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<ArticleSet>
<Article>
<Journal>
				<PublisherName>Sharif University of Technology</PublisherName>
				<JournalTitle>Scientia Iranica</JournalTitle>
				<Issn>1026-3098</Issn>
				<Volume>21</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2014</Year>
					<Month>04</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Free-edge Stresses in General Cross-ply Laminates</ArticleTitle>
<VernacularTitle>Free-edge Stresses in General Cross-ply Laminates</VernacularTitle>
			<FirstPage>387</FirstPage>
			<LastPage>402</LastPage>
			<ELocationID EIdType="pii">3490</ELocationID>
			
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>Hamidreza</FirstName>
					<LastName>Yazdani Sarvestani</LastName>
<Affiliation>Department of Mechanical Engineering, Sharif University of Technology, P.O. Box 11365-9567, Azadi Avenue, Tehran, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2013</Year>
					<Month>09</Month>
					<Day>29</Day>
				</PubDate>
			</History>
		<Abstract>Within the elasticity theory the reduced form of displacement field is obtained for general cross-ply composite laminates subjected to a bending moment. The first-order shear deformation theory of plates and Reddy’s layerwise theory are then utilized to determine the global deformation parameters and the local deformation parameters appearing in the displacement fields, respectively. For special set of boundary conditions an elasticity solution is developed to verify the validity and accuracy of the layerwise theory. Finally, various numerical results are presented within the layerwise theory for edge-effect problems of several cross-ply laminates under the bending moment. The results indicate high stress gradients of interlaminar stresses near the edges of laminates.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">General cross-ply laminate</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Interlaminar stresses</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Elasticity formulation</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">First order shear deformation plate theory</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Layerwise theory</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://scientiairanica.sharif.edu/article_3490_6d57996fa1c73b6c179139e8a2e77711.pdf</ArchiveCopySource>
</Article>
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