Artificial Intelligence Method for Predicting Mechanical Properties of Sand/Glass Reinforced Polymer: a New Model

Document Type : Research Paper

Authors

1 Department of Mechanical Engineering, Kermanshah University of Technology, Kermanshah, 67156-85420, Iran

2 Department of Computer Engineering, Kermanshah University of Technology, Kermanshah, 67156-85420, Iran

Abstract

In this paper, the aim is to propose a new model to obtain the mechanical properties of sand/glass polymeric concrete including modulus of elasticity and the ultimate tensile stress. The neural network soft computation, support vector machine (SVM), and active learning method (ALM) that is a fuzzy regression model are all used to construct a simple and reliable model based on experimental datasets. The experimental data are obtained via the tensile and bending tests of sand/glass reinforced polymer with different weight percentages of sand and chopped glass fibers. The extracted results are then used for training and testing of the neural network models. Two different types of neural networks including feed-forward neural network (FFNN) and radial basis neural network (RBNN) are employed for connecting the properties of the sand/glass reinforced polymer to the properties of the resin and weight percentages of sand and glass fibers. Besides the neural network models, the SVM and ALM models are applied to the problem. The models are compared with each other with respect to the statistical indices for both train and test datasets. Finally, to obtain the properties of the sand/glass reinforced polymer, the most accurate model is presented as an FFNN model.

Keywords


Artificial Intelligence Method for Predicting Mechanical Properties of Sand/Glass Reinforced Polymer: a New Model

  1. Heshmatia, S. Hayati a*, S. Javanmiria, M. Javadianb

a Department of Mechanical Engineering, Kermanshah University of Technology, Kermanshah, 67156-85420, Iran

b Department of Computer Engineering, Kermanshah University of Technology, Kermanshah, 67156-85420, Iran

 

 

KEYWORDS

 

ABSTRACT

Reinforced polymer

Mechanical properties

A new model

Active learning method

Neural networks

In this paper, the aim is to propose a new model to obtain the mechanical properties of sand/glass polymeric concrete including modulus of elasticity and the ultimate tensile stress. The neural network soft computation, support vector machine (SVM), and active learning method (ALM) that is a fuzzy regression model are all used to construct a simple and reliable model based on experimental datasets. The experimental data are obtained via the tensile and bending tests of sand/glass reinforced polymer with different weight percentages of sand and chopped glass fibers. The extracted results are then used for training and testing of the neural network models. Two different types of neural networks including feed-forward neural network (FFNN) and radial basis neural network (RBNN) are employed for connecting the properties of the sand/glass reinforced polymer to the properties of the resin and weight percentages of sand and glass fibers. Besides the neural network models, the SVM and ALM models are applied to the problem. The models are compared with each other with respect to the statistical indices for both train and test datasets. Finally, to obtain the properties of the sand/glass reinforced polymer, the most accurate model is presented as an FFNN model.



1. Introduction

In the last decades, polymeric concrete (PC) has been widely used for new constructions and repairing old constructions due to its good properties, such as rapid setting, high strength, corrosion, and water resistance. Polymer concrete (PC) is fabricated generally by combining the polymers and the fillers. The resin, (e.g. epoxy or polyester) plays the role of a binder instead of cement binders in plain concretes [1]. The unsaturated isophthalic and orthophthalic polyesters can be used as a binder in PC at special conditions such as harsh environments like acid or alkaline media or water [2]. Moreover, epoxy resins are widely used for the manufacturing of polymer concretes due to their suitable mechanical properties and especially their high binding resistance.

Because of the adhesion of the polymeric concrete, repairing both polymer and conventional cement-based concretes are possible. Polymer concrete is an ideal material for underground constructions because of its neutral chemical structure and water impermeability. Conducted studies about mechanical behaviors of such materials under chemical attack situations certify their performance in such situations [3, 4]. While cement-bound mortars cannot resist to chlorine-based acids and the effects of sulfate, polymer-based mortars show resistance both as repair mortar or coating. Polymer concrete also shows good resistance to water and has a high hydraulic capacity thanks to its smoothness [5]. Their adhesion property is the most important property of these materials as they are widely used to reinforce concrete structures [6-12].

Several research works have been conducted for determining the material characteristics of different types of polymer concrete [13-16]. Abdel-Fattah and El-Hawary [17] conducted experiments to study the flexural behavior of polymer concrete (PC) made with epoxy resin and polyester with varying percentages. The results show that the modulus of rupture and ultimate compressive strain for PC were much higher. Thus, the ductility was improved in comparison with the ordinary Portland cement concrete. Komendant et al. [18] investigated the effect of testing temperature on the compressive strength as well as the influence of thermal cycling between 23 and 71 0C on the strength and elastic properties of concrete. They observed that the compressive strength of the concrete is reduced by 3–11% at 43 0C and 11–21% at 71 0C. However, only a few articles have been published in the literature which consider the effect of environment conditions on the PC properties. In some other works [19-22] a numerical analysis approach was used to investigate the mechanical properties of concrete.

Since the PC exhibits brittle failure behavior, improving its post-peak stress-strain behavior is an important aspect for the application of PC. Hence, developing better PC systems and also characterizing the fracture properties and flexural strength in terms of constituents are essential for the efficient use of PC [23, 24]. Chopped strand glass fiber has been applied to polymer composites for improving the strength and controlling the cracking [25, 26]. Thus, before being used in practical and industrial applications, the study of their mechanical properties is necessary. To characterize the failure behavior of the polymer composites with respect to the constituents, some attempts have been made for efficient use [27] or optimizing the mechanical properties [28, 29].

However, since these materials are newly developed, the study of their mechanical properties is much necessary before using them in practical and industrial applications. Analytical methods such as numerical homogenization are used to determine composite material properties [30]. The microstructure interpolation method is also applied for multiple length scale structural optimization [31]. In addition, Akbari et al [32] applied a multi-scale method based on the homogenization technique to investigate the influence of microscopic parameters on the macroscopic behavior of polycrystalline materials under different loading configurations.

Since there is still no mathematical model to obtain the mechanical properties of PCs in general, most of the research work on the mechanical properties are limited to experimental studies [33-41]. Thus, the only way for estimation of the mechanical properties of a PC is through a time consuming and expensive experimental process.

Therefore, in this study, the artificial intelligence (AI) soft computation modeling based on experimental data is chosen to construct a simple and reliable model for the estimation of mechanical properties of the PCs. As an example, Shabani and Mazaheri used the artificial neural network models in numerical modeling of nano-sized ceramic particulates reinforced metal matrix composites [42]. They studied the accuracy of various artificial neural network training algorithms in FEM modeling of Al2O3 nanoparticles reinforced A356 matrix composites. A hybrid artificial intelligence-based model is also used to study the bond strength of CFRP-lightweight concrete composites [43].

The tensile and bending test specimens of sand/glass reinforced polymer concrete with different weight percentages of sand/glass are fabricated. Modulus of elasticity and the ultimate tensile stress are obtained via the tensile and bending tests. The extracted results are then used for training and testing of the neural network models. Different types of neural networks including feed-forward neural network (FFNN), radial basis neural network (RBNN) beside the support vector machine (SVM), and active learning method (ALM) are employed for connecting the properties of the sand/glass reinforced PC to the properties of the resin and weight percentages of sand and chopped glass. All the models are fitted to the problem properly with acceptable accuracy. Finally, a model is presented as a simple formula based on the FFNN structure to obtain the mechanical properties of the sand/glass reinforced PC.

Instead of using expensive experimental studies for the estimation of sand/glass reinforced polymers properties, the presented model can easily be used via any programming software. The presented scheme can also be used for the study of any other complicated material.

2. Methodology

In this section, the utilized methods for obtaining the experimental results and constructing the artificial intelligence (AI) models are discussed. At first, each value of modulus of elasticity for the composite (Ec) or ultimate stress for the composite (σuc) is experimentally obtained with respect to three parameters including the modulus of elasticity for the resin (Er) or ultimate stress for the resin (σur), the weight percentage of sand (%sand), and weight percentage of chopped glass fiber (%glass) in the composite structure. In order to obtain stiffness and ultimate compressive strength of the composite, Ec or σuc for each certain value of Er or σur, %sand, and %glass, ten specimens with similar configurations are made for tensile and bending tests. Therefore, every result is derived as an average result of 5 tensile tests and 5 bending tests. The results for Ec and σuc are obtained for 240 different configurations (as tabulated in Tables A-1, 2, 3, and 4), which means there are over 2400 tests performed to obtain the presented results.

In the next step, the obtained results are used to construct the neural network models. Two separate networks are founded in every section, one for estimation of Ec with respect to Er, wt% of sand, and wt% of glass fiber, and another for estimation of σuc with respect to σur, wt% of sand, and wt% of glass fiber. The modulus of elasticity for both resin and composite (Er and Ec) are in GPa and the ultimate tensile stresses for both resin and composite (σur and σuc) are in MPa. The datasets are divided into two categories consisting of train and test datasets. For the below explained structures of the utilized neural networks, the components of the networks, including weight and bias terms, are acquired via an optimization process to fit the training dataset results in the training procedure. After the training procedure, the network should be tested over the test datasets. The testing observation datasets are not used in training and preserved for testing the generality of the neural network model. The same procedure of training and testing is performed for the ALM model as well. The generality of a method means that the method should give proper results for any other data other than the training data. In this study, 80% of the results are taken as the training datasets (192 observations) and the rest are left for testing of the networks (48 observations). A flow chart of the computational procedure is shown in Fig. 1.

 

 

Fig. 1. A flow chart for prediction of mechanical properties of polymer concrete

Fig. 2. The fabricated metallic mould

 (a)

 

(b)

Fig. 3. Dimensions of the (a) tensile and (b) bending samples

2.1. Experimental Setup

Different types of resins including EPON 828, EPON 862, Epoxy L135i, LY564, and PVA are used to fabricate the test specimens. Sand particles and chopped glass fibers are also used for reinforcement of test specimens. The sand is sieved by two different sieves so all the grains of sand are about 2-4 mm in diameter and also all strands of chopped glass fiber are about 6mm in length.

The preparation of specimens is the most important stage of any testing method. The American Society for Testing and Materials (ASTM) has a tensile test standard designed to determine the tensile properties of unreinforced and reinforced plastics in the form of standard dumbbell (dog-bone) shaped test specimens. The tensile test specimen has the basic shape of a tensile dog bone according to ASTM D 638 (Type I). The dimensions of the specimen are 168mm in length, 13mm in width, and 5mm in thickness (Figs. 2-3).

After preparing the materials, the mould should be prepared, so the process of preparing the mould is as follow:

 

Fig. 4. Removal of specimens from the stainless steel mould

  • Assembling the mould and making sure that both upper and lower parts are well attached.
  • Using a suitable lubricant (machine oil, grease, or any commercially available mould release agent) to avoid the sticking of samples on the mould.
  • Setting the fabricated mould on the flat surface so that the mould does not move during casting the epoxy mixture.
  • Adding sand and chopped glass fiber into the cavities of the mould if necessary.

The next step is preparing the matrix, as mentioned; the matrix is a mixture of resin epoxy, and hardener, so at the beginning, these two materials are mixed well and stirred for more than 5min then the mixture is sonicated in the ultrasonic bath for more than 15min. this process helps the removal of almost all of the bubbles from the matrix so a uniform mixture will be achieved. When a uniform mixture of the resin and hardener is provided, the epoxy mixture must be poured into the cavities on the stainless steel mould. Then the mould should be placed in the oven to cure the samples for 5h at 55℃. Finally, the specimens are ready to be removed from the stainless steel mould, but there might be some unwanted extensions on the contour of the specimens that need to be removed before testing (Fig.4).

When it comes to the testing set up and execution, according to conducted tensile and bending tests, two methods, one for tensile tests and the other one for bending tests, are necessary to follow. Figs. 5 and 6 illustrate the experimental setup for both tensile and bending tests.

For the tensile tests, dog-bone specimens are placed in the top and bottom grips and tightened while one visually observes alignment of the long axis of the specimen with the direction of the pull and for bending tests, the specimen is placed on the two lower edges and the third edge on the top moves down until the specimen is broken. Tensile and bending test specimens are fabricated with different sand and chopped glass fiber weight fractions: 0% to 55% with increments of 5% for sand, and 0% to 15% with increments of 5% for chopped glass fiber. Both tensile and bending tests are performed at room temperature under a crosshead speed of 5mm/min. In addition, it is necessary to be mentioned that for each weight percentage, five tensile and one bending test samples are prepared to achieve more reliable results.

As seen in Appendix A, the specimens with 55% sand have a higher stiffness than other samples. According to this appendix, the ultimate tensile strength for the sample that contains 20% of sand is 5.1637MPa. By increasing the weight percentage of sand, the ultimate tensile strength increases significantly and for specimens containing 40% and 55%, the ultimate tensile strength is 5.6995MPa and 7.1863MPa, respectively. However, for samples that contain 20% and 40% of sand, the Young’s modulus doesn’t change widely but for 55% sand specimen, young’s modulus is about 2.5 times higher than 20% and 40% sand specimens.

To study the effect of chopped glass fiber on the ultimate tensile strength of polymers and also to find out about the influence of increasing the amount of chopped glass fiber on the ultimate tensile strength of specimens, two different amounts of chopped glass fiber are mixed with pure polymer. Tables A-1 to A-4 also include information about the samples having specific amount of chopped glass fiber. As illustrated, by adding 5% extra chopped glass fiber to the polymer, its ultimate tensile strength increases about 30% and as expected in comparison with sand contained specimens, the chopped glass fiber samples have a higher ultimate tensile strength.

The simultaneous influence of adding chopped glass fiber and sand particles is also investigated. Two different percentages are presented in the table; the first specimen contains 40% sand and the second one contains a mixture of 40% sand and 5% chopped glass fiber. According to the presented results in Appendix A, adding 5% of chopped glass fiber can increase the ultimate tensile strength up to 60%. Also, the amount of young’s modulus increases from 1.82GPa to 3.50GPa by adding 5% glass fiber into specimens.

2.2. Feed-Forward Neural Network (FFNN)

Feed-forward neural networks (FFNN) are the most primary neural networks. The FFNNs are successfully utilized to model nonlinear problems or estimate complicated functions. The FFNN is usually used as a simple numerical instrument to estimate the results of complicated phenomena after being trained. The structure may have multiple hidden layers but usually, it consists of one hidden layer and one output layer. Multiple layers may lead to extra complication of the network that causes problems in the training procedure and convergence. The structure of an FFNN with one hidden layer is depicted in the Fig. 5. Note that the shown inputs and output of the system belong to the estimation of the mechanical properties of the sand/glass polymer composite.

The input data should be pre-processed before it is entered into the hidden layer. The pre-processing is a linear transform that maps the minimum and maximum of input data ([xmin, xmax]) into the domain between -1 and 1 ([-1, 1]). In the hidden layer, the mapped input data is multiplied by a weight matrix (Wh) and added to a bias vector (bh). This summation is then applied by a tangent sigmoid (tansig) transfer function. Note that the weight matrix of Wh in the hidden layer is a Nn×Ni matrix of real numbers where Nn is called the number of neurons in the hidden layer and Ni is the dimension of the input vector or the number of input parameters that is equal to 3 for this problem. As mentioned above, the three input parameters of the network are Er or σur, %sand, and %glass. The bias vector of bh in the hidden layer is also an Nn×1 vector of real numbers. The number of neurons is an important factor in a neural network that significantly affects both the accuracy and complexity of that network and it will be discussed later.

In the output layer, a similar process is applied to the output of the hidden layer. The data is multiplied by a weight matrix (Wo) and then added to a bias vector (bo). The transfer function of the output layer is a pure linear (purelin) function that gives the same value of its input as its output. The weight matrix of Wo in the output layer is a No×Nn matrix of real numbers and the bias vector of bo in the output layer is a No×1 vector of real numbers where No is the number of outputs. This problem has one output (Ec or σuc), so No=1. Since the output of the output layer is within the domain of [-1, 1], in order to obtain the real output values a post-process is applied to its outputs. Similar to the pre-process, the post-process is a linear transform but it maps the data from [-1, 1] into the domain between minimum output value and maximum output value ([ymin, ymax]).

After the construction of the neural network structure, the network must be trained. The training process is generally an optimization process for tuning the network parameters including Wh, bh, Wo, and bo.

 

 

Fig. 5. The structure of a single layer FFNN model proposed for estimation of mechanical properties of sand/glass polymer composites

 

Fig. 6. The structure of an RBNN model proposed for estimation of mechanical properties of sand/glass polymer composites

During the training optimization process, the goal is to find a set of network components which minimizes the mean square error (MSE) between the network results and the real results of the training datasets. The MSE value is strictly relevant to the root mean square (RMSE). Training is done with semi-analytical backpropagation approaches such as Levenberg-Marquardt (LM) and Bayesian regularization (BR) or numerical approaches such as genetic algorithm (GA) and particle swarm optimization (PSO).

2.3. Radial Basis Neural Network (RBNN)

The structure of a radial basis neural network (RBNN) is shown in Fig. 6 which looks so similar to a single layer FFNN. The first difference is in the type of the hidden layer transfer function that is a radial basis function. In addition, in the hidden layer, an element by element multiplication operator (.*) is applied to the output of the weight matrix and the bias vector. Moreover, in the structure of RBNNs the pre-process and post-process functions return their input values.

The RBNNs take a lot of neurons, but they are easily designed and trained. RBNN gives excellent results when a lot of training data are available. The training of an RBNN is processed by adding neurons. In an exact RBNN, the number of neurons is equal to the number of input data vectors.

2.4. Support Vector Machine (SVM)

Support vector machine (SVM) is an artificial intelligence method that is widely used for classification and regression problems and it is also known as support vector regression (SVR) method. In this method, an approximate function (f(x)) is trained to fit the training dataset using a minimization method.

 

Fig. 7. The structure of an SVM model proposed for estimation of mechanical properties of sand/glass polymer composites

 The structure of the constructed support vector machine in this study is illustrated in Fig. 7 which takes the resin properties (Er or σur) and weight percentages of sand and glass as inputs and gives the mechanical properties of the sand/glass polymer resin composites (Ec or σuc) as the output. In Fig. 7, the parameters  and  are the Lagrangian multipliers, N is the number of observations and K(xi, x) is the kernel function.

2.5. Active Learning Method (ALM (

ALM is a fuzzy regression algorithm, which works well in uncertain environments [44]. The basic idea of this algorithm is breaking a Multiple Input-Multiple Output (MIMO) system into several simpler Single Input-Single Output (SISO) subsystems as shown in Fig. 8.(a). Afterward, the algorithm combines these subsystems by a fuzzy inference engine in order to achieve the overall behavior of the system. Fig. 8.(b) shows a SISO subsystem of the ALM algorithm called Ink-Drop-Spread (IDS), where two valuable information (Narrow-Path and Spread)are extracted from it. Narrow-Path (NP) and Spread (SP) extracted from each SISO subsystem are then combined by a fuzzy inference unit. Equation (1) shows how these pieces of information are combined. Parameter  is the NP of each SISO subsystem and is the confidence degree of the NP and can be computed by Eq.(2). The ALM algorithm also considers the uncertainty for each data point by using a fuzzy membership function called an ink, as shown in fig. 8.(c). Fig. 8.(d) shows the ink drop spread of 7 data points in an IDS unit. It also shows NP and SP resulted from the IDS unit.

 

Fig. 8. (a) ALM algorithm breaks a multi-input-single-output function into simpler single-input-single output subsystems and combines the results by a fuzzy inference engine. (b) Each single-input-single-output subsystem consists of a plan called an IDS plan and a feature extractor unit which extract two useful pieces of information, Narrow Path (NP) and Spread (SP). (c) The Gaussian membership function which is called an ink. This membership function is considered for each data point in every IDS plans. (d) The inks of 7 data points are spread in an IDS plan which forms a pattern. The NP and SP are extracted from the IDS plan.

 

(1)

where

 

(2)

where is the Spread inverse and  is the membership degree of the data point to each SISO subsystem.

The Narrow path could be obtained by the weighted-average method, as in equation (3).

 

(3)

where d(xi, y) is the darkness value of coordinate (xi, y). The Spread can be computed by equation (4).

 

(4)

where Th is the threshold of the IDS plane which is set by the user (usually Th=0 for modeling purpose).

Until now, numerous successful applications of ALM have been reported in function approximation[45, 46], classification [47-49], clustering [50, 51] and control [45, 52-54]. However, in [55] they show that ALM shows its best advantage when a high level of uncertainty existed in the system.

 

 

 

3. Model Construction and Evaluation

In this section, the neural network models are constructed and evaluated. The models including FFNN, RBNN, SVM, and ALM are trained and tested separately for estimation of Ec and σuc. The models are compared with each other in respect to regression plots and statistical indices such as R2, RMSE, and VAF that are introduced below.

3.1. FFNN Results

The FFNN model is founded and trained twice, once for estimation of Ec in respect to Er, %sand, and %glass and once for estimation of σuc in respect to σur, %sand, and %glass. The models are trained and tested, using 192 datasets for training and 48 datasets for testing, as follows.

3.1.1. FFNN Model for Estimation of Ec

To estimate the modulus of elasticity of the sand/glass polymer composite (Ec), the FFNN model with 8 neurons in the hidden layer (Nn=8) is founded. The number of neurons is attained through a try and error procedure for finding the most exact network with the simplest structure. Hence, different numbers of neurons are applied to the network several times and the convergence of the networks is investigated noting the training and testing datasets. Finally, a single layer FFNN with 8 neurons in the hidden layer was revealed to be the most convergent network. This model also satisfies the simplicity factor with an 8×3 matrix of Wh, an 8×1 vector of bh, a 1×8 matrix of Wo, and a 1×1 vector of bo that generally means 26 components.

The Bayesian-regularization (BR) algorithm is used for training the network which is a fast and exact algorithm. The BR method is essentially a gradient-based method that chooses the first set of network components vector by random. Therefore, every time the BR method solves the problem, it gives different results for the network components. In order to achieve the best possible structure, the training process with the BR method is performed multiple times.

The statistical convergence indices of the finally achieved FFNN for training and testing datasets are shown in Table 1. The regression plots in Fig. 11 show the convergence between the experimental values of Ec and the FFNN results. Noting Fig. 11, the FFNN model gives proper results for both train and test datasets. Therefore, the constructed FFNN model seems to be an exact and general model for the problem. Further model evaluation is presented in the following sections.

 

3.1.2. FFNN Model for Estimation of σuc

To estimate the ultimate tensile stress of the sand/glass polymer composite (σuc), a similar FFNN with 11 neurons in the hidden layer is founded and trained. The statistical indices for comparison of the experimental results with the network results are given in Table 2. The same try and error procedure is applied for training the FFNN with the BR method. The indices show a proper accuracy for the network while the accuracy has a fall in comparison to the previous network.

3.2. RBNN Results

Similar to the previous section, the RBNN structure is constructed and trained once for estimation of the Ec with respect to Er, %sand, and %glass and once for estimation of σuc in respect to σur, %sand, and %glass. The training and testing results are primarily investigated with respect to the mentioned statistical indices.

3.2.1. RBNN Model for Estimation of Ec

For estimation of the modulus of elasticity of the composite, an RBNN with 56 neurons in the hidden layer is created. In order to reach the best accuracy, the spread value of the radial basis layer is taken equal to 10 and the goal mean squared error is taken equal to 0.01. These values for spread and goal are obtained through a try and error process.

The resulted indices for the RBNN results in comparison to the experimentally achieved composite modulus of elasticity are depicted in Table 1. The results show an excellent convergence and generality for the RBNN model.

3.2.2. RBNN Model for Estimation of σuc

A similar RBNN structure for estimation of the ultimate tensile stress of the composite is constructed with 111 neurons in the hidden layer. In order to reach the best accuracy, the spread value of the radial basis layer is taken equal to 8 and the goal mean square error is taken equal to 0.6. The values are obtained after a try and error process.

The statistical indices comparing the RBNN results with the experimentally achieved composite ultimate tensile stress are shown in Table 2. The results show an excellent convergence and a good generality for the RBNN model.

3.3. SVM Results

In this study, the Gaussian kernel function is utilized for the constructed SVM model. The parameter b is the threshold of the SVM system known as the bias term. This structure estimates the problem through an f(x) function with a deviation of ε that is a predefined parameter for accuracy and it is set to be equal to 0.001 in this study. The L1QP solver is used to solve the minimization problem that gives an SVM structure with a set of 192×3 support vectors. All the mentioned SVM settings are achieved through a try and error process to give the best possible results.

3.3.1. SVM Model for Estimation of Ec

The achieved indices for comparison of SVM results with the experimentally resulted values for composite modulus of elasticity are shown in Table 1. The results show proper accuracy for both testing and training procedures.

3.3.2. SVM Model for Estimation of σuc

The indices comparing the SVM results with the experimental values of the composite ultimate tensile stress are shown in Table 2. The results show a poor convergence for the model in training and testing states despite the previous SVM model. Therefore, the SVM model seems not to be proper for this problem.

3.4. ALM Results

In this section, the ALM structure is used for estimation of the Ec with respect to Er, %sand, and %glass, and for estimation of σuc with respect to σur, %sand, and %glass. A primary evaluation is possible noting the regression plots.

3.4.1. ALM Model for Estimation of Ec

The achieved statistical indices for comparison of ALM results with the experimentally resulted values for composite modulus of elasticity are shown in Table 1. The results show an acceptable convergence for the model in the training domain and testing results. The number of partitions in the ALM algorithm is 4,7 and 1 for Er, %sand, and %glass respectively. The Ink radius is also 0.085 and the threshold value is 0.01.

3.4.2. ALM Model for Estimation of σuc

The convergence indices comparing the ALM results with the experimental values of the composite ultimate tensile stress are shown in Table 2. The results show proper accuracy for both testing and training procedures. The number of partitions in the ALM algorithm is 5, 11, and 2 for Er, %sand, and %glass respectively. The Ink radius is also 0.005 and the threshold value is 0.01.

3.5. Model Evaluation

Evaluation of the obtained models for estimation of the mechanical properties of sand/glass polymer composites is performed in this section.  In this regard, the selected performance indices are R2, RMSE, and variance account for (VAF) which their equations can be written as follows:

 

(5)

 

(6)

RMSE =

(7)

where y and y′ are the predicted and measured values, respectively, ỹ is the mean of the y′ values and N is the total number of data. The model will be excellent if R2 = 1, VAF =100 and RMSE = 0.

In the following subsections, the different constructed neural network models are evaluated with respect to the above-mentioned indices. With respect to the statistical indices, the most accurate models are chosen for the problem.

3.5.1. Model Evaluation for Estimation of Ec

The statistical performance indices including R2, RMSE, and VAF for the developed neural network models for estimation of Ec are presented in Table 1. It is observed that the resulted indices for each model are presented for both training and testing datasets.

Since the testing process is much important for generality and even convergence analysis, here it is recommended to consider the testing results as the decisive factor to ascertain the most accurate models. Comparing the resulted indices show that the most accurate model is the RBNN model for estimation of Ec. This model gives an excellent convergence and generality due to both train and test results. The results of the FFNN model are in the next grade with a slight difference. However, the FFNN model still gives excellent accuracy and generality. The poorest results belong to the RBNN model which has acceptable performance for training datasets but it doesn’t give proper results for testing datasets.

Table 1. R2, RMSE, and VAF results of the developed models for estimation of Ec

Method

State

R2

VAF

RMSE

FFNN

Training

0.9980

99.7944

0.1008

Testing

0.9976

99.7621

0.1073

RBNN

Training

0.9981

99.8113

0.0966

Testing

0.9929

99.2118

0.1970

SVM

Training

0.9707

96.5334

0.4219

Testing

0.9249

90.8253

0.6911

ALM

Training

0.9330

89.6778

0.6251

Testing

0.9068

87.9767

0.6850

3.5.2. Model Evaluation for Estimation of σuc

The statistical performance indices including R2, RMSE, and VAF for the developed neural network models for estimation of σuc are presented in Table 2. The aforementioned statistical indices for each model are presented for both training and testing datasets.

Noting the performance indices for the testing process in Table 2, the FFNN model gives the best results for testing datasets. Whilst the RBNN model gives better results for the training process, the FFNN model seems to be the best choice for estimation of σuc and the RBNN model is in the next grade, because, as mentioned above, the testing results have higher importance. The SVM model can also be specified as the poorest model for estimation of σuc.

3.5.3. FFNN Model 5-Folds Cross Validation

The initial evaluation of models shows that the best accuracy and generality are achieved with an FFNN model. To ensure the generality of this model over all observations, a 5-fold cross validation is applied to the structure that is shown in Table 3 and 4 respectively for estimation of Ec and σuc based on mean R2 value.

In the 5-fold cross-validation process, the 240 observations are divided into 5 independent parts including 48 observations. Afterward, the model is trained and tested for 5 times (5 folds). In each fold, one of the separated parts is taken as the test data and the other 4 parts are taken as the training data. In this way, 100% of the dataset is used for both testing and training.

Table 2.R2, RMSE and VAF results of developed models for estimation of σuc

Method

State

R2

VAF

RMSE

FFNN

Training

0.9909

99.0883

1.2172

Testing

0.9904

99.0367

1.1310

RBNN

Training

0.9963

99.6287

0.7740

Testing

0.9383

93.5807

2.9235

SVM

Training

0.92 32

91.2052

3.0487

Testing

0.9129

90.2342

3.8952

ALM

Training

0.9455

93.7121

3.0081

Testing

0.9357

91.5146

3.1182

 

Table 3. The mean R2 results for 5-fold cross-validation of FFNN for Ec estimation

State

Mean R2

Fold 1

Fold 2

Fold 3

Fold 4

Fold 5

Average

Train

0.9980

0.9981

0.9952

0.9967

0.9918

0.9960

Test

0.9976

0.9957

0.9921

0.9907

0.9911

0.9934

 

Table 4. The mean R2 results for 5-fold cross-validation of FFNN model for σuc estimation

State

Mean R2

Fold 1

Fold 2

Fold 3

Fold 4

Fold 5

Average

Train

0.9909

0.9881

0.9892

0.9896

0.9918

0.9899

Test

0.9904

0.9877

0.9889

0.9865

0.9911

0.9889

 

The 5-folds cross validation results are in a closed range. Therefore, the results certify the generality of the FFNN model.

4. Model Presentation

In the previous sections, the models are constructed and investigated in terms of convergence and generality. The best models are chosen and it is time to represent proper models for obtaining the mechanical properties of sand/glass polymer composites. Since in addition to the accuracy the simplicity is an important factor in model presentation, for both estimation problems the FFNN model is presented that has a simple structure with excellent accuracy.

4.1. Model Presentation for Ec

An FFNN model proposed for estimation of the Ec is presented in this section. As mentioned above, in an FFNN model the input vector (x) at first should be mapped from [xmin, xmax] into the [-1, 1] domain through a linear function.

Due to the observations of the problem, the domain of [xmin, xmax] can be stated as 1.636≤Er ≤4 GPa, 0≤%sand≤55 percent, and 0≤%glass≤15 percent. Therefore, the mapped inputs (xp) can be obtained as follows.

 

(8)

Noting Fig. 5, the pre mapping output (yp) that is a value between -1 and 1 is obtained as follows.

 

(9)

The pre mapping output should then be mapped from [-1,1] into [ymin, ymax] domain where ymin=Ecmin= 1.5944 GPa and ymax=Ecmax = 12.4596 GPa. Then the model output (Ec in GPa) will be obtained through a linear mapping as follows.

 

(10)

Having the weight and bias matrices, this model can be applied to estimate the modulus of elasticity for sand/glass polymer composites (Ec) for any in-range datasets using any programming software. The weight and bias matrices are presented as follows.

 

(11)

 

(12)

 

(13)

 

(14)

4.2. Model Presentation for σuc

An FFNN model proposed for estimation of the σuc is presented in this section. Similar to the previous model, at first, the input vector (x) should be mapped from [xmin, xmax] into the [-1, 1] domain through a linear function.

Due to the observations of the problem, the domain of [xmin, xmax] can be stated as 54.48≤σur≤93.540 MPa, 0≤%sand≤55 percent, and 0≤%glass≤15 percent. Therefore, the mapped inputs (xp) can be obtained as follows.

 

(15)

Again, noting Fig. 5, the pre mapping output (yp) that is a value between -1 and 1 is obtained via Eq. 9.

The pre mapping output should then be mapped from [-1, 1] into [ymin, ymax] domain where ymin=σucmin = 7.7242 MPa and ymax=σucmax = 93.540 MPa. Then the model output (σuc in MPa) will be obtained through a linear mapping as follows.

 

(16)

Having the weight and bias matrices, this model can be applied to estimate the modulus of elasticity for sand/glass polymer composites (σuc) for any in-range datasets using any programming software. The weight and bias matrices are presented as follows.

 

(17)

 

(18)

 

(19)

 

(20)

5. Conclusions

In this study, the neural network soft computation modeling based on experimental datasets is used to construct a realistic model for the prediction of mechanical properties of sand/glass polymer composites. The tensile and bending tests are conducted to obtain the modulus of elasticity and the ultimate tensile stress of sand/glass reinforced polymer composite specimens. The extracted results are then used for training and testing of the neural network models. The model is supposed to give the mechanical properties of the sand/glass polymer composite including the modulus of elasticity and ultimate tensile stress in respect to the modulus of elasticity and ultimate tensile stress of the resin and weight percentages of sand and glass in the composite. The ALM and SVM models and two different types of neural networks including FFNN and RBNN are employed for generating a realistic model. All of the models are trained to fit the problem datasets properly through a try and error procedure. The try and error process is performed to minimize the resulted RMSE value as much as possible to obtain the most acceptable configuration of each model. Then, for both training and testing data, the extracted results of ALM, FFNN, RBNN, and SVM models are compared together in terms of accuracy using the statistical indices including R2, RMSE, and VAF. Noting the obtained statistical indices, although all the models are excellent over the training process, the FFNN model is selected as the reference model because of its accuracy over the test data and simple structure. Since the FFNN model gives the best coincidence over the test data, it has the best generality among the obtained models. Finally, the models are presented as a simple formula based on the FFNN structure to obtain the mechanical properties of the sand/glass polymer composite with an excellent agreement with the experimental results.

 

 

 

Appendix A

The experimentally obtained results for modulus of elasticity (Ec) and ultimate tensile stress of the sand glass resin composites (σuc) are tabulated in this section. The neural network results are also added to the tables to perform a comparison between the experimental results and the utilized neural networks. Tables A-1 and 2 give the obtained Ec from experiments and neural networks for training and testing observations.

Tables A-1. Obtained Ec from experiments and neural networks for training observations. (Continued)

Resin type

Er

%sand

%glass

Ec (GPa)

Exp.

FFNN

RBNN

SVM

ALM

EPON 828

 

1.636

0

0

1.636

1.4927

1.6348

1.6365

1.7654

1.636

0

5

1.705

1.6266

1.6996

1.706

1.8187

1.636

0

10

1.9529

1.8152

1.8873

1.9541

1.907

1.636

5

0

1.6457

1.7059

1.7794

1.6477

1.8151

1.636

5

5

1.8827

1.8651

1.8778

1.8823

1.875

1.636

5

10

2.1895

2.0329

2.0373

1.9893

1.9538

1.636

5

15

1.9656

1.9646

2.0446

1.9684

1.9512

1.636

10

0

1.8155

1.9014

1.9023

1.8277

2.0089

1.636

10

5

2.2046

2.0897

2.0609

2.137

2.1045

1.636

10

10

2.0862

2.2417

2.0656

2.146

2.1177

1.636

15

0

2.0789

2.0785

2.0488

2.0254

2.2255

1.636

15

5

2.3276

2.3052

2.356

2.3274

2.3392

1.636

15

10

2.3643

2.4532

2.4642

2.3658

2.2972

1.636

15

15

2.3162

2.3009

2.3186

2.3152

2.3881

Tables A-1. Obtained Ec from experiments and neural networks for training observations. (Continued)

Resin type

Er

%sand

%glass

Ec (GPa)

Exp.

FFNN

RBNN

SVM

ALM

EPON 828

1.636

20

0

2.245

2.2632

2.1761

2.2429

2.4471

1.636

20

5

2.5642

2.5512

2.648

2.5658

2.5651

1.636

20

15

2.7865

2.5672

2.8285

2.7854

2.6601

1.636

25

0

2.5014

2.5515

2.4875

2.5965

2.8449

1.636

25

5

2.9997

2.9451

3.0268

3.0684

3.0332

1.636

25

10

3.1581

3.1879

3.1646

3.2991

3.1275

1.636

30

0

3.066

3.0856

3.0889

3.0656

3.403

1.636

30

5

3.9092

3.6217

3.7912

3.7824

3.6614

1.636

30

10

4

3.9508

4.1586

3.9728

3.6977

1.636

30

15

3.848

3.8682

4.1195

4.0486

3.8228

1.636

35

0

3.5462

3.4027

3.5498

3.376

3.9095

1.636

35

5

4.2758

4.1809

4.1526

4.2748

4.1736

1.636

35

10

4.3625

4.5985

4.3258

4.3623

4.1972

1.636

35

15

4.4736

4.4864

4.2194

4.3816

4.2085

1.636

40

5

4.6202

4.6297

4.7265

4.1006

3.988

1.636

40

10

5.0126

5.0469

5.1909

4.135

4.0632

1.636

45

0

2.4319

2.3287

2.4014

2.6583

2.6061

1.636

45

5

2.9546

2.8804

2.8722

3.2647

2.9679

1.636

45

10

3.2384

3.16

3.1016

3.3486

3.1251

1.636

50

0

2.003

2.0588

2.1179

2.003

2.2269

1.636

50

5

2.2553

2.4284

2.3051

2.2556

2.3456

1.636

50

15

2.4925

2.5655

2.5276

2.4911

2.4037

1.636

55

0

1.6061

1.6123

1.5946

1.6688

2.1605

1.636

55

5

1.6387

1.7033

1.6929

1.6377

2.247

1.636

55

10

1.9237

1.7721

1.8915

1.9231

2.2485

1.636

55

15

1.5944

1.7232

1.5807

1.8692

2.3221

EPON 862

 

2.463

0

0

2.463

2.433

2.4684

2.4635

2.6829

2.463

0

5

2.8439

2.6844

2.7433

2.8421

2.7985

2.463

0

10

2.7831

2.8273

2.9291

2.9027

2.8309

2.463

5

0

2.6704

2.6463

2.6141

2.592

2.6934

2.463

5

5

3.001

2.937

2.9186

2.993

2.8186

2.463

5

10

3.1178

3.0753

3.1137

3.04

2.8499

2.463

10

0

2.8122

2.8607

2.786

2.8103

2.8909

2.463

10

5

3.2144

3.1968

3.1687

3.2157

3.0407

2.463

10

10

3.2564

3.339

3.2806

3.2675

3.078

2.463

10

15

3.1478

3.0622

3.0235

3.15

2.9613

2.463

15

5

3.449

3.4945

3.5005

3.4487

3.454

2.463

15

10

3.5685

3.6587

3.6415

3.5677

3.5313

2.463

15

15

3.5241

3.3683

3.3989

3.4319

3.4332

2.463

20

5

4.0624

3.9148

3.9352

3.8574

3.9666

2.463

20

10

4.3724

4.1381

4.2079

4.095

4.1161

2.463

20

15

3.9014

3.8752

4.0352

3.9458

3.861

2.463

25

0

3.8484

3.9904

3.8945

3.9737

4.1396

2.463

25

5

4.6449

4.6171

4.6176

4.6772

4.4599

2.463

25

10

4.9556

4.9467

4.8587

5.0171

4.6451

2.463

25

15

4.8271

4.753

4.5417

4.8252

4.3583

2.463

30

5

5.7803

5.6622

5.7147

5.7827

5.5543

2.463

30

10

6.0254

6.078

6.1448

6.1539

5.6364

2.463

30

15

5.8519

5.9008

5.986

5.8819

5.6092

2.463

35

0

5.3066

5.4635

5.5599

5.1602

5.8282

 

Tables A-1. Obtained Ec from experiments and neural networks for training observations. (Continued)

Resin type

Er

%sand

%glass

Ec (GPa)

Exp.

FFNN

RBNN

SVM

ALM

EPON 862

2.463

35

10

6.8829

6.8376

6.7699

6.8825

6.4567

2.463

35

15

6.5651

6.5656

6.4596

6.5632

6.1684

2.463

40

0

5.7196

5.8664

5.5984

4.846

5.3591

2.463

40

5

7.1168

7.1167

7.049

6.3204

6.2489

2.463

40

10

7.6231

7.6578

7.6916

6.6002

6.3492

2.463

40

15

7.1352

7.1898

7.3245

6.3382

5.971

2.463

45

0

3.9122

3.7537

3.8314

3.9129

3.87

2.463

45

10

4.8061

4.7216

4.7564

5.3242

4.7573

2.463

45

15

4.5947

4.5545

4.5038

5.18

3.9366

2.463

50

5

3.652

3.6789

3.5364

3.6504

3.7142

2.463

50

10

3.7404

3.738

3.7761

3.7385

3.834

2.463

50

15

3.6405

3.6337

3.6358

3.6383

3.6357

2.463

55

0

2.5412

2.4521

2.4224

2.432

3.5049

2.463

55

10

2.6259

2.71

2.6741

2.6262

3.6745

2.463

55

15

2.4299

2.4547

2.3685

2.4295

3.5162

Epoxy L135i

 

2.6

0

0

2.6

2.5812

2.6064

2.5991

2.7867

2.6

0

10

3.1194

2.9997

3.1026

3.121

2.9346

2.6

0

15

2.9468

2.7743

2.9128

2.9467

2.9332

2.6

5

0

2.7303

2.7942

2.7514

2.7415

2.8477

2.6

5

5

3.0418

3.112

3.0899

3.1824

2.9744

2.6

5

10

3.166

3.2522

3.2901

3.2709

3.0045

2.6

5

15

3.1216

2.9852

3.1413

3.1193

3.0188

2.6

10

0

2.8117

3.0112

2.9313

2.9677

3.0873

2.6

10

10

3.5155

3.5242

3.4798

3.5038

3.2769

2.6

15

0

3.2326

3.2581

3.2099

3.1963

3.4633

2.6

15

5

3.6653

3.6872

3.6923

3.6652

3.6542

2.6

15

10

3.8056

3.8607

3.8405

3.8082

3.7089

2.6

20

0

3.5402

3.6096

3.5425

3.5413

3.9113

2.6

20

5

4.1882

4.1348

4.1551

4.1042

4.1351

2.6

20

10

4.4512

4.3733

4.4344

4.3451

4.2332

2.6

25

0

4.0574

4.2168

4.1284

4.1603

4.4472

2.6

25

5

4.8616

4.8865

4.8865

4.951

4.7739

2.6

25

10

5.1115

5.2371

5.15

5.2878

4.8772

2.6

25

15

4.8537

5.0351

4.8293

5.0442

4.668

2.6

30

0

5.1853

5.1736

5.0724

4.9129

5.3885

2.6

30

5

5.9575

5.9919

6.0316

6.0648

5.8528

2.6

30

10

6.5311

6.4291

6.4769

6.4522

5.9409

2.6

30

15

6.4493

6.2417

6.3004

6.1406

5.9604

2.6

35

5

6.8684

6.7632

6.8863

6.8076

6.7436

2.6

35

10

7.1974

7.2114

7.1748

7.1968

6.8096

2.6

35

15

6.8498

6.9184

6.836

6.8509

6.644

2.6

40

5

7.3229

7.5166

7.4234

6.5443

6.6028

2.6

40

15

7.5562

7.6067

7.7255

6.6157

6.2004

2.6

45

0

4.0099

3.9852

4.0569

4.0114

4.2799

2.6

45

5

4.7793

4.6979

4.7659

5.298

4.9381

2.6

45

15

4.8507

4.7917

4.7711

5.4058

4.2691

2.6

50

5

3.7119

3.8832

3.74

3.7827

3.8905

Tables A-1. Obtained Ec from experiments and neural networks for training observations. (Continued)

Resin type

Er

%sand

%glass

Ec (GPa)

Exp.

FFNN

RBNN

SVM

ALM

LY564

 

2.6

50

10

3.8912

3.9507

3.9765

3.9225

3.946

2.6

50

15

3.822

3.8189

3.8267

3.7955

3.8779

2.6

55

0

2.5189

2.5835

2.5612

2.5216

3.7452

2.6

55

5

2.7755

2.8163

2.6968

2.7768

3.723

2.6

55

15

2.4778

2.5839

2.5091

2.5291

3.738

3.43

0

5

3.9318

3.8859

3.9613

3.9317

3.9038

3.43

0

10

4.1389

4.0647

4.1465

4.1375

3.981

3.43

0

15

3.6576

3.706

3.7671

3.6572

3.808

3.43

5

0

3.539

3.6385

3.5684

3.6065

3.8566

3.43

5

10

4.1923

4.341

4.3342

4.346

4.0849

3.43

10

0

3.8767

3.8689

3.7944

3.8752

4.132

3.43

10

5

4.4269

4.4393

4.4322

4.3774

4.2996

3.43

10

10

4.6294

4.6592

4.6593

4.6286

4.3861

3.43

10

15

4.1826

4.2566

4.3198

4.1836

4.2196

3.43

15

0

4.2495

4.1679

4.204

4.2088

4.693

3.43

15

5

4.7279

4.82

4.854

4.7755

4.9182

3.43

15

10

5.0503

5.0916

5.0561

5.0529

5.0258

3.43

15

15

4.6696

4.703

4.7096

4.66

4.7973

3.43

20

0

4.7226

4.6503

4.7316

4.7401

5.2515

3.43

20

5

5.5105

5.4253

5.5111

5.513

5.5699

3.43

20

10

5.8889

5.7961

5.8586

5.8288

5.6718

3.43

25

0

5.4549

5.5154

5.5325

5.539

6.0618

3.43

25

10

6.8253

6.9831

6.955

7.0986

6.5466

3.43

25

15

6.6779

6.7645

6.6235

6.7906

6.5953

3.43

30

0

6.791

6.8255

6.7031

6.3642

7.751

3.43

30

5

7.9667

7.9285

7.9152

7.967

8.3049

3.43

30

10

8.4853

8.5357

8.4788

8.567

8.316

3.43

30

15

8.2336

8.3231

8.2089

8.2346

8.2492

3.43

35

5

9.1141

8.9359

9.1224

8.6622

9.0615

3.43

35

10

9.462

9.4791

9.5938

9.4653

9.1691

3.43

35

15

9.0873

9.0961

9.1158

9.0868

9.0391

3.43

40

5

9.7099

9.8435

9.5985

8.2205

9.5546

3.43

40

10

10.8167

10.7154

10.5818

9.1011

9.7884

3.43

40

15

10.2464

10.2184

10.1707

8.6959

9.6736

3.43

45

0

5.2811

5.3593

5.3371

5.3021

6.0204

3.43

45

5

6.1173

6.2425

6.2955

6.7522

7.0631

3.43

45

10

6.599

6.6053

6.6945

7.5012

7.6987

3.43

50

0

4.5152

4.3638

4.4731

4.1721

5.0545

3.43

50

5

4.9607

5.0995

4.9557

4.962

5.3887

3.43

50

15

4.9407

4.9868

5.0129

5.003

5.6358

3.43

55

0

3.3862

3.3337

3.4022

3.3867

4.7099

3.43

55

5

3.5763

3.706

3.6271

3.5948

4.8561

3.43

55

10

3.7944

3.8051

3.717

3.7943

4.8097

3.43

55

15

3.3383

3.4101

3.4118

3.3386

4.8492

PVA

 

4

0

0

4

3.9592

3.9811

4.0003

3.8007

4

0

5

4.6013

4.5632

4.6602

4.6004

3.8968

4

0

15

4.4557

4.3911

4.3377

4.4555

3.8314

4

5

0

4.1982

4.1646

4.106

4.1561

3.8687

4

5

10

5.1597

5.0978

5.0165

5.1591

4.0231

Tables A-1. Obtained Ec from experiments and neural networks for training observations.

Resin type

Er

%sand

%glass

Ec (GPa)

Exp.

FFNN

RBNN

SVM

ALM

PVA

 

4

5

15

4.7092

4.6619

4.6259

4.7071

3.9494

4

10

0

4.4106

4.4024

4.3615

4.412

4.2307

4

10

5

5.0298

5.1338

5.1424

5.0297

4.3426

4

10

15

4.9868

5.0051

5.0408

5.0282

4.2441

4

15

0

4.8679

4.7342

4.868

4.8653

4.7266

4

15

10

6.0828

5.9364

5.8875

6.0821

4.9397

4

15

15

5.5673

5.529

5.4859

5.5489

4.8237

4

20

0

5.6188

5.3012

5.5359

5.6172

5.2944

4

20

5

6.4275

6.2644

6.4513

6.3716

5.4925

4

20

15

6.4571

6.446

6.5763

6.458

5.5386

4

25

0

6.3753

6.3349

6.4694

6.6046

6.2599

4

25

5

7.5661

7.4913

7.6465

7.5652

6.6674

4

25

10

8.1871

8.1613

8.2138

8.3889

6.5947

4

25

15

7.7807

7.968

7.8854

7.78

6.5056

4

30

0

7.8374

7.8783

7.7553

7.489

7.7987

4

30

10

10.0792

9.9509

9.8197

9.7948

8.1755

4

35

0

8.8822

9.1164

8.9

7.8053

9.1038

4

35

5

10.5631

10.3888

10.5569

9.2198

9.1202

4

35

10

10.8418

11.0276

11.1924

10.5051

9.1826

4

35

15

10.6245

10.6217

10.6513

9.8523

9.056

4

40

10

12.4596

12.4698

12.219

9.9536

9.6976

4

40

15

11.8771

12.0689

11.8353

9.3784

9.5952

4

45

0

6.1825

6.2744

6.1182

6.1809

6.3094

4

45

5

7.1191

7.2853

7.266

7.3399

7.2566

4

45

10

7.7798

7.7336

7.8053

8.2421

7.7183

4

45

15

7.4583

7.3657

7.5614

7.799

7.2397

4

50

5

5.8808

5.9096

5.76

5.6932

5.1144

4

50

10

6.0961

6.1474

6.0502

6.0943

5.2038

4

50

15

5.936

5.8294

5.8421

5.7838

5.4418

4

55

0

3.9123

3.8047

3.9711

3.9124

4.7411

4

55

10

4.321

4.4381

4.38

4.3235

4.8039

4

55

15

4.1128

4.0168

4.072

4.1138

4.8303

 

Table A-2. Obtained Ec from experiments and neural networks for testing observations. (Continued)

Resin type

Er

%sand

%glass

Ec (GPa)

Exp.

FFNN

RBNN

SVM

ALM

EPON 828

 

1.636

0

15

1.7508

1.8004

1.9141

2.1126

1.8776

1.636

10

15

2.1247

2.1247

1.8742

2.0401

2.1044

1.636

20

10

2.7668

2.7231

2.9085

2.7207

2.5751

1.636

25

15

3.1105

3.0738

2.8813

3.4164

3.0806

1.636

40

0

3.8226

3.704

3.6787

3.2345

3.5

1.636

40

15

4.7555

4.7846

4.9543

4.1572

4.0859

1.636

45

15

3.0413

3.1808

2.9428

3.406

2.6812

1.636

50

10

2.6192

2.4729

2.5973

2.4496

2.4043

EPON 862

 

2.463

0

15

2.5745

2.6286

2.7705

2.8015

2.7665

2.463

5

15

2.9489

2.8331

2.9878

2.9418

2.7988

2.463

15

0

3.037

3.0984

3.0444

3.0301

3.267

2.463

20

0

3.4213

3.4272

3.3463

3.363

3.7444

2.463

30

0

4.9297

4.8876

4.7948

4.7337

5.0843

2.463

35

5

6.5495

6.3992

6.5045

6.5435

6.4195

Table A-2. Obtained Ec from experiments and neural networks for testing observations.

Resin type

Er

%sand

%glass

Ec (GPa)

Exp.

FFNN

RBNN

SVM

ALM

EPON 862

2.463

45

5

4.3986

4.4407

4.5029

5.1228

4.5309

2.463

50

0

3.225

3.1545

3.2384

2.9348

3.5246

2.463

55

5

2.7501

2.6629

2.5483

2.6763

3.5744

Epoxy L135i

 

2.6

0

5

2.9755

2.8577

2.9169

3.0271

2.9074

2.6

10

5

3.2765

3.3769

3.3508

3.4122

3.2461

2.6

10

15

3.1787

3.2252

3.2113

3.3427

3.1985

2.6

15

15

3.7146

3.5519

3.5825

3.6251

3.6334

2.6

20

15

4.2493

4.0973

4.2482

4.1419

4.0903

2.6

35

0

5.7097

5.7987

5.8816

5.3134

6.153

2.6

40

0

6.1966

6.2066

5.9019

4.9669

5.7283

2.6

40

10

8.3001

8.0934

8.1059

6.8987

6.7008

2.6

45

10

5.0163

4.9852

5.0325

5.573

5.0313

2.6

50

0

3.3488

3.3305

3.4193

3.0259

3.8434

2.6

55

10

2.933

2.8658

2.8142

2.7524

3.7663

LY564

3.43

0

0

3.43

3.4292

3.4324

3.3995

3.7631

3.43

5

5

4.0077

4.1476

4.1092

4.1211

4.0046

3.43

5

15

3.9869

3.9536

4.0432

3.8716

3.9208

3.43

20

15

5.5352

5.4734

5.601

5.4941

5.5744

3.43

25

5

6.3653

6.465

6.5267

6.6843

6.6344

3.43

35

0

7.4332

7.7891

7.737

6.7316

8.9812

3.43

40

0

8.064

8.1542

7.6291

6.3239

8.4897

3.43

45

15

6.1622

6.2861

6.4203

7.0878

7.5309

3.43

50

10

5.4649

5.2507

5.2055

5.434

5.6584

PVA

4

0

10

4.7152

4.8082

4.8458

4.8546

3.9485

4

5

5

4.8292

4.8271

4.7803

4.7723

3.9677

4

10

10

5.3758

5.4437

5.4305

5.5265

4.3991

4

15

5

5.6675

5.5581

5.6392

5.5137

4.871

4

20

10

6.8373

6.7644

6.8713

7.0228

5.575

4

30

5

9.1921

9.1902

9.1521

8.7122

8.1813

4

30

15

9.7878

9.7601

9.499

9.1414

8.2542

4

40

0

9.459

9.3793

8.6876

7.3078

8.7371

4

40

5

11.3536

11.3325

10.9768

8.7094

9.5234

4

50

0

5.205

5.0427

5.1444

4.9016

4.9395

4

55

5

4.3439

4.2742

4.2862

4.3554

4.8348

 

In addition, tables A-3 and 4 give the obtained σuc from experiments and neural networks for training and testing observations.

Tables A-3. Obtained σuc from experiments and neural networks for training observations. (Continued)

Resin type

σur

%sand

%glass

σuc (MPa)

Exp.

FFNN

RBNN

SVM

ALM

EPON 828

 

54.48

0

0

54.477

55.7851

54.3753

28.6071

53.6665

54.48

0

5

36.3082

35.7848

36.281

30.9171

36.8057

54.48

0

10

30.6315

32.9579

30.2623

30.6305

30.6278

54.48

5

0

23.9671

23.6017

23.9385

23.9681

31.8989

54.48

5

5

20.7432

23.143

22.134

25.3631

26.6449

54.48

5

10

24.9618

23.4324

23.7432

24.9524

26.9948

54.48

5

15

18.8838

19.727

20.0715

20.7504

23.4039

54.48

10

0

18.9885

18.6467

17.8805

20.0495

20.0443

54.48

10

5

19.9698

20.3107

19.852

20.9314

20.1542

Tables A-3. Obtained σuc from experiments and neural networks for training observations. (Continued)

Resin type

σur

%sand

%glass

σuc (MPa)

Exp.

FFNN

RBNN

SVM

ALM

EPON 828

54.48

10

10

20.5124

20.9277

20.2429

20.5134

20.8776

54.48

15

0

17.4221

17.868

18.9854

17.9012

18.3457

54.48

15

5

20.1246

19.7538

19.9211

18.9475

19.2034

54.48

15

10

17.567

20.4695

18.9727

18.7055

17.8761

54.48

15

15

15.9865

17.5942

15.6247

17.0617

15.9565

54.48

20

0

18.9492

18.0887

17.478

17.8208

18.6015

54.48

20

5

20.6194

20.0834

19.6531

19.6956

19.1031

54.48

20

15

18.828

17.7682

18.1349

18.827

18.128

54.48

25

0

17.1081

19.4391

18.8662

19.1736

19.2334

54.48

25

5

20.7538

21.8283

21.2736

22.2233

20.6393

54.48

25

10

21.5984

22.7008

21.8608

22.7783

21.4166

54.48

30

0

20.4189

21.9521

19.3074

20.6669

21.3748

54.48

30

5

24.758

25.3528

24.1084

24.759

23.7226

54.48

30

10

25.6786

27.2426

25.6839

25.6796

25.2638

54.48

30

15

27.6466

26.0401

27.6297

24.7952

26.3786

54.48

35

0

21.7471

22.4355

22.2766

20.9635

24.0444

54.48

35

5

29.2842

26.9983

29.5374

25.5543

28.3819

54.48

35

10

28.2461

28.4251

28.4495

26.6213

27.7278

54.48

35

15

25.6426

25.8751

26.1514

25.6436

26.3636

54.48

40

5

33.3239

33.6133

34.0794

23.7196

31.7746

54.48

40

10

33.0457

32.7273

31.3768

24.6625

31.5073

54.48

45

0

16.1209

15.9173

14.9302

15.9867

21.8652

54.48

45

5

19.5845

18.5203

19.6499

19.6182

24.7651

54.48

45

10

17.2612

17.5912

18.4914

20.2351

23.0804

54.48

50

0

10.6348

11.6598

10.8134

11.986

12.8481

54.48

50

5

12.8819

13.05

13.1761

14.6316

14.4276

54.48

50

15

14.863

12.643

14.0208

14.864

14.9535

54.48

55

0

8.6975

7.3014

9.1322

8.6985

9.4579

54.48

55

5

10.4607

11.0092

9.7274

10.4597

10.0063

54.48

55

10

8.8147

10.9916

8.9898

10.3994

9.0472

54.48

55

15

10.906

9.6831

11.3177

10.907

10.9876

EPON 862

 

93.54

0

0

93.541

93.4378

93.3295

41.0201

88.3401

93.54

0

5

58.8938

60.3845

59.2767

45.4663

57.9415

93.54

0

10

53.7847

54.8589

53.3707

43.0103

47.3515

93.54

5

0

38.8327

39.4758

39.2174

36.147

48.5309

93.54

5

5

40.1159

38.7513

39.3257

40.053

43.8171

93.54

5

10

39.343

39.4555

40.3507

38.5643

36.7395

93.54

10

0

31.7029

30.649

31.7127

31.7039

32.6646

93.54

10

5

32.7764

33.9836

32.9089

35.3533

31.9062

93.54

10

10

35.0161

35.1153

34.5275

35.0964

32.3582

93.54

10

15

30.8656

30.2336

30.6482

30.7828

28.9016

93.54

15

5

31.651

33.3235

31.467

33.338

30.0068

93.54

15

10

32.0249

34.7433

31.829

34.3984

32.0587

93.54

15

15

30.2123

30.6104

30.5439

30.4933

29.0847

93.54

20

5

35.5225

34.184

35.9735

34.7216

32.5291

93.54

20

10

36.9912

35.8382

37.4358

36.9902

31.2906

93.54

20

15

33.664

32.4064

33.7427

32.8

31.132

93.54

25

0

30.504

32.4715

30.1854

31.9404

30.9079

93.54

25

5

35.3162

37.0186

35.8027

38.4605

33.6806

93.54

25

10

38.9894

39.2488

37.7578

41.6442

36.9359

93.54

25

15

36.1733

36.869

35.9251

36.6757

34.2263

Tables A-3. Obtained σuc from experiments and neural networks for training observations. (Continued)

Resin type

σur

%sand

%glass

σuc (MPa)

Exp.

FFNN

RBNN

SVM

ALM

EPON 862

93.54

30

5

45.4836

42.7199

44.5976

42.1733

36.2845

93.54

30

10

45.8365

46.1767

47.5153

45.8355

43.5178

93.54

30

15

46.0333

45.2624

46.1211

40.0485

41.1862

93.54

35

0

41.7144

41.1883

42.5792

34.8866

38.687

93.54

35

10

50.7261

51.3511

50.0678

46.9509

46.3044

93.54

35

15

48.9149

48.0933

48.2401

40.7833

45.3263

93.54

40

0

45.4966

45.6478

44.8976

32.3603

37.2064

93.54

40

5

56.5135

54.7205

56.0407

40.4256

45.284

93.54

40

10

55.027

55.159

55.7701

43.603

50.5704

93.54

40

15

48.7734

50.4038

49.6235

37.7675

47.9391

93.54

45

0

26.1861

27.0587

26.4718

27.0237

25.3903

93.54

45

10

32.7848

31.4906

32.6608

36.305

35.7858

93.54

45

15

30.2193

30.2171

29.1424

31.4801

34.8454

93.54

50

5

25.5281

24.5602

26.0931

25.5271

22.582

93.54

50

10

27.1563

26.1053

26.9462

27.1553

25.0587

93.54

50

15

23.4901

24.8066

24.1808

23.7326

25.4463

93.54

55

0

12.7127

11.9795

12.3002

14.3428

9.4591

93.54

55

10

19.814

18.8787

19.5389

18.78

15.3274

93.54

55

15

16.4939

17.2131

16.5154

16.7753

16.3944

Epoxy L135i

63.8

0

0

63.8

63.044

63.7129

31.5329

60.4584

63.8

0

10

34.8482

37.3877

35.869

34.6576

34.4867

63.8

0

15

34.7669

34.9074

34.3802

29.506

33.9833

63.8

5

0

26.5677

26.4475

27.0692

26.5667

35.0502

63.8

5

5

28.1749

26.1164

27.2048

28.1759

29.3081

63.8

5

10

28.2638

26.7326

28.5583

28.6536

29.2627

63.8

5

15

23.5082

23.1242

23.1002

24.673

27.0945

63.8

10

0

22.487

20.8013

21.9763

22.4209

22.2481

63.8

10

10

25.0871

23.9804

24.2814

24.0477

23.3522

63.8

15

0

21.2966

20.0098

21.3033

20.3168

20.0143

63.8

15

5

21.6655

22.4806

22.5109

21.6911

20.802

63.8

15

10

22.649

23.6554

22.711

22.4571

20.8616

63.8

20

0

21.1077

20.3644

21.3431

20.5809

20.713

63.8

20

5

24.9714

23.0035

25.3493

23.0355

22.8069

63.8

20

10

26.1248

24.1942

26.9019

24.2013

23.9409

63.8

25

0

22.2055

21.9661

22.888

22.4292

21.3095

63.8

25

5

23.9855

25.0709

24.8856

26.3852

23.6144

63.8

25

10

28.0289

26.5909

26.5657

28.0299

24.9686

63.8

25

15

25.0116

24.4151

24.4738

26.0274

23.9627

63.8

30

0

24.3627

24.9761

24.7499

24.3017

23.0834

63.8

30

5

31.3086

29.1633

29.8134

29.6172

26.4697

63.8

30

10

32.9003

31.7583

32.9678

31.6419

28.7577

63.8

30

15

32.1099

30.9629

31.0439

29.3507

28.1282

63.8

35

5

32.9729

31.8394

32.7447

30.646

31.3332

63.8

35

10

34.2071

33.943

33.4305

32.7751

30.9152

63.8

35

15

30.6413

31.5021

31.5021

30.3359

29.744

63.8

40

5

37.0211

38.7298

38.199

28.4142

34.1393

63.8

40

15

33.6935

35.2069

35.6169

28.0163

32.2392

63.8

45

0

19.5948

18.4032

19.4497

18.2048

20.861

63.8

45

5

22.3963

21.9215

22.2508

23.3542

24.2909

63.8

45

15

20.9516

21.276

21.0648

22.8979

22.6738

63.8

50

5

17.8475

16.0302

17.158

17.1048

16.5144

Tables A-3. Obtained σuc from experiments and neural networks for training observations. (Continued)

Resin type

σur

%sand

%glass

σuc (MPa)

Exp.

FFNN

RBNN

SVM

ALM

Epoxy L135i

63.8

50

10

18.0085

17.4939

17.4705

17.8407

16.8131

63.8

50

15

16.6689

16.3115

16.1391

16.6699

17.5002

63.8

55

0

7.7242

8.3836

8.4857

8.703

8.2936

63.8

55

5

11.6857

12.9163

12.1141

11.6847

10.3264

63.8

55

15

12.3276

12.2931

11.9723

11.3657

12.0598

LY564

 

64.1

0

5

39.0245

40.6347

39.0648

34.2603

39.3257

64.1

0

10

37.4291

37.5401

36.6928

34.7795

34.739

64.1

0

15

35.054

35.0714

35.2687

29.6493

34.0263

64.1

5

0

25.7713

26.5484

25.7775

26.6585

35.0758

64.1

5

10

28.4087

26.8461

28.7279

28.7805

28.9977

64.1

10

0

20.5449

20.8781

20.7271

22.5125

22.0668

64.1

10

5

22.4609

23.072

23.0192

23.6132

22.9495

64.1

10

10

22.8128

24.0844

23.5414

24.1808

23.315

64.1

10

15

21.3262

20.7481

21.3503

21.3272

21.1618

64.1

15

0

20.1777

20.0859

20.2497

20.4143

20.0213

64.1

15

5

21.8033

22.5751

21.1704

21.8043

20.8042

64.1

15

10

22.5225

23.7628

21.5006

22.6018

20.9588

64.1

15

15

20.8315

20.9908

21.1488

20.4861

19.7772

64.1

20

0

20.6901

20.4447

20.6012

20.6911

20.7691

64.1

20

5

25.3537

23.104

24.2863

23.1645

22.8159

64.1

20

10

25.4694

24.3101

25.7822

24.3644

23.93

64.1

25

0

23.2375

22.0544

22.3041

22.5551

21.3796

64.1

25

10

24.7919

26.7196

25.6457

28.214

24.4588

64.1

25

15

23.667

24.5536

23.6699

26.1705

23.2726

64.1

30

0

24.3156

25.0806

24.2722

24.4393

23.1452

64.1

30

5

29.1469

29.2918

29.0916

29.7809

26.14

64.1

30

10

31.2069

31.9066

32.1559

31.8416

27.6752

64.1

30

15

28.7667

31.1205

30.2678

29.5054

27.001

64.1

35

5

30.8115

32.0007

32.0774

30.8125

31.3487

64.1

35

10

32.2961

34.1231

32.7519

32.9767

30.7531

64.1

35

15

32.8246

31.6823

30.9231

30.4951

29.5892

64.1

40

5

39.9969

38.8967

37.5516

28.5672

34.6856

64.1

40

10

37.7834

38.6213

38.7947

30.4819

34.1197

64.1

40

15

36.7074

35.3814

35.22

28.1662

32.6754

64.1

45

0

18.3042

18.4871

19.1071

18.3052

21.1523

64.1

45

5

21.2518

22.0329

21.6617

23.4795

24.5056

64.1

45

10

21.7327

21.4018

20.9227

24.8643

24.6888

64.1

50

0

14.6172

14.027

13.7537

13.1354

14.762

64.1

50

5

14.8741

16.1266

16.5403

17.1947

16.7131

64.1

50

15

14.6985

16.4233

15.4888

16.7622

17.1441

64.1

55

0

8.2047

8.4213

8.1494

8.7419

9.2455

64.1

55

5

13.2265

12.977

11.6169

11.7396

10.8915

64.1

55

10

11.9681

13.5973

12.7754

11.9691

11.3578

64.1

55

15

11.2939

12.37

11.4308

11.4223

11.2346

PVA

 

88.4

0

0

88.4

87.3785

88.2184

40.1492

88.3401

88.4

0

5

58.0149

56.4324

58.1062

44.668

57.8273

88.4

0

15

47.4431

49.5794

47.7702

36.6392

46.7322

88.4

5

0

34.9143

36.7892

35.4358

34.9153

45.4063

88.4

5

10

37.8134

37.1337

37.2791

37.8144

39.3379

88.4

5

15

32.6754

33.092

32.2104

32.6744

39.8552

88.4

10

0

30.1812

28.6504

28.7948

30.2798

33.2321

Tables A-3. Obtained σuc from experiments and neural networks for training observations.

Resin type

σur

%sand

%glass

σuc (MPa)

Exp.

FFNN

RBNN

SVM

ALM

PVA

 

88.4

10

5

33.1177

31.8977

33.9431

33.8328

32.7165

88.4

10

15

27.9683

28.7226

28.7183

29.6834

29.4094

88.4

15

0

27.3056

27.6638

28.5215

27.9204

28.5332

88.4

15

10

33.4942

32.8707

33.8828

33.1125

31.4587

88.4

15

15

29.1202

29.1549

28.2166

29.1713

28.781

88.4

20

0

28.4516

28.2811

27.7565

28.4506

29.7471

88.4

20

5

33.3607

32.1671

31.7839

33.3597

32.3833

88.4

20

15

31.248

30.7829

31.652

31.5499

31.1316

88.4

25

0

30.4368

30.4683

31.5889

31.011

31.6609

88.4

25

5

33.806

34.9086

34.6374

37.3438

33.4372

88.4

25

10

36.8682

37.1825

37.4614

40.6718

34.7206

88.4

25

15

35.7192

34.9862

35.6194

35.7202

33.6541

88.4

30

0

35.0958

34.7494

33.9193

33.6244

34.3946

88.4

30

10

45.0455

43.8283

44.0191

45.0445

42.2271

88.4

35

0

37.7368

38.5081

37.8307

34.1695

39.6489

88.4

35

5

44.2756

45.5733

45.025

42.2702

44.4857

88.4

35

10

47.5922

48.5065

47.665

46.1568

46.1217

88.4

35

15

45.4871

45.4741

46.1369

40.4314

45.474

88.4

40

10

53.4909

52.5752

52.751

42.5687

49.9508

88.4

40

15

49.0269

48.1396

48.5516

37.4389

48.2122

88.4

45

0

25.7723

25.6164

25.6488

25.7713

25.538

88.4

45

5

27.6573

30.7756

28.2249

32.0945

28.0808

88.4

45

10

30.4597

30.0201

30.8047

34.8575

35.114

88.4

45

15

29.4036

29.0303

29.9198

30.9528

34.83

88.4

50

5

21.0814

23.3382

19.9932

23.3265

23.4604

88.4

50

10

23.2548

24.9817

23.2775

25.2698

25.868

88.4

50

15

24.0168

23.7417

23.77

22.8847

26.2897

88.4

55

0

9.7226

11.4795

10.303

12.4537

10.4246

88.4

55

10

15.4023

18.3416

15.9521

16.5919

16.4383

88.4

55

15

15.6262

16.7709

15.3432

15.6272

17.405

Table A-4. Obtained σuc from experiments and neural networks for testing observations. (Continued)

Resin type

σur

%sand

%glass

σuc (MPa)

Exp.

FFNN

RBNN

SVM

ALM

EPON 828

 

54.48

0

15

29.7998

30.0823

26.6042

25.1199

30.2629

54.48

10

15

17.4121

17.6131

16.2024

17.7242

18.109

54.48

20

10

19.815

20.7223

20.0234

19.81

18.2583

54.48

25

15

20.8567

20.0961

22.6467

21.9817

21.8732

54.48

40

0

25.7495

27.9662

24.7482

19.33

29.5634

54.48

40

15

29.6896

29.6644

24.0743

23.7888

30.263

54.48

45

15

17.1096

17.6315

15.6802

19.7169

21.7194

54.48

50

10

15.8807

14.0616

13.2987

14.8667

13.804

EPON 862

 

93.54

0

15

53.4591

52.8081

55.9608

36.6798

46.7325

93.54

5

15

34.4425

35.1894

35.7965

33.3015

37.9233

93.54

15

0

29.6772

29.5657

38.3288

29.3211

27.6659

93.54

20

0

28.7298

30.1983

35.1421

29.6492

28.9666

93.54

30

0

39.2076

36.99

34.4005

34.3574

34.6005

93.54

35

5

47.7201

48.4129

50.9647

43.3086

44.3661

93.54

45

5

31.5052

32.3945

33.6723

33.8725

26.9674

93.54

50

0

23.1285

21.535

17.0385

20.3623

18.1618

93.54

55

5

18.8902

17.543

19.7225

17.8237

15.051

Table A-4. Obtained σuc from experiments and neural networks for testing observations.

Resin type

σur

%sand

%glass

σuc (MPa)

Exp.

FFNN

RBNN

SVM

ALM

Epoxy L135i

 

63.8

0

5

41.3754

40.4716

39.3005

34.1546

38.9264

63.8

10

5

22.6482

22.9788

24.2351

23.5078

23.0271

63.8

10

15

22.9919

20.6479

21.6152

21.1942

21.0386

63.8

15

15

19.6567

20.8838

21.8943

20.3572

19.5821

63.8

20

15

22.7331

21.5253

23.6545

22.3502

22.9722

63.8

35

0

26.5098

26.3948

26.9822

24.6028

28.884

63.8

40

0

30.5193

32.0168

29.362

22.4748

32.2933

63.8

40

10

38.1867

38.4381

39.3833

30.2964

33.7157

63.8

45

10

21.8601

21.284

21.5681

24.7111

24.435

63.8

50

0

15.3592

13.9502

14.1092

13.0662

14.3891

63.8

55

10

13.1852

13.5202

13.3411

11.8986

11.7297

LY564

64.1

0

0

64.1

63.2947

62.3819

31.6266

60.9223

64.1

5

5

25.0281

26.2206

26.5352

28.2804

29.1457

64.1

5

15

22.9794

23.239

23.5386

24.813

26.7794

64.1

20

15

22.2103

21.6465

22.8177

22.4827

22.9126

64.1

25

5

24.0474

25.1814

24.0443

26.5337

23.4785

64.1

35

0

27.6596

26.5292

26.5455

24.7413

29.3063

64.1

40

0

32.4773

32.151

28.9292

22.6002

33.2709

64.1

45

15

20.78

21.3886

20.5739

23.024

22.9381

64.1

50

10

19.201

17.6012

16.7255

17.9525

16.7389

PVA

88.4

0

10

52.3844

51.5799

48.35

42.7977

47.3803

88.4

5

5

38.2215

36.2888

36.2219

38.7993

41.8361

88.4

10

10

32.2776

33.1728

36.3705

33.9565

32.4077

88.4

15

5

30.3516

31.3208

29.7869

31.7967

30.2337

88.4

20

10

33.2876

33.9124

36.688

35.797

31.2878

88.4

30

5

42.5051

40.3622

40.3825

41.2034

35.8992

88.4

30

15

41.8101

43.0555

43.0754

39.4508

40.7033

88.4

40

0

42.5311

43.3462

40.1392

31.4499

38.6923

88.4

40

5

53.315

52.1517

48.6409

39.0871

45.8187

88.4

50

0

20.0375

20.3333

16.1733

18.7405

19.4427

88.4

55

5

17.8948

17.0364

14.54

15.3679

15.6502

 

 

 

 

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[45] Bahrpeyma, F., Zakerolhoseini, A. and Haghighi, H. 2015. Using ids fitted q to develop a real-time adaptive controller for dynamic resource provisioning in cloud's virtualized environment. Applied Soft Computing, 26, pp. 285-298.

[46] Murakami, M. 2008. Practicality of modeling systems using the ids method: Performance investigation and hardware implementation. Ph.D., The University of Electro-Communications.

[47] Firouzi, M. and Shouraki, S.B. 2011. Performance evaluation of active learning method in classification problems. 3rd International Conference on Machine Learning and Computing (ICMLC 2011). Singapore.

[48] Firouzi, M., Shouraki, S.B. and Rostami, M.G. Spiking neural network ink drop spread, spike-ids. In: Yamaguchi, Y., ed. Advances in Cognitive Neurodynamics (III), 2013// 2013 Dordrecht. Springer Netherlands, pp. 59-68.

[49] Firouzi, M., Shouraki, S.B. and Afrakoti, I.E.P. 2014. Pattern analysis by active learning method classifier. Journal of Intelligent & Fuzzy Systems, 26, pp. 49-62.

[50] Javadian, M., Bagheri Shouraki, S. and Sheikhpour Kourabbaslou, S. 2017. A novel density-based fuzzy clustering algorithm for low dimensional feature space. Fuzzy Sets and Systems, 318, pp. 34-55.

[51] Javadian, M. and Shouraki, S.B. 2017. Ualm: Unsupervised active learning method for clustering low-dimensional data. Journal of Intelligent & Fuzzy Systems, 73 (3), pp. 2393-2411.

[52] Firouzi, M., Shouraki, S.B. and Conradt, J. Sensorimotor control learning using a new adaptive spiking neuro-fuzzy machine, spike-ids and stdp. In: Wermter, S., Weber, C., Duch, W., Honkela, T., Koprinkova-Hristova, P., Magg, S., Palm, G. and Villa, A.E.P., eds. Artificial Neural Networks and Machine Learning – ICANN 2014, 2014// 2014 Cham. Springer International Publishing, pp. 379-386.

[53] Sakurai, Y. 2005. A study of the learning control method using pbalm-a nonlinear modeling method. The University of Electro-Communications.

[54] Shahdi, S.A. and Shouraki, S.B. 2002. Supervised active learning method as an intelligent linguistic controller and its hardware implementation. 2nd IASTEAD International Conference on Artificial Intelligence and Applications (AIA'02). Malaga, Spain.

[55] Merrikh-Bayat, F., Shouraki, S.B. and Rohani, A. 2011. Memristor crossbar-based hardware implementation of the ids method. IEEE Transactions on Fuzzy Systems, 19 (6), pp. 1083-1096.

 

 

 

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[49] Firouzi, M., Shouraki, S.B. and Afrakoti, I.E.P. 2014. Pattern analysis by active learning method classifier. Journal of Intelligent & Fuzzy Systems, 26, pp. 49-62.
[50] Javadian, M., Bagheri Shouraki, S. and Sheikhpour Kourabbaslou, S. 2017. A novel density-based fuzzy clustering algorithm for low dimensional feature space. Fuzzy Sets and Systems, 318, pp. 34-55.
[51] Javadian, M. and Shouraki, S.B. 2017. Ualm: Unsupervised active learning method for clustering low-dimensional data. Journal of Intelligent & Fuzzy Systems, 73 (3), pp. 2393-2411.
[52] Firouzi, M., Shouraki, S.B. and Conradt, J. Sensorimotor control learning using a new adaptive spiking neuro-fuzzy machine, spike-ids and stdp. In: Wermter, S., Weber, C., Duch, W., Honkela, T., Koprinkova-Hristova, P., Magg, S., Palm, G. and Villa, A.E.P., eds. Artificial Neural Networks and Machine Learning – ICANN 2014, 2014// 2014 Cham. Springer International Publishing, pp. 379-386.
[53] Sakurai, Y. 2005. A study of the learning control method using pbalm-a nonlinear modeling method. The University of Electro-Communications.
[54] Shahdi, S.A. and Shouraki, S.B. 2002. Supervised active learning method as an intelligent linguistic controller and its hardware implementation. 2nd IASTEAD International Conference on Artificial Intelligence and Applications (AIA'02). Malaga, Spain.
[55] Merrikh-Bayat, F., Shouraki, S.B. and Rohani, A. 2011. Memristor crossbar-based hardware implementation of the ids method. IEEE Transactions on Fuzzy Systems, 19 (6), pp. 1083-1096.