# Impact of High Temperature on the Compressive Strength of ECC

Authors: Xingyan Shang; Zhoudao Lu
Journal: Advances in Materials Science and Engineering
 (2014)

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## Abstract

The influence of different cooling regimes (quenching in water and cooling in air) on the residual mechanical properties of ECC (engineered cementitious composites) exposed to high temperature up to 800°C was discussed in this paper. The specimens quenching in water gained better mechanical properties than the ones cooling in air. The strengthening effect of quenching for specimens subjected to 800°C was more significant than for the ones subjected to 400°C. The microstructural characterization is examined before and after exposure to fire deterioration by using scanning electron microscopy. Results from the microtest well explained the mechanical properties variation of postfire specimens.


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## Body

## 1. Introduction

Concrete is the most widely used construction material in the world. Although it was primarily designed for carrying compressive loads, concrete in real field conditions is also subjected to tensile stresses because of structural loading, shrinkage (if the shrinkage is restrained), chemical attack, and thermal deformations. The tensile strength of concrete is only approximately 10% of its compressive strength, and brittle concrete cracks when subjected to tensile stresses. In recent years, the effort to modify the brittle nature of ordinary concrete has resulted in modern concepts of ultrahigh performance fiber-reinforced cementitious composites (UHP-FRCC), which are characterized by tensile strain-hardening after first cracking. Depending on its composition, its tensile strain capacity can be up to several hundred times those of normal and fiber-reinforced concrete. ECC is a special type of UHP-FRCC designed based on micromechanical principles to strain-harden in tension. It offers high ductility under uniaxial tensile loading and improved durability due to an intrinsically tight crack width of less than 100μm [1, 2]. During the last decade, the use of ECC has considerably grown up, and it was used in a variety of structures in various regions [3, 4].Significant attention has been brought to the study of its rheological, mechanical, and durability related properties of ECC. With an increase in the application of ECC, the risk of exposure to elevated temperatures increases as well. The behavior of ECC exposed to high temperature has to be evaluated in particular.For normal cement based composite, high temperatures caused physical and chemical changes, resulting in its mechanical property deterioration, such as compressive strength and modulus of elasticity. Different cooling regimes, that is, cooling in air, quenching in water, or water spraying, also had a significant influence on the residual mechanical properties of postfire composite [5, 6]. Gencel  [7] researched the effect of heating duration and cooling regimes on mechanical properties of high strength concrete containing different proportions of hematite. Researchers [8] studied the mechanical and physical properties of lightweight concrete after high temperature. The residual properties of ECC after exposure to high temperatures have also been studied by several researchers, mainly on the heating temperatures and mineral admixtures of fly ash and fiber influence [9, 10]. But there are still some aspects remaining to be studied. The main objective of this research is to gain a better understanding of the influence of cooling regimes on the postfire ECC specimens subjected to high temperature up to 800°C.


## 2. Experimental Studies

### 2.1. Materials, Mix Proportions, and Basic Mechanical Properties

The materials used in the production of ECC mixture were Type I Portland cement (C), Class F fly ash (FA), sand, water, polyvinyl alcohol (PVA) fibers, a polycarboxylic ether type high-range water-reducing admixture (HRWR), and hydroxypropyl methylcellulose (HPMC). The mix details are given in Table1. Unlike typical fiber-reinforced cementitious composites, the component characteristics and proportions within the ECC are carefully determined with the use of micromechanical design tools to achieve the desired strain-hardening response [11, 12]. The PVA fibers with a diameter of 39 μm and a length of 8 mm are purposely manufactured with a tensile strength (1620 MPa), elastic modulus (42.8 GPa), and maximum elongation (6.0%) matching those needed for strain-hardening performance. Additionally, the surface of the PVA fibers is coated with a proprietary oiling agent 1.2% by mass to tailor the interfacial properties between fiber and matrix for strain-hardening performance [11].Table 1
Mixture properties of ECC.
ECC
Cement (C) (kg/m3)
650
Fly ash (FA) (kg/m3)
325
Water (W) (kg/m3)
375
PVA fiber (kg/m3)
26
Sand (kg/m3)
480
HRWR (kg/m3)
12
HPMC (kg/m3)
1.90
W/(C + FA)
0.38
FA/C
50%To characterize the direct tensile behavior of the ECC mixtures, the dog-bone specimens were used. Direct tensile tests [13] were conducted under displacement control at a loading rate of 0.005 mm/s. The typical tensile stress-strain curves of the ECC mixtures at 28 days are shown in Figure 1. The ECC composites exhibited a strain capacity of 4.4% at 28 days, with an ultimate strength of about 5 MPa.Figure 1
Typical tensile stress-strain response of ECC at 28 days.


### 2.2. Test Specimen Preparation and Testing

Specimens were removed from the molds at 1 day and kept in a water tank until the age of 28 days. Five specimens were tested under compression immediately after conditioning; these control specimens will be referred to as those tested after exposure to normal curing condition (unheated).Computer controlled furnace was used for the heating of specimens with constant heating rate of about 13.3°C/min to reach the prescribed 200, 400, 600, and 800°C temperature levels. The temperature was measured in the air at a position above the specimen inside the furnace. The temperature was maintained constant for an hour to achieve the thermal steady state condition after the target temperature was reached. It was expected that because of small size of specimens used in this study, the temperature in the center of the specimen reached the target temperature during the one-hour stabilization phase. The heating regime is shown in Figure2. After heating, the samples were subjected to two cooling regimes as given in Table 2. After cooling, the specimens were sealed for 7 days before the compressive test. The compressive test [14] was performed under displacement control at a loading rate of 0.005 mm/s on a closed-loop controlled material testing system with 100 kN capacity. During the compressive tests, the load and the deflection values (obtained from a pair of LVDT’s attached to the test set-up) were recorded on a computerized data acquisition system. Four samples were tested for each heating temperature and cooling regime.Table 2
Two cooling regimes for different curing age ECC specimens.
Temperature
Cooling in room temperature
Quenching in water
200°C
√
None
400°C
√
√
600°C
√
None
800°C
√
√Figure 2
Heating regime for ECC specimens.The specimens are named as follows: temperature-cooling regime, for example, 400 A(W); here A means cooling in air and W means cooling in water for 5 minutes. The weight of each specimen was also measured before and after exposure to calculate the mass loss of fire-deteriorated specimens.


## 2.1. Materials, Mix Proportions, and Basic Mechanical Properties

The materials used in the production of ECC mixture were Type I Portland cement (C), Class F fly ash (FA), sand, water, polyvinyl alcohol (PVA) fibers, a polycarboxylic ether type high-range water-reducing admixture (HRWR), and hydroxypropyl methylcellulose (HPMC). The mix details are given in Table1. Unlike typical fiber-reinforced cementitious composites, the component characteristics and proportions within the ECC are carefully determined with the use of micromechanical design tools to achieve the desired strain-hardening response [11, 12]. The PVA fibers with a diameter of 39 μm and a length of 8 mm are purposely manufactured with a tensile strength (1620 MPa), elastic modulus (42.8 GPa), and maximum elongation (6.0%) matching those needed for strain-hardening performance. Additionally, the surface of the PVA fibers is coated with a proprietary oiling agent 1.2% by mass to tailor the interfacial properties between fiber and matrix for strain-hardening performance [11].Table 1
Mixture properties of ECC.
ECC
Cement (C) (kg/m3)
650
Fly ash (FA) (kg/m3)
325
Water (W) (kg/m3)
375
PVA fiber (kg/m3)
26
Sand (kg/m3)
480
HRWR (kg/m3)
12
HPMC (kg/m3)
1.90
W/(C + FA)
0.38
FA/C
50%To characterize the direct tensile behavior of the ECC mixtures, the dog-bone specimens were used. Direct tensile tests [13] were conducted under displacement control at a loading rate of 0.005 mm/s. The typical tensile stress-strain curves of the ECC mixtures at 28 days are shown in Figure 1. The ECC composites exhibited a strain capacity of 4.4% at 28 days, with an ultimate strength of about 5 MPa.Figure 1
Typical tensile stress-strain response of ECC at 28 days.


## 2.2. Test Specimen Preparation and Testing

Specimens were removed from the molds at 1 day and kept in a water tank until the age of 28 days. Five specimens were tested under compression immediately after conditioning; these control specimens will be referred to as those tested after exposure to normal curing condition (unheated).Computer controlled furnace was used for the heating of specimens with constant heating rate of about 13.3°C/min to reach the prescribed 200, 400, 600, and 800°C temperature levels. The temperature was measured in the air at a position above the specimen inside the furnace. The temperature was maintained constant for an hour to achieve the thermal steady state condition after the target temperature was reached. It was expected that because of small size of specimens used in this study, the temperature in the center of the specimen reached the target temperature during the one-hour stabilization phase. The heating regime is shown in Figure2. After heating, the samples were subjected to two cooling regimes as given in Table 2. After cooling, the specimens were sealed for 7 days before the compressive test. The compressive test [14] was performed under displacement control at a loading rate of 0.005 mm/s on a closed-loop controlled material testing system with 100 kN capacity. During the compressive tests, the load and the deflection values (obtained from a pair of LVDT’s attached to the test set-up) were recorded on a computerized data acquisition system. Four samples were tested for each heating temperature and cooling regime.Table 2
Two cooling regimes for different curing age ECC specimens.
Temperature
Cooling in room temperature
Quenching in water
200°C
√
None
400°C
√
√
600°C
√
None
800°C
√
√Figure 2
Heating regime for ECC specimens.The specimens are named as follows: temperature-cooling regime, for example, 400 A(W); here A means cooling in air and W means cooling in water for 5 minutes. The weight of each specimen was also measured before and after exposure to calculate the mass loss of fire-deteriorated specimens.


## 3. Experimental Results and Discussions

### 3.1. Surface and Internal Characteristics

It is observed that when the ECC specimens were exposed to high temperatures, some changes in color occurred. Figure3 shows that the color of ECC specimens changed from gray at 20°C to light yellow at 800°C due to the loss of water and chemical decomposition. The specimens are small and we cannot write many words on them, so the specimens with “W” mean cooling in water and without “W” mean cooling in air. The color of the specimens subjected to 800°C and then quenching in water turned to dark gray which may be due to the further hydration of the composite.Figure 3
Color changes and surface cracks of postfire specimens.Surface crack patterns of ECC specimens due to the high temperature exposure were almost the same up to 800°C. Cracks became apparent after 400°C, and hairline cracks were monitored above 400°C. Increasing the exposure temperature to 800°C increased the size of microcracking as consistent with pore structure variation of the specimens. However, quenching in the water may help to heal the surface crack due to the further hydration.


### 3.2. Mass Loss

The deterioration of specimens subjected to various elevated temperatures was also assessed by mass loss measurements. Figure4 shows the relation between mass loss (
M
0
-
M
i
)
/
M
0 (in percentage) and temperature of heat-exposed ECC. M
i is the mass after a specific thermal heat exposure, and M
0 is initial mass, prior to heat exposure. As seen in Figure 4, the mass loss increased with the increasing temperature of thermal exposure, a result mainly associated with the liberation of free and physically bound water. At higher temperatures of 600 and 800°C, the weight change of ECC was caused by the dehydration of paste [15]. During a heat treatment up to 400°C, the weight of the melted fibers also had an influence on mass loss.Figure 4
Mass loss of specimens of all curing ages with temperatures.


### 3.3. Microstructure Characterization by Using SEM Observations

The microstructure of specimens was investigated using scanning electron microscope (SEM) observation. The results of the microscopic investigations gave a good explanation of the change in macrobehavior of ECC in comparison to ECC matrix mixtures.To study the behavior of fibers and matrix microstructure after various elevated temperatures, observations with an SEM were performed on samples taken from the core of postfire ECC specimens that had been exposed to a temperature between 200 and 800°C for one hour. The specimens that had been quenched in the water for 5 minutes were also observed. Figure5 shows the SEM micrographs of various postfire ECC specimens exposed to different heating temperature and cooling regimens. Figures 5(a) and 5(b) show the SEM micrographs of ECC specimens for 200 A and 400 A. The fiber did not melt when the specimens were subjected to 200°C. After exposure to 400°C, PVA fibers melt completely, creating additional interconnected pores and small channels in the matrix, and fibers alone constitute a connected network. Therefore, the use of PVA fiber clearly affects porosity at high temperatures. After exposure to 400°C, the number and width of microcracks increase obviously compared to specimens subjected to 200°C from the SEM observation. From Figure 5(c), it can be seen that the hydration products did not decompose totally. For the specimens exposure to 800°C (Figure 5(d)), almost all hydration products appear as ill-crystallized or amorphous structures by losing the characteristic crystal structure. From Figures 5(e) and 5(f), we can see the typical crystal structure of specimens quenching in water and curing for 7 days. The produce of new crystal enhances the strength of specimens which would be discussed in the following section. Additionally, there are more new generated crystals in 800 W specimens than in 400 W specimens, which results in a more significant mechanical increase in 800 W specimens.SEM micrograph of ECC specimens subjected to different heating temperatures and cooling regimes.
(a)
200 A
(b)
400 A
(c)
600 A
(d)
800 A
(e)
400 W
(f)
800 W


### 3.4. Residual Compressive Strength and Stress-Strain Curves

Figure6 shows the influence of temperature on the compressive strength and stiffness of postfire ECC specimens. Relative strength, stiffness, and displacement were the ratios of the strength, stiffness, and displacement of specimens after high temperature to those of the control (unheated) specimens. Each point in Figure 6 was obtained from the average of at least four test specimens. The coefficient of variance (COV) values for the compressive strength values ranged from 2% to 9%. The narrow range of COV values is an indication of the consistent repeatability of the compressive strength test method even for fire-deteriorated specimens.Figure 6
Compressive strength, stiffness, and displacement corresponding to peak load with temperatures.As seen in Figure6 and as expected, exposure to high temperature influenced the residual compressive strength of ECC specimens substantially. However, percent variation in compressive strength can be classified in four distinct patterns of strength loss, 23–200°C, 200–400°C, 400–600°C, and 600–800°C. Temperature no more than 200°C seems to help the strength increase. Mean compressive strength of 28-day ECC specimens increases by 1% after exposure to 200°C. The influence of high temperature exposure on the residual compressive strength is not prominent up to 400°C with the mean compressive strength decreased by 32% after exposure to 400°C. This might be due to the less sensitivity of compressive strength to minor microcracks. Heating up to 400°C generated a relatively small amount of cracking, which did not cause any immediate loss of carrying capacity in compression because the slightly cracked concrete could work as a highly redundant structure [12]. Beyond 400°C, however, compressive strength dropped drastically by 62% and 77% at 600°C and 800°C, respectively. According to the variation of the residual compressive strength, temperature of 600°C and above might be regarded as critical temperature range for the strength loss of ECC. The present test results are in line with the findings of previous studies [9, 10].Residual compressive strength variations are consistent with the pore structure variations in previous studies [16, 17]. The total intruded porosity and percent of pore size between 50 nm and 500 nm increased slightly with the increase in temperature up to 400°C. The increase in porosity up to 400°C is most likely due to the small channels created in ECC by melting PVA fibers with the diameter of 39 μm. However, after exposure to 600°C, the main causes of deterioration in compressive strength might be attributed both to the physical transformation of the matrix and to chemical transformation of hydration products. When the temperature was raised to 600°C, decomposition of the major hydrate, known as tobermorite (gel), was inevitable [18], causing severe increase in the microstructure of its matrix and the loss of binder property.From Figure6, it can be seen that the stiffness of postfire specimens shares a similar but more sensitive tendency [19, 20] with exposure temperatures, which also could be classified into four stages. The mean compressive stiffness of ECC specimens increased by 0.5% after exposure to 200°C, while it decreased by 46%, 78%, and 85% after exposure to 400, 600, and 800°C.Figure7 shows the influence of cooling regimes on the residual mechanical properties. Relative strength, stiffness, and displacement were the ratios of the strength, stiffness, and displacement of specimens cooling in water to those of the specimens cooling in air. For the specimens subjected to heating temperature of 400°C, the compressive strength and stiffness of specimens quenching in water increased by 0.5% and 14% compared to the ones cooling in air, while, for 800°C, the compressive strength and stiffness of specimens quenching in water were 1.10 and 1.62 times to the ones cooling in air. As mentioned in Section 3.3, there are more new generated crystals in 800 W specimens than in 400W specimens, which results in a more significant mechanical increase in 800 W specimens. The result again shows that the stiffness is more sensitive than strength to microcracks, which could also be seen from the result of Figure 8. The meaning of relative ratio is the same with that in Figure 6. Meanwhile, the displacement corresponding to the peak load of 400 W and 800 W decreased by 4% and 24% compared to the specimens cooling in air.Figure 7
Influence of cooling regimes on compressive strength, stiffness, and displacement corresponding to peak load.Figure 8
Relationship of strength and stiffness to mass loss.The stress-strain curves of ECC specimens at room temperature and elevated temperatures are compared in Figure9. Ultimate stress decreased with the increasing temperature, particularly for temperatures exceeding 400°C, while the strain corresponding to the peak strength increased with temperature. The slope decreased with the increase in exposure temperature up to 800°C, indicating a reduction in the stiffness of the ECC. The reduction in ECC stiffness was relatively low up to 400°C; however, beyond 400°C, a dramatic reduction was monitored in the ECC stiffness. As expected, with the increase in exposure temperature, the postpeak stress of the ECC specimens dropped faster, resulting in a smaller postpeak area under the curve. This behavior becomes more evident when the exposure temperature level reaches 800°C: ECC specimens failed soon after reaching their peak strength. This means that increasing the exposed temperature level tends the ductile nature of ECC to brittle nature.Stress-strain curves of ECC specimens for different curing ages.
(a)
Postfire specimens cooling in the air
(b)
Stress-strain curve of specimens subjected to different cooling regimes


## 3.1. Surface and Internal Characteristics

It is observed that when the ECC specimens were exposed to high temperatures, some changes in color occurred. Figure3 shows that the color of ECC specimens changed from gray at 20°C to light yellow at 800°C due to the loss of water and chemical decomposition. The specimens are small and we cannot write many words on them, so the specimens with “W” mean cooling in water and without “W” mean cooling in air. The color of the specimens subjected to 800°C and then quenching in water turned to dark gray which may be due to the further hydration of the composite.Figure 3
Color changes and surface cracks of postfire specimens.Surface crack patterns of ECC specimens due to the high temperature exposure were almost the same up to 800°C. Cracks became apparent after 400°C, and hairline cracks were monitored above 400°C. Increasing the exposure temperature to 800°C increased the size of microcracking as consistent with pore structure variation of the specimens. However, quenching in the water may help to heal the surface crack due to the further hydration.


## 3.2. Mass Loss

The deterioration of specimens subjected to various elevated temperatures was also assessed by mass loss measurements. Figure4 shows the relation between mass loss (
M
0
-
M
i
)
/
M
0 (in percentage) and temperature of heat-exposed ECC. M
i is the mass after a specific thermal heat exposure, and M
0 is initial mass, prior to heat exposure. As seen in Figure 4, the mass loss increased with the increasing temperature of thermal exposure, a result mainly associated with the liberation of free and physically bound water. At higher temperatures of 600 and 800°C, the weight change of ECC was caused by the dehydration of paste [15]. During a heat treatment up to 400°C, the weight of the melted fibers also had an influence on mass loss.Figure 4
Mass loss of specimens of all curing ages with temperatures.


## 3.3. Microstructure Characterization by Using SEM Observations

The microstructure of specimens was investigated using scanning electron microscope (SEM) observation. The results of the microscopic investigations gave a good explanation of the change in macrobehavior of ECC in comparison to ECC matrix mixtures.To study the behavior of fibers and matrix microstructure after various elevated temperatures, observations with an SEM were performed on samples taken from the core of postfire ECC specimens that had been exposed to a temperature between 200 and 800°C for one hour. The specimens that had been quenched in the water for 5 minutes were also observed. Figure5 shows the SEM micrographs of various postfire ECC specimens exposed to different heating temperature and cooling regimens. Figures 5(a) and 5(b) show the SEM micrographs of ECC specimens for 200 A and 400 A. The fiber did not melt when the specimens were subjected to 200°C. After exposure to 400°C, PVA fibers melt completely, creating additional interconnected pores and small channels in the matrix, and fibers alone constitute a connected network. Therefore, the use of PVA fiber clearly affects porosity at high temperatures. After exposure to 400°C, the number and width of microcracks increase obviously compared to specimens subjected to 200°C from the SEM observation. From Figure 5(c), it can be seen that the hydration products did not decompose totally. For the specimens exposure to 800°C (Figure 5(d)), almost all hydration products appear as ill-crystallized or amorphous structures by losing the characteristic crystal structure. From Figures 5(e) and 5(f), we can see the typical crystal structure of specimens quenching in water and curing for 7 days. The produce of new crystal enhances the strength of specimens which would be discussed in the following section. Additionally, there are more new generated crystals in 800 W specimens than in 400 W specimens, which results in a more significant mechanical increase in 800 W specimens.SEM micrograph of ECC specimens subjected to different heating temperatures and cooling regimes.
(a)
200 A
(b)
400 A
(c)
600 A
(d)
800 A
(e)
400 W
(f)
800 W


## 3.4. Residual Compressive Strength and Stress-Strain Curves

Figure6 shows the influence of temperature on the compressive strength and stiffness of postfire ECC specimens. Relative strength, stiffness, and displacement were the ratios of the strength, stiffness, and displacement of specimens after high temperature to those of the control (unheated) specimens. Each point in Figure 6 was obtained from the average of at least four test specimens. The coefficient of variance (COV) values for the compressive strength values ranged from 2% to 9%. The narrow range of COV values is an indication of the consistent repeatability of the compressive strength test method even for fire-deteriorated specimens.Figure 6
Compressive strength, stiffness, and displacement corresponding to peak load with temperatures.As seen in Figure6 and as expected, exposure to high temperature influenced the residual compressive strength of ECC specimens substantially. However, percent variation in compressive strength can be classified in four distinct patterns of strength loss, 23–200°C, 200–400°C, 400–600°C, and 600–800°C. Temperature no more than 200°C seems to help the strength increase. Mean compressive strength of 28-day ECC specimens increases by 1% after exposure to 200°C. The influence of high temperature exposure on the residual compressive strength is not prominent up to 400°C with the mean compressive strength decreased by 32% after exposure to 400°C. This might be due to the less sensitivity of compressive strength to minor microcracks. Heating up to 400°C generated a relatively small amount of cracking, which did not cause any immediate loss of carrying capacity in compression because the slightly cracked concrete could work as a highly redundant structure [12]. Beyond 400°C, however, compressive strength dropped drastically by 62% and 77% at 600°C and 800°C, respectively. According to the variation of the residual compressive strength, temperature of 600°C and above might be regarded as critical temperature range for the strength loss of ECC. The present test results are in line with the findings of previous studies [9, 10].Residual compressive strength variations are consistent with the pore structure variations in previous studies [16, 17]. The total intruded porosity and percent of pore size between 50 nm and 500 nm increased slightly with the increase in temperature up to 400°C. The increase in porosity up to 400°C is most likely due to the small channels created in ECC by melting PVA fibers with the diameter of 39 μm. However, after exposure to 600°C, the main causes of deterioration in compressive strength might be attributed both to the physical transformation of the matrix and to chemical transformation of hydration products. When the temperature was raised to 600°C, decomposition of the major hydrate, known as tobermorite (gel), was inevitable [18], causing severe increase in the microstructure of its matrix and the loss of binder property.From Figure6, it can be seen that the stiffness of postfire specimens shares a similar but more sensitive tendency [19, 20] with exposure temperatures, which also could be classified into four stages. The mean compressive stiffness of ECC specimens increased by 0.5% after exposure to 200°C, while it decreased by 46%, 78%, and 85% after exposure to 400, 600, and 800°C.Figure7 shows the influence of cooling regimes on the residual mechanical properties. Relative strength, stiffness, and displacement were the ratios of the strength, stiffness, and displacement of specimens cooling in water to those of the specimens cooling in air. For the specimens subjected to heating temperature of 400°C, the compressive strength and stiffness of specimens quenching in water increased by 0.5% and 14% compared to the ones cooling in air, while, for 800°C, the compressive strength and stiffness of specimens quenching in water were 1.10 and 1.62 times to the ones cooling in air. As mentioned in Section 3.3, there are more new generated crystals in 800 W specimens than in 400W specimens, which results in a more significant mechanical increase in 800 W specimens. The result again shows that the stiffness is more sensitive than strength to microcracks, which could also be seen from the result of Figure 8. The meaning of relative ratio is the same with that in Figure 6. Meanwhile, the displacement corresponding to the peak load of 400 W and 800 W decreased by 4% and 24% compared to the specimens cooling in air.Figure 7
Influence of cooling regimes on compressive strength, stiffness, and displacement corresponding to peak load.Figure 8
Relationship of strength and stiffness to mass loss.The stress-strain curves of ECC specimens at room temperature and elevated temperatures are compared in Figure9. Ultimate stress decreased with the increasing temperature, particularly for temperatures exceeding 400°C, while the strain corresponding to the peak strength increased with temperature. The slope decreased with the increase in exposure temperature up to 800°C, indicating a reduction in the stiffness of the ECC. The reduction in ECC stiffness was relatively low up to 400°C; however, beyond 400°C, a dramatic reduction was monitored in the ECC stiffness. As expected, with the increase in exposure temperature, the postpeak stress of the ECC specimens dropped faster, resulting in a smaller postpeak area under the curve. This behavior becomes more evident when the exposure temperature level reaches 800°C: ECC specimens failed soon after reaching their peak strength. This means that increasing the exposed temperature level tends the ductile nature of ECC to brittle nature.Stress-strain curves of ECC specimens for different curing ages.
(a)
Postfire specimens cooling in the air
(b)
Stress-strain curve of specimens subjected to different cooling regimes


## 4. Conclusions

The influence of cooling regimes on the mechanical properties of ECC specimens subjected to elevated temperatures was investigated in this paper and the following conclusions can be drawn.(1)
The color of ECC specimens changed from gray at 20°C to light yellow at 800°C; the specimens quenching in water turned to dark grey. Hairline cracks were monitored above 400°C and quenching in the water helps to heal the surface crack. The mass loss increased with the increasing temperature of thermal exposure.
(2)
The compressive strength can be classified into four distinct patterns of strength loss: 23–200°C, 200–400°C, 400–600°C, and 600–800°C. From 23 to 200°C, the compressive strength of specimens increases with temperature. The influence of high temperature exposure on the residual compressive strength is not prominent up to 400°C. Beyond 600°C, ECC specimens showed severe deterioration.
(3)
The cooling regime of quenching in water helped the strength and stiffness recovery. Ultimate stress decreases with the increasing temperature, while the strain corresponding to the peak strength increases with temperature. High temperature causes a reduction in the stiffness of ECC. Increasing the exposed temperature level tends the ductile nature of ECC to brittle nature.



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*Source: 919078-2014-06-25.xml*