A simple equivalent plate model for dynamic bending stiffness of three-layer sandwich panels with shearing core
Equivalent or condensed plate models are being used in various industries to reduce the computation time in finite element modelling. Out of the available equivalent plate models, the model developed by J.L. Guyader in 1978 exhibits high agreement with Lamb wave theory but it requires some time for...
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Veröffentlicht in: | Journal of sound and vibration 2021-05, Vol.500, p.116025, Article 116025 |
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creator | Arasan, U. Marchetti, F. Chevillotte, F. Jaouen, L. Chronopoulos, D. Gourdon, E. |
description | Equivalent or condensed plate models are being used in various industries to reduce the computation time in finite element modelling. Out of the available equivalent plate models, the model developed by J.L. Guyader in 1978 exhibits high agreement with Lamb wave theory but it requires some time for implementation. Therefore, in this paper, a simple model is proposed to quickly compute the dynamic equivalent parameters of a three-layer sandwich panel. Although the model is formulated from only four parameters, which could be easily computed via the asymptotic and transition behaviours of the sandwich panel, it is shown to be able to capture the equivalent dynamic response for the entire frequency range. |
doi_str_mv | 10.1016/j.jsv.2021.116025 |
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Out of the available equivalent plate models, the model developed by J.L. Guyader in 1978 exhibits high agreement with Lamb wave theory but it requires some time for implementation. Therefore, in this paper, a simple model is proposed to quickly compute the dynamic equivalent parameters of a three-layer sandwich panel. 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Although the model is formulated from only four parameters, which could be easily computed via the asymptotic and transition behaviours of the sandwich panel, it is shown to be able to capture the equivalent dynamic response for the entire frequency range.</description><subject>Engineering Sciences</subject><subject>Equivalent plate model</subject><subject>Flexural rigidities</subject><subject>Sandwich panels</subject><subject>Wavenumbers</subject><issn>0022-460X</issn><issn>1095-8568</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNp9kE1Lw0AURQdRsFZ_gLvZukidr0waXJWiVii4UXA3vMy8MRPSpM7Elv57GyouXV143PPgHkJuOZtxxvV9M2vSbiaY4DPONRP5GZlwVubZPNfzczJhTIhMafZxSa5SahhjpZJqQvoFTWGzbZHi13fYQYvdQLctDEg3vcOW-j5Sd-hgEyytsHOh-6RpCN53mBLtPR3qiJi1cMBIE3RuH2xNt9Bhm-g-DDVNNUIcMdtHvCYXHtqEN785Je9Pj2_LVbZ-fX5ZLtaZlYUasrLyJePgKgWVEE5VUsBcA1eSu8KDznOhvNKgK1dIUEUpK51LLnPLURa2klNyd_pbQ2u2MWwgHkwPwawWazPemCwYLwXb8WOXn7o29ilF9H8AZ2a0axpztGtGu-Zk98g8nJjjTNwFjCbZgJ1FFyLawbg-_EP_ADu5g3Y</recordid><startdate>20210526</startdate><enddate>20210526</enddate><creator>Arasan, U.</creator><creator>Marchetti, F.</creator><creator>Chevillotte, F.</creator><creator>Jaouen, L.</creator><creator>Chronopoulos, D.</creator><creator>Gourdon, E.</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>AAYXX</scope><scope>CITATION</scope><scope>1XC</scope><scope>VOOES</scope><orcidid>https://orcid.org/0000-0002-6746-4403</orcidid></search><sort><creationdate>20210526</creationdate><title>A simple equivalent plate model for dynamic bending stiffness of three-layer sandwich panels with shearing core</title><author>Arasan, U. ; Marchetti, F. ; Chevillotte, F. ; Jaouen, L. ; Chronopoulos, D. ; Gourdon, E.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c374t-9bf901adb4ab22d4b32a86a1431d7fa65524f46a6bd73a4793b653135c1e37cb3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Engineering Sciences</topic><topic>Equivalent plate model</topic><topic>Flexural rigidities</topic><topic>Sandwich panels</topic><topic>Wavenumbers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Arasan, U.</creatorcontrib><creatorcontrib>Marchetti, F.</creatorcontrib><creatorcontrib>Chevillotte, F.</creatorcontrib><creatorcontrib>Jaouen, L.</creatorcontrib><creatorcontrib>Chronopoulos, D.</creatorcontrib><creatorcontrib>Gourdon, E.</creatorcontrib><collection>CrossRef</collection><collection>Hyper Article en Ligne (HAL)</collection><collection>Hyper Article en Ligne (HAL) (Open Access)</collection><jtitle>Journal of sound and vibration</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Arasan, U.</au><au>Marchetti, F.</au><au>Chevillotte, F.</au><au>Jaouen, L.</au><au>Chronopoulos, D.</au><au>Gourdon, E.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A simple equivalent plate model for dynamic bending stiffness of three-layer sandwich panels with shearing core</atitle><jtitle>Journal of sound and vibration</jtitle><date>2021-05-26</date><risdate>2021</risdate><volume>500</volume><spage>116025</spage><pages>116025-</pages><artnum>116025</artnum><issn>0022-460X</issn><eissn>1095-8568</eissn><abstract>Equivalent or condensed plate models are being used in various industries to reduce the computation time in finite element modelling. Out of the available equivalent plate models, the model developed by J.L. Guyader in 1978 exhibits high agreement with Lamb wave theory but it requires some time for implementation. Therefore, in this paper, a simple model is proposed to quickly compute the dynamic equivalent parameters of a three-layer sandwich panel. Although the model is formulated from only four parameters, which could be easily computed via the asymptotic and transition behaviours of the sandwich panel, it is shown to be able to capture the equivalent dynamic response for the entire frequency range.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.jsv.2021.116025</doi><orcidid>https://orcid.org/0000-0002-6746-4403</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | Engineering Sciences Equivalent plate model Flexural rigidities Sandwich panels Wavenumbers |
title | A simple equivalent plate model for dynamic bending stiffness of three-layer sandwich panels with shearing core |
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