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<ArticleSet>
<Article>
<Journal>
				<PublisherName>Amirkabir University of Technology</PublisherName>
				<JournalTitle>Amirkabir Journal of Mechanical Engineering</JournalTitle>
				<Issn>2008-6032</Issn>
				<Volume>54</Volume>
				<Issue>2</Issue>
				<PubDate PubStatus="epublish">
					<Year>2022</Year>
					<Month>04</Month>
					<Day>21</Day>
				</PubDate>
			</Journal>
<ArticleTitle>Investigation of Interlaminar Mode-I Fracture Toughness of Corrugated Composite Plates</ArticleTitle>
<VernacularTitle>Investigation of Interlaminar Mode-I Fracture Toughness of Corrugated Composite Plates</VernacularTitle>
			<FirstPage>415</FirstPage>
			<LastPage>432</LastPage>
			<ELocationID EIdType="pii">4679</ELocationID>
			
<ELocationID EIdType="doi">10.22060/mej.2022.20071.7163</ELocationID>
			
			<Language>FA</Language>
<AuthorList>
<Author>
					<FirstName>Sayed Amir</FirstName>
					<LastName>Safipour</LastName>
<Affiliation>Department of Mechanical Engineering, Kermanshah University of Technology, Kermanshah, Iran</Affiliation>

</Author>
<Author>
					<FirstName>Mahmood</FirstName>
					<LastName>Heshmati</LastName>
<Affiliation>Department of Mechanical Engineering, Kermanshah University of Technology, Kermanshah, Iran</Affiliation>

</Author>
</AuthorList>
				<PublicationType>Journal Article</PublicationType>
			<History>
				<PubDate PubStatus="received">
					<Year>2021</Year>
					<Month>05</Month>
					<Day>24</Day>
				</PubDate>
			</History>
		<Abstract>In this study, delamination of the corrugated composite plates made of unidirectional glass fibers and polyester resin has been investigated. The samples are fabricated by hand lay-up process based on the ASTM-D5528 standard. Using experimental tests, the strain energy release rate in mode I has been calculated for composite corrugated specimens by the prevalent method of interlaminar failure. Also, the samples were simulated as a double cantilever beam by Abaqus software, and the mechanical properties of unidirectional glass/polyester composite and the results of the numerical solution are also obtained. Fracture surfaces of experimental samples were analyzed by scanning electron microscope. Force-displacement curves obtained from experimental and numerical methods have been compared to find the material behavior and calculate the strain energy release rate for different samples with three pre-crack lengths. The results show that the corrugated composite plates have a higher interlaminar fracture toughness rather than flat samples and the four-wave sample with a crack length of 60 and 65 mm has the highest values of the strain energy rate released, equal to 963.77  J/m&lt;sup&gt;2&lt;/sup&gt; and 705.95  J/m&lt;sup&gt;2&lt;/sup&gt;, respectively.</Abstract>
			<OtherAbstract Language="FA">In this study, delamination of the corrugated composite plates made of unidirectional glass fibers and polyester resin has been investigated. The samples are fabricated by hand lay-up process based on the ASTM-D5528 standard. Using experimental tests, the strain energy release rate in mode I has been calculated for composite corrugated specimens by the prevalent method of interlaminar failure. Also, the samples were simulated as a double cantilever beam by Abaqus software, and the mechanical properties of unidirectional glass/polyester composite and the results of the numerical solution are also obtained. Fracture surfaces of experimental samples were analyzed by scanning electron microscope. Force-displacement curves obtained from experimental and numerical methods have been compared to find the material behavior and calculate the strain energy release rate for different samples with three pre-crack lengths. The results show that the corrugated composite plates have a higher interlaminar fracture toughness rather than flat samples and the four-wave sample with a crack length of 60 and 65 mm has the highest values of the strain energy rate released, equal to 963.77  J/m&lt;sup&gt;2&lt;/sup&gt; and 705.95  J/m&lt;sup&gt;2&lt;/sup&gt;, respectively.</OtherAbstract>
		<ObjectList>
			<Object Type="keyword">
			<Param Name="value">Corrugated composite plates</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">delamination</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">Fracture Toughness</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">strain energy</Param>
			</Object>
			<Object Type="keyword">
			<Param Name="value">failure mode I</Param>
			</Object>
		</ObjectList>
<ArchiveCopySource DocType="pdf">https://mej.aut.ac.ir/article_4679_97788494d0cb9c4ad37af9a76290b361.pdf</ArchiveCopySource>
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