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P,I I
Crack width from [mm];
LM:N
∆ I
I Reading of [mm];
Stress [MPa]; LM:N
I
Secant modulus of elasticity as calculated using the readings from
[MPa];
LR SHℎ LM:N
I
LM:N
[ Gauge length of [mm].
The elastic portion of the deformation was removed from the overall LVDT reading and
the rest of the deformation was taken as the crack width since there was no multiple
190
5. TEST RESULTS
crack observed. If result of the equation (5.11) was negative, the crack width was taken
as zero. Test observations show that in all cases the crack formed simultaneously on all
faces, but some occasional out-of-plane bending was observed, causing some
“compressive readings” on the LVDT: this did not mean that the face of the specimen
was surely in compression, though, as the LVDTs were located on a plane offset from
the face of the dog-bone. Thus, it was reasonable take the crack width as zero until the
equation (5.11) yielded a positive value; once that every LVDT has his procedure
completed, the values of crack width were averaged to obtain the tensile stress versus
crack width relationship.
Ending, linear interpolation was used to determine the tensile stress at regular intervals
of crack width (or tensile strain) for each specimen, so the average response of the
specimen tested in each set could be found.
5.3.4 Results of Data Analysis
The results of data analysis are summarized in the following Table 5.6 and Table 5.7,
which includes the tangent modulus of elasticity , the first-cracking tensile strength
,
, the strain corresponding to the first-cracking tensile strength the maximum
tensile strength and the strain corresponding to the maximum tensile strength
\
:
\ C
@ ] ^
A^ ^
<
Specimen Fibers
] F ⁄ ⁄
C @
2] 2]
(MPa) (MPa) (xDE ) A A^ A
^
ID Type
(%) [CV] [CV] [CV]
38,600 4.35 0.148
DC-P1 - - 0.514 4560
[9.31] [4.52] [9.70]
29,000 3.90 0.184
DC-P2 1.0 Steel 0.495 3680
[15.2] [11.5] [26.0]
35,700 4.49 0.132
DC-P3 2.0 MSN 0.629 5000
[20.8] [4.59] [9.2]
Table 5.6: Dog-bone Pre-cracked Tests Results Summarized. 191
5. TEST RESULTS
Specimens in this experimental program did non exhibit strain hardening behavior, as
the fiber volume fraction was too low to present such behavior (Bentur, 2007).
The effect of fiber addition on the properties of the concrete prior to cracking is
viewable in the reduction of the Elastic Modulus of Elasticity in tension in the previous
table: this modulus of elasticity was reasonably similar to that suggested in the
Canadian Concrete Design Handbook, which states that the secant modulus of elasticity
for concrete may be taken as: 2
4500
= (5.12)
Moreover, the cracking stresses for all concretes were reasonably similar, ranging from
0.5 0.63
2 2
and . =
AD
` ` at
Aa Aa
< = = `
at at
= ^_ ^b Aa
= =
Specimen Fibers of
^_ ^b
ID Type (MPa) (MPa) 3mm
(%) (mm) (mm) (MPa)
DC-P2 1.0 Steel 3.20 0.14 3.52 0.65 1.60
DC-P3 2.0 MSN 1.58 0.47 1.78 2.51 1.73
Table 5.7: Dog-bone Post-cracked Tests Results Summarized.
The cracking strain was similarly unaffected; after cracking, however, the results were
different than for plain concrete: the plain concrete exhibited a brittle failure, whereas
for FRC specimens a ductile and more gradual reduction in load was observed.
5.3.5 Influence of fiber content, fiber type, loading protocol and concrete matrix
strength
Results obtained by Susetyo shows that the influence of fiber content changes the
behavior of the all specimen: by increasing the amount of fibers in the concrete matrix,
improves the tensile behavior of the concrete. When 0.5% fiber by volume was added to
192
5. TEST RESULTS
the matrix, although a strength reduction was observed immediately after cracking, the
concrete still retained a small amount of residual strength (Susetyo, 2009). Increasing
fibers up to 1.0% and 1.5% did not alter the pre-cracking response of the concrete than
by 0.5% of fiber by volume, but the post-cracking behavior was improved remarkably.
The influence of fiber type is viewable by the main differences obtained: shorter steel
fibers were more effective than the longer fibers, at volume fraction of 1.0%, maybe due
to the fact that there is a larger number of individual fibers in the mix for shorter steel
fibers, at a given volume fraction.
At large crack width the SFRC with shorter fibers began to lose the load-carrying
capacity rapidly and the residual stress dropped below that of the longer MSN fibers.
The response of MSNFRC specimens was different: the drop after cracking was larger
than SFRC regardless to the volume fraction; moreover, a large crack width was
required before the macro-synthetic fibers began engaged.
However, despite to this initial drop, the MSNFRC response regained some strength: in
most cases the maximum residual tensile stress occurred at a much greater crack width
than with the SFRC specimen, as much as 150% of the stress at engagement.
At a crack width of 2.4 mm to 2.8 mm, steel fibers began to lose bond strength due to
the straightening of the end-hook; the macro-synthetic fibers performed more favorably
at this level of cracking (Carnovale, 2013).
The flexibility of the fiber is a significant properties that affect the engagement of the
macro-synthetic fibers. At first cracking, some fibers were oriented in non-orthogonal
directions to the crack. These fibers had to become bent around the matrix entrance
points at both sides of the crack and become aligned with the direction of the load,
before becoming effective: this does not happen instantly and some crack opening is
required to allow this alignment to occur. This explain the requirement of a relatively
large crack opening before that these fibers become engaged.
Therefore, at a small crack widths, only fibers perfectly aligned perpendicular to the
crack can transmit significant tensile stress across the crack.
Influence on loading protocol in response of MSNFRC and SFRC exhibited different
engagement characteristics: cyclic dogbones have similar engagement characteristics
than those by monotonic load, whereas for the MSNFRC have a different response, with
193
5. TEST RESULTS
little to no difference in residual load-carrying capacity when compared to the
monotonically loaded.
Ending, the concrete matrix strength has an important rules in the behavior of the
specimens: a high concrete matrix strength was indicated by stress at which the concrete
first cracked, and this means that a higher concrete strength would result in a higher
first-cracking stress (Susetyo, 2009).
Watching the post-cracking behavior of the specimens, they seem to don’t be
significantly influenced by the strength of the concrete matrix: the only difference is the
interfacial shear strength between the fibers and the concrete matrix (higher in high
strength concrete matrix than in the normal one) so at the onset of first cracking, the
fibers in high strength concrete specimens were subjected to a higher tensile stress than
those in normal strength concrete specimens.
Lastly, the increased interfacial shear stress at the onset of cracking may have resulted
in an amount of bond slip available before the fibers were fully de-bonded similar to
that in normal strength concrete, despite the higher interfacial shear strength of high
concrete strength (Susetyo, 2009).
5.4 Prisms - Modulus of Rupture Tests
In this section, results of the Modulus of Rupture (MORs) are summarized and
discussed in accordance with the ASTM C1609/C169M (2010).
For each batch two specimens were constructed, and tested at various age from 48 to 99
days, based on the availability of laboratory machinery.
5.4.1 Previous Tests
Previous tests done by Susetyo show that fiber addition increase the flexural strength of
the concrete. Improvements ranging from 30% to 300% were obtained in previous
experimental test, depending on the fiber content and the type of fibers used.
Improvements were also more pronounced in test sets made with normal strength
concrete than those made with high strength concrete; higher flexural strength
194
5. TEST RESULTS
improvements were obtained also by adding fiber to the normal strength concrete than
to the high strength concrete.
Even with a small amount of fiber, the flexural behavior of the concrete was much more
ductile than that of the plain concrete: the plain concrete fails immediately after
cracking, whereas the fiber reinforced specimens deform significantly before the failure
improving the energy absorption capacity of the element.
5.4.2 Test Observation
This kind of test show a variability in results: the unforeseen location of the crack had a
big effect on the cracking load and on the post-cracked peak load. The closer the crack
was to the mid-span of the specimen, the higher the cracking and peak loads in the four-
point bending condition.
Test set DC-P1 exhibited brittle behavior, since no fibers were present to transfer the
load across the crack, and failed immediately after the prism cracked.
Like dog-bones, by adding fibers in the matrix, a control in the abrupt opening was
obtained and in all cases, the FRC specimens exhibited an ability to carry residual
flexural loads after first cracking and the load-carrying capacity decreased steadily and
gradually as the crack continued to open.
For FRC specimens, a strain hardening behavior in flexure was observed.
A slight drop in load was observed after cracking, accompanied by a slight change in
stiffness as the load continued to increase: multiple cracks or crack extensions formed
until the peak load was reached.
It was observed that further deformations were localized at one of the cracks and the
load-carrying capacity began to drop in a rapid yet controlled fashion; a problem with
the DC-P2 prisms was found after testing both modulus: the midspan LVDTs were not
switched to collect data, and no results are so available.
Following pictures shows the modulus of rupture tested in this experimental program:
195
5. TEST RESULTS
Figure 5.23: DC-P1 modulus of rupture test crack pattern.
Figure 5.24: DC-P2 modulus of rupture test crack pattern.
Steel fibers and macro-synthetic fibers show different behavior for the modulus of
rupture tests: steel fibers specimen show a slight drop in load after cracking,
accompanied by a slight change in stiffness as the load continued to increase.
The macro-synthetic specimen shows a sudden drop in load at the onset of cracking
similar that of the MSNFRC dogbones and this drop continued to the point at which the
fibers became sufficiently engaged; from there the response softened, yet load increased
until the post-cracked peak was attained. After reaching this secondary peak, the load
carrying capacity dropped gradually as the crack mouth continued to open. 196
5. TEST RESULTS
Figure 5.25:
5. D