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<ArticleSet>
<Article>
<Journal>
				<PublisherName>Isfahan University of Technology</PublisherName>
				<JournalTitle>Journal of Computational Methods in Engineering</JournalTitle>
				<Issn>2228-7698</Issn>
				<Volume>39</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Numerical Simulation of Particle Separation in the Fluid Flow in a Microchannel Including Spiral and Acoustic Regions</ArticleTitle>
<VernacularTitle>Numerical Simulation of Particle Separation in the Fluid Flow in a Microchannel Including Spiral and Acoustic Regions</VernacularTitle>
			<FirstPage>1</FirstPage>
			<LastPage>21</LastPage>
			<ELocationID EIdType="pii">3208</ELocationID>
			
<ELocationID EIdType="doi">10.47176/jcme.39.2.0571</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>F.</FirstName>
					<LastName>Shabani</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>M.</FirstName>
					<LastName>Saghafian</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>D.</FirstName>
					<LastName>Saeidi</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>F.</FirstName>
					<LastName>F. Momennasab</LastName>
<Affiliation></Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</History>
		<Abstract>Particulate separation has many applications in medicine, biology and industry. In this research, the separation of polystyrene particles with a diameter of 10, 20 and 30 μm in the fluid flow of a microchannel is investigated. The microchannel consists of a spiral region and a straight region under the influence of acoustic waves. In the spiral region, the particles under hydrodynamic effects undergo the initial separation; then the particles enter the straight region of the microchannel, and the final separation of the particles is done by the force generated and exerted through the acoustic waves. The effects of acoustic frequency and the number of spiral region loops on separation are investigated. The results show that for measured dimensions and parameters, at 1 MHz acoustic wave, when the number of loops is 2 for the spiral region, the particles at the end of the path are in a suitable position for separation. In addition, the results show that the separation of particles with this hybrid system is better than that done by the simple methods, and the separation rate can be as high as 100%
 </Abstract>
			<OtherAbstract Language="FA">Particulate separation has many applications in medicine, biology and industry. In this research, the separation of polystyrene particles with a diameter of 10, 20 and 30 μm in the fluid flow of a microchannel is investigated. The microchannel consists of a spiral region and a straight region under the influence of acoustic waves. In the spiral region, the particles under hydrodynamic effects undergo the initial separation; then the particles enter the straight region of the microchannel, and the final separation of the particles is done by the force generated and exerted through the acoustic waves. The effects of acoustic frequency and the number of spiral region loops on separation are investigated. The results show that for measured dimensions and parameters, at 1 MHz acoustic wave, when the number of loops is 2 for the spiral region, the particles at the end of the path are in a suitable position for separation. In addition, the results show that the separation of particles with this hybrid system is better than that done by the simple methods, and the separation rate can be as high as 100%
 </OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Acoustic wave</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Spiral microchannel</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Particle separation</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">microfluidics</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcme.iut.ac.ir/article_3208_2ef248c04979d6b3a7b283ec3dc32cca.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Isfahan University of Technology</PublisherName>
				<JournalTitle>Journal of Computational Methods in Engineering</JournalTitle>
				<Issn>2228-7698</Issn>
				<Volume>39</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Design of a Constrained Nonlinear Controller using Firefly Algorithm for Active Suspension System</ArticleTitle>
<VernacularTitle>Design of a Constrained Nonlinear Controller using Firefly Algorithm for Active Suspension System</VernacularTitle>
			<FirstPage>23</FirstPage>
			<LastPage>44</LastPage>
			<ELocationID EIdType="pii">3209</ELocationID>
			
<ELocationID EIdType="doi">10.47176/jcme.39.2.7461</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Z.</FirstName>
					<LastName>Z. Ahangari Sisi</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>M.</FirstName>
					<LastName>Mirzaei</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>S.</FirstName>
					<LastName>Rafatnia</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>B.</FirstName>
					<LastName>Alizadeh</LastName>
<Affiliation></Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</History>
		<Abstract>Active vehicle suspension system is designed to increase the ride comfort and road holding of vehicles. Due to limitations in the external force produced by actuator, the design problem encounters the constraint on the control input. In this paper, a novel nonlinear controller with the input constraint is designed for the active suspension system. In the proposed method, at first, a constrained multi-objective optimization problem is defined. In this problem, a performance index is defined as a weighted combination of the predicted responses of the nonlinear suspension system and control input. Then, this problem is solved by the modified firefly optimization algorithm to find the constrained optimal control input. To evaluate the performance of the proposed method, the results of the unconstrained and constrained controllers are provided and discussed for various road excitations. The results show a remarkable increase in the ride comfort with the limited force, while other suspension outputs including the suspension travel and tire deflection being in the acceptable ranges. In addition, these controllers are compared with Sliding Mode Control (SMC) and Nonlinear Model Predictive Control (NMPC) in the presence of model uncertainty.</Abstract>
			<OtherAbstract Language="FA">Active vehicle suspension system is designed to increase the ride comfort and road holding of vehicles. Due to limitations in the external force produced by actuator, the design problem encounters the constraint on the control input. In this paper, a novel nonlinear controller with the input constraint is designed for the active suspension system. In the proposed method, at first, a constrained multi-objective optimization problem is defined. In this problem, a performance index is defined as a weighted combination of the predicted responses of the nonlinear suspension system and control input. Then, this problem is solved by the modified firefly optimization algorithm to find the constrained optimal control input. To evaluate the performance of the proposed method, the results of the unconstrained and constrained controllers are provided and discussed for various road excitations. The results show a remarkable increase in the ride comfort with the limited force, while other suspension outputs including the suspension travel and tire deflection being in the acceptable ranges. In addition, these controllers are compared with Sliding Mode Control (SMC) and Nonlinear Model Predictive Control (NMPC) in the presence of model uncertainty.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Active suspension system</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Nonlinear control</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Constrained optimal control</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Input constraint</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Firefly algorithm</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcme.iut.ac.ir/article_3209_1271a7029c9df08643b631b02cf9e116.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Isfahan University of Technology</PublisherName>
				<JournalTitle>Journal of Computational Methods in Engineering</JournalTitle>
				<Issn>2228-7698</Issn>
				<Volume>39</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</Journal>
<ArticleTitle>A New Recursive Formulation for the Mixed Redundancy Strategy in Reliability Optimization Problems</ArticleTitle>
<VernacularTitle>A New Recursive Formulation for the Mixed Redundancy Strategy in Reliability Optimization Problems</VernacularTitle>
			<FirstPage>45</FirstPage>
			<LastPage>58</LastPage>
			<ELocationID EIdType="pii">3210</ELocationID>
			
<ELocationID EIdType="doi">10.47176/jcme.39.2.7471</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>M.</FirstName>
					<LastName>Abouei Ardakan</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>S.</FirstName>
					<LastName>Talkhabi</LastName>
<Affiliation></Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</History>
		<Abstract>One of the common approaches for improving the reliability of a specific system is to use parallel redundant components in subsystems. This approach, which is known as the redundancy allocation problem (RAP), includes the simultaneous selection of the component type and its level for each subsystem in order to maximize the system reliability.Traditionally, there are two redundancy strategies, namely active and standby, for the redundant components. Recently, a new powerful strategy called mixed strategy has been developed. It has been proved that the mixed strategy has a better performance when compared to both previous strategies. The main issue in utilizing the mixed strategy is its complicated formulation and sophisticated calculations, leading to a time-consuming procedure for solving the problems. Hence, in this paper, a new formulation based on the recursive approach is introduced to ease the calculation of the mixed strategy. In the new formulation, the complex double integral calculations are removed and the calculation times is reduced. The proposed recursive formulation provides a general statement for the mixed strategy formula which is not changed by altering the number of components in each subsystem. This flexibility and stability in the formula can be very important, especially for large scale cases. In order to evaluate the new approach and to compare its performances with the previous formulation, a benchmark problem with 14 subsystems is considered and the results of the two formulation are compared with each other.</Abstract>
			<OtherAbstract Language="FA">One of the common approaches for improving the reliability of a specific system is to use parallel redundant components in subsystems. This approach, which is known as the redundancy allocation problem (RAP), includes the simultaneous selection of the component type and its level for each subsystem in order to maximize the system reliability.Traditionally, there are two redundancy strategies, namely active and standby, for the redundant components. Recently, a new powerful strategy called mixed strategy has been developed. It has been proved that the mixed strategy has a better performance when compared to both previous strategies. The main issue in utilizing the mixed strategy is its complicated formulation and sophisticated calculations, leading to a time-consuming procedure for solving the problems. Hence, in this paper, a new formulation based on the recursive approach is introduced to ease the calculation of the mixed strategy. In the new formulation, the complex double integral calculations are removed and the calculation times is reduced. The proposed recursive formulation provides a general statement for the mixed strategy formula which is not changed by altering the number of components in each subsystem. This flexibility and stability in the formula can be very important, especially for large scale cases. In order to evaluate the new approach and to compare its performances with the previous formulation, a benchmark problem with 14 subsystems is considered and the results of the two formulation are compared with each other.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Reliability optimization</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Redundancy allocation problem</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Mixed strategy</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Recursive functions</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcme.iut.ac.ir/article_3210_731309c4bb223491a9f67eac5214fb2e.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Isfahan University of Technology</PublisherName>
				<JournalTitle>Journal of Computational Methods in Engineering</JournalTitle>
				<Issn>2228-7698</Issn>
				<Volume>39</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</Journal>
<ArticleTitle>The Nonlinear Bending Analysis for Circular Nano Plates Based on Modified Coupled Stress and Three- Dimensional Elasticity Theories</ArticleTitle>
<VernacularTitle>The Nonlinear Bending Analysis for Circular Nano Plates Based on Modified Coupled Stress and Three- Dimensional Elasticity Theories</VernacularTitle>
			<FirstPage>59</FirstPage>
			<LastPage>72</LastPage>
			<ELocationID EIdType="pii">3211</ELocationID>
			
<ELocationID EIdType="doi">10.47176/jcme.39.2.7491</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Z.</FirstName>
					<LastName>Barouei</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>M.</FirstName>
					<LastName>Jabbarzadeh</LastName>
<Affiliation></Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</History>
		<Abstract>In this paper, the nonlinear bending analysis for annular circular nano plates is conducted based on the modified coupled stress and three-dimensional elasticity theories. For this purpose, the equilibrium equations, considering nonlinear strain terms, are calculated using the least energy potential method and solved by the numerical semi-analytical polynomial method. According to the previous works, there have been no studies calculating all boundary conditions numerically based on three-dimensional elasticity. Typically, the research done on three-dimensional elasticity is either finite element or only for a simply-supported boundary condition. In this research, for the first time, the nonlinear analysis of bending is calculated with the help of three-dimensional elasticity for a variety of boundary conditions. Also, with the help of the modified couple stress theory, the results on the nano-scale scale have been studied. In the following, while validating the results, we investigate the changes in the scale parameter for the types of boundary conditions, the effect of changing the parameter of scale in different thicknesses, and the impact of the parameter of scale on the linear and nonlinear results.</Abstract>
			<OtherAbstract Language="FA">In this paper, the nonlinear bending analysis for annular circular nano plates is conducted based on the modified coupled stress and three-dimensional elasticity theories. For this purpose, the equilibrium equations, considering nonlinear strain terms, are calculated using the least energy potential method and solved by the numerical semi-analytical polynomial method. According to the previous works, there have been no studies calculating all boundary conditions numerically based on three-dimensional elasticity. Typically, the research done on three-dimensional elasticity is either finite element or only for a simply-supported boundary condition. In this research, for the first time, the nonlinear analysis of bending is calculated with the help of three-dimensional elasticity for a variety of boundary conditions. Also, with the help of the modified couple stress theory, the results on the nano-scale scale have been studied. In the following, while validating the results, we investigate the changes in the scale parameter for the types of boundary conditions, the effect of changing the parameter of scale in different thicknesses, and the impact of the parameter of scale on the linear and nonlinear results.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Nonlinear bending</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Circular Nano plates</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Three-dimensional elasticity theory</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Modified coupled stress</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Semi-analytical polynomial method</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcme.iut.ac.ir/article_3211_6b620aedfa4cf153467265629501dd61.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Isfahan University of Technology</PublisherName>
				<JournalTitle>Journal of Computational Methods in Engineering</JournalTitle>
				<Issn>2228-7698</Issn>
				<Volume>39</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Buckling Analysis of Variable Stiffness Composite Laminates by Semi-Analytical Finite Strip Method</ArticleTitle>
<VernacularTitle>Buckling Analysis of Variable Stiffness Composite Laminates by Semi-Analytical Finite Strip Method</VernacularTitle>
			<FirstPage>73</FirstPage>
			<LastPage>95</LastPage>
			<ELocationID EIdType="pii">3212</ELocationID>
			
<ELocationID EIdType="doi">10.47176/jcme.39.2.4912</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>R.</FirstName>
					<LastName>Keshavarzi</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>Sh.</FirstName>
					<LastName>Hatami</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>Sh.</FirstName>
					<LastName>Hashemi</LastName>
<Affiliation></Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</History>
		<Abstract>Plates made of laminated composite materials with variable stiffness can have wide applications in various branches of engineering due to such advantages as high strength /stiffness to weight ratio. In these composites, curved fibers are used to reinforce each lamina instead of the straight fibers. In this paper, the application of finite strip method for the buckling analysis of moderately thick composite plates with variable stiffness is investigated. For buckling analysis, a semi-analytical finite strip method based on the first-order shear deformation theory is employed. In this method, all displacements are presumed by the appropriate harmonic shape functions in the longitudinal direction and polynomial interpolation functions in the transverse direction. The minimum potential energy method has been used to develop the stability formulations. This analysis examines the effect of using curved fibers instead of straight fibers on the laminate composites. The critical loads obtained from this analysis are compared with those of other researchers and the efficiency and accuracy of the developed finite strip method are confirmed. Comparison of the analysis results of these plates shows that changing the slope of the fibers can lead to a significant change in the buckling response. Also, increasing the number of the terms of shape functions in the longitudinal direction has a significant effect on the convergence to the desired results.</Abstract>
			<OtherAbstract Language="FA">Plates made of laminated composite materials with variable stiffness can have wide applications in various branches of engineering due to such advantages as high strength /stiffness to weight ratio. In these composites, curved fibers are used to reinforce each lamina instead of the straight fibers. In this paper, the application of finite strip method for the buckling analysis of moderately thick composite plates with variable stiffness is investigated. For buckling analysis, a semi-analytical finite strip method based on the first-order shear deformation theory is employed. In this method, all displacements are presumed by the appropriate harmonic shape functions in the longitudinal direction and polynomial interpolation functions in the transverse direction. The minimum potential energy method has been used to develop the stability formulations. This analysis examines the effect of using curved fibers instead of straight fibers on the laminate composites. The critical loads obtained from this analysis are compared with those of other researchers and the efficiency and accuracy of the developed finite strip method are confirmed. Comparison of the analysis results of these plates shows that changing the slope of the fibers can lead to a significant change in the buckling response. Also, increasing the number of the terms of shape functions in the longitudinal direction has a significant effect on the convergence to the desired results.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Buckling</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Laminated composite</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Variable stiffness</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Finite Strip Method</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">First-order shear deformation theory</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcme.iut.ac.ir/article_3212_0aae0fede9a4d278e2f9a171e62fc76b.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Isfahan University of Technology</PublisherName>
				<JournalTitle>Journal of Computational Methods in Engineering</JournalTitle>
				<Issn>2228-7698</Issn>
				<Volume>39</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Estimation of the Stress Intensity Factors for Surface Cracks in Spherical Electrode Particles Subject to Phase Separation</ArticleTitle>
<VernacularTitle>Estimation of the Stress Intensity Factors for Surface Cracks in Spherical Electrode Particles Subject to Phase Separation</VernacularTitle>
			<FirstPage>97</FirstPage>
			<LastPage>117</LastPage>
			<ELocationID EIdType="pii">3213</ELocationID>
			
<ELocationID EIdType="doi">10.47176/jcme.39.2.7851</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>S.</FirstName>
					<LastName>Esmizadeh</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>H.</FirstName>
					<LastName>Haftbaradaran</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>F.</FirstName>
					<LastName>Mossaiby</LastName>
<Affiliation></Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</History>
		<Abstract>Experiments have frequently shown that phase separation in lithium-ion battery electrodes could lead to the formation of mechanical defects, hence causing capacity fading. The purpose of the present work has been to examine stress intensity factors for pre-existing surface cracks in spherical electrode particles during electrochemical deintercalation cycling using both analytical and numerical methods. To this end, we make use of a phase field model to examine the time-dependent evolution of the concentration and stress profiles in a phase separating spherical electrode particles. By using a geometrical approximation scheme proposed in the literature, stress intensity factors at the deepest point of the pre-existing surface cracks of semi-elliptical geometry are calculated with the aid of the well-established weight function method of fracture mechanics. By taking advantage of a sharp-interphase core-shell model, an analytical solution for the maximum stress intensity factors arising at the deepest point of the surface cracks during a complete deintercalation half-cycle is also developed. Numerical results for evolution of the concentration profile and the distribution of the hoop stresses in the particle are presented; further, the stress intensity factors found numerically based on the phase field model are compared with those predicted by the analytical core-shell model. The results of the numerical model suggest that the maximum stress intensity factor could significantly vary with changes in the surface flux, increasing potentially by a factor of two within the range of parameters considered here, when the concentration difference between the two phases is decreased.</Abstract>
			<OtherAbstract Language="FA">Experiments have frequently shown that phase separation in lithium-ion battery electrodes could lead to the formation of mechanical defects, hence causing capacity fading. The purpose of the present work has been to examine stress intensity factors for pre-existing surface cracks in spherical electrode particles during electrochemical deintercalation cycling using both analytical and numerical methods. To this end, we make use of a phase field model to examine the time-dependent evolution of the concentration and stress profiles in a phase separating spherical electrode particles. By using a geometrical approximation scheme proposed in the literature, stress intensity factors at the deepest point of the pre-existing surface cracks of semi-elliptical geometry are calculated with the aid of the well-established weight function method of fracture mechanics. By taking advantage of a sharp-interphase core-shell model, an analytical solution for the maximum stress intensity factors arising at the deepest point of the surface cracks during a complete deintercalation half-cycle is also developed. Numerical results for evolution of the concentration profile and the distribution of the hoop stresses in the particle are presented; further, the stress intensity factors found numerically based on the phase field model are compared with those predicted by the analytical core-shell model. The results of the numerical model suggest that the maximum stress intensity factor could significantly vary with changes in the surface flux, increasing potentially by a factor of two within the range of parameters considered here, when the concentration difference between the two phases is decreased.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Lithium ion battery</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Phase separation</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Phase field modeling</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Fracture mechanics</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcme.iut.ac.ir/article_3213_9bd5ee6fe55aaeb673025dbcb8f939c1.pdf</ArchiveCopySource>
</Article>

<Article>
<Journal>
				<PublisherName>Isfahan University of Technology</PublisherName>
				<JournalTitle>Journal of Computational Methods in Engineering</JournalTitle>
				<Issn>2228-7698</Issn>
				<Volume>39</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Solution of Harmonic Problems with Weak Singularities Using Equilibrated Basis Functions in Finite Element Method</ArticleTitle>
<VernacularTitle>Solution of Harmonic Problems with Weak Singularities Using Equilibrated Basis Functions in Finite Element Method</VernacularTitle>
			<FirstPage>119</FirstPage>
			<LastPage>146</LastPage>
			<ELocationID EIdType="pii">3214</ELocationID>
			
<ELocationID EIdType="doi">10.47176/jcme.39.2.6242</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>O.</FirstName>
					<LastName>Bateniparvar</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>N.</FirstName>
					<LastName>Noormohammadi</LastName>
<Affiliation></Affiliation>

</Author>
<Author>
					<FirstName>A. M.</FirstName>
					<LastName>Salehi</LastName>
<Affiliation></Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2022</Year>
					<Month>12</Month>
					<Day>31</Day>
				</PubDate>
			</History>
		<Abstract>In this paper, Equilibrated Singular Basis Functions (EqSBFs) are implemented in the framework of the Finite Element Method (FEM), which can approximately satisfy the harmonic PDE in homogeneous and heterogeneous media. EqSBFs are able to automatically reproduce the terms consistent with the singularity order in the vicinity of the singular point. The newly made bases are used as the complimentary enriching part along with the polynomial bases of the FEM to construct a new set of shape functions in the elements adjacent to the singular point. It will be shown that the use of the combined bases leads to the quality improvement of the solution function as well as its derivatives, especially in the vicinity of the singularity.</Abstract>
			<OtherAbstract Language="FA">In this paper, Equilibrated Singular Basis Functions (EqSBFs) are implemented in the framework of the Finite Element Method (FEM), which can approximately satisfy the harmonic PDE in homogeneous and heterogeneous media. EqSBFs are able to automatically reproduce the terms consistent with the singularity order in the vicinity of the singular point. The newly made bases are used as the complimentary enriching part along with the polynomial bases of the FEM to construct a new set of shape functions in the elements adjacent to the singular point. It will be shown that the use of the combined bases leads to the quality improvement of the solution function as well as its derivatives, especially in the vicinity of the singularity.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">singularity</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Harmonic</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Equilibrated basis functions</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">finite element method</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jcme.iut.ac.ir/article_3214_89d4402dc03d3b7318bbac10203034ab.pdf</ArchiveCopySource>
</Article>
</ArticleSet>
