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In-Place
Testing of CMU Walls
Another Alternative
Introduction
One of the fundamental
assumptions used for the design of masonry is that
each component including block, mortar, and
grout combines to create one homogeneous
unit. This assumption is especially important when
considering lateral loads and flexural moments in a
direction perpendicular to the wall. For most
codes, this homogenous condition is assumed to
occur as a product of good quality assurance
measures, which typically include visual inspection
of the block and reinforcement layout, clean and
adequate grout spaces, good consolidation
practices, and testing of either assembled prisms
or individual components by the unit strength
method.
For those projects that must
conform to the State Chapters of the
California Building Code, additional testing on the
finished masonry member is required to verify
in-place compressive strength, and that adequate
bond or shear strength has developed between the
inside face of the masonry unit shell and the
grouted interior.
The following article has
been written to share some recent experiences on
these supplemental testing requirements
particularly as they relate to determining actual
in-place shear capacity. It also discusses the
development of an alternative on-site testing
procedure that was ultimately used to assess the
behavior of a typical wall segment where
traditional testing procedures yielded unacceptable
results.
Overview of Masonry Cores
and Shear/Bond Strength
As mentioned above, projects
governed by the State Chapters of the
CBC require the testing of samples taken from
finished masonry components in addition to the
testing of sampled materials or prisms taken during
wall construction. Specifically, it requires that
at least two 6 cores be taken for each 5,000
square feet of floor or wall area with one core
tested in compression, while the other core is
tested in shear. Samples are generally taken by the
special inspection agency 28 days after walls are
completed at locations without horizontal or
vertical reinforcing. Where tested in shear,
samples must achieve a shear-strength of 2.5
Ö
fc across the section.
Figures 1 and 2 illustrate
the typical method of sampling cores and the
guillotine apparatus generally used to perform the
shear tests. The intent of these tests is to verify
that the finished wall can achieve the compression
strength assumed during design and that an
appropriate couple or moment capacity can be
developed between the reinforcing steel and
compression face of the block during flexural
loading conditions. Note that with the guillotine
test, the apparatus loads the specimen in opposing
directions at the interface of the shell and grout
zone, essentially measuring bond strength across
this joint.
Figure 3 depicts the
traditional stress distribution and force couple
assumed for the design of concrete or masonry
members, where the ultimate strength design
approach is used. For this particular example, the
assumed compression zone extends past the width of
the face shell and engages a portion of the
interior grout. Depending upon the quantity of
steel reinforcing and block strength, this
compression zone may fall entirely within the width
of the face shell. In either case, composite action
and development of the steel reinforcing can only
occur where adequate resistance to shear flow
occurs between the inside face of the block and
grout. This requirement for bond is similar to that
of adjacent wood sections in glue laminated beams
or the use of headed anchor studs to create
composite action across the interface of a steel
beam and concrete on metal deck. For the case of a
masonry member, the critical section is the natural
joint at the face-shell grout interface as noted in
Figure 3.
Deciphering Poor Test
Results
While the core tests required
by California State Amendments provide a good
indication of wall integrity, the method of
sampling and their results are often the subject of
some uncertainty. For example, one half of all
cores taken through the wall surface are ultimately
tested for compression in a direction perpendicular
to actual field conditions and would appear to
neglect the individual compressive strain
characteristics of the block, mortar and grout.
Where initial test results in
compression prove to be unacceptable, another
alternative may be to saw cut one or two full block
course out of the existing wall and test it in
compression. Although somewhat more time consuming
and destructive, this approach yields a sample that
better represents actual field conditions.
Cores taken through walls can
also be compromised during the extraction process
due to dull blades, improper setup or excessive
vibration in the coring machine. All of these
factors could compromise the samples and are most
significant where the samples are eventually tested
in shear. Where initial tests results are poor,
these factors should be investigated and corrected
for any subsequent testing.
Poor Results and
Additional Testing
Where initial test procedures
produce unacceptable test results, additional
testing is often required. Since no specific
guidance is given within the California Building
Code for this re-testing, the Engineer of Record
and the Governing Agency must exercise some
judgment.
Similar to the procedure used
to investigate low concrete strength, and as
specified in Chapter 19 of the CBC, supplemental
testing could include three additional masonry
cores taken at areas adjacent to any location with
poor initial test results. As a general rule of
thumb, the test values are often combined and
results noted as acceptable if the average of these
tests are greater than the required compression or
shear strength and if no single test capacity falls
below 75% of the specified value.
Where tests continue to be
poor, other alternatives may be investigated. Where
inadequate shear capacities are the problem, one
option could include the re-evaluation of the block
wall neglecting the contribution of the face shell
under flexural loads and possibly assuming some
degree of fixity at either the footing or
subsequent floors. A more costly option could be to
provide an external buttress system to limited
flexural moments within the wall. Where these
options do not work or are too disruptive, the
engineer may want to consider an in-place testing
method as described below.
Figure 1
Coring for Wall Sample

Figure 2
Testing with Guillotine Apparatus

Figure 3
Assumed Stress Distribution and Force
Couple
On-Site Testing-Case
Study
As noted above, it is not
uncommon to have several cores that exhibit poor
grout-to-face shell bonds during testing or samples
where the face shell completely separates during
extraction. Some publications actually suggest that
this percentage may be up to 33% for all samples
taken. This percentage may include those samples
where the face shells separate during extraction
and those with low shear results when tested. The
question becomes, when is this percentage excessive
and an indicator that the block-grout bond may have
been compromised due to poor grout quality,
excessive material shrinkage or poor consolidation?
On one recent project,
initial failure rates due to either low shear test
results or complete face shell separation during
the extraction process were approximately 47%.
Areas exhibiting poor test results were then
re-tested with a minimum of three carefully
extracted cores and the results averaged.
Unfortunately, failure rates remained close to 33%
with many samples continuing to experience a
complete face shell separation during the
extraction process.
Based upon the results, it
became obvious that the grout had failed to
adequately bond to the CMU at many locations
raising concern over the walls ability to
adequately carry future flexural loads.
Interestingly, virtually every core tested in
compression exhibited acceptable strength when
compared to expected values. Shear test results
were also consistently poor on one particular side
of a wall versus the other and generally exhibited
very high values on the opposite face. This
phenomenon occurred consistently throughout
virtually every building constructed during the
same time period and prompted a great degree of
speculation. Suggestions for this condition
included greater sun exposure on one side of the
wall versus the other, the effects of hot weather,
poor consolidation, excessive mix shrinkage, poor
water quality, and the possible adverse effects of
the admixture, which was required to reduce early
water loss and to provide expansive action to
counteract initial mix shrinkage.
Data
Examination
Although the high degree of
poor test results clearly indicated that a less
than desirable bond had occurred between the inside
face of CMU and the grouted interior, the degree to
which this poor bonding affected the overall
flexural capacity was not fully known. It was
recognized that core samples taken at isolated
locations account for only a miniscule fraction of
the total bond area that would be engaged under
flexural loading conditions and that significant
bonding at only some areas would most likely be
sufficient to create full composite action and
development of the reinforcing steel. It was also
noted that the natural extension of the web across
this possible weakened plane also aided in the
flexural development of the entire wall section,
although initial calculations indicated that the
capacity was not entirely sufficient. Under
flexural deformations, it also seemed reasonable to
assume that some degree of aggregate interlocking
would occur, also aiding the development of the
composite section.
Regardless of the suspicions
that the walls might perform favorably, the high
rate of failed tests together with the fact that
these poor results were generally present on one
side, could not be ignored. After extensive
evaluation of all data, the position taken by the
EOR was that the walls must be tested by a
different procedure so that the actual flexural
strength under field conditions could be
determined.
Evaluation
Intent/Goals
Once an in place testing was
agreed upon by all parties, a protocol document was
developed so that the intent and applicability of
the testing procedure could be reviewed by all
parties. As a guideline, this protocol document was
written to be in general conformance with ASTM E
72-98 Standard Test Methods of Conducting
Strength Tests of Panels for Building
Construction.
The basic goal of the test
was to capture the actual load-deflection
characteristics of the wall under incremental
static loading. Of particular interest, was the
development of a load-deflection curve, where
distinct limit states such as the cracking, yield,
and ultimate moment capacities could be plotted and
compared to expected values based upon assumptions
of full composite action.
Since these walls were part
of the lateral-force resisting system, the ability
of sections to continue to carry full moment
capacity at large displacement was also of
interest. As such, good wall ductility was another
criteria required for acceptable wall performance.
Test
Specimen
Due to the time and expense
involved for the proposed testing process, a single
wall was chosen for evaluation purposes. The wall
chosen was adjacent to several locations where at
least 5 previous test cores had indicated
unacceptable face shell grout bond properties. The
direction of loading for the wall was also chosen
such that the side experiencing all unacceptable
test results would be subject to compression during
loading.
To simplify evaluation of the
final data, it became clear that the fixity both at
the wall base and second floor level would
significantly stiffen the wall and make evaluation
and comparison of distinct limit states more
difficult. As such, it was decided to physically
separate a section of wall on all four sides and
construct an apparatus that would develop an almost
perfect-pinned condition at both the top and bottom
of the wall.
Figure 4 below illustrates a
section of the wall tested. Actual test results for
mortar, block and grout were also reviewed to
ensure these assumed material strengths were
reasonable. A pacometer was also used to verify
reinforcing layout was as expected. Material
properties assumed for the wall are also listed
below:
fm= 1,500 psi, Es=
29,000 ksi, Em = 1,125 ksi
fy = 60,000 psi,
Mortar: Type S (1,900 psi)
Grout: 2,000 psi.
Figure 4
Test Specimen
Test
Apparatus
The test apparatus used to
support and load the wall consisted of a pair of
vertical frames constructed from steel wide flange
beams, tube sections, and channels. The frame was
designed with significant stiffness and utilized
both slip-critical bolted or welded connections to
ensure that relative deflection within the fame was
not significant. A timber wall was also included at
the back of the apparatus to support the air bag
used for loading.
Figures 5 and 6 illustrate
the supports used at the top and bottom of the
wall. The top connection was designed to allow
rotation, as well as accommodate vertical slip. The
bottom connection was also designed to allow
rotation, but was restrained vertically and carried
the complete weight of the wall. Once the test
assembly was fully constructed and the bottom
connection completely intact, a 2-inch section was
cut away from the bottom of the wall. This ensured
that the wall was completely supported at the
bottom bracket and allowed free rotation.
Figure 5
Connection at Base of Test Specimen

Figure 6
Connection at Top of Test
Specimen
Test Instrumentation,
Loading, and Observations
The test was conducted on
site with the assistance of a qualified special
inspection agency experienced with similar tests
conducted within a lab environment. After the frame
was in place, the wall was loaded with a 4 x
8 air bag in accordance with ASTM E 72-02, so
that a uniform pressure was achieved over a portion
of the wall. This produced a pattern of loading
that was close to expected under seismic conditions
and one that was reasonably achieved under field
conditions. One major goal was to apply a pattern
of load that could be easily equated to applied
moments with each change in wall
pressure.
Instrumentation
Horizontal out-of-plane
deflection of the wall was measured at the top,
bottom and midpoint mid-height of the wall by use
of LVDT (Linear Variable Differential Transformer)
devices. Manual gages were also placed at the
mid-height of the wall to provide an additional
check. Data will be instantaneously captured by a
data acquisition system. All gages were capable of
measuring horizontal deflections to within 0.01
inch (0.25 mm) and were supported independently
from the test frame and the wall to ensure that
actual wall deflections were appropriately
captured. Pressure within the air bag was measured
by a manometer.
A Data Acquisition System
(DAS) was used to collect and store instantaneous
input and output data. Input data is the applied
uniformly distributed load (pressure) and output is
the deflections. The advantage of a DAS was that
the data was stored without mechanical means and
that the graph could be plotted during the course
of the testing.
Loading
Out-of-plane loading of the
wall panel specimen was achieved by pressurizing a
rubberized airbag in contact with the face of the
wall in increments of .05 psi (7.2 psf).
Displacements and corresponding loads were
automatically recorded in equal time increments up
to the end of the test.
Since the air bag could not
cover the entire height of the wall, simple
formulas were developed to equate applied loading
with corresponding internal moments and shear
forces based upon simply supported beam theory and
partial uniform loading. Figure 7 below indicated
this relationship. These formulas were used to
convert applied pressure into approximate wall
moments so that they could be plotted against wall
displacements.
Figure 7
Simplified Shear and Moment Diagram
Other Test
Observations
Crack and distress patterns
on the backside of the test wall panel were also
noted and recorded at periodic loading increments.
The side in contact with the airbag was also
examined at several stages during the test and
after the test was completed to note any cracks or
spalling. Upon completion of the test, final
observations were made, which included all visible
crack patterns, the approximate airbag contact area
and residual wall deflections taken up to a week
after the test was completed. Exact reinforcing
layout was also confirmed by destructive methods.
Other Test
Observations
Crack and distress patterns
on the backside of the test wall panel were also
noted and recorded at periodic loading increments.
The side in contact with the airbag was also
examined at several stages during the test and
after the test was completed to note any cracks or
spalling. Upon completion of the test, final
observations were made, which included all visible
crack patterns, the approximate airbag contact area
and residual wall deflections taken up to a week
after the test was completed. Exact reinforcing
layout was also confirmed by destructive methods.
Test
Results/Discussion
As previously noted, the
basic goal of the test was to capture the actual
load-deflection characteristics of the wall under
incremental static loading and compare these
results to those that would be expected based upon
general engineering principals, assuming a full
composite section. Of particular interest, was the
comparison of cracking, yield, and ultimate moment
capacities, as well as overall wall ductility.
Attention was also given to any indication of any
premature bond slip between the face shell and the
grouted interior and to all cracking patterns which
developed.
Comparison of
load-Deflection Data
Actual load-Deflection data
for the wall tested is presented below in Figure 8
and consists of a plot of Recorded Mid-Height
Displacement Data and Effective
Mid-Height Displacement Data. The second plot
is provided to account for the decreasing contact
area between the air bag and the back of the wall,
which became noticeable after about 2 of
recorded deflection. This second plot has been
interpolated from the original data based upon
measurements of the actual bag contact area during
the test.
Test
Results/Discussion
As previously noted, the
basic goal of the test was to capture the actual
load-deflection characteristics of the wall under
incremental static loading and compare these
results to those that would be expected based upon
general engineering principals, assuming a full
composite section. Of particular interest, was the
comparison of cracking, yield, and ultimate moment
capacities, as well as overall wall ductility.
Attention was also given to any indication of any
premature bond slip between the face shell and the
grouted interior and to all cracking patterns which
developed.
Comparison of
load-Deflection Data
Actual load-Deflection data
for the wall tested is presented below in Figure 8
and consists of a plot of Recorded Mid-Height
Displacement Data and Effective
Mid-Height Displacement Data. The second plot
is provided to account for the decreasing contact
area between the air bag and the back of the wall,
which became noticeable after about 2 of
recorded deflection. This second plot has been
interpolated from the original data based upon
measurements of the actual bag contact area during
the test.
Within this same graph, three
simplified plots are also presented for
hypothetical walls with composite design strengths
that vary from 1500 psi (original design strength)
to 3500 psi. These simplified plots were developed
based upon general moment-curvature relationships
as indicated below in Table 1, and converted to
load (psf) versus deflection data by the formulas
previously presented in figure 7.
Comparison of the actual wall
data and the three curves clearly indicate good
flexural wall performance in spite of the
unacceptable shear test results previously reported
by conventional tests. In fact, up to the
theoretical yield moment, results for the
Effective Mid-Height Displacement are
remarkably close to those results predicted for a
wall with a design-strength of 2500 psi. Above this
theoretical yield point, the tested wall continues
to exhibit excellent flexural resistance with its
ultimate capacity approximately 10% higher than
that predicted by the same curve. This increase in
ultimate moment capacity is probably due to higher
compressive strengths in the CMU block, an
increased slope in the assumed steel
strain-hardening profile and ultimate strength, or
slight inaccuracies in measuring the effective
contact area of the air bag.
Wall Displacements and
Ductility
At a mid-height deflection of
approximately 6, the LVDT devices used in
conjunction with the data acquisition system became
inoperable. Beyond this point, data was collected
by means of the manual dial gages and were
confirmed by physical hand measurement taken
relative to the adjacent CMU wall. The test was
continued to a final wall displacement of
approximately 9 and was then terminated due
to the possibility of damage to the testing
equipment. This produced a displacement ductility
of approximately 7.9, which was better than
expected.
At the conclusion of the
test, the air bag was completely removed from back
of the specimen and the compression face was
completely examined. This visual observation
yielded no signs of spalling, suggesting that the
wall may have been able to achieve an even higher
displacement ductility. Observations were also made
during the test on the back of the wall where the
air bag began to pull away from the edges. No
indications of cracking or spalling were present,
also suggesting that the effects of the air bag
contributing to confinement were negligible at the
displacements achieved.
Table 1-Numerical Results
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Effective
Data
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1500
psi
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2500
psi
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3500
psi
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Mcr
Dcr
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102,176
.040
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72,057
.067
|
93,025
.052
|
110,069
.044
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My
D
y
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212,850
(6)
1.15
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226,175
1.51
|
242,074
1.24
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248,887
1.15
|
Mu
D
u
åsu
å
mu
|
283,800
9.125
NA
NA
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227,614
5.32
.007
.003
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250,476
6.91
.011
.003
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266,715
9.37
.016
.003
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NOTES:
1. Mcr, My, Mu- Cracking,
yield, Ultimate Moments (inch-#)
2. D
cr, D
y, D
u- Cracking, yield,
Ultimate Deflections (inches)
3.
å
su = Computed Steel
Strain at Mu
4.
å
mu = Computed Masonry
Strain at Mu
5.
å
sh = Stain Hardening
assumed at .006 and .02 of Es
6. Assume My,
D
y at .75 x Mu
Conclusions
Results obtained by the
in-place testing program clearly indicated that the
wall sampled could achieve flexural capacities and
ductilities as good as those calculated by
engineering principles despite poor initial
shear/bond test results by traditional methods.
In the authors opinion,
these results are most-likely due to the natural
keying of the block webs across the critical cold
joint, as well as the frictional interlocking
between the grout and shell face as the wall begins
to deform.
It is also the authors
opinion that traditional core tests, as specified
in the California Building Code, continue to
provide useful information on the finished wall
construction by examining in-place compressive
strength, shear/bond strength, and perhaps
most-importantly, a sample which can be visually
examined for proper consolidation, possible
aggregate segregation or even complete voids.
For this particular project,
it is important to note that virtually all tests
conducted for in-place compressive strength had
acceptable results indicating sufficient grout
integrity as placed. Based upon the findings of
this investigation and in particular, the favorable
load-deflection performance of the wall tested,
this association is considered relevant and should
probably be considered in conjunction with any poor
shear/ bond test results before walls are
ultimately rejected and/or re-constructed.
Since the placement of grout
generally requires a high slump mix, some grout
shrinkage is inevitable and is probably the largest
contributor to poor shear-bond test results. To
help mitigate this problem and avoid a similar
situation, it is the authors opinion that the
control of water and proper consolidation, and
re-consolidation of grout in a timely manner is
essential. For this particular project, the rate of
acceptance for specimens tested for shear/bond
strength dramatically improved, although not
entirely eliminated, where additional care was
provided during the consolidation process.

References
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1.
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1998 California
Building Code
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2.
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ASTM E 72-98
Standard Test Method of Conducting
Strength Tests of Panels for Building
Construction
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3.
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Abboud, B.E.,
Flexural Behavior of Reinforced
Concrete Masonry Walls under Out-of-Plane
Monotonic Loads
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This issue of "Masonry
Chronicles" was written by Colin Blaney S.E.,
Principal with the Crosby Group, Redwood City,
California.
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