# Comprehensive Testing Techniques for the Measurement of Shrinkage and Structural Changes of Fine-Grained Cement-Based Composites during Ageing

Authors: Barbara Kucharczyková; Libor Topolář; Petr Daněk; Dalibor Kocáb; Petr Misák
Journal: Advances in Materials Science and Engineering
 (2017)

---

## Abstract

The paper deals with an experimental analysis focusing on the utilization of a specific measurement technique for determining the development of shrinkage and for monitoring structural changes in fine-grained cement-based composites during their ageing. Advanced measurement equipment and procedure allowing simultaneous measurement of length changes, mass losses, acoustic responses, and temperature development were designed and verified by the experimental investigation. The main scope of the experiments performed was focused on finding the relationships between the characteristics being investigated while maintaining a uniform test setup. For the purpose of the experimental measurement, three fine-grained cement composite mixtures were designed and manufactured. The mixtures differed in the water-to-cement ratio (w/c) and in the amount of plasticizer. The measurement outputs are presented in the form of diagrams showing the relations between the studied parameters, such as relative length changes, mass losses, temperature progress, and acoustic emission (AE) activity during solidification of the composites. The measurement results showed close relations between the examined characteristics. The progress of relative length changes together with the progress of mass losses and temperature development is reflected in the AE activity. The advanced measurement procedure and technique provided valuable information about the behaviour of cement-based composites during early setting and long-term hardening.


---

## Body

## 1. Introduction

The determination of the volume change development and crack formation in cement-based composites is currently receiving attention from civil engineers and concrete producers. Along with the design of new materials, factors influencing volume changes appear throughout the whole period of their setting and hardening [1, 2]. Progress in technology and the composition of building materials require advancements in test procedures for determining the physical and mechanical parameters of new materials. The current testing approach is based on the earliest possible identification of disruptions in the internal structure of structural elements, which facilitates early diagnostics of the problem allowing relevant precautions to be taken in order to prevent later collapse of the structure being designed.The reason why this area is being focused on is because many problems with cracking of cement composites arise at early ages [3–5]. In civil engineering, crack formation and propagation are closely associated with tensile strength (the value of which is generally only about 10 percent of that of compressive strength) and with fracture parameters. At early ages, there are internal stresses generated by volume changes but the strength of the element is not yet fully developed. Controlling the variables that affect volume change can minimize high stresses and cracking [4, 6, 7]. Recent measurements suggest the necessity of assessing the magnitude of shrinkage in two consecutive stages of a composite’s ageing, at an early age and at later ages [7–10]. Early-age measurements reveal differences in the development of volume changes as well as differences in the initiation and propagation of cracks which cannot normally be identified with traditional measurement made after specimens have been removed from moulds (typically after 24 hours) [11]. Literature offers a number of approaches to determine the value of cement-based composite shrinkage [12–14]. However, these methods mostly determine separate components of shrinkage at an early age, for example, methods for determining plastic or autogenous shrinkage [5, 6, 9, 13, 15–18] and methods for determining the shrinkage due to drying (defined mainly in the standards of various countries). Contemporary approaches to shrinkage measurement are based primarily on the determination of relative length changes. In most cases, measurement begins after removing specimens from moulds, which is typically no sooner than 24 hours of ageing. In important or complicated concrete structures, such as bridges, suspended slabs, or structures with a complex shape, shrinkage can be measured directly on a concrete element using a special type of wire strain gauge designed to be embedded directly in the concrete. Such gauges are typically fixed to the reinforcement cage of the element by means of rebar extensions [19–23]. Guidelines reflecting recent progress in theoretical and experimental research in the field of cement composite creep and shrinkage (especially concrete) have been published under RILEM TC-242-MDC (chair Zdeněk P. Bažant) [24].In recent years, the method of acoustic emission (AE) has also been widely used as supplemental measurement in the nondestructive monitoring of changes in a specimen’s internal structure during static and dynamic loading tests as well as for the monitoring of the behaviour of composite materials during setting and hardening [11, 25, 26]. The AE method is considered to be a “passive” nondestructive technique because it usually identifies defects as they develop during the test [27] and allows the monitoring of changes in the behaviour of materials over a long period of time without moving any of their components. This, together with its ability to detect crack propagation taking place not only on the surface but also deep inside the material, makes the technique quite unique.A crack developing in a material is accompanied by the release of stored strain energy, which is then consumed by nucleating new external surfaces (cracks) and emitting elastic waves known as AE waves. The elastic waves propagate inside a material and are detected by an AE sensor. With the exception of contactless sensors, AE sensors are directly attached to the surface [28].In practice, there are situations where attaching a sensor directly onto the surface is not possible, for example, installation onto a part of an element that is inaccessible or onto a surface which reaches very high temperatures. Detection sensitivity can be increased by using a waveguide. A typical case in civil engineering is the placement of a waveguide into a prepared hole in a fresh composite. An acoustic waveguide is a physical structure for guiding sound waves, that is, a sound-propagation duct that behaves like a transmission line. The duct contains some sound-propagation medium [8].


## 2. Experimental Part

### 2.1. Materials

Three fine-grained cement composite mixtures were designed and manufactured for the purposes of the experiment. They differed in the water-to-cement ratio (w/c) and in the amount of plasticizer. Compositions of mixtures are based on the standard ČSN EN 196-1 [29]. The fresh composite was made with standardized quartzite sand (maximum nominal grain size of 2 mm pursuant to ČSN EN 196-1 [29]) and CEM I 42.5 R Portland cement and water at a ratio of 3 : 1 : 0.5 (S : C : W), 3 : 1 : 0.47, and 3 : 1 : 0.35 with the addition of SIKA SVC 4035 superplasticizer (polycarboxylate ether-based technology) at an amount of 1% by cement mass. A mixing device with controllable mixing speed was used to prepare the fresh mixtures. Six specimens with the dimensions of 100 × 60 × 1000 were prepared from each mixture. Table 1 shows basic information about the composition, manufacturing, and fresh-state properties. The workability was determined using the flow table with a calibrated scale designed for the testing of fresh mortars pursuant to ČSN EN 1015-3 [30]. Bulk density of the fresh composite was determined in accordance with ČSN EN 1015-6 [31] using a calibrated vessel with the volume of 1 dm3.Table 1
Composition and properties of fresh composites.
Components and properties
Units
Composite ID
0
III
IV
Sand
kg
45.9
45.9
45.9
Cement I 42.5 R
kg
15.3
15.3
15.3
Water
kg
7.65
7.16
5.35
Superplasticizer SVC 4035
% by cement mass
—
—
1.0
w/c ratio
—
0.5
0.47
0.35
Mixing speed
Revolutions/min
20
30
40
Workability
mm
140
128
135
Bulk density
kg/m3
2200
2210
2280


### 2.2. Test Equipment and Procedures

#### 2.2.1. Determination of Length Changes

The measurement procedure designed to determine the progress of cement composites’ shrinkage was designed to simultaneously record relative length changes, mass losses caused by free drying, temperature inside the tested specimens, and AE activity due to structural changes during solidification. The ambient temperature and relative humidity were also monitored. The measurement of shrinkage was performed using measurement equipment standardized pursuant to the Austrian standard OENORM B 3329:2009-06-01 [32]. Special moulds of 1000 mm in length and with a 60 × 100 mm cross section were used for recording the length changes measured along the central axis of the specimens using an inductive sensor leaning against the movable head of the mould. These moulds are primarily designed for cement composite shrinkage measurement in the early stages of setting and hardening. Special markers designed at the Brno University of Technology (BUT) were used to perform subsequent long-term measurement of relative deformation [33]. These markers were embedded into the upper surface of the cement composite placed in the shrinkage moulds. This way, two gauging bases were created for further measurement (see ‎Figure 1). This arrangement enabled the capture of the total relative length change of the composite since the time at which the composite is placed into the mould until its long-term ageing after the specimen has been removed from the shrinkage mould. Details about the marker types and their drawing and arrangement can be found in [33]. A polyethylene foam mat (MIRELON) of 2 mm in thickness was placed on the bottom and along both sides of the shrinkage moulds in order to ensure that the specimen can move freely in the mould. The shrinkage moulds were filled with a fine-grained cement composite and placed onto a special weighing table that enables continuous recording of mass losses caused by free drying of the specimen surfaces. For more details about the weighing table, see [34].Figure 1
Arrangement of measurement devices (1: shrinkage mould; 2: weighing table; 3: acoustic emission sensor with a waveguide; 4: temperature probe; 5: markers for long-term measurement).A thermal sensor COMET was embedded at one end of the shrinkage moulds in order to measure the temperature inside the specimens. The ambient temperature and relative humidity were recorded by an automatic gauging station COMET.This measurement configuration enabled simultaneous measurement of all investigated parameters of the composite placed in a shrinkage mould. The final arrangement of the measurement devices before starting the measurement is shown in ‎Figure1.Note that the measurement in shrinkage moulds can only be started after the composite has set a little so that the movable head of the mould is not pushed out under the composite’s own weight. Due to the consistency of the fresh composite, measurement was started approximately one hour after the composite was poured into the moulds. The length change was measured on the specimens in the moulds, which were placed on the weighing table standing on hard rubber pads in a climate control chamber at a temperature of 21 ± 2°C and relative humidity of 60 ± 10% until the composite was 3 days old. The top surface of the composite was not protected from drying. During this time, the chamber was locked, which prevented people from entering the chamber so that the measurement could continue undisturbed. Also, the shrinkage moulds and all measurement devices were secured against movement.Once early measurement was finished, the specimens were extracted from the moulds, placed on the table, and left to dry freely in the climate chamber at a stable temperature of 21 ± 2°C and relative humidity of 60 ± 10%. The following measurements were performed using a strain gauge which was fixed onto the surface of the specimens. The positions of the gauging points were predefined by the markers embedded at spacing of 200 mm. The specimens were left to dry freely throughout the entire time of the measurement and were weighed at regular intervals.


#### 2.2.2. Determination of Structural Changes by Acoustic Emission Method

Changes in the specimens’ internal structure during the early stage of setting and hardening were monitored using the nondestructive passive method of AE. Magnetic AE sensors (type IDK09 with 35 dB preamplifier) were placed in positions predefined by the embedded steel probes (waveguides) (see ‎Figure1). Drawing on experience from previous measurements, the threshold was set to the value of 72 μV. The threshold value of the signals was set with the aim of eliminating background noise and recording only the signals produced by the formation of the material’s microstructure and internal cracking. The measurement chain consists of the measurement sensor attached to the waveguide followed by a preamplifier with a gain of 35 dB and finally there is a data recorder with a software preamplifier with a gain of 40 dB. The internal structure changes were monitored with two AE sensors placed in each shrinkage mould: the first one was placed near the movable head (AE2) and the second one was located near the other end of the mould (AE3). This way, the progress of events occurring during the cement composites’ setting and hardening was recorded continuously. AE signals were being detected for 72 hours by the measuring equipment DAKEL XEDO with two channels. The measurement of AE was started together with the measurement of relative length changes, mass losses, and temperature. To eliminate outside noise, guard sensors were placed on the bottom of the frame of the shrinkage moulds. This setup ensured that AE waves coming from the area being measured hit the sensors on the waveguides before hitting any of the guards. Conversely, waves from outside hit at least one of the guards before hitting the sensors on the waveguides.


## 2.1. Materials

Three fine-grained cement composite mixtures were designed and manufactured for the purposes of the experiment. They differed in the water-to-cement ratio (w/c) and in the amount of plasticizer. Compositions of mixtures are based on the standard ČSN EN 196-1 [29]. The fresh composite was made with standardized quartzite sand (maximum nominal grain size of 2 mm pursuant to ČSN EN 196-1 [29]) and CEM I 42.5 R Portland cement and water at a ratio of 3 : 1 : 0.5 (S : C : W), 3 : 1 : 0.47, and 3 : 1 : 0.35 with the addition of SIKA SVC 4035 superplasticizer (polycarboxylate ether-based technology) at an amount of 1% by cement mass. A mixing device with controllable mixing speed was used to prepare the fresh mixtures. Six specimens with the dimensions of 100 × 60 × 1000 were prepared from each mixture. Table 1 shows basic information about the composition, manufacturing, and fresh-state properties. The workability was determined using the flow table with a calibrated scale designed for the testing of fresh mortars pursuant to ČSN EN 1015-3 [30]. Bulk density of the fresh composite was determined in accordance with ČSN EN 1015-6 [31] using a calibrated vessel with the volume of 1 dm3.Table 1
Composition and properties of fresh composites.
Components and properties
Units
Composite ID
0
III
IV
Sand
kg
45.9
45.9
45.9
Cement I 42.5 R
kg
15.3
15.3
15.3
Water
kg
7.65
7.16
5.35
Superplasticizer SVC 4035
% by cement mass
—
—
1.0
w/c ratio
—
0.5
0.47
0.35
Mixing speed
Revolutions/min
20
30
40
Workability
mm
140
128
135
Bulk density
kg/m3
2200
2210
2280


## 2.2. Test Equipment and Procedures

### 2.2.1. Determination of Length Changes

The measurement procedure designed to determine the progress of cement composites’ shrinkage was designed to simultaneously record relative length changes, mass losses caused by free drying, temperature inside the tested specimens, and AE activity due to structural changes during solidification. The ambient temperature and relative humidity were also monitored. The measurement of shrinkage was performed using measurement equipment standardized pursuant to the Austrian standard OENORM B 3329:2009-06-01 [32]. Special moulds of 1000 mm in length and with a 60 × 100 mm cross section were used for recording the length changes measured along the central axis of the specimens using an inductive sensor leaning against the movable head of the mould. These moulds are primarily designed for cement composite shrinkage measurement in the early stages of setting and hardening. Special markers designed at the Brno University of Technology (BUT) were used to perform subsequent long-term measurement of relative deformation [33]. These markers were embedded into the upper surface of the cement composite placed in the shrinkage moulds. This way, two gauging bases were created for further measurement (see ‎Figure 1). This arrangement enabled the capture of the total relative length change of the composite since the time at which the composite is placed into the mould until its long-term ageing after the specimen has been removed from the shrinkage mould. Details about the marker types and their drawing and arrangement can be found in [33]. A polyethylene foam mat (MIRELON) of 2 mm in thickness was placed on the bottom and along both sides of the shrinkage moulds in order to ensure that the specimen can move freely in the mould. The shrinkage moulds were filled with a fine-grained cement composite and placed onto a special weighing table that enables continuous recording of mass losses caused by free drying of the specimen surfaces. For more details about the weighing table, see [34].Figure 1
Arrangement of measurement devices (1: shrinkage mould; 2: weighing table; 3: acoustic emission sensor with a waveguide; 4: temperature probe; 5: markers for long-term measurement).A thermal sensor COMET was embedded at one end of the shrinkage moulds in order to measure the temperature inside the specimens. The ambient temperature and relative humidity were recorded by an automatic gauging station COMET.This measurement configuration enabled simultaneous measurement of all investigated parameters of the composite placed in a shrinkage mould. The final arrangement of the measurement devices before starting the measurement is shown in ‎Figure1.Note that the measurement in shrinkage moulds can only be started after the composite has set a little so that the movable head of the mould is not pushed out under the composite’s own weight. Due to the consistency of the fresh composite, measurement was started approximately one hour after the composite was poured into the moulds. The length change was measured on the specimens in the moulds, which were placed on the weighing table standing on hard rubber pads in a climate control chamber at a temperature of 21 ± 2°C and relative humidity of 60 ± 10% until the composite was 3 days old. The top surface of the composite was not protected from drying. During this time, the chamber was locked, which prevented people from entering the chamber so that the measurement could continue undisturbed. Also, the shrinkage moulds and all measurement devices were secured against movement.Once early measurement was finished, the specimens were extracted from the moulds, placed on the table, and left to dry freely in the climate chamber at a stable temperature of 21 ± 2°C and relative humidity of 60 ± 10%. The following measurements were performed using a strain gauge which was fixed onto the surface of the specimens. The positions of the gauging points were predefined by the markers embedded at spacing of 200 mm. The specimens were left to dry freely throughout the entire time of the measurement and were weighed at regular intervals.


### 2.2.2. Determination of Structural Changes by Acoustic Emission Method

Changes in the specimens’ internal structure during the early stage of setting and hardening were monitored using the nondestructive passive method of AE. Magnetic AE sensors (type IDK09 with 35 dB preamplifier) were placed in positions predefined by the embedded steel probes (waveguides) (see ‎Figure1). Drawing on experience from previous measurements, the threshold was set to the value of 72 μV. The threshold value of the signals was set with the aim of eliminating background noise and recording only the signals produced by the formation of the material’s microstructure and internal cracking. The measurement chain consists of the measurement sensor attached to the waveguide followed by a preamplifier with a gain of 35 dB and finally there is a data recorder with a software preamplifier with a gain of 40 dB. The internal structure changes were monitored with two AE sensors placed in each shrinkage mould: the first one was placed near the movable head (AE2) and the second one was located near the other end of the mould (AE3). This way, the progress of events occurring during the cement composites’ setting and hardening was recorded continuously. AE signals were being detected for 72 hours by the measuring equipment DAKEL XEDO with two channels. The measurement of AE was started together with the measurement of relative length changes, mass losses, and temperature. To eliminate outside noise, guard sensors were placed on the bottom of the frame of the shrinkage moulds. This setup ensured that AE waves coming from the area being measured hit the sensors on the waveguides before hitting any of the guards. Conversely, waves from outside hit at least one of the guards before hitting the sensors on the waveguides.


## 2.2.1. Determination of Length Changes

The measurement procedure designed to determine the progress of cement composites’ shrinkage was designed to simultaneously record relative length changes, mass losses caused by free drying, temperature inside the tested specimens, and AE activity due to structural changes during solidification. The ambient temperature and relative humidity were also monitored. The measurement of shrinkage was performed using measurement equipment standardized pursuant to the Austrian standard OENORM B 3329:2009-06-01 [32]. Special moulds of 1000 mm in length and with a 60 × 100 mm cross section were used for recording the length changes measured along the central axis of the specimens using an inductive sensor leaning against the movable head of the mould. These moulds are primarily designed for cement composite shrinkage measurement in the early stages of setting and hardening. Special markers designed at the Brno University of Technology (BUT) were used to perform subsequent long-term measurement of relative deformation [33]. These markers were embedded into the upper surface of the cement composite placed in the shrinkage moulds. This way, two gauging bases were created for further measurement (see ‎Figure 1). This arrangement enabled the capture of the total relative length change of the composite since the time at which the composite is placed into the mould until its long-term ageing after the specimen has been removed from the shrinkage mould. Details about the marker types and their drawing and arrangement can be found in [33]. A polyethylene foam mat (MIRELON) of 2 mm in thickness was placed on the bottom and along both sides of the shrinkage moulds in order to ensure that the specimen can move freely in the mould. The shrinkage moulds were filled with a fine-grained cement composite and placed onto a special weighing table that enables continuous recording of mass losses caused by free drying of the specimen surfaces. For more details about the weighing table, see [34].Figure 1
Arrangement of measurement devices (1: shrinkage mould; 2: weighing table; 3: acoustic emission sensor with a waveguide; 4: temperature probe; 5: markers for long-term measurement).A thermal sensor COMET was embedded at one end of the shrinkage moulds in order to measure the temperature inside the specimens. The ambient temperature and relative humidity were recorded by an automatic gauging station COMET.This measurement configuration enabled simultaneous measurement of all investigated parameters of the composite placed in a shrinkage mould. The final arrangement of the measurement devices before starting the measurement is shown in ‎Figure1.Note that the measurement in shrinkage moulds can only be started after the composite has set a little so that the movable head of the mould is not pushed out under the composite’s own weight. Due to the consistency of the fresh composite, measurement was started approximately one hour after the composite was poured into the moulds. The length change was measured on the specimens in the moulds, which were placed on the weighing table standing on hard rubber pads in a climate control chamber at a temperature of 21 ± 2°C and relative humidity of 60 ± 10% until the composite was 3 days old. The top surface of the composite was not protected from drying. During this time, the chamber was locked, which prevented people from entering the chamber so that the measurement could continue undisturbed. Also, the shrinkage moulds and all measurement devices were secured against movement.Once early measurement was finished, the specimens were extracted from the moulds, placed on the table, and left to dry freely in the climate chamber at a stable temperature of 21 ± 2°C and relative humidity of 60 ± 10%. The following measurements were performed using a strain gauge which was fixed onto the surface of the specimens. The positions of the gauging points were predefined by the markers embedded at spacing of 200 mm. The specimens were left to dry freely throughout the entire time of the measurement and were weighed at regular intervals.


## 2.2.2. Determination of Structural Changes by Acoustic Emission Method

Changes in the specimens’ internal structure during the early stage of setting and hardening were monitored using the nondestructive passive method of AE. Magnetic AE sensors (type IDK09 with 35 dB preamplifier) were placed in positions predefined by the embedded steel probes (waveguides) (see ‎Figure1). Drawing on experience from previous measurements, the threshold was set to the value of 72 μV. The threshold value of the signals was set with the aim of eliminating background noise and recording only the signals produced by the formation of the material’s microstructure and internal cracking. The measurement chain consists of the measurement sensor attached to the waveguide followed by a preamplifier with a gain of 35 dB and finally there is a data recorder with a software preamplifier with a gain of 40 dB. The internal structure changes were monitored with two AE sensors placed in each shrinkage mould: the first one was placed near the movable head (AE2) and the second one was located near the other end of the mould (AE3). This way, the progress of events occurring during the cement composites’ setting and hardening was recorded continuously. AE signals were being detected for 72 hours by the measuring equipment DAKEL XEDO with two channels. The measurement of AE was started together with the measurement of relative length changes, mass losses, and temperature. To eliminate outside noise, guard sensors were placed on the bottom of the frame of the shrinkage moulds. This setup ensured that AE waves coming from the area being measured hit the sensors on the waveguides before hitting any of the guards. Conversely, waves from outside hit at least one of the guards before hitting the sensors on the waveguides.


## 3. Results and Discussion

The measurement results are presented below. Table2 and ‎Figure 2 show the development of compressive strength and dynamic modulus of elasticity determined for all the mixtures being examined. The results confirm general presumptions. The highest values of both parameters were found in mixture IV (loww/c with the addition of plasticizer).Table 2
Values of compressive strength and dynamic modulus of elasticity.
Composite ID
Age of specimens [days]
3
28
90
3
28
90
Compressive strength [N/mm2]  (standard deviation)
Dynamic modulus of elasticity [N/mm2]  (standard deviation)
0
27.28(1.84)
36.53(2.57)
37.62(2.32)
27340(669)
27735(724)
28693(492)
III
30.80(1.92)
42.38(4.01)
49.03(3.87)
29487(473)
30698(424)
31047(610)
IV
50.61(2.90)
54.90(5.49)
62.10(5.08)
36962(782)
37500(786)
37903(854)Figure 2
Development of compressive strength (a) and dynamic modulus of elasticity (b) during composite ageing.
(a)
(b)Concerning shrinkage measurement, the following trends were found. ‎Figure3 shows the progress of relative deformation and mass losses determined at an early age. The data were obtained from measurements performed on the specimens in shrinkage moulds placed on a weighing table. As shown below, different progress of shrinkage and mass losses were recorded for the mixtures being investigated (see ‎Figure 3). Shortly after the start of the measurement, both mixtures without plasticizer were expanding (length increment), while specimens with plasticizer were shrinking rapidly (see ‎Figure 3(a)).Figure 3
Relative deformations and mass losses measured during the first 72 hours of specimen ageing.
(a)
(b)Also, the progress of mass losses recorded within the first 72 hours of ageing is different in mixtures which contain plasticizer and which do not. The mass losses of both composites without plasticizer are higher than in the case of the composite with plasticizer (see ‎Figure3(b)). This progression is closely linked with the adjustment of water content. Once plasticizer is added, water content is reduced which influences the progress of volume changes as well as mass losses. Thus, thew/c ratio of the composites without plasticizer was rather high (see Table 1). No component segregation in fresh mixture was observed during either the mixing or the manufacturing of the test specimens. On the other hand, a relatively large amount of water rose to the upper surface of the test specimens after their manufacturing and storing. This phenomenon is commonly known as bleeding [35]. Gradually, during the solidification of the composite, a part of the water evaporates from the specimen surface, causing mass losses, while some amount is drawn back into the pore structure of the composite, contributing to the composite’s expansion [9].It is known and has been proven by previous experimental measurements [36] that the addition of plasticizer also has a substantial influence on cement hydration. The addition of superplasticizer retards cement hydration and has a critical influence on its overall progress. The margin of hydration retardation is strongly dependent on the amount and properties of the cement and plasticizer used in the composite mixture [37].The progress of shrinkage corresponds well with the progress of temperature measured inside the test specimens (see ‎Figure4). In case of composites without superplasticizer, the highest temperature was recorded approximately 11 hours after the start of measurement. At that same time, a surge of expansion (length increment) can be seen as well. This length increment can be ascribed to the cement composites’ thermal expansion. It was proved by earlier measurements that the initial expansion is typical for cement composites with a highw/c ratio [4]. The origin of this expansion is not fully understood and is the object of ongoing research. Similar relationship between temperature and progress of deformation was recorded in the composite with superplasticizer. The presence of the superplasticizer retarded early hydration and delayed temperature growth by approximately 5 hours (in comparison with the composite without the plasticizer). A dormant period accompanied by short expansion during the progress of shrinkage was observed after the maximum temperature was measured.Figure 4
Relative deformations and temperature measured inside the test specimen (during the first 72 hours of specimen ageing).Next progress of shrinkage in all mixtures is affected by the setup of the experiment. Note that in this stage of measurement the test specimens are placed in the shrinkage moulds and only the specimens’ upper surface is not protected from drying. This fact is also reflected in the progress of mass losses whereas the most prominent effect was observed in mixture IV (see ‎Figures3(b) and 9(b)).Concerning the AE measurement, different results were again obtained for mixtures with and without superplasticizer. The acoustic waves recorded by the measurement equipment were converted to a number of overshoots for the purposes of result interpretation. This number of overshoots indicates the number and size of structural changes taking place within a certain period. Note that there is not a strict relationship between a particular structural change and the number of overshoots. This number can be defined as a relative value relating to the setting of the measurement sensitivity that must always be the same for all measurements performed as part of comparative tests. At the start of measurement, a high number of AE signals’ overshoots exceed the adjusted threshold value (see ‎Figure5). The high number of AE overshoots is due to the physical and chemical changes which take place in this early setting phase. During the first hours of composite solidification, plastic shrinkage is taking place. The movement of particles and the formation of new hydration products are the primary sources of the acoustic waves’ formation. The data show that, in this early setting phase, the mixture with plasticizer (composite IV, ‎Figure 6) exhibited a lower number of AE overshoots than both mixtures without plasticizer, composites 0 and III (‎Figure 5). This is closely connected with thew/c ratio and initial bleeding observed in composites without superplasticizer. After the initial setting was finished, no notable structural changes were recorded for the mixtures without plasticizer until 20 hours of age (see ‎Figure 5). The mixture with superplasticizer behaved rather differently; after the initial activity, another acoustic response was recorded at the time of initial temperature growth. Within the same period, a surge of shrinkage was recorded too (see ‎Figures 4 and 6). This behaviour is associated with the loww/c ratio (of mixture IV), retardation of early hydration, and temperature growth due to the presence of plasticizer (as mentioned above). After 20 hours of ageing, more acoustic activity was recorded again in all the mixtures. Taking into account the fact that all of the composites had hardened by this stage, it is possible that the increased AE activity originated from the creation of microcracks (the highest AE activity recorded in mixture 0 with the highestw/c ratio) and continuing formation of microstructure. Determining whether the AE activity is actually due to the formation of microcracks would require further research to verify that relationship. The lowest AE activity was recorded in mixture IV. This behaviour is connected with the rapid growth of strength which is typical for composites with a loww/c ratio with the addition of a superplasticizer (see Table 2 and ‎Figure 2).Figure 5
Relative deformations and AE overshoots measured during the first 72 hours of specimen ageing for mixtures without a superplasticizer.Figure 6
Relative deformations and AE overshoots measured during the first 72 hours of specimen ageing for mixture with a superplasticizer.The AE responses are also presented in connection with the progress of relative deformations and mass losses of the mixtures. The results are presented in Figures7(a), 7(b), and 8 showing curves representing the relationship between the relative length changes (ε) and mass losses (m) of the specimens during the first 72 hours of ageing together with the AE responses recorded during the same period. ‎Figure 7 shows the results for mixtures without superplasticizer. The graphs show that the progress of the initial part of the ε
-
m relationship is in both mixtures affected by their initial expansion (length increment) caused by thermal expansion and water reabsorption. Supposing that the increased initial AE activity due to plastic settlement and the initial formation of the composite microstructure are not taken into account, there are two other significant factors which lead to an increase in the AE activity during composite solidification: actual thermal conditions inside the test specimens and rapid changes in the progress of shrinkage.Figure 7
Relationship between deformations and mass losses together with the AE overshoots measured during the first 72 hours of specimen ageing for mixtures without a superplasticizer.
(a)
(b)Figure 8
‎ Relationship between deformations and mass losses together with the AE overshoots measured during the first 72 hours of specimen ageing for mixture with superplasticizer.Figure 9
Progress of relative deformations and mass losses measured over the whole time of specimen ageing.
(a)
(b)Figure7(a) shows measurement results for the mixture with the highestw/c ratio. The first appearance of increased AE activity (a high number of overshoots) between 25 and 40 hours of age corresponds to the time when the temperature measured inside the test specimens dropped to its steady-state value. Within this time period, the temperature no longer contributes to the specimen expansion. The second period with high AE activity is visible at the time when the expansion (length increment) is changed to the shrinkage (length decrement). The curvature of the ε
-
m relationship is also visibly changed. Similar results were recorded also in mixture III (see ‎Figure 7(b)). Results obtained for mixture IV are rather different because the progress of shrinkage and mass losses were not affected by initial expansion and the temperature growth was delayed due to the presence of superplasticizer. Nevertheless, the results shown in ‎Figure 8 indicate that the increased AE activity corresponds to the changes in curvature of the ε
-
m relationship.Concerning the results of long-term measurement, it can be stated that the addition of superplasticizer has a substantial influence on the total progress of relative deformations (see ‎Figure9). The initial rapid growth of shrinkage influences also its final values which are more than two times higher than the values recorded in the cement composite without the superplasticizer with aw/c ratio of 0.5. The period of expansion appears not to be very significant in terms of magnitude. However, the initial expansion delayed the start of shrinkage by more than 20 hours. This delay can be of great benefit to the later development of physical and mechanical properties of cement composites. The total progress of mass losses corresponds well with the water content of the mixtures (see Table 1). The lowest mass loss was recorded in the composite with the superplasticizer with aw/c ratio of 0.35.The relationship between relative length changes and mass losses was observed over the whole time of the cement composite ageing (see ‎Figure10). However, the initial part of the curve is influenced by water reabsorption and thermal expansion.Figure 10
Relationship between deformations and mass losses measured over the whole time of specimen ageing.


## 4. Conclusion

The main aim of the experiments performed was to present comprehensive test techniques that can be used for the determination of shrinkage development in fine-grained cement-based composites and for monitoring structural changes throughout their ageing. The experimental investigation made use of advanced measurement equipment and procedure allowing the simultaneous measurement of length changes, mass losses, acoustic responses, and temperature development. The results were compared in terms of the overall behaviour of the studied materials with respect to a uniform setup of the test equipment (accuracy, sensitivity, curing conditions, etc.). Based on the results, it can be stated that the measurement technique described in the paper and used in the experiment fully satisfies the requirements for early-age diagnostics of the material’s behaviour. The measurement of relative length changes together with the recorded progress of mass losses and temperature measured inside the test specimens provided comprehensive information about the behaviour of the material in the early stage of its setting and hardening. The possibility of continuing to measure the relative length changes as well as mass losses of the test specimens, after they were removed from moulds, provided data about the continuous progress of the investigated characteristics during the whole time of the composites’ setting and hardening. The method of acoustic emission appears to be another suitable tool for continuous nondestructive monitoring of the structural changes taking place while the materials solidify. The conclusions presented in the article contain only a small fraction of the information contained in the AE data. The aim of the performed measurements was to compare the results obtained by measurements of three different mixtures manufactured, cured, stored, and measured under the same conditions. In this case, the absolute number of overshoots is not very important. Responses of the changes in the internal structure are strongly dependent on the material’s composition (the same response can induce a different number of overshoots in different materials). More important for the presented measurements was to record the moment and time spectrum (interval) of the overshoots’ appearance. Therefore, it was important to keep the same test setup across all measurements.The possibility of determining the occurrence of microcracks during the setting and hardening of cement composites may be of great use in the early diagnostics of material failures in the future. The number of microcracks present in the cement composites substantially affects their final mechanical properties (i.e., strength, modulus of elasticity, fracture parameters, durability, etc.). The application of the AE method for continuous monitoring of cement composites during the setting and hardening can be useful for early detection of micro disruptions. This information about the behaviour of the material may be later used for improving the material composition or adjusting the curing method which can lead to the design of cement composite structures with better properties. Data obtained from the experiment are of great use in the creation of new and verification of existing computational models designed for the prediction of the progress of volume changes and microcrack development in cement-based composites.



---

*Source: 3832072-2017-01-15.xml*