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<!DOCTYPE ArticleSet PUBLIC "-//NLM//DTD PubMed 2.7//EN" "https://dtd.nlm.nih.gov/ncbi/pubmed/in/PubMed.dtd">
<ArticleSet>
<Article>
<Journal>
				<PublisherName>Sharif University of Technology</PublisherName>
				<JournalTitle>Scientia Iranica</JournalTitle>
				<Issn>1026-3098</Issn>
				<Volume>25</Volume>
				<Issue>5</Issue>
				<PubDate PubStatus="epublish">
					<Year>2018</Year>
					<Month>10</Month>
					<Day>01</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Investigation into stiffness degradation progress in glass/vinylester laminated beams under large deformations</ArticleTitle>
<VernacularTitle></VernacularTitle>
			<FirstPage>2389</FirstPage>
			<LastPage>2403</LastPage>
			<ELocationID EIdType="pii">4220</ELocationID>
			
<ELocationID EIdType="doi">10.24200/sci.2017.4220</ELocationID>
			
			<Language>EN</Language>
<AuthorList>
<Author>
					<FirstName>A. R.</FirstName>
					<LastName>Nazari</LastName>
<Affiliation>Department of
Civil and Environmental Engineering, Amirkabir University of Technology, Tehr
an, Ira</Affiliation>

</Author>
<Author>
					<FirstName>Mohammad Z.</FirstName>
					<LastName>Kabir</LastName>
<Affiliation>Department of Civil Engineering, AmirKabir University of Technology, Tehran, Iran</Affiliation>

</Author>
<Author>
					<FirstName>H.</FirstName>
					<LastName>Hosseini - Toudeshky</LastName>
<Affiliation>Department of
Aerospace Engineering, Amirkabir University of Technology,
Tehran, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2015</Year>
					<Month>10</Month>
					<Day>05</Day>
				</PubDate>
			</History>
		<Abstract>There are many reports indicating that the maximum measured stress in the composite laminated beams under flexural loading appears different from that under tensile loading. The current study compares the results of Hashin failure criteria in the form of stress and strain components for prediction of failure strength in GFRP laminated beams. In the experimental program the composite laminates were tested under tensile and three-point-bending (3PB) loads. Then, it was trying to predict the flexural failure in laminates based on the measured ultimate stresses and strains in the tensile tests. The strain-based failure criteria employed in the FE models could achieve more admissible predictions for maximum load carrying capacity in the laminates compared to the stress-based criteria. Progressive failure analyses showed that due to higher elastic modulus of laminates under bending load, the maximum experienced stress under bending load becomes larger.</Abstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Flexural strength</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">GFRP laminate</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Progressive failure</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Hashin criteria</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Large deformations</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://scientiairanica.sharif.edu/article_4220_35d02fef7d9a24e237057162abab82b7.pdf</ArchiveCopySource>
</Article>
</ArticleSet>
