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Article

Hybrid Ensemble Model for Predicting the Strength of FRP Laminates Bonded to the Concrete

by
Anas Abdulalem Alabdullh
1,
Rahul Biswas
2,
Jitendra Gudainiyan
3,
Kaffayatullah Khan
1,*,
Abdullah Hussain Bujbarah
1,
Qasem Ahmed Alabdulwahab
1,
Muhammad Nasir Amin
1 and
Mudassir Iqbal
4
1
Department of Civil and Environmental Engineering, College of Engineering, King Faisal University, Al-Ahsa 31982, Saudi Arabia
2
Department of Applied Mechanics, Visvesvaraya National Institute of Technology, Nagpur 440010, India
3
Department of Civil Engineering, GLA University, Mathura 281406, India
4
Department of Civil Engineering, University of Engineering and Technology, Peshawar 25120, Pakistan
*
Author to whom correspondence should be addressed.
Polymers 2022, 14(17), 3505; https://doi.org/10.3390/polym14173505
Submission received: 10 July 2022 / Revised: 11 August 2022 / Accepted: 17 August 2022 / Published: 26 August 2022
(This article belongs to the Special Issue Fiber-Reinforced Polymer Composites in Construction Materials)

Abstract

:
The goal of this work was to use a hybrid ensemble machine learning approach to estimate the interfacial bond strength (IFB) of fibre-reinforced polymer laminates (FRPL) bonded to the concrete using the results of a single shear-lap test. A database comprising 136 data was used to train and validate six standalone machine learning models, namely, artificial neural network (ANN), extreme machine learning (ELM), the group method of data handling (GMDH), multivariate adaptive regression splines (MARS), least square-support vector machine (LSSVM), and Gaussian process regression (GPR). The hybrid ensemble (HENS) model was subsequently built, employing the combined and trained predicted outputs of the ANN, ELM, GMDH, MARS, LSSVM, and GPR models. In comparison with the standalone models employed in the current investigation, it was observed that the suggested HENS model generated superior predicted accuracy with R2 (training = 0.9783, testing = 0.9287), VAF (training = 97.83, testing = 92.87), RMSE (training = 0.0300, testing = 0.0613), and MAE (training = 0.0212, testing = 0.0443). Using the training and testing dataset to assess the predictive performance of all models for IFB prediction, it was discovered that the HENS model had the greatest predictive accuracy throughout both stages with an R2 of 0.9663. According to the findings of the experiments, the newly developed HENS model has a great deal of promise to be a fresh approach to deal with the overfitting problems of CML models and thus may be utilised to forecast the IFB of FRPL.

1. Introduction

Reinforced concrete structures are composite materials of concrete and reinforcement which are subjected to wear and tear throughout the structure’s life span [1]. This emphasises the need for proper maintenance and sustainability of RC structures. To address the self-strengthening factors in a structure’s construction process, many new technologies have been introduced and implemented [2]. Fibre-reinforced polymer (FRP) laminates bonded to the concrete prism comprise one of the retrofitting methods which facilitates an increase in the structural capacity performance of beams [3,4,5], columns [6,7], and beam–column joints [8,9,10,11]. The FRP plates exhibit outstanding resistance to corrosion [12], fatigue [13,14], creep, and hygrothermal deformations [15] and lead to lightweight and high-strength structures that can substitute the use of structural reinforcement. Different types of FRPs, namely CFRP, BFRP, and GFRP, are used in structural applications owing to their cost and benefits. Although CFRP is expensive, it has very good mechanical characteristics and corrosion, creep, and fatigue resistances. Contrarily, GFRP and BFRP have relatively weak mechanical characteristics and corrosion resistance, especially when exposed to the alkaline environment of concrete [16,17,18]. They are ductile, easy to install, and possess no magnetic properties, all of which are advantages of the FRP [19,20,21,22,23,24,25,26].
The reinforced concrete structure proceeds through different failure patterns. The cracks are possibly generated from the concrete, which leads to the failure of the concrete [27,28,29,30,31,32,33]. The FRP laminates are widely used for retrofitting reinforced concrete structures. The various failure patterns FRP is subjected to are rupture, concrete crushing, shear cracking, and delamination [34]. The rupture and crushing phenomenon in FRP occurs when the ends of the plates are tightly anchored. The FRP is commonly reported to fail due to debonding [35]. Debonding failure occurs in different conditions such as those of increasing temperature or the degradation of resin due to dynamic loading and thermal loading [36]. Irreversible interfacial debonding occurs due to the diffusion of water molecules in the plates and the interfacial bond failure is affected by bond quality due to workmanship [37]. The composite action between the concrete prism and FRP is responsible for the failure of strengthening members [38].
The flexural strengthening of beams can be achieved by increasing the efficiency of bonding or by providing a suitable interface between the concrete and FRP [39]. Most of the premature failures are due to inappropriate preparation of the interface between the concrete and FRP. Epoxy interlocking in near-surface mounting techniques can be used in such conditions. The smooth interface is generally extracted by the removal of the deteriorated surface layer of the concrete until the exposure of the coarse aggregates. The exposed surface of the concrete is concealed by sandblasting and removal of dust is carried out by using a special brush; additionally, the cleaning can be conducted with solvents and by drying before installing the FRP sheets. This essentially creates interfacial consistency and enhancement in the ultimate rupture strength by delayed debonding. The FRP can be used directly on concrete or laminates placed in the grooves and then packed using high-adhesive materials [38]. They can even be externally bonded to the grooves made on the concrete surface [40]. The Near Surface-Mounted Retrofit (NSMR) method is also widely used owing to its high resistance against environmental conditions [41,42]. Using epoxy mortars, the FRP bar is put into a slit in the cover concrete and joined to the concrete. Since FRP is not exposed on, it is beneficial in mitigating the aforementioned environmental effects even if it necessitates additional concrete slit formation work. The methods are considered according to the surface area, availability of materials and equipment, safety, and cost.
The single-lap shear test (SST) is an experimental procedure that can be conducted to calculate interfacial bond strength (IBS) between FRP and concrete prisms and its fundamental results are reliable and simple [43,44,45]. Many empirical or semi-empirical formulations have been conducted under the fundamental of IBS on experimental results from SSTs [29]. The empirical relations and the models generated seemed to correlate with the experimental data established. The basic simplified assumptions have been used in empirical relations, although the models have not been validated for new data. Artificial intelligence (AI) has commonly been used to obtain an optimistic solution for regression and classification of problems in engineering problems [46,47,48,49,50,51,52,53,54,55,56]. It can not only be used for experimental observations, but can also authenticate them by assigning new data sets [47,48,49,50,51,57,58,59,60,61,62,63,64,65,66,67,68,69,70,71,72,73,74,75,76].
Vu and Hoang [77] used the non-linear capabilities of the least square support vector machine to predict the punching shear capacity of FRP-reinforced concrete beams, which helped them to achieve the coefficient of determination (R2) equalling 0.99. Hong [78] used an artificial neural network (ANN) to determine the punching shear capacity of steel-fibre-reinforced concrete slabs. Abuodeh [79] studied the behavior of RC beams concerning their shear capacity under a neural interpretation diagram (NID) and recursive feature elimination (RFE) algorithm.
In the brief, we can state that AI models have proved to be very feasible and reliable for experimental results when it comes to the prediction of IBS of FRP plates or punching shear capacity of FRP-reinforced concrete beams. AI models such as multilinear regression, support vector machine, and ANN were used to forecast the IBS of laminates to the concrete prism by Su et al. [80]. The observation for the training and validation of the data resulted in the accuracy of R2 equalling 0.81 and 0.91, but the developed models can be developed based on their accuracy. We can also use gene expression programming (GEM), which is a robust technique used to form an intact relationship between input and output attributes, in the form of a simple mathematical equation. However, the ANN models provide no information about the basis of the relationship between the mathematical equations and attributes related to each other [81,82,83], and hence an overall parametric analysis should be conducted to investigate the effects of input attributes on IBS as they have an efficient command over the type of strengthening techniques in terms of efficiency and viability.
Taking these considerations into account, a hybrid ensemble approach was used to forecast ISB of FRP laminates externally bonded to the concrete prism on groves in this study. Using data from a custom database, we presented, analysed, and discussed six widely used conventional soft computing techniques: an artificial neural network (ANN) [84], extreme machine learning (ELM) [85], the group method of data handling (GMDH) [86], the multivariate adaptive regression splines (MARS) [87], the least squares-support vector machine (LSSVM) [81], and Gaussian process regression (GPR) [88]. When the conventional machine learning (CML) models were combined with an ANN model, a hybrid ensemble technique was proposed. For “unstable” models, an ensemble model works on a high level to improve their performance. It is worth noting that in many situations, an ensemble model comprised of multiple machine learning (ML) models outperforms a single model. The hybrid ensemble model (HENS) [89,90] presented in this paper comprised six CML models and one ANN. FRP laminates externally bonded on the concrete prism utilising SSTs results were predicted using conventional and HENS models, respectively, to aggregate the CML models’ output. Eight performance indices were used to evaluate the prediction performance of the models used, including ANN, ELM, GMDH, MARS, LSSVM, GPR, and HENS. The suggested HENS model’s benefits and applicability were confirmed by comparisons with CML models based on experimental data. The research plays an important role to explore the potential of the HENS model in the prediction of the ISB of FRP laminates externally bonded to the concrete prism on the groves using SST results (anchorage made on one end of FRP to the concrete prism shown in Figure 1). For better representation of the results, the study also includes the visual interpretation of results using an accuracy matrix and Taylor diagram.

2. Research Significance

In order to solve the challenges associated with using empirical formulas to forecast the IBS of FRP, it was clear that an alternative approach was required as soon as possible. For this purpose, the approaches of soft computing, with their proficiency for non-linear modelling, have emerged as a significant class of prediction tools, providing answers to the ever-increasing complexity of optimisation issues. In this research, an enhanced application of CML algorithms was presented for the estimation of IBS of FRP using a hybrid ensemble technique. The traditional feed-forward ANN was chosen for the construction of the HENS model because of its straightforward network topology, its capacity to deal with varying degrees of complexity, its ease of application, and its capability to provide highly non-linear modelling. The findings of this research will provide engineers with tools to predict the IBS of FRP and will make it easier to design FRP constructions that are less complex and more durable while also improving the level of accuracy with which such designs can be made.

3. Soft Computing Techniques

3.1. ANN

Artificial neurons [84] are conceptually developed from biological neurons, which are made up of elements that operate in parallel and are organised in ways that resemble biological neural networks. Each artificial neuron receives inputs and generates a single output that can be transmitted to a number of other neurons. There are three essential layers of ANN: the input layer, the output layer, and the hidden layer. The outputs of neurons are achieved by calculating the weighted total of all the inputs, which is then multiplied by the weights of the connections between the inputs and the neurons. Later, a bias term is added to this total. The weighted sum is processed through a (typically non-linear) activation function to create the output. The system generates a result that is similar to the target result. For this study, a single hidden layer was used to develop the model.
For x R d , w i t h   K i j   x i ,   x j i , j = 1 , , n for all pairs of x R d could make K X , X the covariance matrix.

3.2. ELM

ELM is a novel soft computing approach that aims to bridge the gap between machine learning and biological learning mechanisms [85]. Extreme refers to a strong approach with learning capabilities comparable to the human brain in this context. Unlike ANNs, which require hidden neuron tuning during the learning phase, an ELM, whether it is a single- or multi-hidden layer feed-forward network, does not require any tuning. ELM has been effectively used in learning capacity for feature learning, clustering, regression, and classification applications in recent years [85,91]. ELM was created as a quick-learning, single-layer feed-forward network (SLFN) with high generalisation capacity, making it easier to build than other soft computing approaches.
In an ELM, the input data are mapped to an M-dimensional ELM random feature space and the network output is mapped according to the following equation:
f M x = h i x
where h i = hidden nodes output for input x; M = dimensionality of the ELM random feature space; β i = output weight matrix between the hidden nodes and the output nodes.

3.3. GMDH

The group method of data handling (GMDH) is a set of techniques for computer-based structure identification and mathematical modelling [86]. The majority of GMDH algorithms employ an inductive self-organising method to generate a multi-parametric model. Inductive GMDH algorithms allow for the automatic discovery of data interrelationships, the selection of an ideal model or network architecture, and the improvement of the accuracy of current algorithms. The group method of data handling is a collection of methods for solving various issues. It includes methods for parametrics, clustering, analogue complexion, rebinarisation, and probability. This inductive technique is focused on sorting out more complex models and selecting the best solution with the minimum possible external criteria. Basic models include not just polynomials, but also non-linear, probabilistic functions and cauterisations. A GMDH model with several inputs and one output that is a subset of the base function’s components is written as:
Y x 1 , , x n = a 0 + i = 1 m a i f i
where elementary functions’ dependency on different sets of inputs is denoted by f i , a i are coefficients, and m represents the number of the base-function components.
GMDH methods use multiple component subsets of the base function (in eqn), termed as partial models, in order to obtain the optimal answer. The least squares approach is used to estimate the coefficients of these models. The number of partial model components in GMDH algorithms is continuously increased until the minimal value of an external criterion indicates a model structure with optimal complexity. This is referred to as model self-organisation.

3.4. MARS

Jerome H. Friedman [87] proposed multivariate adaptive regression splines (MARS) as a type of regression model in 1991. It is a non-parametric regression approach, which may be seen as an extension of linear models, that incorporates nonlinearities and interactions between variables automatically. MARS may be thought of as an ensemble of linear functions linked together by one or more hinge functions. The results of mixing linear hinge functions may be seen in the figure below, where the black dots represent observations, and the red line is a MARS model forecast (Figure 2).
The algorithm is divided into two stages: forward and backward. In the forward step, it generates a large number of candidate basis functions in pairs. On the other hand, a pair of functions will be incorporated into the model if it lowers the overall model error. In the first phase, the maximum number of functions that the model generates with a hyper-parameter may be adjusted. Whereas, the pruning step, also known as the backward stage, goes over each function one by one and deletes those that do not contribute any value to the model. This is accomplished through the use of a cross-validation-based generalised cross-validation (GCV) score. It is only a rough estimate of the real cross-validation score, with the goal of penalising model complexity. A set of linear functions may be put forward as in the following simple equation:
f x = α 0 + i = 1 k α i B i x
where, f x is the output and i = 1 k α i B i x .Weighted sum of basis functions is denoted by B i x . Each α i c i term represents a constant coefficient.

3.5. LSSVM

A least-square support vector machine (LSSVM) is a supervised machine learning method that may be used for both regression and classification. It was created by Vapnik in 1995 [92] and is based on statistical learning theory. SVM techniques project data into a high-dimensional feature space and employ kernels to classify nonlinearly separable datasets [93,94]. In multidimensional space, an SVM model is essentially a representation of various classes in a hyperplane. SVM will generate the hyperplane in an iterative manner in order to reduce the error. SVM’s objective is to split datasets into classes such that a maximum marginal hyperplane (MMH) may be found. The data points closest to the hyperplane, or the points of a data set that, if deleted, would change the location of the dividing hyperplane, are called support vectors. As a result, they might be regarded as important components of data collection. In general, the accuracy of the SVR model is determined by the kernels used and their parameters. The radial basis function (RBF) has been shown to perform well as a kernel function for SVM in several forecasting experiments) [95].
For a data set ω = x i , y i i = 1 , 2 n where x R d is a d-dimensional input vector space and y R is an output in a 1-dimensional vector space, SVM regression can estimate the relationship between x and y. In the SVM approach, the risk function is minimized by minimizing both empirical risk and ω 2 .
R = 1 2 ω 2 + C C l ε ( y i f x i )
where the regression data vector is ω and the loss is denoted by l ε , which presents the difference between y i (real output) and f x i . A positive constant value C C is needed to fix the abovementioned. l ε ( y i f x i ) will be 0 for y i f x i < ϵ . Otherwise, it is equal to y i f x i   . The risk function can be minimized with the following function:
f x , α , α * = i = 1 l α i * α i φ x i , φ x + b
where α i * . α i = 0 and α i * . α i 0 , φ x i , φ x is a product of kernel function and b is a bias term.

3.6. GPR

Supervised learning has two key components, and their approaches are classification and regression issues. Gaussian process regression is one of the most appealing supervised learning nonparametric techniques for predictions among the many approaches [96]. Considering a data set:
ω =   x i , y i i = 1 , 2 n
where x R d is a d-dimensional input vector space and y R is an output in a 1-dimensional vector space, GPR regression can estimate the relationship between x and y. The conditional distribution of outcomes due to certain inputs is important for understanding the link between inputs and outputs in the regression technique. A joint Gaussian distribution covers a finite number of random variables in the Gaussian process. The Gaussian process f(x) can specify the mean and covariance functions:
Mean   function   m ( x ) :   m x : m x = E f x
Covariance function or kernel function K x , x :   K x , x = f x m x f x m x .

4. Data Processing and Analysis

4.1. Descriptive Statistics and Statistical Analysis

Previous research yielded 136 experimental findings for a single lap-shear test [80], all of which were factored into the development of a HENS using CML. It is abundantly clear that the elastic modulus of FRP multiplied by the thickness of the fibre (Ef tf, GPa-mm), which is also known as the axial stiffness, the width of the FRP (bf, mm), the concrete compressive strength (fc, MPa), the width of the groove (bg, mm), and the depth of the groove (hg, mm) were all utilised as input variables, while the ultimate capacity (P, KN) was the desired variable. Table 1 presents the descriptive statistics of the input and output parameters. From this table, one can see that the Ef tf parameter ranged from 12.90 to 78.20 with a skewness of 0.58, the bf parameter ranged from 60 to 6270, the bg and hg parameter ranged from 10 to 1405, and the fc parameter ranged from 48.20 to 4585.40. However, the output value p ranged from 4.76 to 25.49 with a skewness of 0.80. After the descriptive analysis that was described above revealed that the collected database had a wide range of experimental data, statistical analysis was carried out in order to measure the degree of correlation (DOC) between the aforementioned parameters. This was carried out in order to draw the appropriate conclusions. According to the information presented by the Pearson Correlation in Figure 3, the DOC between p and other parameters (with the exception of Ef, tf, and bf) was smaller when all of the parameters were examined. This is the conclusion reached by the information. On the other hand, it was shown that the DOC between Ef tf and bf was substantially higher.

4.2. Sensitivity Analysis

In general, sensitivity analysis (SA) is a technique that is used to determine how changes in input parameters affect the response of the proposed models. This will assist us in identifying the input parameters based on their influence on the result. The Cosine Amplitude Method [51] was used in this work to calculate the amount of influence of the inputs on the response, i.e., the IBS of FRP. The data pairings in this study were represented in a data array, X, as follows in Equation (7):
X = x 1 , x 2 , x 3 , , x i , , x n
and variable 𝑥𝑖 in 𝑋 is a length vector of 𝑚 as in Equation (8).
x i = x i 1 , x i 2 , x i 3 , , x i m
The correlation between the strength of the relation (𝑅𝑖𝑗) and datasets of 𝑥𝑖 and 𝑥𝑗 are provided by Equation (9).
R i j = k = 1 m x i k x j k k = 1 m x i k 2 k = 1 m x j k 2
The graphical representation of 𝑅𝑖𝑗 shows the relation between the IBS of FRP and the input parameters as shown in Figure 4. SA reveals that the Ef tf has the greatest influence on IBS with a strength value of 0.89 followed by bf and hg with strength values of 0.84 and 0.73 respectively. The parameters, bg and fc have strengths of about 0.67 and 0.69, respectively. It can be concluded that all the five parameters have higher influences on the interfacial bond strength and hence were considered in predicting the output.

4.3. Performance Parameters

To evaluate the effectiveness of the developed models, eight distinct performance indices (Equations (10)–(17) were calculated). These included the determination coefficient (R2), performance index (PI), variance account factor (VAF), Willmott’s index of agreement (WI), root mean square error (RMSE), mean absolute error (MAE), RMSE observation standard deviation ratio (RSR), and weighted mean absolute percentage error (WMAPE) [59,86,89,97,98,99,100,101,102,103,104,105,106,107,108,109,110,111,112,113,114,115,116,117,118,119]. The values of these indices should be identical to their ideal values, which are provided in Table 2. This will ensure that the prediction model is error-free. Take note that the ability of any predictive model to generalise is evaluated by determining various metrics, such as the degree of correlation, the associated error, the amount of variation, and so on, from these various aspects. This evaluation is carried out in order to determine the generalisation capacity of the model.
R 2 = i = 1 n ( y i y m e a n ) 2 i = 1 n ( y i y ^ i ) 2 i = 1 n ( y i y m e a n ) 2
P I = a d j . R 2 + 0.01 V A F R M S E
V A F   % = 1 v a r ( y i y ^ i ) v a r ( y i ) × 100
W I = 1   i = 1 n ( y i y ^ i ) 2 i = 1 n y ^ i y m e a n +   y i y m e a n   2
R M S E = 1 n i = 1 n ( y i y ^ i ) 2
M A E = 1 n i = 1 n y ^ i y i
R S R = R M S E 1 n i = 1 n ( y i y m e a n ) 2
W M A P E = i = 1 n y i y ^ i y i × y i i = 1 n y i

5. Results and Discussion

5.1. Simulation of Soft Computing Models

By analysing 136 tests, we hoped to be able to forecast FRP’s interfacial bond strength. The goal of this research was to determine how the five input parameters affect the IBS using the most efficient CML models. After that, the outputs of the created CML models were aggregated using the ANN and the HENS model was built. To train the models, 70% of the dataset (i.e., the training dataset of 110 instances) was used, while the remaining data (28 instances) were used for testing. The prediction success was evaluated using eight performance parameters. With these indices, we could assess how well our models worked by comparing the actual and anticipated values and measuring correlation coefficients, variances, and related errors. The created models and their outputs are presented in the following subsections for a more in-depth comparison. The flowchart of developed models has been shown in Figure 5.

5.1.1. ANN Model

It was determined that only five hidden layers were necessary, and the best model was found via trial and error. For example, Table 3 provides a breakdown of the model’s performance parameters. When ANN was being trained, it had an accuracy rate of over 91% (R2 = 0.9159), whereas when it was being tested, its accuracy rate increased to 92% (R2 = 0.9290). In terms of MAE (training = 0.0448 and testing = 0.0514) and RMSE (training = 0.0594 and testing = 0.0620), the best training results for the best feed-forward ANN structure were adopted with five inputs. For the training and testing datasets, the experimental and expected values of the ANN model are displayed in Figure 6 and Figure 7.

5.1.2. ELM Model

In contrast, in order to figure out the structure of the ELM, the number of hidden neurons, which can range anywhere from 2 to 30, was counted. In this particular research project, the sigmoid activation function was put to use in order to choose the most effective ELM model. The optimal number of hidden neurons was determined to be six, which was arrived at through a process of trial and error. The model performance is tabulated in the Table 3 and Table 4. It was observed that the ELM model attained the R2 value of 0.7881 in training, whereas it improved little to the value of 0.8647 in the testing phase (Table 3 and Table 4).

5.1.3. GMDH

The best-performing GMDH model was determined by a trial-and-error method with a maximum of five layers of neurons. The value of alpha was set to 0.6 to achieve the best result. When GMDH was being trained, it had an accuracy rate of over 91% (R2 = 0.9154), whereas when it was being tested, its accuracy rate increased to 93% (R2 = 0.9359). Table 3 and Table 4 provide a breakdown of the model’s performance parameters.

5.1.4. MARS Modelling

Initial parameters, such as the maximum number of BFs, GCV penalty per knot, maximum number of interactions, and so on, need to be tuned properly in MARS modelling in order to produce the best predictive model, as was explained in the methodology section (refer to Section 3.4). Table 5 contains the final values of the effective parameters, which may be found by following this process.
For the purpose of constructing the MARS model, which is used for forecasting the desired output, piecewise linear combinations of BFs were employed in this method. In order to arrive at an accurate calculation of the IFB of FRP, each of the five variables were first analysed under a variety of scenarios, and then the ‘states’ were formulated. In the beginning, the MARS will build a number of linear combinations (also known as linear BFs), and then, at the end, it will produce a model (MARS) to predict the desired output (y). The specifics of the BFs that make up the MARS model are provided in Table 5, and the equation that represents the final model may be seen below (17).
The expression that is presented in Equation (17) can be utilised as a ready-made solution for problems that require a more realistic approach. FRP’s IFB may be calculated with an accuracy of R2 (training = 0.8941, testing = 0.8816), RMSE (training = 0.0675, testing = 0.0722), and MAE (training = 0.0499, testing = 0.0541). Table 6 presents the other performance characteristics in order to facilitate a detailed evaluation of the model.
y = 0.31222   + 0.41602 * B F 1   0.61344 * B F 2   + 0.20701 * B F 3 0.25568 * B F 4   + 0.33178 * B F 5   0.50944 * B F 6 0.32458 * B F 7   0.39979 * B F 8   5.3741 * B F 9 + 4.692 * B F 10   0.9563 * B F 11   + 18.166 * B F  

5.1.5. LSSVM Model

The performance of LSSVM depends on two parameters i.e., Sigma and gamma. For the optimum modelling by trial and error, the values of those parameters were found as 60.38 and 6656.09, respectively. The elapsed time for the execution of the model was found to be 0.0016 s. The best performing LSSVM yielded an R2 of 0.9346 in training with a value of WMAPE of 0.1107, whereas for testing the values were 0.9226 and 0.1523 respectively.

5.1.6. GPR Model

Two critical parameters that can be found through an initial round of trial-and-error are S (width of rbf) and ε (gaussian noise), both of which are discussed in the technique section (refer to Section 3.6). S = 0.50 and ε = 0.01 can be used as design settings for GPR’s parameters. IBF values were predicted almost accurately by the GPR model during training, but a substantial variance was detected during testing. Figure 6 and Figure 7 show a scatter plot comparison of the actual and projected values for the training and testing datasets. Generalisation capability was demonstrated by the GPR model’s prediction accuracy (R2 = 0.9775; RMSE = 0.0306 in training, R2 = 0.8404; RMSE = 0.0944) in both stages. Table 3 and Table 4 provide further information on the various performance metrics.

5.1.7. HENS Modelling

The results of six separate CML models were reported earlier in the section. As indicated in Table 3, all of the generated models were able to accurately estimate the IFB of FRP. Given the huge size of the testing dataset, the comparatively strong R2 (ranging from 0.7811 to 0.9775) and low RMSE (ranging from 0.0306 to 0.0938) prediction values show this (110 instances). However, a close examination of the data shows that GPR was the best standalone model, whereas ELM was the poorest. Other performance indices, such the WMAPE and PI, support GPR’s prediction performance at all levels, in contrast to the R2 and RMSE values. Furthermore, it is important to remember that a model that performs well in testing and has a high level of accuracy is generally considered to be a robust model. As a result, improving their validation performance may make it possible to construct an even more robust model. As a result, the ensemble technique was used in this work without any additional ML models being included. Once these issues are resolved, this will be a more positive outcome for everyone. Without enough data, the computer models produced a wide range of outputs with variable degrees of accuracy. When multiple models are combined, there is a lower chance of selecting the erroneous one. In this study, a HENS model was utilised to combine the six CML models used to forecast the IFB of FRP in an attempt to apply ensemble modelling. The standard feed-forward ANN was used to build the suggested HENS model, which aggregates the outputs of all six CML models as inputs and outputs the actual IFB value, as mentioned in the methodology section (refer to Section 3). Figure 5 depicts the HENS model’s implementation approach in the form of a flowchart, which makes it easy to see how amalgamation works. Table 3, Table 4, Table 5 and Table 6 show the HENS model’s ability to accurately anticipate outcomes. When compared with the solo CML models that had been created, the ensemble hybrid model yielded the best predictions. Table 3’s CML models were compared, and the HENS model achieved substantial results in all phases, R2 (training = 0.9783, testing = 0.9287), VAF (training = 97.83, testing = 92.87), RMSE (training = 0.0300, testing = 0.0613), and MAE (training = 0.0212, testing = 0.0443)) when compared. The predictability of the constructed model, which includes HENSM, was assessed using R2, VAF, RMSE, MAE, and other performance criteria. Staggered plots show how projected and actual values compare for training and testing datasets, respectively, in Figure 6 and Figure 7. The suggested HENS model is thoroughly evaluated in the following sections to ensure its robustness and generalisability.

5.2. Taylor Diagram

As shown in Figure 8 and Figure 9, the Taylor diagram was utilised to analyse the performance of the hybrid support vector machine models for testing and training datasets respectively. This diagram establishes whether or not the model is able to accurately forecast the intended result. In order to obtain a relative measure of how well the three models compare to one another, we looked at three distinct statistical criteria (RMSE, correlation coefficients, and standard deviation ratios). As the reference point, we use the centred RMSE, which is defined as the distance from the measured point. In the reference model, both the standard deviation and the correlation coefficient were both configured to have a value of 1. It is clear from looking at the graph that the values of the standard deviation and correlation coefficient for all seven models during the training phase were quite near to 1. It is possible to draw the conclusion from the graph that the ELM model had the lowest correlation in training, whereas the GPR and HENS model delivered the best performance during the training phase. Out of all five models, the HENS model had the best performance for the testing dataset. As a result, it is possible to draw the conclusion that the HENS model has the best overall performance because it produced satisfactory results for both datasets.

5.3. Accuracy Matrix

To better demonstrate the values of performance indices, a recently proposed heat map-shaped graphical assessment, called accuracy matrix, was tested to visualise the model efficiency [120]. This matrix displays multiple statistical parameters to measure the model’s predictive performance for the training and testing datasets. Figure 10 displays the accuracy matrix for the performance indices determined in this study. It indicates the accuracy of the performance parameters (in percentage) by comparing them with their corresponding ideal values. For example, the ideal value of MAE is 0 and, in the present work, the value of MAE for the training subset was determined to be 0.0448 for the ANN model (see Table 3. Thus, it can be estimated that the ANN model attained 96% ((1 − 0.0448) × 100%) accuracy in terms of MAE. On the other hand, the values of R2 and PI were obtained as 0.9421 and 1.7957 in the testing phase, respectively, for HENS (see Table 4), which shows that HENS attained 94% ((0.9421/1) × 100%) and 90% ((1.7957/2) × 100%) accuracy in terms of R2 and PI, respectively. A similar procedure was followed for the other parameters as well. However, it may be noted that the parameters such as VAF, which are determined in percentage terms, should be converted in their decimal form before implementing the abovementioned procedure.

6. Conclusions

It is important to note that an accurate and trustworthy estimate of the concrete IFB of FRP laminates can aid with cost/performance optimisation while also saving time. The estimation of IFB of FRPL was reported in the current work. In this work, six independent machine learning models—ANN, ELM, GMDH, MARS, LSSVM, GPR, and a HENS model—were introduced. A trustworthy experimental database made up of 136 FRPs was employed for this purpose. To train and validate the used models, the obtained dataset was split into training and testing subsets. Several statistical techniques were used to compare and analyse the accuracy of all models. Through the study, the following conclusions were drawn:
  • A conventional model, GPR provided the best result in training (R2 = 0.9775, VAF = 97.74, RMSE = 0.0306, and RSR = 0.15) whereas the GMDH model provided the best result in testing (R2 = 0.9359, VAF = 92.08, RMSE = 0.0655, and RSR = 0.2953).
  • It was observed from the experimental data that the suggested HENS model achieved the maximum prediction accuracy by minimising the particular flaws of CML models. Additionally, it is clear that the current HENS model (R2 = 0.9663, VAF = 96.60, RMSE = 0.0383, and RSR = 0.1847) was the best-performing model among the other models, according to Table 6, was able to handle the overfitting problem of the GPR model and exhibited all the desired trends in the parametric study of FRP, confirming the superiority of the suggested method at all levels.
  • The HENS model had high potential to forecast the intended IFB of FRPL bonded to concrete, as shown by the parametric analysis, and was extremely easy to implement. It also has a very cheap computational cost (only 10 s), is representational, and performed better than the standalone models.
In conclusion, this study successfully used an ensemble ML model to predict the IFB of FRPL bonded to concrete. It seems to be a precise and yet computationally effective technique. However, a thorough analysis of the outcomes suggests that the suggested strategy could be further enhanced in the future, possibly including a thorough evaluation of the HENS model approach for complicated issues in many technical and scientific domains. As far as the authors are aware, this study is the first to apply a hybrid ensemble of CML models to forecast IFB or FRPL bonded to concrete.

Author Contributions

Conceptualization, A.A.A., R.B., M.I. and J.G.; methodology, A.H.B., Q.A.A., J.G., R.B., K.K. and M.I.; software, K.K., M.N.A. and M.I.; validation, Q.A.A., M.I. and M.N.A.; formal analysis, J.G. and M.I.; investigation, M.I., R.B. and K.K.; resources, A.A.A. and K.K.; data curation, M.I.; writing—original draft preparation, R.B. and M.I.; writing—review and editing, M.I. and R.B.; visualization, R.B., J.G. and M.I.; supervision, A.A.A. and K.K.; project administration, M.N.A. and K.K.; funding acquisition, K.K. and M.N.A. All authors have read and agreed to the published version of the manuscript.

Funding

This work was supported by the Deanship of Scientific Research, Vice Presidency for Graduate Studies and Scientific Research, King Faisal University, Saudi Arabia (Project No. GRANT409).

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

The data used in this research have been properly cited and reported in the main text.

Acknowledgments

The authors acknowledge the Deanship of Scientific Research, Vice Presidency for Graduate Studies and Scientific Research, King Faisal University, Saudi Arabia (Project No. GRANT409).

Conflicts of Interest

The authors declare no conflict of interest.

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Figure 1. Single-lap shear test: (a) FRP externally bonded on concrete; (b) FRP externally bonded on the grooves of concrete (reprinted/adapted with permission from Su et al. [80]).
Figure 1. Single-lap shear test: (a) FRP externally bonded on concrete; (b) FRP externally bonded on the grooves of concrete (reprinted/adapted with permission from Su et al. [80]).
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Figure 2. Example of a MARS model [62].
Figure 2. Example of a MARS model [62].
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Figure 3. Pearson correlation with heat map.
Figure 3. Pearson correlation with heat map.
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Figure 4. Sensitivity analysis of input parameters to output parameters.
Figure 4. Sensitivity analysis of input parameters to output parameters.
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Figure 5. Flowchart of the implementation approach of the HENS Model.
Figure 5. Flowchart of the implementation approach of the HENS Model.
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Figure 6. Tested vs. predicted graph of training data.
Figure 6. Tested vs. predicted graph of training data.
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Figure 7. Tested vs. predicted graph of testing data.
Figure 7. Tested vs. predicted graph of testing data.
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Figure 8. Taylor diagram of the training data.
Figure 8. Taylor diagram of the training data.
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Figure 9. Taylor diagram of the testing data.
Figure 9. Taylor diagram of the testing data.
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Figure 10. Accuracy matrix for (a) training, (b) testing, and (c) total datasets.
Figure 10. Accuracy matrix for (a) training, (b) testing, and (c) total datasets.
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Table 1. Descriptive statistics of the collected dataset [80].
Table 1. Descriptive statistics of the collected dataset [80].
Descriptive
Statistic
Input VariablesTarget
Variable
Elastic Modulus of FRP x Thickness of FRP, Ef tfWidth of FRP, bfConcrete
Compressive Strength, fc
Width of Groove, bgDepth of Groove, hgUltimate
Capacity, p
UnitGPa-mmmmMPammmmKN
Mean40.3346.1033.727.9410.3312.05
Standard Error2.181.010.730.210.300.37
Median39.1050.0032.7010.0010.0011.11
Mode78.2060.0026.7010.0010.009.87
Standard Deviation25.4111.818.492.473.454.32
Sample Variance645.42139.5272.156.1011.9318.65
Kurtosis−1.23−1.49−1.11−1.90−0.880.30
Skewness0.58−0.130.49−0.36−0.090.80
Range65.3030.0025.505.0010.0020.73
Minimum12.9030.0022.705.005.004.76
Maximum78.2060.0048.2010.0015.0025.49
Sum5484.806270.004585.401080.001405.001638.72
Count136.00136.00136.00136.00136.00136.00
Confidence Level (95.0%)4.312.001.440.420.590.73
Table 2. Ideal values of different performance parameters.
Table 2. Ideal values of different performance parameters.
IndicesR2PIVAFWIRMSEMAERSRWMAPE
Ideal Value1210010000
where y and y ^ are the actual and estimated output; n is the total number of observations; and y m e a n is the average of the actual values.
Table 3. Performance indices for the training dataset.
Table 3. Performance indices for the training dataset.
IndicesANNELMGMDHMARSLSSVMGPRHENS
R20.91590.78810.91540.94960.93460.97750.9783
PI1.76741.47221.76681.85091.81391.92331.9256
VAF91.499778.813491.494794.958393.455697.749397.8314
WI0.97670.93760.97680.98690.98270.99430.9945
RMSE0.05940.09380.05950.04580.05210.03060.0300
MAE0.04480.07350.04310.03570.03910.02140.0212
RSR0.29160.46030.29170.22450.25580.15000.1474
WMAPE0.12540.20760.12170.10040.11070.06040.0601
Table 4. Performance indices for the testing dataset.
Table 4. Performance indices for the testing dataset.
IndicesANNELMGMDHMARSLSSVMGPRHENS
R20.92900.86470.93590.91210.92260.84040.9421
PI1.77211.61481.77591.73551.75661.54891.7957
VAF92.197586.465392.081691.082191.786683.703092.8774
WI0.97760.96200.97400.97690.97530.95600.9775
RMSE0.06200.08230.06550.06650.06550.09040.0613
MAE0.05140.07160.05190.04820.05260.07570.0443
RSR0.27940.37080.29530.29960.29500.40760.2764
WMAPE0.14890.20750.15050.13950.15230.21920.1284
Table 5. Basis function of the MARS model.
Table 5. Basis function of the MARS model.
Basis FunctionModels
BF1max (0, Ef tf − 0.18989)
BF2max (0, 0.18989 − Ef tf)
BF3max (0, bf − 0.66667)
BF4max (0, 0.66667 − bf)
BF5BF1 ×max (0, bf − 0.33333)
BF6BF1 × max (0, 0.33333 − bf)
BF7BF3 × max (0, fc − 0.39216)
BF8BF1 × max (0, fc − 0.54118)
BF9BF1 × max (0, 0.54118 − fc)
BF10BF1 × max (0, 0.59608 − fc)
BF11BF3 × max (0, Ef tf − 0.40123)
BF12max (0, fc − 0.98824) × max (0, Ef tf + 0)
Table 6. Performance indices for the total dataset.
Table 6. Performance indices for the total dataset.
IndicesANNELMGMDHMARSLSSVMGPRHENS
R20.91840.80520.91670.94080.93030.94520.9663
PI1.77191.51121.76771.82861.80251.83951.8927
VAF91.659480.515391.498694.069292.989994.505796.6002
WI0.97690.94350.97630.98460.98110.98590.9911
RMSE0.05990.09170.06070.05060.05500.04870.0383
MAE0.04610.07310.04480.03820.04180.03210.0258
RSR0.28880.44150.29240.24360.26520.23470.1847
WMAPE0.13000.20760.12730.10800.11880.09140.0734
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Alabdullh, A.A.; Biswas, R.; Gudainiyan, J.; Khan, K.; Bujbarah, A.H.; Alabdulwahab, Q.A.; Amin, M.N.; Iqbal, M. Hybrid Ensemble Model for Predicting the Strength of FRP Laminates Bonded to the Concrete. Polymers 2022, 14, 3505. https://doi.org/10.3390/polym14173505

AMA Style

Alabdullh AA, Biswas R, Gudainiyan J, Khan K, Bujbarah AH, Alabdulwahab QA, Amin MN, Iqbal M. Hybrid Ensemble Model for Predicting the Strength of FRP Laminates Bonded to the Concrete. Polymers. 2022; 14(17):3505. https://doi.org/10.3390/polym14173505

Chicago/Turabian Style

Alabdullh, Anas Abdulalem, Rahul Biswas, Jitendra Gudainiyan, Kaffayatullah Khan, Abdullah Hussain Bujbarah, Qasem Ahmed Alabdulwahab, Muhammad Nasir Amin, and Mudassir Iqbal. 2022. "Hybrid Ensemble Model for Predicting the Strength of FRP Laminates Bonded to the Concrete" Polymers 14, no. 17: 3505. https://doi.org/10.3390/polym14173505

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