the confining
pressure and the axial chamber pressure. The specimen stresses
are given by the following equations:
a2 - 03 - P3
At ^1 - (prp3) xl 0]_ - Ö3 + AOj^
where»
A_ - piston area P A - specimen area
P, ■ axial chamber pressure
Po ■ confining chamber pressure
Aa. ■ deviator stress
a,, 02 and Q« - principal stresses.
Reference to Fig. 1 and the above equations confirms that
if P, - P«, Ao- - 0 and the specimen is under hydrostatic
stress (a, - a« ■ o^). For P« - 0, the specimen is unconfined,
with Oj - a3 - 0 and «^ - ^a^ - p^^ A /Ar.
The 4 in., 6 in., and 14 in. dia. pressure chambers
are incorporated into a central control panel and instrumentation
system and are operated by a common pumping system. A schematic
of this layout is given in Fig. 2.
In each of the tests to be performed in this program
the rock core is loaded hydrostatically up to the predetermined
confining pressure, and then the axial pressure is increased
gradually to the desired value. It is planned to run at least
one load-unload-reload cycle on each specimen. During the
reload the axial stress is increased until the core fails or
the capacity of the cell is attained, whichever is lower.
NT RESEARCH INSTITUTE
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Cross-connections have been provided between the confining
and axial pressure sections of the cells, to obtain true
hydrostatic loading during the hydrostatic phase of each
experiment.
Large Pressure Chamber
Because of the unique design of the 48-In. diameter
pressure vessel, it deserves separate discussion in this
report. Detailed descriptions of the design and chamber may 12 be found elsewhere ' . A schematic of the vessel layout is
depicted in Figure 3, and a photograph of it is shown in
Figure 4. Essentially the vessel is comprised of a 48-in.
I.D., 86-in. working length hollow cylinder capable of with-
standing 20,000 psi internal static pressure. The ends of
this hollow chamber can be closed with steel plugs, which
react against a flexible frame built up of strap steel. The
cylindrical chamber walls consist of 12-in. long, 13 1/2 in. thick
steel rings, placed end to end and held together by a single
3/4 in. thick steel liner along the inside diameter. The
reaction structure consists of a basic frame held together by
steel strap wrapped around it. The entire vessel weighs
140 tons, which is substantially less than conventionally
designed chambers having the same capabilities. The cell can
withstand axial loads of over 36 x 10 lb.
The pumping and control systems for this unit are
simpler than those for the smaller chambers. A separate
pump is used at each end of the chamber, as is seen in the
schematic in Figure 5. Accumulators are not used because the
chamber volume itself is large in comparison with other
available pressure chambers.
The operation of this chamber is similar to that of
the smaller chambers, except that the turn-around time between
tests is on the order of a week Instead of an hour. The
tests in this chamber differed slightly from those in the IIT RESEARCH INSTITUTE
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Details of illustrations in this document may be better
I Ftg. 4 PHOTOGRAPH OF 48" PRESSURE CHAMBER
8
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a
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r smaller test cells. In order to maintain seal Integrity, a
positive pressure differential of about 200 psl will be maintained
across the sliding piston during the "hydrostatic" portions
of the trlaxlal tests, and the axial pressure will not be allowed
to drop below 400 psl at the bottom of the load-unload-reload
cycle. If the&e precautions are not taken, there would have
been danger of upsetting the piston seal, thus aborting the
remainder of the test.
Specimen Reparation
The 12-In. and 32-in. dla. cores of Charcoal Black
gvanlte were obtained from the Cold Spring Granite Company,
Cold Spring, Minnesota, and the 12-lno and 36-in. dla. specimens
of Indiana limestone were ordered from Rechal Stone Co., Glen-
view, Illinois. These specimens required no further preparation.
Extra rock was ordered with each of the two types, so as to
permit coring of the 2-in. and 4-in. dla. specimens. The smaller
cores were cut parallel to the axis of the larger cores so as
not to Introduce complications due to anlsotropy. One direction
along all the cores of Indiana limestone were marked at the
quarry. It was also marked on the cores drilled In the laboratory.
End preparation of the 2-ln. and 4-in. dla. cores
consisted of facing on a lathe until the ends were plane and
parallel to 0.001 Inches. The larger cores will be capped in
a specimen cage to permit handling. The capping material tc be
used Is a steel-filled epoxy. The cage, tie rods were designed
with end fittings that would accept tensile load only. Since
the maximum tensile load that could be applied to the cage by
these tie roads corresponds to 30 psl compressIce stress in
the rock specimen, the effect of the cage on the rock will
be negligible.
An airay of foil strain gages have been mounted on each
specimen. The number used ranged from three resettes on the
2-ln. cores to thirty rosettes on the 32-ln. cores. These were
lir RISEARCH INSTITUTE
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two element rosettes with 1/4 in. gage length placed with the
direction of rolling parallel to the specimen axis. The gage
placement procedure included the following steps:
grind the rock surface
* apply two thin coats of gage cement
JL,
visually inspect for voids in the cement
base
it affix and wire gages
apply two coats of gage cement for water proofing
check gage for continuity and response (soft eraser) and replace if necessary.
The instrumented cores will be waterproofed with latex
cement over the foil gages, and at least two coats of latex
paint with a thickening agent over the entire rock surface.
Waterproofing is very important in a triaxial test since
both the loading conditions and the character of the rock
can be changed by intrusion of oil into the rock voids. In
those tests where the specimens can not be loaded to failure
on the second load cycle, the specimen will be recovered
intact and stripped of paint for visual inspection.
Instrumentation and Data Reduction
The foil strain gage on the rock specimen provide the
mechanical properties information required in this project.
These gages are driven by a bank of bridge balance units, wired
to provide temperature and pressure compensation for the leads.
Temperature gages are provided in the chamber adjacent to the
rock specimens to monitor environmental temperature. The data
are recorded by a Hewlett-Packard series 2012 data acquisition
system that scans all data channels on demand, printing the
IIT RESEARCH INSTITUTE
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voltages on paper tape. As the data system scans the strain
gages, the axial and confining pressures are read on Heise
bourdon gages, and these readings are manually Inserted on
the printed data system output.
Data reduction Is performed using lITRI's Unlvac 1108
computer. The printed data system output Is keypunched and
Input In an editing program. This program reads all the raw
data and prints It out In a convenient array for checking.
This program also plots the strain data so that any keypunching
errors or bad strain readings can easily be found and corrected,
After the data has been checked In Che editing program It Is
Input In an analysis program. This program solves the strain-
gage bridge equation Individually for each gage, and computes
the elastic moduli. The reduced data are printed out, and
the following computer plots are provided:
• devlator stress vs. shear strain
• volumetric stress vs. mean stress
• axial and radial strain vs. axial stress
• bulk, shear and elastic moduli vs. mean
stress.
These plots will be Included in an appendix to the final
report as the most meaningful and convenient method for
presenting the experimental data. Finally, the reduced stress
and strain data are punched by the computer to provide ready
access to the data for further analysis and model fitting.
Nondestructive Test Program
A series of nondestructive tests was planned for all
specimens in order to measure any anisotropy and to locate
any inhomogenelties in the larger specimens. These tests
Included Schmidt hammer. Shore scleroscope and dilatational
wave velocity. These tests are now complete with the exception
of the 12-in. dia granite specimens.
IIT RESEARCH INSTITUTE
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Schmidt Hammer
Schmidt hammer readings were taken at each gage
location, with the following exceptions. The 32-in. dia
and 36-in. dia cores were tested at every second gage location,
for a total of 18 tests on each core, and the 3-in. dia and
4-in. dia cores were tested on the ends only. The readings
on the small cores was strongly influenced by the boundary
conditions on the side of the specimen opposite the hammer
impact because of the small core diameter. After experimenting
with various seating and clamping arrangements, it was decided
to conduct these tests along the longest core dimension
available. Each Schmidt hammer test consisted of 8 readings,
the first 3 of which were discarded and the last b of which were averaged to give the Schmidt hammer value at that
location. This procedure is necessary because of local crushing
that occurs during the first few impacts at a point.
The Schmidt hammer data is summarized in Table 1.
Note that the values for the 2-in. dia cores is low in both
cases. This is attributed to the small specimen size,
rather than any actual difference in character. The numbers
in parenthesis are grand means excluding the 2-in. dia specimens,
and represent the best overall values for the two rock types.
Shore Scleroscope
The Shore scleroscope indicates hardness by the
measuring rebound of a small diamond tipped striker dropped
on the rock. A test consists of 10 readings taken near a
single point. The instrument is moved approximately 0.1 in.
between readings so the striker does not fall in the small
conical depression left by a previous reading. In granite,
the scleroscope reading depends strongly upon the type of
grain impacted. Tests were conducted near alternate gage
locations on the 12-in., 32-in., and 36-in. dia specimens,
and at all gage locations on the small cores. The results IIT RESEARCH INSTITUTE
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Table 1 SCHMIDT HAMMER SUMMARY
Indiana Limestone Charcoal Black Granite
Core Dla. Mean Number Mean Number
2 in. 24 24 35 14
! 4 in. 28 10 48 10 j
| 12 in. 28 90 - -
36 in. (32 in.) 30 54 50 54
1 All Specimens 28
(29)*
178
(154)
47
(49)
78
(64)
Parenthesis indicates 2 in. dia specimens exluded from mean.
IIT RESEARCH INSTITUTE
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are tabulated In Table 2. An Indication of the scatter Involved
Is shown in Figure 6, which is a histogram of the 54 individual
readings taken on the three 36-in. dia limestone specimens.
Acoustic Velocity Mapping
The velocity of the dilatational wave was measured at
all gage locations on all cores (with the exception of the 12-in.
dia cores which are not yet tested). The system used for the
small cores is shown in Fig. 7A. The input signal is a single
cycle square wave. This is amplified and used to drive a 1 MHz
piezoelectric transmitting transducer. The signal transmitted
through the rock is received by a similar transducer and displayed
on a dual beam oscilloscope through an internal variable delay
line. This signal is compared with the input signal, and the
variable delay line adjusted to achieve coincidence. The elapse
time is then read from the delay line. The system delay is easily
measured by removing the rock specimen and placing the transducers
face to face. Figure 7B shows the system used for the 32-in. and
36-in. dia cores. A mechanical delay line was introduced to allow
the use of rapid sweep rates, and a preamp boosted the received
signal. The operating frequency ranged from 300 kHz for the
large cores to 1 MHz for the small specimens. A check was made
to determine if the frequency response of the rock influenced
the apparent time of arrival by making measurements on a single
2-in. dia specimen at frequencies between 10 kHz and 2 MHz.
The results are plotted in Fig. 8, and indicate no variation in
time of arrival across the entire frequency range. The amplitude
of the received signal is, of course, strongly dependent on input
frequency.
The anisotropy of the Indiana limestone was investigated
by evaluating the three 36-in. dia cores. The 45 individual
acoustic velocity tests on these cores had a mean value of 4.021
km/sec, with 957. confidence levels at + 0.017 km/sec and a
standard deviation of 0.058 km/sec. This value of 4.021 +
MT RESEARCH INSTITUTE
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Table 2 SHORE SCLEROSCOPE SUMMARY
Indiana Limestcr.e. Chare:al B: .ack Granite
Core Dia. Hear. Nw.tr.:: er Mean Number
I 2 in. 12 36 6-* 21 1
| 4 in. 15 30 83 15
12 in. 14 45 - -
32 in. (36 In.) 14 54 75 54
All Specimens 14 165 74 90 |
IIT RESEARCH INSTITUTE
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Oscilloscope
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Fig. 7A ACOUSTIC VELOCITY SYSTEM FOR SMALL CORES
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Fig. 7B ACOUSTIC VELOCITY SYSTEM FOR LARGE CORES
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0.017 km/sec is taken as the acoustic velocity in Indiana
limestone. These 45 readings may be separated into 3 groups
of 15 readings, each group spaced at 60 degree intervals
around the axis of the core, or as 5 groups of 9 readings,
each group spaced at 10 in. intervals down the length of the
core. In this fashion we can consider the variation in acoustic
velocity as a function of direction in the horizontal plane,
or as a function of the vertical depth in the bedding plane.
This nonemclature, and the variation of acoustic velocities as
a function of direction and depth are indicated in Figure 9.
Note that in all cases, the 95% confidence levels for the
individual subgroups include the mean value of 4.021 km/sec
computed for the entire 45 reading group.
Looking at the variation of acoustic velocity, it appears
that the maximum velocity would be measured along a diameter
between 2-5 and 3-6, along a quarry bearing of N-80o-W, and
the lowest velocity would lie along a bearing of N-10o-E. The
maximum variation is on the order of 1 1/2 percent of the mean
value. Considering the variation of acoustic velocity with
depth, there may exist a trend of increasing velocity with
depth. The slight reversal of this trend at row #5 may be a
real effect caused by the presence of the bedding plane in the
formation. In any case, the variation is on the order of 1%
or less. The acoustic velocities for all subgroups lie near
or within the 957« confidence levels for the entire group of
measurements.
Unconfined Compression Tests
Unconfined compression tests were conducted on three
specimens each of Indiana limestone and Charcoal Black
granite. These specimens were instrumented and the following
plots are included as an appendix to this report:
deviator stress vs. shear strain
mean stress vs. volumetric strain
NT RESEARCH INSTITUTE
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Specimen Orientation and Array of Measurement Locations
1 —
u
•2 3
2 —
I r 5 —
4
^4.05 r- I ^•4.00
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4-—4- s -J -1 4.021 + 0. 017
T^ T? 3^ Direction of Measurement (column to column)
SU.05
4.021 + 0.017
<u >
12 3 4 5
Depth of Measurement (row number)
Fig. 9 ACOUSTIC VELOCITIES IN 36-IN. DIA INDIANA LIMESTONE
21
axial stress vs. axial and lateral strains
The failure stresses for the individual tests are indicated
in Table 3.
The orientation directions of the 32-in. dia and 12-in.
dia Charcoal Black granite cores were not marked by the quarry.
In all, 102 acoustic velocity determinations were made on the
2-in., 4-in. and 32-in. dia granite specimens These tests
had a mean value of 4.661 km/sec with 957» confidence levels
of + 0.047 km/sec with 95% confidence levels of + 0 047 km/sec
and a standard deviation of 0.240 km/sec. The value 4.661 +
0.047 km/sec is taken as the acoustic velocity in Charcoal
Black granite. Additional insight into anisotropy can be
gained by evaluating the acoustic data from the 2-in. dia
and 4-in. dia cores, which were cut at IITRI from a single
piece of granite, and were orientated with respect to an
arbitrary direction marked on the parent core. This evaluation
will be carried out in the future.
Triaxial Tests
Triaxial tests at confining pressures of 2000 psi
and 4000 psi were conducted on Indiana limestone. These
data have been keypunched, but not yet run on the data
reduction program.
NT RESEARCH INSTITUTE
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Table. 3 UNCONFINED COMPRESSIVE STRENGTH
Gran ita Limes tone
Test Failura Stress Test Failure Stress
14
15
17
17.4 ksi
23.1 ksi
18.2 ksi
20
21
22
4.18 ksi
4.38 ksi |
4.00 ksi
Mean 19.5 ksi Mean 4.19 ksi |
The data reduction for the unconfined tests is identical with that
which will be used for the triaxial tests.
MT RESEARCH INSTITUTE
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REFERENCES
1. Finlayson, L. A., Large Segmented High Pressure Chamber
Design, IITRI Internal Report dated March 4, 1970, p. 9.
2. Cornish, R. K. and Finlaysonj L. A., Reaction Frame for
Restraining High Loads, U. S. Patent No. 3,476,281,
Issued November 4, 1969, p. 4.
NT RESEARCH I JSTITUTE
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APPENDIX
Data from Unconfined Compression Tests
The plotted output for the six unconfined compression
tests is included or. the following pages. Each test includes
the following plots:
deviator stress vs. shear strain
mean stress vs. volumetric strain
axial stress vs. axial and lateral strains
The pertinent identification data are noted on each plot.
IIT RESEARCH INSTITUTE
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