Restrained Shrinkage Mechanism of Ultra High Performance ... · 2) There were no cracks of UHPC...
Transcript of Restrained Shrinkage Mechanism of Ultra High Performance ... · 2) There were no cracks of UHPC...
KSCE Journal of Civil Engineering (0000) 00(0):1-12
Copyright ⓒ2019 Korean Society of Civil Engineers
DOI
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pISSN 1226-7988, eISSN 1976-3808
www.springer.com/12205
Structural Engineering
Restrained Shrinkage Mechanism of Ultra High Performance Concrete
Jun-Yan Wang*, Chen Bian**, Ru-Cheng Xiao***, and Biao Ma****
Received March 6, 2019/Accepted August 1, 2019/Published Online
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Abstract
The understanding and controlling of the restrained shrinkage is critical for the application of ultra high performance concrete(UHPC). This study made an analysis of restrained shrinkage mechanism of four kinds of UHPCs based on the direct tensile testaccompanied with acoustic emission (AE) source location, free shrinkage test and restrained shrinkage test (ASTM C1581-04 (2004)ring test). The effects of UHPC tensile properties (strain softening or strain hardening) and high performance calcium sulphoaluminate(HCSA, a new kind of expansion agent) dosages (0%, 3% and 6% by mass of total binder) were investigated. The restrained shrinkagecracking mechanism of strain hardening UHPC and strain softening UHPC was analyzed based on AE analysis method under directtensile loading. The results indicates that strain hardening UHPC shows multiple micro-defects to relax the restrained tensile stressmarginally while strain softening UHPC shows several hairline cracks to relax the restrained tensile stress evidently. In ASTM C1581-04(2004) ring test, the restrained shrinkage of strain hardening UHPC with HCSA dosage of 0%, 3% and 6% at 80d is 141 με, 96 με and 16με, respectively. The HCSA expansion agent can effectively reduce the restrained shrinkage of UHPC and the influence on the structure.
Keywords: UHPC, restrained shrinkage mechanism, expansive agent, ASTM C1581-04 (2004) ring test, AE analysis method
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1. Introduction
Ultra high performance concrete (UHPC) is composed of
compact cementitious matrix combined with a high amount of
fibers (Murali et al., 2018; Yoo et al., 2017; Yoo et al., 2016),
which exhibits high strength and excellent resistance against
aggressive environments (Charron et al., 2007; Denarié et al.,
2011). The distinguishing characteristics of UHPC make it an
attractive option for some civil engineering construction and
repair application (Ren et al., 2019; Yoo et al., 2016). For
example, steel-UHPC composite deck system as shown in Fig. 1
(a) can increase the stiffness and reduce the self-weight of the
structure compared with the traditional steel-concrete composite
deck system (Wang et al., 2016), the existing structure strengthened
with UHPC as shown in Fig. 1(b) can overcome the drawbacks
in the existing structure strengthened with fiber polymer such as
delamination and brittle failure retrofitting (Prem et al., 2018). In
above structures, UHPC is restrained by the steel slab with the
stud shear connector or the existing structure.
Given the very low water-to-binder ratio (w/b), UHPC can
exhibit high degree of self-desiccation that can cause significant
autogenous shrinkage (Xie et al., 2018; Valipour et al., 2018;
Yoo et al., 2019). It may lead to the generation of the high tensile
stress of UHPC in restrained condition, making UHPC vulnerable
to cracking. This can limit some of the potential applications of
UHPC where shrinkage plays a major role such as long-span
bridges, thin pavement overlays. The control of shrinkage
characteristics of such applications is critical for the service life
of structures. One kind of effective methods to control the
shrinkage of UHPC is the incorporation of expansive agent (EA)
(Corinaldesi et al., 2015).
At present, the relevant researches on the restrained shrinkage
of UHPC seem obviously insufficient. There are no standard test
methods to assess the restrained shrinkage behavior of UHPC.
Different methods were used to simulate the restrained condition
of UHPC, such as axially or linearly restrained condition (Yoo et
al., 2015), plate/slab-shaped geometry (Yoo et al., 2014) or
restrained circular ring (Park et al., 2014; Yoo et al., 2013; Wang,
2012). These studies are summarized in Table 1.
It can be seen from Table 1 that the benefit of admixture on the
shrinkage compensation of UHPC was mainly about a synergistic
effect in the combined use of shrinkage reducing agent (SRA)
and EA. The effectiveness of EA on reducing the shrinkage of
UHPC was confirmed. However, EA used in these studies
mainly aimed at applying in the normal concrete, which was
unstable in long term used in UHPC. It is necessary to invent a
suitable kind of EA for UHPC with a low w/b. Shunzeng Zhao et
al. (2009) has invented a new kind of EA, namely high performance
TECHNICAL NOTE
*Professor, Key Laboratory of Advanced Civil Engineering Materials, Tongji University, Shanghai 201804, China (Corresponding Author, E-mail:
**Ph.D. Student, Key Laboratory of Advanced Civil Engineering Materials, Tongji University, Shanghai 201804, China (E-mail: [email protected])
***Professor, College of Civil Engineering, Tongji Univ., Shanghai 200092, China (E-mail: [email protected])
****Professorate Senior Engineer, Shanghai Municipal Engineering Design Institute (Group) Co., Ltd., Shanghai 200092, China (E-mail: [email protected])
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calcium sulphoaluminate (HCSA) which is especially suitable
for high performance concrete that has a low w/b. HCSA has
numerous advantages such as the high expansion energy, the rapid
expansion rate and the significant expansion in humidity insulation.
As a result, it is supposed to be a proper method to add HCSA into
UHPC to reduce the shrinkage of UHPC, which needs to be verified
by an experimental study. Among various experimental methods,
the ring test is the most appropriate for evaluating the effectiveness
of EA due to its high cracking sensitivity. In addition, the ring test is
economical and convenient to conduct. Therefore, ASTM C1581-
04 (2004) ring test has been chosen to study the restrained shrinkage
behavior of UHPC and the effect of HCSA on the shrinkage
compensation of UHPC in this paper.
The tensile properties of UHPC under direct tensile loading is the
foundation to evaluate the restrained shrinkage cracking behavior of
UHPC. In some previous studies, restrained shrinkage behavior of
UHPC has been studied through the combination of direct tensile
test, free shrinkage test and restrained shrinkage test as summarized
in Table 1. However, these researches mainly focused on the
quantitative calculation of restrained tensile stress, tensile strength
and restraint degree of UHPC, hardly involving the analysis of
restrained shrinkage mechanism based on direct tensile test. It is
supposed that different tensile behaviors of UHPCs lead to different
restrained shrinkage mechanisms and there is a dearth of information
on the restrained shrinkage mechanisms.
Based on the tensile properties, UHPC is divided into three
types in 2016 MCS-EPFL recommendation (M.C.S.-E.P.F.L,
2016): UO (strain softening), UA (ultimate tensile strain is
higher than 1,500 με) and UB (ultimate tensile strain is higher
than 2,000 με). Namely there are two kinds of UHPCs: strain
softening UHPC and strain hardening UHPC. The shrinkage
cracking risk of UHPC in restrained condition basically depends
on the crack width controlling ability of UHPC under direct
tensile loading. The popular method to judge the crack width
controlling ability of UHPC is using the crack width measurement
instrument which is at the macro level and not accurate. Acoustic
emission (AE) technique has been proved to be an effective
method at the micro level to illustrate the relationship between
the crack width controlling ability and the different tensile
Fig. 1. UHPC used in Civil Engineering Construction and Repair
Application: (a) Steel-UHPC Composite Deck System in
Shanghai, 2019, (b) Normal Concrete beam Strengthened
with UHPC in Shanghai, 2017
Table 1. Literature Review of Restrain Shrinkage of UHPC & UHPFRC
Details of specimen Contents Main conclusions Ref.
Effect of shrinkage-reducing admix-ture (SRA) on the free and restrainedautogenous shrinkage of UHPFRCwith three SRA ratios of 0%, 1%and 2% and three reinforcementratios of 1.3%, 2.9% and 8.0%
1) 28d tensile strength of UHPFRC slightlyincreased with an increase in the SRA contentup to 2%;2) Tensile strengths were higher than the autoge-nous shrinkage stresses. Autogenous shrinkagestress decreased at lower reinforcement ratiosand higher SRA contents;3) A higher degree of restraint was obtainedwith a higher reinforcement ratio, but it wasmarginally influenced by the SRA content.
Yoo et al., 2015
Combined effect of SRA and expan-sive admixture (EA) on the shrink-age and cracking behaviors ofrestrained UHPFRC slabs with threedifferent thicknesses (40, 60, and80 mm)
1) Combined use of SRA and EA has a benefi-cial effect on increasing strength, free shrink-age and reducing shrinkage crack width ofUHPC;2) Higher UHPC thickness improves the shrink-age cracking resistance;
Yoo et al., 2014
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behaviors of UHPCs (Wang et al., 2018). Thus, the direct tensile
test accompanied with AE technique can be used to well explain
the shrinkage cracking mechanism of UHPC in restrained
condition at the micro level.
In this study, the direct tensile test accompanied with AE source
location, free shrinkage test and restrained shrinkage test (ASTM
C1581-04 (2004) ring test) were conducted to further understand the
restrained shrinkage mechanism of UHPC. Four kinds of UHPCs
were used, namely three kinds of strain hardening UHPCs with
different HCSA dosages (0%, 3% and 6% by mass of total binder)
and one kind of strain softening UHPC. Based on the tensile
behavior accompanied with AE analysis method, the restrained
shrinkage mechanism of UHPC was elaborated from three aspects
of the restrained stress, relaxation degree and strain transfer
modelling.
2. Experimental Program
2.1 UHPC Materials
In this study, two volume fractions of steel fiber (1%, 2%) and
three dosages of HCSA by mass of total binder (0%, 3% and
6%) were used to make four kinds of UHPCs, namely SSU-0,
SHU-0, SHU-3 and SHU-6, whose mix proportions are listed in
Table 2. The physical properties of the used steel fibers are
summarized in Table 3. HCSA as a kind of EA was added to
UHPC matrix to reduce the shrinkage of UHPC. Its chemical
composition is shown in Table 4.
A laboratory mixer with sixty-liter capacity was used to
Table 1. (continued)
Details of specimen Contents Main conclusions Ref.
Effects of EA and SRA on themechanical and shrinkage prop-erties of UHPC
1) The free shrinkage strain was obviouslyreduced by including SRA and EA;2) The inner steel strain was also decreased byincorporating SRA and EA.
Park et al., 2014
Influence of ring size on therestrained shrinkage behavior ofUHPFRC
1) UHPFRC ring specimen with a thinner steelring had a higher strain level than that of athicker steel ring;2) The stress relaxation of UHPFRC were sel-dom affected by the diameter of the steel ringand the ring specimen with a thicker steel ringpresented a higher maximum stress relaxation;3) A higher degree of restraint was obtainedwith a thicker steel ring than that with a thin-ner steel ring.
Yoo et al., 2013
Influence of super absorbent poly-mer (SAP) on the restrained shrink-age behavior of UHPC
1) SAP could improve the restrained shrinkagebehavior of UHPC;2) There were no cracks of UHPC with steelfibers in ring test.
Wang, 2012
Note: UHPFRC is Ultra High Performance Fiber Reinforced Concrete
Table 2. Mix Proportions of Four Kinds of UHPCs/(kg/m3)
No. Cement Silica fume Filler Silica sand Water Superplasticizer Steel fiber HCSA
SHU-0 745.0 223.5 223.5 998.3 179.0 13.1 157.0 0
SHU-3 722.7 216.8 216.8 998.3 179.0 13.1 157.0 35.8
SHU-6 700.3 210.1 210.1 998.3 179.0 13.1 157.0 67.2
SSU-0 745.0 223.5 223.5 998.3 179.0 13.1 78.5 0
Table 3. Properties of Steel Fiber
Tensile strength /MPa Elastic modulus /GPa Length/mm Diameter /µm Aspect ratio Density/(kg/m3)
2,500 200 16 200 80 7850
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prepare the UHPC mixture. UHPC premixed powder was firstly
dry-mixed for about 1 minute. Water was then added gradually
and mixed for another 3 minutes. When the mixture showed the
suitable workability, steel fibers were dispersed into the mixture
and mixed for another 3 minutes. Finally, the UHPC mixture was
poured into the molds without vibration due to its self-compacting
property. The used UHPCs are shown in Fig. 2.
The 28d average elastic modulus (three 100 mm × 100 mm ×
300 mm prisms) and 28d average compressive strength (three
100 mm cubic specimens) of SHU-0, SHU-3 SHU-6 and SSU-0
were tested according to Chinese standard GB/T31387-2015
(2015). The results are shown in Table 5.
2.2 Action Mechanism of HCSA
The main hydration equations of HCSA are Eqs. (1) and (2).
There are two expansive sources in HCSA. CaO is the main
expansive origin whereas anhydrite (CaSO4) and C4A3S are the
secondary expansive origin. The main hydration products of HCSA
are Ca(OH)2 and ettringite (AFt), motivating the expansion of
UHPC. Because CaO was hydrated preferentially to C4A3 , the
early expansion energy is provided mainly by Ca(OH)2. However,
AFt is relatively slow to generate and fill the pores and defects
gradually to make the matrix compact and dense (Zhao et al., 2012).
(1)
(2)
2.3 Test Methods
2.3.1 Direct Tensile Test Accompanied with AE Source
Location
Direct tensile test was conducted through a universal testing
machine (WDW-300 servo-controlled testing system) running in
S
( )22
OHCaOHCaO →+
6CaO C4A3S 8CaSO4 96H2O 3 C3A 3CaSO4 32H2O⋅ ⋅( )→+ + +
Table 4. Chemical Composition of HCSA/%
Loss SiO2 Al2O3 Fe2O3 CaO MgO SO3 Total
1.19 1.50 10.61 1.37 65.60 2.08 17.50 99.85
Fig. 2. Used UHPC in This Paper
Table 5. Basic Mechanical Properties of Four Kinds of UHPCs
No.Average Elastic modulus/GPa 28d average compressive
strength/MPa2d 7d 28d
SHU-0 41.2 44.6 47.4 138.7
SHU-3 42.1 44.7 47.4 138.1
SHU-6 41.9 45.0 47.7 136.0
SSU-0 41.0 42.3 47.0 117.8
Fig. 3. Direct Tensile Test System for UHPC: (a) Specimen Dimensions, (b) AE Transducers Layout, (c) Direct Tensile Test Setup
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the displacement control manner of 0.3 mm/min. The direct
tensile test system is given in Fig. 3: 1) Dog-bone shaped
specimen was fabricated according to the dimension as shown in
Fig. 3(a). The width (50 mm) of the specimens is longer than
three times of the length of the fibers (16 mm), which reduces the
influence of the fiber orientation distribution; 2) A set of
customize fixture was used to avoid secondary flexural stress
and to ensure a centric-loading condition as shown in Fig. 3(c);
3) A test frame was amounted to the specimen to measure the
tensile elongation by using two linear variable differential
transformers (LVDTs), whose gauge length was 150 mm. During
the direct tensile test, the crack width measuring instrument with
0.01 mm resolution was used to detect the maximum crack
width.
AE source location to characterize the damage evolution
process of UHPC was carried out in parallel with the direct
tensile test as shown in Fig. 3(c). Eight AE transducers were
placed in a rectangular array just above the surface of double
sides of the tensile specimens as shown in Fig. 3(b), aiming at
picking up AE signals caused by the damage of specimens. More
details about AE analysis method can be found in reference
(Wang et al., 2018).
Direct tensile tests accompanied with AE source locations for
SHU-0, SSU-0 at 2d, 7d, 28d and 80d were done to investigate
their tensile strength development and damage revolution
process. Besides, direct tensile tests for SHU-3 and SHU-6 at
28d were also carried out. Each test has three specimens. UHPC
specimens were cured in a room at the temperature of 20 ± 2oC
and 50% humidity.
2.3.2 Free Shrinkage Test
Three prismatic specimens with dimensions of 100 mm × 100
mm × 515 mm were prepared for SHU-0, SHU-3 SHU-6 and
SSU-0, respectively. The fresh UHPC mixture was casted into
the mold and the free shrinkage was measured over a period of
28d. Free shrinkage of UHPC was determined at 20 ± 2oC and
50% humidity. The setup is shown in Fig. 4. The free shrinkage
strain of UHPC was measured with non-contact method at 0-2d
whereas the free shrinkage strain of UHPC was measured with
contact method at 3d − 28d.
2.3.3 Restrained Shrinkage Test (ACTM C1581 ring test)
Restrained shrinkage test of SHU-0, SHU-3 SHU-6 and SSU-
0 was carried out according to ASTM C1581-04 (2004) in a
controlled environmental chamber at 20 ± 2oC and 50%
humidity. Details of the mold and specimen are shown in Fig. 5.
Four strain gauges were attached at quarter points (one per
quadrant) on the inner steel ring midway up the height using a
data logger system whose frequency was set as 5Hz. After
casting UHPC, the initial strain value of inner steel ring was set
to be zero and began to monitor the strain value until 80d. One
day after casting UHPC, the outer ring mold of the specimen was
removed. Meanwhile, the crack width measuring instrument
with 0.01 mm resolution was used to detect the crack width once
a day.
3. Test Results and Discussion
3.1 Tensile Performance of Strain Hardening UHPC and
Strain Softening UHPC at Different Ages
3.1.1 Tensile Stress-strain Curves
Average tensile stress-strain curves of SHU-0 (strain hardening
UHPC) and SSU-0 (strain softening UHPC) at different ages
(2d, 7d, 28d and 80d) are shown in Fig. 6. As shown in Fig. 6(a),
the tensile stress-strain curves of SHU-0 (at 2d, 7d, 28d and 80d)
consist of elastic stage, strain hardening stage and strain softeningFig. 4. Test Setup to Measure the Free Shrinkage of UHPC with
Non-contact Method
Fig. 5. ASTM C1581 Ring Test: (a) ASTM C1581 Ring Test, (b)
UHPC Ring Test Specimen
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stage. The maximum crack width of SHU-0 at different ages at a
tensile strain of 1,000 με is about 0.02 mm which is invisible to
naked eyes. It is well known that strain hardening UHPC
exhibits high ductility by forming multiple micro-cracks in the
strain hardening stage (Makita et al., 2014). By contrast, the
tensile stress-strain curves of SSU-0 (2d, 7d, 28d and 80d) as
shown in Fig. 6(b) consist of elastic stage and strain softening
stage. The maximum crack width of SSU-0 at different ages is
about 0.12 mm at a tensile strain of 1,000 με.
The tensile properties of SHU-0 and SSU-0 are illustrated in
Table 6. It can be observed that the elastic tensile strength of
SHU-0 and SSU-0 increase significantly with the increase of
age. At the age of 28d, the elastic limit tensile strength of SHU-0
is 9.2 MPa and its ultimate tensile strength is 11.4 MPa, and the
elastic limit tensile strength of SSU-0 is about 9.7 MPa.
However, the age has negligible effect on the elastic limit tensile
strain of SHU-0 and SSU-0, which is about 100 με − 200 με. At
different ages (2d, 7d, 28d and 80d), the ultimate tensile strain of
SHU-0 is about 4,000 με − 5,000 με and the residual tensile
strength of SSU-0 at a tensile strain of 2,000 με is about 80% of
its elastic limit tensile strength.
3.1.2 AE Source Distribution Maps
AE source location can effectively detect the internal damage
of UHPC under direct tensile loading to further analyze its crack
width controlling ability at the micro level. AE source distribution
maps of SHU-0 and SSU-0 at different ages (2d, 7d, 28d and
80d) before the tensile strain of 1,000 με are shown in Fig. 7. The
values in brackets in Fig. 7 are the total numbers of AE sources
that can be registered in the range of 50 mm × 100 mm × 500
mm of specimens.
For strain hardening UHPC, SHU-0 is taken for an example to
illustrate the damage evolution owing to the similar tensile
stress-strain responses of SHU-0, SHU-3 and SHU-6. It can be
seen from Fig. 7(a) that there are hardly AE sources during
elastic stage (0 − 200 με). However, AE sources are homogeneously
distributed during 200 με − 1,000 με, which means that the
Fig. 6. Tensile Stress-strain Curves of SHU-0 and SSU-0 at Differ-
ent Ages: (a) Tensile Stress-strain Curve of SHU-0, (b)
Tensile Stress-strain Curve of SSU-0
Fig. 7. AE Source Distribution Maps of SHU-0 and SSU-0 at Dif-
ferent Ages: (a) AE Source Distribution Map of SHU-0, (b)
AE Source Distribution Map of SSU-0
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internal damages caused by multiple micro-cracks (below 0.02
mm) are distributed over the specimen, indicating a uniform
stress state (Li et al., 2000). The AE sources might be motivated
by UHPC matrix cracking and fiber-matrix debonding. AE analysis
method provides strong evidence to the multiple micro-cracking
mode of strain hardening UHPC during its strain hardening
stage.
For strain softening UHPC (SSU-0) shown in Fig. 7(b), some
AE sources are accumulated at the elastic limit strains (159 με at
2d, 131 με at 7d, 191 με at 28d and 201 με at 80d) and these AE
sources are mainly distributed at the single plane corresponding
to the localized crack. With the increase of tensile strain, the
number of AE sources increase significantly. The AE sources
might be motivated by UHPC matrix cracking and fiber pull-out
action. AE analysis method makes a clear explanation to the
single macro-cracking mode of strain softening UHPC.
3.2 Effect of HCSA Dosage on the Tensile Stress-strain
Curve Of Strain Hardening UHPC at the Age of 28d
Tensile stress-strain curves of SHU-0, SHU-3 and SHU-6 at
28d are shown in Fig. 8. All the specimens exhibit the strain
hardening behavior and the ultimate tensile strength is about 11 −
12 MPa and the ultimate tensile strain is about 4,000 με− 5,000 με,
meaning that these three kinds of UHPCs all belong to strain
hardening UHPC and HCSA has no influence on the strain
hardening characteristics. Specific values are summarized in
Table 6. As shown in Table 6, the addition of HCSA may slightly
increase both of the elastic tensile strength and ultimate tensile
strength of strain hardening UHPC. The maximum crack width
of SHU-0, SHU-3 and SHU-6 at a strain of 1,000 με is below
0.02 mm which is invisible to naked eyes.
3.3 Free Shrinkage of Four Kinds of UHPCs
Free shrinkage strain-age curves of SHU-0, SHU-3, SHU-6
and SSU-0 are shown in Fig. 9. The shrinkage values are plotted
as negative while the expansion values are shown as positive.
For four kinds of UHPCs, the free shrinkage strain εsh shows a
very steep increase at the early age. After certain points (about
1d), slight expansion is observed. Then with the increase of age,
the free shrinkage εsh increases slowly. At 28d, the free shrinkage
strain εsh of SHU-0, SHU-3 SHU-6 and SSU-0 are 1,006 με, 600
με, 462 με and 1197 με, respectively. The free shrinkage of SHU-
0 is smaller than that of SSU-0 due to the higher ratio of steel
fibers of SHU-0, showing that steel fibers can contribute to the
reduction of the free shrinkage of UHPC. Besides, the free
shrinkage of strain hardening UHPC decreases accordingly with
the increase of HCSA dosages from 0% to 6%. It indicates that
HCSA has a positive effect on decreasing the free shrinkage of
UHPC.
3.4 Restrained Shrinkage of Four Kinds of UHPCs
Average compressive strain of inner steel ring-age curves of
SHU-0, SHU-3 SHU-6 and SSU-0 are plotted in Fig. 10. The
compressive strain of inner steel ring is approximately equal to
the restrained shrinkage strain εst of UHPC due to the low ratio of
thickness and radius.
It is supposed that the value of strain gauge should increase
smoothly and continuously with the increase of age if UHPC
doesn’t crack in ASTM C1581-04 (2004) ring test. Therefore, a
rapid and instantaneous fluctuation of the value of strain gauge
indicates cracking of UHPC according to ASTM C1581-04
(2004).
Fig. 8. Tensile Stress-strain Curves of SHU-0, SHU-3 and SHU-6
at 28d
Table 6. Tensile Properties of Four Kinds of UHPCs
No. Age/dElastic
limit tensile strength/MPa
Elastic limit tensile
strain/με
Ultimate tensile
strength/MPa
Ultimate tensile
strain/με
SHU-0
2 3.3 160.5 4.3 1,998.6
7 5.8 162.7 9.5 4,397.0
28 9.2 220.3 11.4 4,561.4
80 11.5 206.7 14.1 4,743.3
SHU-3 28 10.7 224.5 12.0 4,000.0
SHU-6 28 11.3 200.2 12.8 4,271.3
SSU-0
2 4.2 199.7 N.A N.A
7 6.1 200 N.A N.A
28 9.7 191.5 N.A N.A
80 11.3 215.5 N.A N.A
Fig. 9. Free Shrinkage Strain-age Curve of SHU-0, SHU-3, SHU-
6 and SSU-0
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The restrained shrinkage strain εst of SHU-0 and SSU-0
develop greatly and smoothly during the early age of 14d and
their values are similar which are about 100 με. After that, the
curves of SHU-0 still vary continuously and no crack can be
detected by the crack width measuring instrument with 0.01 mm
resolution, and the restrained shrinkage strain εst of SHU-0 is
about 141 με at 80d. By contrast, there are several evident
instantaneous fluctuations of the strain gauge value of SSU-0
and four hairline cracks (0.035 mm, 0.05 mm, 0.04 mm and 0.02
mm) are checked as shown in Fig. 11. The restrained shrinkage
strain εst of SSU-0 is about 99 με at 80d. It shows that the
restrained shrinkage strain εst of SHU-0 increases continuously in
the crack-free state while the restrained shrinkage strain εst of
SSU-0 decreases due to cracking. As a result, SHU-0 has a better
crack width controlling ability than SSU-0, considering the effect
of the restrained shrinkage on cracking of UHPC.
On the other hand, the restrained shrinkage strain εst of SHU-
3, SHU-6 are about 96 με and 16 με, respectively at 80d, lower
than that of SHU-0. Thus, HCSA can mitigate the restrained
shrinkage of strain hardening UHPC effectively. It is supposed
that HCSA can reduce the restrained tensile stress of strain
hardening UHPC. Besides, no crack can be detected in SHU-3,
SHU-6 by the crack width measuring instrument with 0.01 mm
resolution.
4. Restrained Shrinkage Mechanism of UHPC inASTM C1581-04 (2004) Ring Test
4.1 Restrained Shrinkage Cracking Mechanism of Strain
Hardening UHPC and Strain Softening UHPC based
on Their Direct Tensile Properties
4.1.1 Restrained Tensile Stress Analysis
In this paper, the maximum tensile criterion (Hossain et al.,
2004; Moon et al., 2006) was chosen to analyze the failure
mechanism of UHPC in ASTM C1581-04 (2004) ring test. The
maximum tensile criterion is to analyze the relationship between
the “load response” (restrained tensile stress) of UHPC and its
“tensile resistance” (uniaxial tensile strength).
The “load response” of UHPC induced by its own shrinkage in
ASTM C1581-04 (2004) ring can be calculated directly with the
monitored strain of the inner steel ring, because the stress of
UHPC is presumed to be approximately uniform (See et al.,
2003). The stress calculation of UHPC ring and inner steel ring
can be simplified as the plane stress model shown as Fig. 12.
There exists fictitious interface pressure Pres at the interface
Fig. 10. Compressive Strain of Inner Ring-age Curve of SHU-0,
SHU-3, SHU-6 and SSU-0
Fig. 11. Cracking Diagram of SSU-0
Fig. 12. Idealization of Restrained Ring Specimen (Yoo et al., 2013)
Restrained Shrinkage Mechanism of Ultra High Performance Concrete
Vol. 00, No. 0 / 000 0000 − 9 −
between the inner steel ring and the UHPC ring. ric and ris refer to
the inner radius of UHPC ring and inner steel ring, respectively,
roc and ros refer to the outer radius of UHPC ring and inner steel
ring, respectively.
The fictitious interface pressure Pres (Yoo et al., 2013) can be
computed as the pressure which generates a strain that is
equivalent to the monitored steel strain of the inner ring using
Eq. (3):
(3)
Where Es is the elastic modulus of the inner ring (210 GPa)
and εst is the monitored steel strain of the inner steel ring. The
restrained tensile stress of UHPC refers to the circumferential
normal stress. The maximum restrained tensile stress σres-max is
calculated with Eq. (4) (Yoo et al., 2013):
(4)
The “tensile resistance” of UHPC at different ages (2d, 7d, 28d
and 80d) by the direct tensile test is used to plot the tensile
strength-age curve. The maximum restrained tensile stress-age
curve and the tensile strength-age curve of strain hardening
UHPC (SHU-0) and strain softening UHPC (SSU-0) are plotted
in Fig. 13.
For strain hardening UHPC as shown in Fig. 13(a), the elastic
limit tensile strength and the ultimate tensile strength are
considered as two thresholds to judge the stress state of SHU-0.
Once the maximum restrained tensile stress σres-max of SHU-0
exceeded its elastic limit tensile strength, multiple invisible
micro-defects whose existence was verified in section 3.1.2 were
generated in UHPC matrix. The steel fibers acted as stitches and
managed to control the propagation of these multiple invisible
micro-defects (Yousefieh et al., 2017; Brandt et al., 2008). Thus,
the maximum restrained tensile stress σres-max was kept below the
ultimate tensile strength by many times of marginal instantaneous
stress relaxation, which was in accordance with the measurement
result of no detected cracks (below 0.01 mm) in the ASTM
C1581-04 (2004) ring test before 80d. Finally, the maximum
restrained tensile stress σres-max of SHU-0 was kept at about 8.7
MPa at 80d.
For strain softening UHPC as shown in Fig. 13(b), once the
maximum restrained tensile stress σres-max of SSU-0 exceeded its
elastic limit tensile strength, the matrix cracked, the steel fibers
debonded and were pulled out between two cracked sections,
then the crack localized, which was verified in section 3.1.2, to
relax the tensile stress instantaneously. The relaxed tensile stress
was smaller than that of the normal concrete due to the high
residual tensile strength of SSU-0. The maximum restrained
tensile stress σres-max of SSU-0 was reduced to below its elastic
limit tensile strength by four times of evident instantaneous
stress relaxation, which was in accordance with the measurement
result of four hairline cracks (0.035 mm, 0.05 mm, 0.04 mm and
0.02 mm) at the surface of SSU-0. Finally, the maximum restrained
tensile stress σres-max of SSU-0 was decreased to 8.1 MPa at 80d.
4.1.2 Strain Transfer Modelling
A strain transfer modelling of UHPC based on the shrinkage
behavior is proposed and shown in Fig. 14. When UHPC is
under the restrained condition, the difference between free
shrinkage strain εsh and restrained shrinkage strain εst transforms
into tensile strain caused by restrained tensile stress of UHPC,
which is made up of two parts: elastic tensile strain εet (recoverable
tensile deformation) and plastic tensile strain εpt (irrecoverable
tensile deformation). Namely, the strain exists in the form of εsh
in the free condition, while the strain exists in the form of εst, εet
and εpt in the restrained condition. The elastic tensile strain εet is
the ratio of the tensile stress of UHPC to its elastic modulus.
The underlying mechanism of plastic tensile strain εpt for strain
hardening UHPC is different from that for strain softening
UHPC. Based on the direct tensile properties accompanied with
AE analysis method of SHU-0 and SSU-0, the plastic tensile
strain εpt of SHU-0 is the irrecoverable deformation mainly
caused by multiple invisible micro-defects which are related to
its multiple micro-cracking mode under direct tensile loading.
Pres
ros
2
ris
2
–( )
2ros
2--------------------Esεst=
( )( )
( ) ( )( )
2 2 2 2 2 2
22 2 2 22
os oc os is os oc
res max res s st
osoc os oc os
r r r r r r
P Err r r r
σ ε−
+ − +
= =
− −
Fig. 13. Restrained Tensile Stress Analysis of SHU-0 and SSU-0:
(a) Restrained Tensile Stress Analysis of SHU-0, (b)
Restrained Tensile Stress Analysis of SSU-0
Jun-Yan Wang, Chen Bian, Ru-Cheng Xiao, and Biao Ma
− 10 − KSCE Journal of Civil Engineering
By contrast, the plastic tensile strain εpt of SSU-0 is the irrecoverable
deformation mainly caused by several hairline cracks which are
related to its single macro-cracking mode under direct tensile
loading. The details of this point are illustrated by the AE sources
distribution given in Fig. 14, where the uniform distribution of
AE sources are caused by the multiple micro-defects generated
in strain hardening UHPC and the localized distribution of AE
sources are caused by the several hairline cracks in strain
softening UHPC.
4.2 Calculation of Relaxation Degree of Four Kinds of
UHPCs
To exclude the effect of the expansion by hydration heat during
the early age (about 1d), the analysis of relaxation degree caused
by UHPC shrinkage in ASTM C1581-04 (2004) ring test was
conducted from the time of 2d.
The restrained tensile stress and the theoretical elastic tensile
stress can be used together to describe the effect of stress
relaxation of UHPC in the restrained condition. The maximum
restrained tensile stress σres-max of UHPC can be calculated by Eq.
(4). The maximum theoretical elastic tensile stress σela-max can be
calculated by Eq. (5) (Yoo et al., 2013). The effect of stress
relaxation is represented by the relaxation degree λ, which is
defined as the amount of relaxed stress σrel of UHPC relative to
the maximum theoretical elastic tensile stress σela-max as Eq. (6)
(Altoubat et al., 2017).
(5)
(6)
Where νs and νc are the Poisson’s ratios for steel (0.3) and
UHPC (0.2), respectively. Ec is the elastic modulus of UHPC
which is taken from Table 5. The larger the relaxation degree λ is,
the weaker the interaction between UHPC and steel ring is.
Relaxation degree-age curves of SHU-0, SHU-3, SHU-6 and
SSU-0 are shown in Fig. 15. As shown in Fig. 15, for SHU-0 and
SSU-0 without HCSA, the relaxation degree decreased within
the range of 2-6 days and finally became stable at 28d. SHU-0
showed a lower relaxation degree λ of 0.78 than SSU-0 of 0.81 at
28d, which meant that the interaction between SHU-0 and steel
ring was stronger than that of SSU-0, namely SHU-0 accumulated
more restrained tensile stress than SSU-0. It will become a
negative factor when SHU-0 is applied in the steel-UHPC composite
deck system as shown in Fig. 1(a). From the comparison of
SHU-0, SHU-3 and SHU-6, it can be observed that SHU-3 and
SHU-6 reached the stable state at around 3 days, which was
earlier than SHU-0. It was possibly due to the addition of HCSA.
At the latter age (7d − 28d), the relaxation degree of SHU-0
decreased smoothly, while that of SHU-3 and SHU-6 was almost
stable with the slight fluctuations. It may be related to the effect
of HCSA expansion agent. HCSA expansion agent can be
( )( ) ( ) ( ) ( )
2 2
2 2 2 21 1 1 1
c s os oc sh
ela max
c s is s os s c os c oc
E E r r
E ν r ν r E ν r ν r
ε
σ−
+=
⎡ ⎤ ⎡ ⎤+ + − + − + +⎣ ⎦ ⎣ ⎦
maxela
maxres1λ
−
−
−=
σ
σ
Fig. 14. Strain Transfer Modelling of UHPC: (a) Strain Hardening UHPC, (b) Strain Softening UHPC
Fig. 15. Relaxation Degree-age Curves of SHU-0, SHU-3, SHU-6
and SSU-0
Restrained Shrinkage Mechanism of Ultra High Performance Concrete
Vol. 00, No. 0 / 000 0000 − 11 −
affected by the air moisture, which leads to the fluctuations. The
relaxation degree λ of SHU-3, SHU-6 at 28d was 0.8, 0.88,
respectively. It can be found that the relaxation degree λ of strain
hardening UHPC increased with the increase of HCSA dosage
from 0% to 6%, which meant that HCSA can be used to reduce
the interaction between strain hardening UHPC and steel ring
caused by the restrained shrinkage and reserve more tensile
capacity for strain hardening UHPC in the service condition.
HCSA will benefit the application of strain hardening UHPC in
the steel-UHPC composite deck system.
5. Conclusions
In this study, the restrained shrinkage mechanism of UHPC
was analyzed based on its tensile properties accompanied with
AE analysis method, free shrinkage behavior and restrained
shrinkage performance. The effects of UHPC tensile properties
(strain softening or strain hardening) and HCSA dosages (0%,
3% and 6% by mass of total binder) were investigated. The
restrained shrinkage cracking mechanism of strain hardening
UHPC and strain softening UHPC was analyzed, and the effect
of HCSA dosages on the restrained shrinkage and relaxation
degree of strain hardening UHPC was studied. Based on the
experimental results, the following conclusions can be drawn:
1. Strain hardening UHPC has a better crack width controlling
ability than strain softening UHPC, considering the effect of
the restrained shrinkage on cracking of UHPC. The crack
width of strain hardening UHPC is lower than 0.01 mm
while there are four hairline cracks (0.035 mm, 0.05 mm,
0.04 mm and 0.02 mm) generated in strain softening UHPC
in ACTM C1581 ring test.
2. In the restrained condition, the restrained stress of strain
hardening UHPC is released by the generation of many mar-
ginal instantaneous stress relaxations, while the restrained
stress strain softening UHPC is released by the generation of
several evident instantaneous stress relaxations.
3. In the restrained condition, free shrinkage strain transforms into
restrained shrinkage strain, elastic tensile strain and plastic ten-
sile strain for UHPC. The plastic tensile strain is the irrecover-
able deformation mainly caused by multiple invisible micro-
defects for strain hardening UHPC and mainly caused by sev-
eral hairline cracks for strain softening UHPC.
4. In ASTM C1581-04 (2004) ring test, the restrained shrink-
age of strain hardening UHPC with HCSA dosage of 0%,
3% and 6% at 80d is 141 με, 96 με and 16 με, respectively.
The relaxation degree of strain hardening UHPC with
HCSA dosage of 0%, 3% and 6% at 28d is 0.78, 0.8 and
0.88, respectively. The HCSA expansion agent can effec-
tively reduce the restrained shrinkage of UHPC and the
influence on the structure.
Acknowledgements
This work was supported by the Science and Technology
Department of Zhejiang Province (grant number 2019-GXKY-
01), the National Nature Science Foundation of China (grant
number 51609172) and the Shanghai Municipal Science and
Technology Project [grant number 17DZ1204200]. The financial
supports are greatly appreciated.
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