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The Study on the Whole Stress–Strain Curves of Coral Fly Ash-Slag Alkali-Activated Concrete under Uniaxial Compression

This study aimed to research the whole stress–strain curves of coral Fly Ash-Slag Alkali-Activated Concrete (CAAC) in different strength grades. Fly ash-slag alkali-activated concrete was used as cementing materials to produce coral aggregate concrete. A monotonic loading test was conducted on the prismatic specimens to obtain elastic modulus (Ec), Poisson’s ratio (μ) and the constitutive relationship of CAAC under uniaxial compression. When the strain of CAAC reached the maximum value, the specimen was split and damaged rapidly. As the strength grade increased, the ratio of residual stress (σri) to peak stress (σ0i) decreased in the range of 0.17–0.28. The Ec of CAAC increased gradually, and μ increased to the peak value and then decreased. According to the test results, the constitutive equation of CAAC can be expressed by piecewise expression, which can better reflect all the experimental characteristics. It was also found that CAAC has many similar characteristics with coral concrete and lightweight aggregate concrete. To improve the strength and toughness of CAAC, some fibers, such as organic fiber, can be added to expand the application of CAAC in engineering projects.


Introduction
In recent years, with the rapid development of urban construction, the amount of cement used worldwide has surged. At the end of the last century, the global cement consumption exceeded 2.2 billion tons per year [1]. According to Elchalakani [2], the production of ordinary Portland cement reached 3.7 billion tons in 2017, which was accompanied by 3 billion tons of CO 2 emissions, accounting for about 7% of the total global emissions. Statistics released by the European Cement Association [3] showed that the cement output of the European Union was about 170 million tons in 2016, making it one of the major cement producers in the world. In 2016, China produced more than half of the world's properties of CPC by preparing different types of CPC specimens. In 2012, Lei [56] found that CPC and lightweight aggregate concrete (LPC) have similar characteristics in strength development, failure mechanism and failure performance. In 2013, Yingtao [57] studied CPC and OPC with the same mix ratio and the performance differences in frost resistance and corrosion resistance. They found that fly ash or slag can be added to CPC to improve its freezing and corrosion resistance. The above research provides important reference for the application of CPC.
The combination of geopolymer binders and coral aggregates reduces the consumption of sand and cement and achieves eco-friendly concrete production. The whole stress-strain curve of uniaxial compression is the basis for studying the bearing capacity and deformation of concrete structures [58]. For the whole stress-strain curves of CPC and LPC, there have been some research results [59][60][61]. However, the whole stress-strain curve of CAAC that uses coral instead of ordinary aggregate has not been studied in detail.
In this study, fly ash-slag and coral aggregates were combined to prepare alkali-activated coral aggregates concrete with three strength grades. From the perspective of structural design, the whole stress-strain curve of CAAC was systematically studied and compared with normal weight alkali-activated concrete (NAAC) with limestone aggregates, CPC and LPC of the same strength grades. It is of great significance to provide basic constitutive relation for the application of CAAC.

Materials
The binder materials used in this study were fly ash (FA) and ground granulated blast furnace slag (GGBFS), which obtained from China Resources mixing Station, Nanning, China. The chemical compositions and physical properties of the FA and GGBFS are listed in Table 1. Two types of coarse aggregates were used in this research project: coral aggregates ( Figure 1) and limestone aggregates (Qinzhou, China). Limestone with a maximum size of 20 mm and aggregate crushing value of 23% was employed as coarse aggregates for NAAC. The coral comes from some islands and reefs in Beihai City, Guangxi Zhuang Autonomous Region, China. The coral with a maximum size of 20 mm (Figure 2b), cylinder compressive strength of 2.12 MPa and 24 h water absorption ratio of 14.2% was used as coarse aggregates for CAAC. Natural river sand (Figure 2a) with fineness modulus of 2.4 was used as fine aggregates for all concrete mixtures. The fineness modulus, specific gravity, water absorption, aggregates crushing value and cylinder compressive strength of different aggregates were determined according to Chinese National Standard GB/T 17431-1998 [62], as listed in Table 2. 2b), cylinder compressive strength of 2.12 MPa and 24 h water absorption ratio of 14.2% was used as coarse aggregates for CAAC. Natural river sand (Figure 2a) with fineness modulus of 2.4 was used as fine aggregates for all concrete mixtures. The fineness modulus, specific gravity, water absorption, aggregates crushing value and cylinder compressive strength of different aggregates were determined according to Chinese National Standard GB/T 17431-1998 [62], as listed in Table 2.

Mixture Proportions and Specimen Preparation
The alkali activator used in this study is a mixture of NaOH solid and sodium silicate (SS) solution. For all AAC mixtures and mixtures containing additional water, the ratio of sodium silicate solution to NaOH was constant at 2.5. The chemical composition of SS solution was Na2O = 13.6%, SiO2 = 29.9% and H2O = 56.5% by mass. The specific gravity and the modulus of SS solution were 1.35 and 3.0, respectively. The solution of alkali activator was prepared by dissolving NaOH pellets with 99% purity in sodium silicate solution for 24 h. Potable tap water was used in all concrete mixes, and poly-carboxylic type superplasticizer (SP) with a specific gravity of 1.18 and pH 7 was used in NAAC and CAAC mixtures.

Mixture Proportions and Specimen Preparation
The alkali activator used in this study is a mixture of NaOH solid and sodium silicate (SS) solution. For all AAC mixtures and mixtures containing additional water, the ratio of sodium silicate solution to NaOH was constant at 2.5. The chemical composition of SS solution was Na 2 O = 13.6%, SiO 2 = 29.9% and H 2 O = 56.5% by mass. The specific gravity and the modulus of SS solution were 1.35 and 3.0, respectively. The solution of alkali activator was prepared by dissolving NaOH pellets with 99% purity in sodium silicate solution for 24 h. Potable tap water was used in all concrete mixes, and poly-carboxylic type superplasticizer (SP) with a specific gravity of 1.18 and pH 7 was used in NAAC and CAAC mixtures.
The term water/solid (W/S) ratio in AAC was defined as the ratio of the total mass of water in the mixture to the sum of the mass of blended FA-GGBFS powder material, NaOH solids and sodium silicate solids. The W/S ratio determines the strength of AAC. In this experiment, the slump value of the designed AAC was 15-22 cm. Therefore, the dosage of superplasticizer for each mixture with different W/S ratio was modified to achieve the specified slump value.
In addition, the minimum target compressive strength of CAAC should exceed 20 MPa for application to structural concrete members. In 2013, Vora et al. [63] found that the compressive strength of alkali-activated concrete decreased with the increase of water-binder ratio. Alkali activated concrete is composed of coarse aggregate, fly ash, ground granulated blast furnace slag, sodium silicate, NaOH, river sand, water and superplasticizer. According to the research of Yinfeng et al. [64] and a series of trial matches, three different strength grades of alkali-activated concrete were designed. The mix proportions are shown in Table 3. At present, there is no standard available as a reference for the mixing procedure of AAC, especially for structural-grade lightweight AAC. In this study, FA, GGBFS and aggregates were first stirred in a drum mixer for 5 min when NAAC was made. Then, the alkali activator solution and the mixture of water and superplasticizer were gradually added to the mixer, and the stirring process lasted another 5 min. Before the preparation of CAAC, it was necessary to soak the coral aggregate in tap water to remove impurities and reduce the concentration of chloride ion and then dry them. During the preparation, the coral aggregates were firstly wetted with little sodium silicate solution and stirred for 2 min, and then FA, GGBFS and river sand were added and stirred for 2 min. Finally, the alkali activator solution, superplasticizer and water were added gradually and stirred for 5 min. All the AAC concretes were put into the steel model and vibrated on the shaking table for about 10-20 s. It is noted that sodium silicate solution treatment of coral aggregates in the casting procedure of AAC can help to improve the quality of coral aggregates particle by reducing water absorption and increasing strength.
For each strength grade mixture, three 100 mm × 100 mm × 100 mm cubes and three 100 mm × 100 mm × 300 mm prisms were cast. After casting, all specimens were covered with plastic film to prevent water loss. The specimens were taken out of the mold after 24 h and placed in a curing room at 25 ± 5 • C and relative humidity of 50-55% for 30 days.

Test Methods
In this study, the uniaxial compression tests were performed on RMT-201 rock and concrete mechanical test system at the Structural Laboratory of Guangxi University, Nanning, China. The maximum loading range of the testing machine was 1500 kN, with an accuracy of 0.001 kN, and the minimum loading rate was 0.001 mm/s. According to the Chinese National Standard GB/T 50081-2002 [65], the compressive stress-strain relationship test was carried out on prism specimens with size of 100 mm × 100 mm × 300 mm; at the same time, elastic modulus and Poisson's ratio of different concrete mixtures could be estimated. The instruments used in the test were displacement transducers and recorders [66]. The load, displacement and strain were collected by corresponding data acquisition system and stored in computer during the experiment process.
The test equipment and the schematic diagram of the loading device are shown in Figure 3. The displacement-controlled loading mode was adopted with a loading speed of 0.002 mm/s. A linear variable differential transformer with a measurement range of ± 5 mm and precision of 400 µε/mm was used to measure the axial (vertical) displacement and the lateral displacement. At the same time, to improve the accuracy of the measurement and reduce the influence of the end of the specimen and the supporting plate on the test results, the axial and lateral strains of the AACs were also measured by the strain gauges. The horizontal strain gauge was used to measure the transverse strain, while the vertical strain gauge was not only used to measure the longitudinal strain but also used to check whether the specimen was flat. Load was measured with a load sensor mounted on the top of the specimen. The load, strains, axial and lateral deformation of specimens were collected and recorded by the Donghua-DH3818Y static strain testing system (Liyang, China), and 100 data points were recorded per second. According to the cube compressive strength obtained before this study, the peak load was estimated, and the specimens were preloaded once before formal loading with 10-20% of the peak load. After formal loading, it terminated when the load dropped to 15% of the peak load [67,68].
strain gauge was not only used to measure the longitudinal strain but also used to check whether the specimen was flat. Load was measured with a load sensor mounted on the top of the specimen. The load, strains, axial and lateral deformation of specimens were collected and recorded by the Donghua-DH3818Y static strain testing system (Liyang, China), and 100 data points were recorded per second. According to the cube compressive strength obtained before this study, the peak load was estimated, and the specimens were preloaded once before formal loading with 10-20% of the peak load. After formal loading, it terminated when the load dropped to 15% of the peak load [67,68].
The axial deformation in this study is the average value of the vertical LVDT and the axial strain gauges. The complete failure process of the specimen can be seen in the loading process. During the test, it is necessary to observe and record the form and development of the crack and the shedding phenomenon on the surface of the specimen. During the loading process, the strain gauge will be damaged when the crack penetrates, so the strain gauge generally measures the data before the specimen cracks.

Elastic Modulus and Poisson's Ratio
According to the American Society for Testing Materials (ASTM) [69], the elastic modulus calculation formula is as follows: where ε1 is the axial strain (0.0005); σ1 is the major principal stress; ε2 is the longitudinal strain; and σ2 is the stress corresponding to 40% of peak load. The Poisson's ratio, μ, was calculated as follows: where εt1 and εt2 are the transverse strains corresponding to ε1 and ε2, respectively.

Compressive Failure Mode
The whole experimental process has three parts: (1) When the force on the specimen reached 0.10-0.20 times the peak load, the peeling phenomenon of CAAC occurred, which indicated that the specimen was in the compaction stage. (2) When the force on the specimen reached 0.6-0.85 times the The axial deformation in this study is the average value of the vertical LVDT and the axial strain gauges.
The complete failure process of the specimen can be seen in the loading process. During the test, it is necessary to observe and record the form and development of the crack and the shedding phenomenon on the surface of the specimen. During the loading process, the strain gauge will be damaged when the crack penetrates, so the strain gauge generally measures the data before the specimen cracks.

Elastic Modulus and Poisson's Ratio
According to the American Society for Testing Materials (ASTM) [69], the elastic modulus calculation formula is as follows: where ε 1 is the axial strain (0.0005); σ 1 is the major principal stress; ε 2 is the longitudinal strain; and σ 2 is the stress corresponding to 40% of peak load. The Poisson's ratio, µ, was calculated as follows: where ε t1 and ε t2 are the transverse strains corresponding to ε 1 and ε 2 , respectively.

Compressive Failure Mode
The whole experimental process has three parts: (1) When the force on the specimen reached 0.10-0.20 times the peak load, the peeling phenomenon of CAAC occurred, which indicated that the specimen was in the compaction stage. (2) When the force on the specimen reached 0.6-0.85 times the peak load, small longitudinal cracks appeared on the surface of the specimen. Most cracks developed slowly and steadily. (3) When the loading continued, the crack continued to develop and extend to both ends of the specimen, and eventually led to the failure of the specimen. This indicates that the crack at this stage is not in stable development. These phenomena showed that CAAC was very brittle. With the increase of CAAC strength grade, the damage pattern was more serious and unpredictable. The failure characteristics of the NAAC and CAAC specimens were found to be similar, both with diagonal shear failure. The typical failure patterns are illustrated in Figure 4. For different strength grades of AACs, the failure modes were very similar. both ends of the specimen, and eventually led to the failure of the specimen. This indicates that the crack at this stage is not in stable development. These phenomena showed that CAAC was very brittle. With the increase of CAAC strength grade, the damage pattern was more serious and unpredictable. The failure characteristics of the NAAC and CAAC specimens were found to be similar, both with diagonal shear failure. The typical failure patterns are illustrated in Figure 4. For different strength grades of AACs, the failure modes were very similar.

Measured Stress-Strain Curve
Based on the load and displacement of the specimen, the stress-strain curve is plotted in Figure  5. The results show that the shape of the stress-strain curves of CAAC were very similar at different strength grades. From the beginning of loading to 0.60-0.70 times the peak load, the strain increased almost linearly and the curve began to bend. When the strain reached 0.65-0.70 times the peak strain, the turning point of the strain began to appear. The slope of the convex curve changed little, but, when the stress was close to 0.85-0.90 times the peak stress (σ0), the slope of the curve changed greatly. It can be seen that, when the stress was greater than σ0, the stress decreased rapidly, the curve dropped rapidly and the specimen was destroyed quickly and suddenly. This shows that CAAC is brittle and easily damaged when the strain is close to σ0. Meanwhile, the stress-strain curves of NAAC were similar to the curve of OPC, as shown in Figure 6. Fitting curve for CAAC-C40 α=1. 17, β=7.76 Fitting curve for CAAC-C50 α=1.03, β=9. 37 Lateral strain(×10 -3 ) Axial strain(×10 -3 )

Measured Stress-Strain Curve
Based on the load and displacement of the specimen, the stress-strain curve is plotted in Figure 5. The results show that the shape of the stress-strain curves of CAAC were very similar at different strength grades. From the beginning of loading to 0.60-0.70 times the peak load, the strain increased almost linearly and the curve began to bend. When the strain reached 0.65-0.70 times the peak strain, the turning point of the strain began to appear. The slope of the convex curve changed little, but, when the stress was close to 0.85-0.90 times the peak stress (σ 0 ), the slope of the curve changed greatly. It can be seen that, when the stress was greater than σ 0 , the stress decreased rapidly, the curve dropped rapidly and the specimen was destroyed quickly and suddenly. This shows that CAAC is brittle and easily damaged when the strain is close to σ 0 . Meanwhile, the stress-strain curves of NAAC were similar to the curve of OPC, as shown in Figure 6.

.2. Measured Stress-Strain Curve
Based on the load and displacement of the specimen, the stress-strain curve is plotted in Figure  . The results show that the shape of the stress-strain curves of CAAC were very similar at different trength grades. From the beginning of loading to 0.60-0.70 times the peak load, the strain increased lmost linearly and the curve began to bend. When the strain reached 0.65-0.70 times the peak strain, he turning point of the strain began to appear. The slope of the convex curve changed little, but, hen the stress was close to 0.85-0.90 times the peak stress (σ0), the slope of the curve changed reatly. It can be seen that, when the stress was greater than σ0, the stress decreased rapidly, the curve ropped rapidly and the specimen was destroyed quickly and suddenly. This shows that CAAC is rittle and easily damaged when the strain is close to σ0. Meanwhile, the stress-strain curves of AAC were similar to the curve of OPC, as shown in Figure 6. Fitting curve for CAAC-C40 α=1.17, β=7. 76 Fitting curve for CAAC-C50 α=1.03, β=9.37

Mechanical Properties
The peak stress (σ0), peak strain (ε0), residual stress (σr) and ultimate strain (εu) of CAAC and NAAC in three strength grades were measured, as listed in Table 4. The symbols σ0i, σri, ε0i and εui represent the mean value of σ0, σr, ε0 and εu of the corresponding concrete specimens, respectively. For CAAC, the value of σri/σ0i was in the range of 0.17-0.28, decreasing with the increase of strength grade, which may indicate that the damage of CAAC is more serious with the increase of strength grade. The value of εu/ε0 was in the range of 1.72-1.94, which increased at first and then decreased as the strength grade increased. Figure 7 shows the relationship between σ0 and ε0 of CAAC and NAAC. It can be seen that σ0 and ε0 tended to increase with the increase of strength grade, which may indicate that the anti-failure ability and safety factor of CAAC and NAAC increase with the increase of strength grade [70]. Note: σ0 is peak stress, σr is residual stress, ε0 is peak strain and εu is ultimate strain; σ0i, σri, ε0i and εui are mean values of σ0, σr, ε0 and εu of the corresponding concrete specimens, respectively; S1 and S2 are the standard deviations of peak stress and residual stress, respectively; and P1 and P2 are the  32, n=2.12 Fitting curve for NAAC-C40 m=8.06, n=6. 72 Fitting curve for NAAC-C50 m=6. 68, n=12.78 Lateral strain(×10 -3 ) Axial strain(×10 -3 ) Figure 6. Whole stress-strain curves of NAAC in different strength grades.

Mechanical Properties
The peak stress (σ 0 ), peak strain (ε 0 ), residual stress (σ r ) and ultimate strain (ε u ) of CAAC and NAAC in three strength grades were measured, as listed in Table 4. The symbols σ 0i , σ ri , ε 0i and ε ui represent the mean value of σ 0 , σ r , ε 0 and ε u of the corresponding concrete specimens, respectively. For CAAC, the value of σ ri /σ 0i was in the range of 0.17-0.28, decreasing with the increase of strength grade, which may indicate that the damage of CAAC is more serious with the increase of strength grade. The value of ε u /ε 0 was in the range of 1.72-1.94, which increased at first and then decreased as the strength grade increased. Figure 7 shows the relationship between σ 0 and ε 0 of CAAC and NAAC. It can be seen that σ 0 and ε 0 tended to increase with the increase of strength grade, which may indicate that the anti-failure ability and safety factor of CAAC and NAAC increase with the increase of strength grade [70].   Note: σ 0 is peak stress, σ r is residual stress, ε 0 is peak strain and ε u is ultimate strain; σ 0i , σ ri , ε 0i and ε ui are mean values of σ 0 , σ r , ε 0 and ε u of the corresponding concrete specimens, respectively; S 1 and S 2 are the standard deviations of peak stress and residual stress, respectively; and P 1 and P 2 are the standard deviations of peak strain and ultimate strain, respectively.

Establish the Whole Stress-Strain Curve of CAAC
As shown in Figure 5, the stress-strain curves of CAAC with different strength grades could be characterized by three stages: linear ascending stage, nonlinear ascending stage and descending stage. The whole stress-strain curve had its own obvious characteristics in the ascending and descending stages, respectively. Different functions were selected to fit the experimental results. By comparing with OPC and LPC, according to the research of Zhen et al. [71], the formula for the ascending stage was as follows: where x = ε/ε 0 , ε is the strain, ε 0 is the peak strain, y = σ/σ 0 , σ is the stress, σ 0 is the peak stress and α is the control parameter of ascending stage curve. Figure 5 shows that, during the descending stage, the decline of CAAC was greater than that of OPC, because CAAC is more brittle than OPC. Therefore, the OPC equation found by Zhenhai et al. [72] in the descending stage is not suitable for CAAC. The descending curve needs to be consistent with the experimental results. The formula for the descending stage was as follows: where x = ε/ε 0 , ε is the strain, ε 0 is the peak strain, y = σ/σ 0 , σ is the stress, σ 0 is the peak stress and β is the control parameter of descending stage curve. Because the stress-strain curve of NAAC is similar to that of OPC, the analytical expression of uniaxial compression of OPC in Chinese code GB/T 50010-2010 [73] was used to express the NAAC curve, as shown in Formula (5).
where f c is peak stress; ε 0 is peak strain; m is a parameter of ascending stage; and n is a parameter of the descending stage. The normalized whole stress-strain curves of the CAAC in different strength grades is shown in Figure 8, and the curves were similar in the ascending stage. At the same time, the higher the strength grade was, the faster the decline in the descending stage was, the more serious the damage was and the smaller the relative residual stress was [50]. These trends showed that the brittleness of CAAC increased with the increase of strength grade, which was consistent with the performance of OPC. The whole stress-strain curve equation of CAAC with each strength grade has its own related parameters: α and β represent the parameters of ascending stage and descending stage, respectively, and R 2 is the correlation coefficient (Table 5). Note: R 2 1 is the correlation of parameter α in the ascending stage; R 2 2 is the correlation of parameter β in the descending stage; and the closer the value of R 2 is to 1, the better are the fitting results. was and the smaller the relative residual stress was [50]. These trends showed that the brittleness of CAAC increased with the increase of strength grade, which was consistent with the performance of OPC. The whole stress-strain curve equation of CAAC with each strength grade has its own related parameters: α and β represent the parameters of ascending stage and descending stage, respectively, and R 2 is the correlation coefficient (Table 5).  R is the correlation of parameter α in the ascending stage; 2 2 R is the correlation of parameter β in the descending stage; and the closer the value of R 2 is to 1, the better are the fitting results.

Comparison of Whole Stress-Strain Curve for Different Types of Concrete
In Figure 9, the whole stress-strain curves of CAAC, NAAC, CPC [70] and LPC [74] are compared. It can be seen that CAAC, NAAC, CPC and LPC showed similar trends in the ascending stage, while there were significant differences in the descending stages. When the strength grade was the same, the descending stage of CAAC was the steepest, which was basically consistent with CPC, indicating that CAAC is more brittle than NAAC and LPC. This further showed that: (a) The strength of corals is lower than that of ordinary stones, volcanic rocks and shales. When the pressure reaches its maximum, the corals will quickly break. (b) The surface of coral is rough and has many pores, which increases the contact area of the interface larger. This is conducive to increasing mechanical interlock and enhancing the combination of coral aggregates and alkali-activated cementing materials [70]. The damage mainly occurs in aggregates and cementing materials, but rarely at the interface. This failure pattern indicates an increase in brittleness of CAAC.

Comparison of Whole Stress-Strain Curve for Different Types of Concrete
In Figure 9, the whole stress-strain curves of CAAC, NAAC, CPC [70] and LPC [74] are compared. It can be seen that CAAC, NAAC, CPC and LPC showed similar trends in the ascending stage, while there were significant differences in the descending stages. When the strength grade was the same, the descending stage of CAAC was the steepest, which was basically consistent with CPC, indicating that CAAC is more brittle than NAAC and LPC. This further showed that: (a) The strength of corals is lower than that of ordinary stones, volcanic rocks and shales. When the pressure reaches its maximum, the corals will quickly break. (b) The surface of coral is rough and has many pores, which increases the contact area of the interface larger. This is conducive to increasing mechanical interlock and enhancing the combination of coral aggregates and alkali-activated cementing materials [70]. The damage mainly occurs in aggregates and cementing materials, but rarely at the interface. This failure pattern indicates an increase in brittleness of CAAC.

Elastic Modulus and Poisson's Ratio of CAAC
The elastic modulus (E c ) and Poisson's ratio (µ) of CAAC measured in the test are listed in Table 6. The results indicate that, when the strength grade increased, E c increased gradually and µ increased at first and then decreased. With higher strength grade of CAAC, the relative amount of coral aggregate and the combined surface area of aggregate and cementing material were reduced, which led to the decrease of transverse restraint of concrete and the value of µ decreased [70].

Elastic Modulus and Poisson's Ratio of CAAC
The elastic modulus (Ec) and Poisson's ratio (μ) of CAAC measured in the test are listed in Table  6. The results indicate that, when the strength grade increased, Ec increased gradually and μ increased at first and then decreased. With higher strength grade of CAAC, the relative amount of coral aggregate and the combined surface area of aggregate and cementing material were reduced, which led to the decrease of transverse restraint of concrete and the value of μ decreased [70].   Figure 10 shows the comparison of E c for CAAC, NAAC, CPC and LPC. The results show that the E c of CAAC is lower than that of NAAC and CPC, but very close to CPC, and higher than LPC. The E c of NAAC is the largest. It can be inferred that the type of aggregates has a great influence on E c ; the surface characteristics, shape, rigidity and cementing material all have great influence on E c . According to the OPC and LPC in the E c and f cu regression formula proposed by Faxing et al. [75], the elastic modulus of CAAC can be predicted by the following formula: where E c and f cu represent elastic modulus (GPa) and cube compressive strength (MPa), respectively.  Figure 10 shows the comparison of Ec for CAAC, NAAC, CPC and LPC. The results show that the Ec of CAAC is lower than that of NAAC and CPC, but very close to CPC, and higher than LPC. The Ec of NAAC is the largest. It can be inferred that the type of aggregates has a great influence on Ec; the surface characteristics, shape, rigidity and cementing material all have great influence on Ec. According to the OPC and LPC in the Ec and fcu regression formula proposed by Faxing et al. [75], the elastic modulus of CAAC can be predicted by the following formula: where Ec and fcu represent elastic modulus (GPa) and cube compressive strength (MPa), respectively.

Performance Comparison
The whole stress-strain curve, E c and µ of CAAC, NAAC, CPC and LPC were compared and analyzed, and the following results were obtained. When the strength grade is the same, the brittleness order for different types of concrete is as follows: CAAC > CPC > LPC > NAAC. The order of E c is as follows: NAAC > CAAC = CPC > LPC. The brittleness and elastic modulus of CAAC limit its application in engineering construction. Therefore to expand the application scope of CAAC, it is necessary to improve its strength and toughness. Studies have shown that, to improve the strength of coral, superfine cement mortar and silicon mortar can be added on the surface of coral to form organic or inorganic covering layer to increase the density and rigidity [49]. To prevent CAAC from cracking, organic fiber can be added to CAAC [76]. These measures can produce CAAC with high strength and high toughness.

Potential Application of CAAC
CAAC, which uses coral as coarse aggregates, is similar to CPC in engineering properties and is expected to be applied in engineering construction. Compared with the traditional OPC, CAAC has smaller elastic modulus and larger Poisson's ratio, thus it is suitable for foundations and infrastructures with lower rigidity requirements. Compared with LPC-based concrete, CAAC has similar mechanical properties, and coral can be used to replace some lightweight aggregates. In coastal areas, coral is often treated as waste, and it can be used as aggregates for concrete to save material. In addition, compared with OPC and LPC, CAAC has the greatest brittleness. For some important buildings and structures, this characteristic is often disadvantageous. However, CAAC is recommended for structures such as foundations and walkways, which are subjected to static loads.

Conclusions
The whole stress-strain curve of CAAC, which uses geopolymer and coral instead of cement and stone, was compared with NAAC, CPC and LPC. According to the test results, the following conclusions can be obtained:

1.
Brittleness is the main cause of CAAC uniaxial compression damage. The CAAC would be divided into multiple cylinders as a splitting failure. The cracks of the specimen are mainly vertical cracks and inclined cracks. In addition, the failure of specimens usually occurs on the slope.

2.
According to the whole stress-strain curve of CAAC, the shapes and characteristics vary with different strength grades. As the strength grade increases, the Poisson's ratio (µ) increases at first and then decreases. The reason is that the bond surface area between coral and cementing material decreases, which leads to the decrease of lateral restraint of concrete.

3.
For the whole stress-strain curves of CAAC, NAAC, CPC and LPC, there is no significant difference in the ascending stages, but there is a great difference in the descending stages. At the same strength grade, the descending stage of CAAC is the steepest compared with NAAC and CPC, which is basically consistent with CPC, indicating that CAAC is more brittle than NAAC and LPC. Superfine cement mortar and silicon mortar can be used to increase the strength of coral. It is recommended to add organic fiber to CAAC to improve the strength and toughness.