<?xml version="1.0" encoding="UTF-8"?>
<!DOCTYPE ArticleSet PUBLIC "-//NLM//DTD PubMed 2.7//EN" "https://dtd.nlm.nih.gov/ncbi/pubmed/in/PubMed.dtd">
<ArticleSet>
<Article>
<Journal>
				<PublisherName>Shahrood University of Technology</PublisherName>
				<JournalTitle>Journal of Solid and Fluid Mechanics</JournalTitle>
				<Issn>2251-9475</Issn>
				<Volume>10</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2020</Year>
					<Month>06</Month>
					<Day>21</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Layered finite element analysis of laminated composite plates by using unsymmetric membrane element and non-conforming bending element</ArticleTitle>
<VernacularTitle>Layered finite element analysis of laminated composite plates by using unsymmetric membrane element and non-conforming bending element</VernacularTitle>
			<FirstPage>141</FirstPage>
			<LastPage>152</LastPage>
			<ELocationID EIdType="pii">1870</ELocationID>
			
<ELocationID EIdType="doi">10.22044/jsfm.2020.9230.3085</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>H.</FirstName>
					<LastName>Sangtarash</LastName>
<Affiliation>Civil Engineering, Sistan and Baluchestan University, Zahedan, Iran.</Affiliation>

</Author>
<Author>
					<FirstName>H.</FirstName>
					<LastName>Ghohani Arab</LastName>
<Affiliation>Civil Engineering, Sistan and Baluchestan University, Zahedan, Iran.</Affiliation>

</Author>
<Author>
					<FirstName>M. R</FirstName>
					<LastName>Sohrabi</LastName>
<Affiliation>Civil Engineering, Sistan and Baluchestan University, Zahedan, Iran.</Affiliation>

</Author>
<Author>
					<FirstName>M.R.</FirstName>
					<LastName>Ghasemi</LastName>
<Affiliation>Civil Engineering, Sistan and Baluchestan University, Zahedan, Iran.</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2019</Year>
					<Month>12</Month>
					<Day>27</Day>
				</PubDate>
			</History>
		<Abstract>This study presents a new quadrilateral element for layered finite element analysis of laminated composite plates which is obtained through assemblage of membrane and plate bending elements. The membrane component is a new unsymmetric quadrilateral element with drilling degrees of freedom, in which two different types of displacement fields are used as the test and trial functions. The test function is a new kind of displacement field with drilling degrees of freedom obtained by using interpolation along the element edges. The trial function is a stress field computed through analytical solutions of Airy stress function. The bending component of lroposed element is a non-conforming plate element that its displacement is computed using third-order deformation modes and the rotational field of element is defined by using first-order Jacobean matrix. The results of numerical benchmark problems show that the the proposed element is capable for analysis of laminated composite plates with varius geometry and boundary. The maximum error of the proposed element among the considered numerical problems is only 1.5 percent.</Abstract>
			<OtherAbstract Language="FA">This study presents a new quadrilateral element for layered finite element analysis of laminated composite plates which is obtained through assemblage of membrane and plate bending elements. The membrane component is a new unsymmetric quadrilateral element with drilling degrees of freedom, in which two different types of displacement fields are used as the test and trial functions. The test function is a new kind of displacement field with drilling degrees of freedom obtained by using interpolation along the element edges. The trial function is a stress field computed through analytical solutions of Airy stress function. The bending component of lroposed element is a non-conforming plate element that its displacement is computed using third-order deformation modes and the rotational field of element is defined by using first-order Jacobean matrix. The results of numerical benchmark problems show that the the proposed element is capable for analysis of laminated composite plates with varius geometry and boundary. The maximum error of the proposed element among the considered numerical problems is only 1.5 percent.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Laminated composite plates</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Numerical Analysis</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Layered finite element method</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Membrane element</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://jsfm.shahroodut.ac.ir/article_1870_468a611bb4e73c282a538272d786eddf.pdf</ArchiveCopySource>
</Article>
</ArticleSet>
