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Experimental and numerical investigation of debonding in the composite sandwich structures with a foam-composite core under TPSB test
In the present study, the delamination between the face sheet and core in the sandwich structures with a hybrid corrugated core in the mix mode of failure under the three-point sandwich beam (TPSB) test is evaluated numerically and experimentally. The system response for different cores of the sandw...
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Published in: | Journal of the Brazilian Society of Mechanical Sciences and Engineering 2022-12, Vol.44 (12), Article 604 |
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container_title | Journal of the Brazilian Society of Mechanical Sciences and Engineering |
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creator | Vahidi Bidhendi, Mohammad Rahimi, Gholam Hosein Gazor, Mohammad Sajjad Zangoei, Amir Reza |
description | In the present study, the delamination between the face sheet and core in the sandwich structures with a hybrid corrugated core in the mix mode of failure under the three-point sandwich beam (TPSB) test is evaluated numerically and experimentally. The system response for different cores of the sandwich structure is compared to each other. By performing the experimental tests, the samples with different corrugated are scrutinized from various aspects, including the force–displacement diagram and the strain energy release rate diagram relative to the crack length. ABAQUS finite element software and CZM (cohesive zone modeling) method are used for numerical analysis. It is disclosed that in the studied systems, the more crack length, the more the amount of strain energy release rate, so that is generally an upwards trend in the mix-mode of failure. Additionally, it should be noted that the charts drop sharply after reaching their maximum strain energy release rate. Finally, the load–displacement curves of the specimens are extracted and compared to those of experimental data. The outcomes of the present investigation provide valuable practical tips for engineers and designers in designing composite sandwich structures. |
doi_str_mv | 10.1007/s40430-022-03907-y |
format | article |
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Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.</rights><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c319t-9edd03564ac442ab30fc49e72fb39720a5ff44b5336cf261a7c5ce04f47eedc53</citedby><cites>FETCH-LOGICAL-c319t-9edd03564ac442ab30fc49e72fb39720a5ff44b5336cf261a7c5ce04f47eedc53</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Vahidi Bidhendi, Mohammad</creatorcontrib><creatorcontrib>Rahimi, Gholam Hosein</creatorcontrib><creatorcontrib>Gazor, Mohammad Sajjad</creatorcontrib><creatorcontrib>Zangoei, Amir Reza</creatorcontrib><title>Experimental and numerical investigation of debonding in the composite sandwich structures with a foam-composite core under TPSB test</title><title>Journal of the Brazilian Society of Mechanical Sciences and Engineering</title><addtitle>J Braz. Soc. Mech. Sci. Eng</addtitle><description>In the present study, the delamination between the face sheet and core in the sandwich structures with a hybrid corrugated core in the mix mode of failure under the three-point sandwich beam (TPSB) test is evaluated numerically and experimentally. The system response for different cores of the sandwich structure is compared to each other. By performing the experimental tests, the samples with different corrugated are scrutinized from various aspects, including the force–displacement diagram and the strain energy release rate diagram relative to the crack length. ABAQUS finite element software and CZM (cohesive zone modeling) method are used for numerical analysis. It is disclosed that in the studied systems, the more crack length, the more the amount of strain energy release rate, so that is generally an upwards trend in the mix-mode of failure. Additionally, it should be noted that the charts drop sharply after reaching their maximum strain energy release rate. Finally, the load–displacement curves of the specimens are extracted and compared to those of experimental data. The outcomes of the present investigation provide valuable practical tips for engineers and designers in designing composite sandwich structures.</description><subject>Beams (structural)</subject><subject>Corrugated sheet</subject><subject>Delamination</subject><subject>Engineering</subject><subject>Finite element method</subject><subject>Mathematical models</subject><subject>Mechanical Engineering</subject><subject>Numerical analysis</subject><subject>Sandwich structures</subject><subject>Strain energy release rate</subject><subject>Technical Paper</subject><issn>1678-5878</issn><issn>1806-3691</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp9kMtKAzEUhgdRUKsv4CrgOnpymUlnqcUbCArqOqSZk3aKTWqSUfsAvrfRCt25Orf_Pz98VXXC4IwBqPMkQQqgwDkF0YKi653qgI2hoaJp2W7pGzWm9ViN96vDlBYAgtdNfVB9XX2uMPZL9Nm8EuM74odlWdgy9f4dU-5nJvfBk-BIh9Pgu97PyonkORIblquQ-owkFetHb-ck5TjYPERM5KPPc2KIC2ZJt0obIpLBdxjJ8-PTJckl46jac-Y14fFfHVUv11fPk1t6_3BzN7m4p1awNtMWuw5E3UhjpeRmKsBZ2aLibipaxcHUzkk5rYVorOMNM8rWFkE6qRA7W4tRdbr5u4rhbSjBehGG6Euk5koyYCCbtqj4RmVjSCmi06tCyMS1ZqB_cOsNbl1w61_cel1MYmNKRexnGLev_3F9A_2zhps</recordid><startdate>20221201</startdate><enddate>20221201</enddate><creator>Vahidi Bidhendi, Mohammad</creator><creator>Rahimi, Gholam Hosein</creator><creator>Gazor, Mohammad Sajjad</creator><creator>Zangoei, Amir Reza</creator><general>Springer Berlin Heidelberg</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20221201</creationdate><title>Experimental and numerical investigation of debonding in the composite sandwich structures with a foam-composite core under TPSB test</title><author>Vahidi Bidhendi, Mohammad ; Rahimi, Gholam Hosein ; Gazor, Mohammad Sajjad ; Zangoei, Amir Reza</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c319t-9edd03564ac442ab30fc49e72fb39720a5ff44b5336cf261a7c5ce04f47eedc53</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Beams (structural)</topic><topic>Corrugated sheet</topic><topic>Delamination</topic><topic>Engineering</topic><topic>Finite element method</topic><topic>Mathematical models</topic><topic>Mechanical Engineering</topic><topic>Numerical analysis</topic><topic>Sandwich structures</topic><topic>Strain energy release rate</topic><topic>Technical Paper</topic><toplevel>online_resources</toplevel><creatorcontrib>Vahidi Bidhendi, Mohammad</creatorcontrib><creatorcontrib>Rahimi, Gholam Hosein</creatorcontrib><creatorcontrib>Gazor, Mohammad Sajjad</creatorcontrib><creatorcontrib>Zangoei, Amir Reza</creatorcontrib><collection>CrossRef</collection><jtitle>Journal of the Brazilian Society of Mechanical Sciences and Engineering</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Vahidi Bidhendi, Mohammad</au><au>Rahimi, Gholam Hosein</au><au>Gazor, Mohammad Sajjad</au><au>Zangoei, Amir Reza</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental and numerical investigation of debonding in the composite sandwich structures with a foam-composite core under TPSB test</atitle><jtitle>Journal of the Brazilian Society of Mechanical Sciences and Engineering</jtitle><stitle>J Braz. 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It is disclosed that in the studied systems, the more crack length, the more the amount of strain energy release rate, so that is generally an upwards trend in the mix-mode of failure. Additionally, it should be noted that the charts drop sharply after reaching their maximum strain energy release rate. Finally, the load–displacement curves of the specimens are extracted and compared to those of experimental data. The outcomes of the present investigation provide valuable practical tips for engineers and designers in designing composite sandwich structures.</abstract><cop>Berlin/Heidelberg</cop><pub>Springer Berlin Heidelberg</pub><doi>10.1007/s40430-022-03907-y</doi></addata></record> |
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subjects | Beams (structural) Corrugated sheet Delamination Engineering Finite element method Mathematical models Mechanical Engineering Numerical analysis Sandwich structures Strain energy release rate Technical Paper |
title | Experimental and numerical investigation of debonding in the composite sandwich structures with a foam-composite core under TPSB test |
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