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Article

CO2 Emission Optimization of Concrete-Filled Steel Tubular Rectangular Stub Columns Using Metaheuristic Algorithms

1
Department of Civil Engineering, Turkish-German University, İstanbul 34820, Turkey
2
Department of Civil, Geological and Mining Engineering, Polytechnique Montréal, Montréal, QC H3T 1J4, Canada
3
Department of Civil Engineering, İstanbul University-Cerrahpaşa, İstanbul 34320, Turkey
4
Department of Civil and Environmental Engineering, Temple University, Philadelphia, PA 19122, USA
5
College of IT Convergence, Gachon University, Seongnam 13120, Korea
*
Authors to whom correspondence should be addressed.
Sustainability 2021, 13(19), 10981; https://0-doi-org.brum.beds.ac.uk/10.3390/su131910981
Submission received: 2 August 2021 / Revised: 27 September 2021 / Accepted: 29 September 2021 / Published: 3 October 2021

Abstract

:
Concrete-filled steel tubular (CFST) columns have been assiduously investigated experimentally and numerically due to the superior structural performance they exhibit. To obtain the best possible performance from CFST columns while reducing the environmental impact, the use of optimization algorithms is indispensable. Metaheuristic optimization techniques provide the designers of CFST members with a very efficient set of tools to obtain design combinations that perform well under external loading and have a low carbon footprint at the same time. That is why metaheuristic algorithms are more applicable in civil engineering due to their high efficiency. A large number of formulas for the prediction of the axial ultimate load-carrying capacity N u of CFST columns are available in design codes. However, a limitation of the usage of these design formulas is that most of these formulas are only applicable for narrow ranges of design variables. In this study a newly developed set of equations with a wide range of applicability that calculates N u in case of rectangular cross-sections is applied. In order to optimize the cross-sectional dimensions, two different metaheuristic algorithms are used, and their performances are compared. The reduction in CO2 emission is demonstrated as a function of cross-sectional dimensions while considering certain structural performance requirements. The outcome of the more recently developed social spider algorithm is compared to the outcome of the well-established harmony search technique. The objective of optimization was to minimize CO2 emissions associated with the fabrication of CFST stub columns. The effects of varying the wall thickness as well as the concrete compressive strength on CO2 emissions are visualized by using two different optimization techniques.

1. Introduction

Concrete-filled steel tubular (CFST) columns have several advantages like no formwork requirement, higher ductility and strength compared to the conventional reinforced concrete columns. It is known that a significant amount of CO2 emission is associated with the production of concrete and steel. Since concrete and steel are the most widely used construction materials in the world due to their strength and durability, there is a concerted effort among the construction industry to reduce their carbon footprint. To provide an idea about the magnitude of CO2 emissions related to this industry, the production of 1 kg of concrete is associated with the emission of around 0.12 kg of CO2 into the atmosphere, whereas the production of 1 kg of steel causes emissions of 1.38 kg of CO2 [1]. A detailed list of CO2 emissions corresponding to different classes of concrete is provided in Table 1. It should be noted that the values provided in Table 1 pertain to the production process of concrete and not the entire lifecycle. Although the usual process of structural design prioritizes the optimization of the total structural weight or cost, in line with the commitment of the construction industry to reduce the emission of greenhouse gases, the optimization of CO2 emissions associated with a structure can be adopted as a new structural design practice. Yeo et al. [2] showed that reinforced concrete frames designed under the consideration of CO2 footprint can have 5 to 10% lower CO2 emission compared to a structure designed under cost considerations. Arama et al. [3] analyzed CO2 emissions and cost optimization of reinforced concrete cantilever soldier piles. The volume of concrete was found to have a decisive effect on CO2 emissions and costs compared to the weight of steel used in construction.
Paik et al. [4] investigated the effect of using a voided slab system instead of an ordinary reinforced concrete slab on CO2 emissions. Overall, a 15% reduction in CO2 emissions was observed in the case of voided slabs. In Table 1, C25, C40, C60, and C80 are the concrete classes with 25 MPa, 40 MPa, 60 MPa, and 80 MPa compressive strength, respectively. The amounts of CO2 emission associated with the production of 1 m3 of each concrete class are provided in Table 1.
The ACI and AISC codes include different procedures for the calculation of the ultimate load-carrying capacity N u of CFST stub columns. The major shortcoming of these procedures is that they can only be utilized if the design variables are within certain ranges. In the case of rectangular CFST columns, these design variables are the yield strength of the steel casing f y , the compressive strength of the concrete core f c , and the side lengths of the cross section. For instance, AISC equations are applicable only if f y     525   MPa and 21   MPa   f c   70   MPa . Tao et al. [5], Uy et al. [6], and Wang et al. [7] described N u as the maximum load if this load level is reached at an axial strain less than 0.01. Otherwise, N u is defined as the load level at which the axial compressive strain reaches 0.01. Sakino et al. [8] carried out a comprehensive research program including 114 tests with hollow and concrete-filled steel casings under concentric axial loads for the experimental study of CFST stub columns. The tensile strength of the steel casings in these experiments was in a range between 400 MPa and 800 MPa, while the compressive strength of the concrete changed between 20 MPa and 80 MPa.
The prediction equations of N u by Wang et al. [7] deal with the contributions of both steel casing and concrete core of the CFST columns for the axial compressive capacity. The following equations from (1) to (5) are repre-sented for rectangular CFST stub columns.
N u = N s + N c
N s = η s f y A s ,   N c = η c f c A c
η s = 0.91 + 7.31 10 5 f y 1.28 10 6 + 2.26 10 8 f y D t 2
η c = 0.98 + 29.5 f y 0.48 k s 0.2 t f y D f c 1.3
k s = 1 3 B 2 t H 2 t 2
Where N s is for the steel casing contribution under axial loading and N c presents the concrete contribution. Also, A s is the cross section of the steel casing and A c is the area of the concrete core. The steel casing has a confining effect on the concrete activated by axial loads. The factors η s and η c provided in Equations (3) and (4) introduce the effects of the confinement on the steel and concrete components. Due to this confinement, circumferential stresses are generated in the steel casing, which results in a decrease in wall thickness. Decreased wall thicknesses can cause smaller axial load carrying capacity. In addition to circumferential stresses, another factor that would adversely affect axial load carrying capacity is local buckling of the steel casing. The reduction factor η s in Equation (2) incorporates the effects of decreasing wall thicknesses and local buckling into the prediction equation. On the other hand, the confinement has a beneficial effect on the concrete core, which is expressed through the amplification factor η c . In Equations (3) and (4), D is the equivalent diameter of the rectangular cross section calculated with D = B 2 + H 2 , where B and H are the width and height of the cross section, respectively, as shown in Figure 1. The parameter k s in Equations (4) and (5) is the equivalent confining coefficient that incorporates the lack of concrete confinement due to the rectangular shape of the cross section into the equations. The parameter ranges for which Equations (1)–(5) are applicable are listed in Table 2.
Yan et al. [9] carried out an experimental program including the testing of 16 concentrically loaded square CFST stub columns under uniaxial compression. In these studies, ultra-high performance concrete classes have been used with compressive strengths ranging between 100 and 140 MPa. The yield stress in these experiments ranged between 445 and 670 MPa. All specimens possessed a side length of 100 mm and a B / H ratio of 1. The thickness of the steel casing ranged between 4.9 and 18.5 mm. Wu et al. [10] studied the effect of increasing the column size on the compressive strength of the member since mostly larger sized members are used for practical applications compared to those tested in laboratory settings. Six CFST stub columns with square cross sections were tested under concentrically applied axial compressive loads. The side length of the square cross section ranged between 300 and 750 mm in these experiments. It was observed that as the size of the cross section increases, the favorable effect of confinement on the concrete core tends to decrease. Nguyen et al. [11] conducted an experimental program consisting of six CFST stub column specimens with square cross sections. Particularly, the cross sections were chosen to be slender. Uniaxial compressive loads were applied in a concentric manner. The equations proposed by Wang et al. [7] were applied to all of the specimens documented in [9,10,11]. The predicted ultimate loads are compared to the measured N u values in Figure 2. It was observed that a coefficient of determination of R 2 = 0.94 could be achieved by using Equations (1)–(5). Excluding the large-sized specimens with 750 mm side lengths, this coefficient could be increased to 0.99.
The current study deals with CFST stub columns with rectangular cross sections under uniaxial concentric loading conditions. The main objective of the study is to obtain design configurations that minimize CO2 emissions associated with the production process of the structure while maintaining the compressive strength of the structure above a certain level. To this end, two different metaheuristic optimization techniques have been applied and their performances have been compared. The following Methods section contains the implementation procedure for these two algorithms. In addition to that, numerical examples are presented for both methods in Appendix. The optimized cross-sectional dimensions are tabulated for three different levels of concrete compressive strength in the Results section. The iteration processes are visualized for both optimization techniques at different ultimate load-carrying capacity levels. Most of the research investigations in the field of CFST columns have been focused on experimental testing and finite element modelling of these structures. The optimal design of CFST structures with respect to carbon emission is a mostly neglected field of research. The current study aims to draw attention to this important field because of its environmental significance.

2. Methods

Metaheuristic algorithms have been used on many challenging optimization problems. Metaheuristic techniques are based on the premise that natural phenomena such as the behavior of spider colonies are suitable for the optimization of engineering systems since these natural phenomena also tend to develop towards their optimum states. This assumption was warranted since many engineering systems could be successfully optimized by using metaheuristic techniques. Some of these techniques can be further improved by tuning the parameters they depend on. Particularly, these techniques are well known to converge to the global optima quickly and reliably without excessive computational effort. The metaheuristic algorithms most widely adopted in the field of engineering include harmony search algorithm [12,13], particle swarm optimization [14], artificial bee colony technique [15,16], ant colony algorithm [17], and Jaya algorithm [18]. In addition to metaheuristic techniques, cellular automata based methods have also been used in structural engineering optimization. Tajs-Zielinska and Bochenek [19] successfully applied cellular automata based techniques to the problem of structural topology optimization. The current study is focused on a newly proposed technique called social spider algorithm and its applicability relative to the optimization of CFST columns. Furthermore, the performance of this technique is compared to the time-tested methodology of harmony search optimization. The first application of the social spider optimization (SSO) to an engineering problem was by Alrashidi et al. [20]. In [20], the SSO technique is applied to the problem of wind speed characterization. Cakiroglu et al. [21] applied the SSO technique to the cost and CO 2 emission optimization of CFST columns with circular cross sections. SSO was developed by Cuevas et al. [22].

2.1. Social Spider Optimization

The algorithm takes its name from a spider species called the social spider. This spider species dwell in colonies consisting of male and female spiders. The males in these colonies are further classified as dominant and non-dominant males [23]. The SSO algorithm mimics the interactions of these three different groups of social spiders to solve optimization problems. In this algorithm, a spider represents a solution candidate that can be a set of N real numbers where N is the number of variables being optimized. After the random generation of an initial population of solution candidates within predefined variable ranges, gender is assigned to each solution candidate. In the next phase of the algorithm, the entire population moves towards an overall better performing configuration based on certain rules defined with Equations (6)–(11).
w i = F s i F s w o r s t F s b e s t F s w o r s t
I i , j = w j e d i , j   2
f i k + 1 = f i k + α I i , c s c f i k + β I i , b s b f i k + δ γ 1 2   f o r   ε < P F f i k α I i , c s c f i k β I i , b s b f i k + δ γ 1 2   f o r   ε P F
W M M = h = 1 N m m h k w N f + h h = 1 N m w N f + h
m i k + 1 = m i k + α I i , f s f m i k + δ γ 1 2   f o r   w N f + i > w N f + m m i k + α W M M m i k   f o r   w N f + i w N f + m
r = j = 1 n ( v j h i g h v j l o w ) 2 n
In order to classify the spiders according to their fitness, a weight is assigned to each solution candidate, as shown in Equation (6), where F s i denotes the fitness of the solution candidate with the index i . The fitness function plays a crucial role in this optimization process. In the case of CO2 emission minimization, F can be a function that returns the amount of CO2 emission associated with a solution candidate s i . Consequently, solution candidates with lower CO2 emissions also have better fitness and greater weight. Since the fitness of s i is inversely proportional to the amount of CO2 emissions, F s i can also return the inverse of the mass of CO2 associated with s i so that better fitness is reflected in Equation (6) as w i becomes greater. An illustration of the development of a randomly generated population by using Equations (6)–(11) can be observed in Appendix A.
The spiders are attracted or repelled by each other in proportion to the intensity of the vibrations they receive from each other. These intensities are calculated using Equation (7), where d i , j is the Euclidean distance between the solution candidates with the indices i and j . Equations (8) and (10) show the female and male iteration steps, respectively. In Equation (8), f î k + 1 is the state of a female spider (solution candidate) after the updates, and m î k + 1 is the updated state of a male spider in Equation (10). In these equations, α ,   β ,   γ ,     and     δ are random numbers between zero and one. As Equation (8) shows, the female spider update steps consist of three different components. The first of these components is the attraction of the female spider towards the nearest spider in the colony that also performs better. The vibration intensity of this spider is denoted with I i , c . This kind of attraction is also visualized in Figure 3. The next component of the female spider update is the attraction towards the best-performing member in the entire colony, and its vibration intensity is denoted by I i , b . The third component of the female iteration is a random movement represented by the δ γ 1 2 term. The second line of Equation (8) represents the case in which the female spider f i is repelled by the nearest better-performing and best-performing members of the colony, which may occur depending on the value of the variable ε . In each iteration, ε is assigned a new value between zero and one which is compared to the threshold value P F . Here, P F takes values between zero and one and higher values of P F in order to have a greater probability of attraction instead of repulsion of the female spider as a consequence. In Equation (10), the first line of the equation describes the attraction of a dominant male spider towards the nearest female in the colony. On the other hand, the second line describes the movement of a non-dominant male towards the weighted mean of the entire male population, which is denoted by W M M . In Equation (9), N f and N m are the total numbers of female and male spiders in the colony, respectively. In Equation (10), s f denotes the nearest female spider to m i , and w N f + m is the weight of the median member of the male population. The addition of new members to the colony happens through the mating process in which dominant males mate with female spiders within their radius of mating. In Equation (11), r denotes the radius of mating. Here, v j h i g h and v j l o w are the upper and lower bounds of the j-th design variable, and n is the total number of design variables. The spiders that are involved in mating influence the properties of the newly generated spiders in proportion to their weights. Depending on their quality, the newly generated spiders either replace the worst-performing spiders in the population or are discarded. A flowchart of the social spider algorithm is provided in Figure 4. Further details about this algorithm can be found in [21].

2.2. Harmony Search Algorithm

A metaheuristic algorithm that found application in diverse areas of engineering is the harmony search technique that was invented by Geem [12]. Initially conceived for the optimization of discrete-valued data, the technique eventually evolved in such a manner that it applies to a wide range of problems including water network design [24,25], analysis of plane stress systems [26], design of retaining walls [27], vehicle routing [28], and stacking sequence optimization of laminated composite plates [29].
The starting point of harmony search optimization is the choice of the design parameters and the objective function. In the case of rectangular CFST columns, these design variables are the side lengths of the column cross section. In this study, the objective quantity to be minimized was chosen to be the CO2 emission associated with manufacturing the columns. The goal of the study is to determine the best type of column cross section based on CO2 emissions associated with different design configurations. Once the design parameters are chosen, an initial set of parameter vectors has to be generated randomly while considering the optimization constraints. This set of randomly generated design parameters constitutes an initial population that is expected to move towards an optimum solution through the harmony search iterations. After each iteration step, the members of the population are ranked according to their performance (in this case, the CO2 emission). The newly generated parameter vectors are compared to the existing members of the population, and they replace the worst-performing member in the case where they perform better than some of the existing population members. The harmony search iterations are repeated until the newly generated members no longer exhibit significant improvements compared to the existing population members.
The parameters that play a decisive role in the harmony search iterations are the harmony memory consideration rate H M C R and the pitch adjustment rate P A R . These parameters take different values in each iteration step and are calculated as H M C R = 0.5     1 i t e r / m a x i t e r and P A R = 0.05     1 i t e r / m a x i t e r . Here, i t e r stands for the index of the current harmony search iteration, and m a x i t e r stands for the maximum number of iterations. Equation (12) shows the computation steps for the newly generated member of the population using H M C R and P A R .
k = i n t r a n d H M S , x i , n e w = x i , m i n + r a n d × x i , m a x x i , m i n ,     i f   H M C R > r a n d x i , k + r a n d 2 P A R × x i , m a x x i , m i n ,     i f   H M C R r a n d
In Equation (9), r a n d 0 , 1 and r a n d 2 1 / 2 , 1 / 2 ; H M S is the total number of parameter vectors in the population; x i , k is the i t h design variable in the k t h member in the population of parameter vectors; k is the integer value nearest to the product r a n d H M S ; and x i , m i n and x i , m a x are the minimum and maximum values of the variable with the index i in a parameter vector, respectively.
In the initial step of randomly populating the design vectors as well as in the subsequent iteration steps, certain constraints need to be imposed on the design variables. In addition to the parameter ranges listed in Table 2, the constraint of minimum ultimate load-carrying capacity N u , m i n was placed on each design vector such that, throughout the optimization process, only the design configurations that satisfy certain predetermined load carrying capacity requirements were accepted as valid design configurations. A flow chart of this algorithm is provided in Figure 5. A numerical example of the harmony search algorithm can be found in Appendix B.

3. Results

CO2 emissions were optimized based on the concrete classes like C25, C40, and C60. The ultimate axial load capacity N u , m i n is set for each class and used as optimization constraints with the constraints of the cross-section areas. By using the harmony search and social spider algorithms, the cross-sectional width and height of the member are optimized while keeping N u above the threshold value at all times. The cross-sectional dimensions that do not satisfy the N u , m i n constraints are discarded during the harmony search and social spider iterations. In these optimizations, the cross-sectional height H and width B are the optimization variables such that modifying these dimensions results in different volumes of concrete and steel used in the manufacturing of the CFST stub columns which, in turn, results in different amounts of CO2 emission. For both techniques, the optimization process has been repeated at six different levels of the tube wall thickness and four different levels of the axial load carrying capacity for the concrete classes C25, C40, and C60. As the optimization objective, the CO2 emission associated with the production of a CFST stub column with unit height is selected. The results obtained from both the harmony search and social spider algorithms are visualized in the following sections. In Figure 6, the results of the harmony search optimization process are presented at four different levels of ultimate load carrying capacity for rectangular columns with concrete class C25 and the wall thickness kept constant at 5 mm. The black and red curves in Figure 6 indicate the minimum and average CO2 emissions, respectively, in the entire population of solution candidates at each iteration step. From Figure 6, it is clear that less than fifty harmony search iterations were sufficient to observe a convergence of the minimum CO2 emission at all N u , m i n levels. Moreover, at each level of N u , m i n , the average CO2 emission converges towards the minimum CO2 emission curve within the first fifty iterations. The optimum CO2 emissions as well as the corresponding cross-sectional dimensions are listed in Table 3. In all optimizations, the steel tube’s yield strength was kept constant at 800 MPa. In order to visualize the variations in the optimization process for all levels of wall thickness, three-dimensional surface plots were generated at each level of N u , m i n . Figure 7 shows the surface plots for the concrete class C25. These surface plots show a slight increase in CO2 emissions as the wall thickness increases towards 15 mm.
Similar to Figure 6, Figure 8 and Figure 9 show the minimum and average CO2 emission curves for C40 and C60 concrete classes and t = 7 mm and t = 9 mm wall thicknesses, respectively. Furthermore, Figure 10 and Figure 11 show three-dimensional surface plots of CO2 emissions for these concrete classes. In all of these optimization attempts, the harmony search algorithm was able to reach convergence to a minimum CO2 emission value in less than 50 iterations. By using the harmony search optimization, average minimum CO2 emissions of 48.8 kg, 50.0 kg, and 51.1 kg could be achieved for C25, C40, and C60 concrete classes, respectively. A comparison of the values listed in Table 3 for different levels of N u , m i n shows that as the requirement for the N u , m i n increases so does the corresponding CO2 emission. Furthermore, increased concrete strength results in greater CO2 emissions. As listed in Table 1, concrete classes with higher strength are associated with more increased CO2 release. According to Table 3, the B/H ratio of the optimum configurations varies between 0.6 and 0.85. The distribution of these ratios can be observed in Figure 12.
Figure 13, Figure 14 and Figure 15 show the outcome of social spider optimization for CFST stub columns with rectangular cross sections for C25, C40, and C60 concrete classes for the wall thicknesses t = 5 mm, t = 7 mm, and t = 9 mm, respectively. The corresponding surface plots of CO2 emissions can be observed in Figure 16, Figure 17 and Figure 18. Although a quick convergence in less than 50 iterations could be observed in some of these optimization cases, in most cases a significantly larger number of iterations were necessary to obtain convergence to a minimum. Furthermore, the B/H ratios of the obtained optimum configurations did not present a regular pattern comparable to the harmony search results. A list of the optimized cross-sectional dimensions obtained from the social spider optimization of rectangular cross sections can be observed in Table 4. By using social spider optimization, average CO2 emissions of 51.4 kg, 53.9 kg, and 54.0 kg could be achieved for C25, C40, and C60 concrete classes, respectively. A comparison of average CO2 emissions obtained by using harmony search and social spider optimizations can be observed in Table 5. The increased CO2 emissions by higher strength concrete can be attributed to the greater amounts of CO2 released in the production of higher strength concrete. For each concrete class, increased requirement for N u , m i n was accompanied by higher CO2 emissions. The frequency distribution of the B / H ratios obtained by using the social spider algorithm is shown in Figure 19. Unlike the result of the harmony search optimization, no clustering of the B / H ratios in a certain range of values could be observed. A comparison of the average CO2 emissions achieved by using SSO and harmony search algorithms for a rectangular cross section can be observed in Figure 20 for the concrete classes C25, C40, and C60. The harmony search procedure delivered better-performing configurations for all wall thicknesses and concrete classes. The results obtained from the harmony search method were about 6.2% lower CO2 emission than SSO for rectangular cross sections.

4. Discussion

The current study demonstrated the optimization results obtained by using the well-established harmony search algorithm and a newly developed metaheuristic technique called social spider optimization. The objective of the optimization was to reduce CO2 emissions related to the production process of CFST stub columns with rectangular cross-section under concentric loading. The optimized cross-sectional dimensions have been tabulated for C25, C40, and C60 concrete classes. On average, the production related CO2 emissions obtained by using the harmony search algorithm were 5.1, 7.8, and 5.4% lower than the CO2 emissions obtained by using the social spider optimization. Both of these algorithms are non-gradient-based and evolutionary, while the social spider optimization starts with the assumptions that the natural development of social spider colonies would be a suitable fit for modeling various engineering systems. Although this assumption was warranted in the case of cross-section optimization of CFST columns, the performance of the technique is not necessarily superior to other evolutionary techniques such as the time-tested harmony search method. The performance of the harmony search algorithm can be significantly enhanced through parameter tuning, which is not the case for the social spider algorithm. The differences in the outcome of the two optimization techniques could also be attributed to the differences in the speed of convergence. As it is also demonstrated in the numerical examples of Appendix A and Appendix B, the social spider algorithm comes with a significantly higher complexity, which may have an adverse effect on the convergence speed and the number of iterations needed to converge to the global optima. As a result, after a given number of iterations, the algorithm with greater speed of convergence is expected to deliver better designs.
Further differences in the outcome of the two algorithms were observed in the B / H values corresponding to the optimum designs. The frequency distributions of optimum B / H for the two algorithms showed that the optimum B / H values obtained through the social spider optimization do not exhibit a regular pattern as it was observed in the harmony search algorithm. The different results obtained through these methods can be attributed to the inherent randomness of both techniques. There are various randomly generated parameters built into both of these algorithms. Particularly, the social spider optimization has a larger number of these parameters attempting to mimic the random behaviors of spiders in nature, which could results in the differences in the distribution of the optimum B / H ratios.
The focus of the current study was to minimize carbon emissions while keeping the compressive strength of the CFST stub columns above a certain level. On the other hand, a major priority of the design engineers is to assure the high strength of the structure. Due to the significance of using high strength materials, future studies in this field can include multi-objective optimization techniques having both CO2 emissions and concrete compressive strengths as the objectives of optimization.

5. Conclusions

CFST members have been widely used in the field of structural engineering due to the enhanced mechanical properties that they provide. Due to increased awareness about the sustainability of construction and the carbon footprint associated with concrete, steel, and construction industries, there is an ongoing effort to reduce CO2 emissions caused by the production of various construction materials. At the same time, it is responsible for structural engineers to design structures such as CFST columns in an optimum way so that they satisfy the load-carrying capacity requirements. Therefore, there is an increasing interest in the application of metaheuristic optimization techniques to structural optimization problems in recent years since these techniques have demonstrated that they are able to tackle many engineering problems more effectively. The social spider optimization algorithm is one of the newly developed metaheuristic techniques that can be effectively applied to design optimization problems. This study demonstrates a comparison between social spider optimization and harmony search algorithm applications for CFST columns. In terms of convergence speed and the quality of the optimization outcome, the harmony search algorithm was observed to be significantly superior compared to the social spider algorithm. The configurations obtained by using the harmony search algorithm resulted in a 6.2% lower CO2 emissions on average. Furthermore, the speed of convergence of the harmony search method was observed to be an order of magnitude better than the social spider algorithm in most optimization cases. Moreover, it was observed that the configurations with greater concrete compressive strength also resulted in increased CO2 emission. Furthermore, the results of the harmony search optimization showed clustering of the optimum B / H ratios in a range from 0.6 to 0.75. Future research in this field can include CFST columns with various slenderness properties and column heights. In addition to the outer steel casing, another inner steel tube can be introduced. Moreover, the effect of using lightweight fiber-reinforced composite materials as casing can be investigated.

Author Contributions

C.C. and G.B. generated the analysis codes. The text of the paper was formed by C.C., K.I., G.B., S.K. and Z.W.G. The figures were prepared by C.C. and K.I.; G.B. and Z.W.G. supervised the research direction. All authors have read and agreed to the published version of the manuscript.

Funding

This research was supported by the Energy Cloud R&D Program through the National Research Foundation of Korea (NRF) funded by the Ministry of Science, ICT (2019M3F2A1073164).

Conflicts of Interest

The authors declare no conflict of interest.

Appendix A

An Example of the Social Spider Algorithm

The steps of the social spider algorithm are elaborated on a numerical example with a population of 10 spiders with 7 of them being female. All members of the population have a steel wall thickness of 5   mm , concrete compressive strength of 60   M P a , and steel yield stress of 800   M P a . In Table A1, F s i returns for each spider the inverse of the corresponding CO2 emission in kg, and w i is the corresponding weight which is calculated by using Equation (6). It is assumed that all population members have sufficient compressive strength ( N u N u , m i n ).
Table A1. Initial spider population.
Table A1. Initial spider population.
s i f 1 f 2 f 3 f 4 f 5 f 6 f 7 m 1 m 2 m 3
H 446928651455160339249184558125219815894
B 195294815954105132827791681296574
F ( s i ) 10 3 0.270.744.04.910.514.240.194.50.800.54
w i 10 2 1.6111.680.71006.7185.8091.412.97.3
According to Table A1, m 1 is the male spider with the best fitness among the male population and, therefore, is classified as dominant. The median member of the male population m 2 and the worst-performing member m 3 are classified as non-dominant. The weights of the entire population are normalized so that the best performing member f 4 has w i = 1 and the worst-performing member f 7 has w i = 0 .
Next, we store the Euclidean distances and perceived vibration intensities between the spiders in 10 by 10 matrices, as shown in Table A2 and Table A3. The Euclidean distances are calculated by using the independent variables B and H as d i s t s i , s j = B j B i 2 + H j H i 2 . Afterwards these distances are normalized so that they can be plugged into Equation (7).
Table A2. Matrix of distances.
Table A2. Matrix of distances.
f 1 f 2 f 3 f 4 f 5 f 6 f 7 m 1 m 2 m 3
f 1 00.3260.7480.5920.1820.6730.1430.7510.5470.342
f 2 0.32600.4750.2670.1830.3520.4300.4680.3240.526
f 3 0.7480.47500.3470.6530.2340.7920.0350.2161
f 4 0.5920.2670.34700.4350.1270.6930.3220.3360.745
f 5 0.1820.1830.6530.43500.5330.3170.6480.4800.349
f 6 0.6730.3520.2340.1270.53300.7560.2050.2920.859
f 7 0.1430.4300.7920.6930.3170.75600.8010.5790.444
m 1 0.7510.4680.0350.3220.6480.2050.80100.2320.994
m 2 0.5470.3240.2160.3360.4800.2920.5790.23200.829
m 3 0.3420.52610.7450.3490.8590.4440.9940.8290
Table A3. Matrix of vibration intensities.
Table A3. Matrix of vibration intensities.
f 1 f 2 f 3 f 4 f 5 f 6 f 7 m 1 m 2 m 3
f 1 0.0160.1040.4620.7040.0650.54600.5200.0960.065
f 2 0.0150.1160.6450.9310.0650.75800.7340.1170.055
f 3 0.0090.0930.8070.8870.0440.81200.9130.1240.027
f 4 0.0110.1080.71610.0560.84400.8240.1160.042
f 5 0.0160.1120.5270.8270.0670.64600.6000.1030.065
f 6 0.0100.1030.7640.9840.0510.85800.8760.1190.035
f 7 0.0160.0970.4310.6190.0610.48400.4810.0930.060
m 1 0.0090.0930.8060.9010.0440.82300.9140.1230.027
m 2 0.0120.1050.7700.8930.0530.78800.8660.1300.037
m 3 0.0140.0880.2970.5740.0590.41000.3400.0650.073
In Table A2, the spiders listed in the first column are the ones perceiving the vibrations, and the spiders listed in the first row are the ones emitting the vibrations. Therefore, the table is not symmetrically populated. The column of f 7 consists of zeros since f 7 is the worst-performing member and has zero weight. Once the vibration intensities are determined, the next step is to calculate the attractions/repulsions of each spider towards the other colony members. First, we will demonstrate the female iteration based on Equation (8) on the member f 1 . Let P F = 0.7 and ε = 0.28 , where ε is a randomly generated parameter between 0 and 1. Since ε < P F , the first row of Equation (8) applies to this iteration. In Equation (A1), the parameters α , β , δ , and   γ are randomly generated. The closest member to f 1 that has greater weight than f 1 is f 5 , and the best-performing member of the population is f 4 . Therefore, in Equation (A1), I 1 , c = I 1 , 5 and I 1 , b = I 1 , 4 .
f 1 0 = 4469 1952 α = 0.489 ,   β = 0.119 ,   δ = 0.785 ,   γ = 0.899 f 1 1 = f 1 0 + α I 1 , 5 f 5 0 f 1 0 + β I 1 , 4 f 4 0 f 1 0 + δ γ 1 2 = 4469 1952 + 0.489 0.065 3924 1051 4469 1952 + 0.119 0.704 1603 54 4469 1952 + 0.785 0.899 1 / 2 0.785 0.899 1 / 2 = 4212 1765
As Equation (A1) shows, the updated version of f 1 0 is f 1 1 = 4212 1765 . At this stage, the performance of this newly generated member has to be compared to f 1 0 . This comparison shows that F f 1 1 = 3.1 10 4 > F f 1 0 = 2.68 10 4 . Therefore, f 1 1 will replace f 1 0 in the next iteration.
We demonstrate the iterations for dominant and non-dominant males on m 1 and m 3 , respectively. Equation (A2) models the attraction of m 1 to the nearest female f 3 .
m 1 0 = 1252 168 α = 0.489 ,   δ = 0.785 ,   γ = 0.899 m 1 1 = m 1 0 + α I 1 , 3 f 3 0 m 1 0 + δ γ 1 2 = 1252 168 + 0.489 0.806 1455 159 1252 168 + 0.785 0.899 1 2 0.785 0.899 1 2 = 1332 165
The resulting m 1 1 has a fitness score of F m 1 1 = 4.27 10 3 < F m 1 0 = 4.50 10 3 . Therefore, the newly generated m 1 1 will be discarded. In order to model the non-dominant male iteration, we need to calculate the weighted mean of the entire male population (WMM) as shown in Equations (9) and (A3).
m 3 0 = 5894 574 ,   α = 0.489 W M M = m 1 0 w 1 0 + m 2 0 w 2 0 + m 3 0 w 3 0 w 1 0 + w 2 0 + w 3 0 = 1252 168 0.914 + 1981 1296 0.129 + 5894 574 0.073 0.914 + 0.129 + 0.073 = 1640 325 m 3 1 = m 3 0 + α W M M m 3 0 = 5894 574 + 0.489 1640 325 5894 574 = 3814 452 F m 3 1 = 9.5 10 4 > F m 3 0 = 5.36 10 4
Since the newly generated m 3 1 has greater fitness score, it will replace m 3 0 in the next iteration.
The final step in the SSO iteration is mating between the dominant male and the females within the radius of mating. The radius of mating is determined by the upper and lower bounds of the design variables and the total number of design variables. By using Equation (11), the radius of mating for this example is calculated as in Equation (A4).
r = 3000 36 + 6000 36 4 = 2232
After scaling to the interval 0 , 1 , r becomes 0.385. According to Table A2, f 3 , f 4 , and f 6 are within the radius of mating of m 1 . In the mating process, the properties of the newly generated member are assigned through a weighted combination of all the members involved in mating as in Equation (A5).
s n e w = w 3 f 3 + w 4 f 4 + w 6 f 6 + w 1 m 1 w 3 + w 4 + w 6 + w 1 = 0.807 1455 159 + 1603 54 + 0.858 918 328 + 0.914 1252 168 0.807 + 1 + 0.858 + 0.914 = 1316 173
The fitness factor of s n e w is F ( s n e w ) = 4.25 10 3 , which is better than the worst-performing member f 7 . Therefore, s n e w will replace f 7 in the next iteration.

Appendix B

An Example of the Harmony Search Algorithm

Since the harmony search method also needs a randomly generated initial population of design vectors, we can start with the population in Table A1 that was generated for the SSO algorithm. Furthermore, we can use the same performance metric that was used for SSO and denoted with the function F according to which the members of the population will be ranked. The first step in this method is the calculation of the H M C R parameter as H M C R = 0.5 1 i / N , where i is the number of the current iteration, and N is the total number of iterations. The second parameter needed in the harmony search algorithm is the pitch adjustment rate P A R , which is calculated as P A R = 0.05 1 i / N = H M C R / 10 . In the first iteration, H M C R and P A R have the values of 0.498 and 0.0498, respectively. Next, we generate two random numbers r a n d = 0.612 and r a n d 2 = 0.781 . Since H M C R < r a n d , we apply the second row of Equation (9) as in Equation (A6). Here, we require the parameter k , which is the nearest integer to r a n d 10 = 7 . The population member with index 7 is f 6 = 918 ,   328 . Equation (A6) shows the first iteration for the first member of the population f 1 = 4469 ,   1952 .
f 1 1 = 918 328 + 0.781 0.0498 5894 918 2779 54 = 1112 434
The steel and concrete strength as well as the steel wall thickness are chosen to be the same as in Appendix A. The performance of the newly generated design vector f 1 1 is calculated as F f 1 1 = 3.02 10 3 > F f 1 0 = 0.27 10 3 . Since the newly generated vector performs better, it will replace the initial design vector in the next iteration.

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Figure 1. Dimensions of a rectangular CFST column.
Figure 1. Dimensions of a rectangular CFST column.
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Figure 2. Correlation of predicted and measured N u values (a) including large-sized specimens and (b) excluding large-sized specimens.
Figure 2. Correlation of predicted and measured N u values (a) including large-sized specimens and (b) excluding large-sized specimens.
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Figure 3. The attraction of s1 towards the nearest better-performing colony member s3.
Figure 3. The attraction of s1 towards the nearest better-performing colony member s3.
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Figure 4. SSO flowchart.
Figure 4. SSO flowchart.
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Figure 5. Flowchart of the harmony search optimization.
Figure 5. Flowchart of the harmony search optimization.
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Figure 6. Harmony search optimization of a rectangular cross section relative to CO2 emissions (C25) ( t = 5   mm ).
Figure 6. Harmony search optimization of a rectangular cross section relative to CO2 emissions (C25) ( t = 5   mm ).
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Figure 7. Harmony search steps for six different wall thicknesses (C25).
Figure 7. Harmony search steps for six different wall thicknesses (C25).
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Figure 8. Harmony search optimization of a rectangular cross section relative to CO2 emissions (C40) (t = 7 mm).
Figure 8. Harmony search optimization of a rectangular cross section relative to CO2 emissions (C40) (t = 7 mm).
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Figure 9. Harmony search optimization of a rectangular cross section relative to CO2 emissions (C60) (t = 9 mm).
Figure 9. Harmony search optimization of a rectangular cross section relative to CO2 emissions (C60) (t = 9 mm).
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Figure 10. Harmony search steps for six different wall thicknesses (C40).
Figure 10. Harmony search steps for six different wall thicknesses (C40).
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Figure 11. Harmony search steps for six different wall thicknesses (C60).
Figure 11. Harmony search steps for six different wall thicknesses (C60).
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Figure 12. B / H distribution obtained through harmony search optimization.
Figure 12. B / H distribution obtained through harmony search optimization.
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Figure 13. Social spider optimization of a rectangular cross section relative to CO2 emissions (C25) (t = 5 mm).
Figure 13. Social spider optimization of a rectangular cross section relative to CO2 emissions (C25) (t = 5 mm).
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Figure 14. Social spider optimization of a rectangular cross section relative to CO2 emissions (C40) (t = 7).
Figure 14. Social spider optimization of a rectangular cross section relative to CO2 emissions (C40) (t = 7).
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Figure 15. Social spider optimization of a rectangular cross section to CO2 emissions (C60) (t = 9).
Figure 15. Social spider optimization of a rectangular cross section to CO2 emissions (C60) (t = 9).
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Figure 16. SSO steps for six different wall thicknesses (C25).
Figure 16. SSO steps for six different wall thicknesses (C25).
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Figure 17. SSO steps for six different wall thicknesses (C40).
Figure 17. SSO steps for six different wall thicknesses (C40).
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Figure 18. SSO steps for six different wall thicknesses (C60).
Figure 18. SSO steps for six different wall thicknesses (C60).
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Figure 19. B / H distribution obtained through the social spider optimization.
Figure 19. B / H distribution obtained through the social spider optimization.
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Figure 20. Comparison of two algorithms for (a) C25, (b) C40, and (c) C60.
Figure 20. Comparison of two algorithms for (a) C25, (b) C40, and (c) C60.
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Table 1. CO2 emissions of different concrete classes pertaining to the production process [1].
Table 1. CO2 emissions of different concrete classes pertaining to the production process [1].
Concrete ClassC25C40C60C80
CO2 emission (kg/m3)215272350394
Table 2. Parameter ranges for which Equations (1) and (2) are applicable [7].
Table 2. Parameter ranges for which Equations (1) and (2) are applicable [7].
Width to thickness ratio 12     B / t     100
Height to Width ratio 1     H / B     2
Yield strength of the steel tube 175   MPa     f y     960   MPa
Compressive strength of the concrete 20   MPa     f c     120   MPa
Steel wall thickness (mm) 3     t     30
Table 3. Minimum CO2 emissions for rectangular cross section obtained from harmony search optimization.
Table 3. Minimum CO2 emissions for rectangular cross section obtained from harmony search optimization.
Concrete ClassNu,min
(kN)
Min. CO2 Emission (kg)H
(mm)
B
(mm)
T
(mm)
B/H
C25600062.131024550.79
500052.426820550.77
400042.722416550.74
200022.41278450.66
C40600067.826822550.84
500056.623619150.81
400045.520115750.78
200023.21198450.71
C60600074.623820150.85
500061.320917650.84
400048.418314450.79
200023.71108350.76
C25600065.225317770.70
500055.121814870.68
400044.718012070.67
200023.31006370.63
C40600068.722917470.76
500057.519914770.74
400046.316912070.71
200023.6976570.67
C60600071.820916570.79
500059.518114470.80
400047.415711670.74
200023.6936570.70
C25600067.521214290.67
500056.918112090.66
400046.21529690.63
200024835490.65
C40600069.619914290.71
500058.317412090.69
400046.91449990.69
200024.0825590.67
C6060007118713990.74
500059.116212090.74
400047.31379990.72
200024.1805690.70
C25600069.2185119110.64
500059.1158101110.64
400047.213084110.65
200024.37449110.66
C40600070.4177122110.69
500059.0153103110.67
400047.412884110.66
200024.67449110.66
C60600070.9169121110.72
500059.1146104110.71
400047.612387110.71
200024.77251110.71
C25600070.6163106130.65
500059.414090130.64
400047.911675130.65
200025.06746130.69
C40600071.2160106130.66
500059.513891130.66
400048.011577130.67
200025.26747130.70
C60600071.1154108130.70
500059.713493130.69
400048.211278130.70
200025.36648130.73
C25600071.514896150.65
500060.012882150.64
400048.510770150.65
200025.66345150.71
C40600071.814698150.67
500060.412784150.66
400049.010671150.67
200025.96346150.73
C60600071.914398150.69
500060.512585150.68
400049.110473150.70
200026.06247150.76
Table 4. Minimum CO2 emissions for rectangular cross section obtained from social spider optimization.
Table 4. Minimum CO2 emissions for rectangular cross section obtained from social spider optimization.
Concrete
Class
N u , m i n ( kN ) Min. CO2 Emission (kg)H
(mm)
B
(mm)
T
(mm)
B/H
C2560006534223350.68
500053.928020250.72
400043.619919050.96
200023.21537250.47
C40600067.825323850.94
500060.643511150.26
400046.528511350.40
200027.13253650.11
C60600075.222921150.92
500062.423415850.68
400048.618914050.74
200024.21168050.69
C25600069.435813370.37
500055.521415270.71
400049.123010370.45
200024.31036470.62
C40600071.829413770.47
500066.24557470.16
4000502598570.33
200024.61006670.66
C60600073.328212570.44
500059.720013170.66
400052.83096670.21
200025.31124270.38
C25600076.630711190.36
500058.922110290.46
400052.12167690.35
200024.2934990.53
C40600075.95146090.12
500058.515513590.87
400047.31708990.52
200024.31064390.41
C60600076.517016590.97
500064.72229690.43
400049.81419690.68
200026.91154490.38
C25600069.3159139110.87
500058.9132122110.92
400051.819960110.3
200025.28843110.49
C40600077.753045110.09
500064.325667110.26
400055.434936110.1
200027.09642110.44
C60600071.721895110.44
500065.225366110.26
400049.317364110.37
200024.47250110.69
C25600075.719496130.5
500059.7119106130.89
400055.318355130.3
200025.27541130.55
C40600075.4180100130.56
500065.731543130.14
400055.618456130.30
200025.47940130.51
C6060008123979130.33
500063.715884130.53
400055.718338130.21
200025.86351130.81
C25600075.720275150.37
500063.717364150.37
400050.710674150.70
200026.27141150.58
C4060008246536150.08
500066.732736150.11
400049.19679150.82
200029.48340150.48
C6060008428258150.21
500060.113678150.57
400049.19187150.96
200027.67740150.52
Table 5. Comparison of CO2 emissions corresponding to harmony search (HS) and social spider (SSO) algorithms.
Table 5. Comparison of CO2 emissions corresponding to harmony search (HS) and social spider (SSO) algorithms.
Minimum CO2 Emission (kg)
C25C40C60
HS48.850.051.1
SSO51.453.954.0
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Cakiroglu, C.; Islam, K.; Bekdaş, G.; Kim, S.; Geem, Z.W. CO2 Emission Optimization of Concrete-Filled Steel Tubular Rectangular Stub Columns Using Metaheuristic Algorithms. Sustainability 2021, 13, 10981. https://0-doi-org.brum.beds.ac.uk/10.3390/su131910981

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Cakiroglu C, Islam K, Bekdaş G, Kim S, Geem ZW. CO2 Emission Optimization of Concrete-Filled Steel Tubular Rectangular Stub Columns Using Metaheuristic Algorithms. Sustainability. 2021; 13(19):10981. https://0-doi-org.brum.beds.ac.uk/10.3390/su131910981

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Cakiroglu, Celal, Kamrul Islam, Gebrail Bekdaş, Sanghun Kim, and Zong Woo Geem. 2021. "CO2 Emission Optimization of Concrete-Filled Steel Tubular Rectangular Stub Columns Using Metaheuristic Algorithms" Sustainability 13, no. 19: 10981. https://0-doi-org.brum.beds.ac.uk/10.3390/su131910981

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