Equivalent tensile elastic modulus measurement of cross-ply composite plates using S1 mode of Lamb wave
This paper proposes a simple and effective Lamb wave-based measurement method for the elastic moduli of cross-ply composite plates with large thickness, considered equivalent to a single-layer orthotropic plate with nine independent elastic constants. Due to the low-frequency signals required for me...
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Veröffentlicht in: | Journal of physics. Conference series 2024-09, Vol.2822 (1), p.012114 |
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creator | Zeng, Jiaqi Liu, Yaolu Jiang, Youqiang Wang, Yunlin Hu, Ning |
description | This paper proposes a simple and effective Lamb wave-based measurement method for the elastic moduli of cross-ply composite plates with large thickness, considered equivalent to a single-layer orthotropic plate with nine independent elastic constants. Due to the low-frequency signals required for measuring large thickness plates and the large wavelength of the low-frequency signals, the size of composite plates is highly required. Therefore, it is considered to use the first order symmetric (S1) mode wave to increase the signal frequency and reduce the wavelength. The effects of elastic constants on the phase velocities of the S1 mode are investigated. The phase velocity of the S1 mode depends only on the equivalent tensile elastic modulus and in-plane Poisson’s ratio in the low-dispersive frequency-thickness product regime. Moreover, the in-plane Poisson’s ratio of cross-ply laminates changes sufficiently small to neglect its effect on the phase velocities of the S1 mode. Therefore, the tensile elastic moduli of the cross-ply laminated plates can be estimated using the S1 mode, and the mapping relations between the phase velocities of S1 mode and the elastic moduli are established. The proposed approach has been numerically and experimentally tested on cross-ply glass fiber reinforced laminates with large thickness, and validated by theoretical values and conventional tensile tests. |
doi_str_mv | 10.1088/1742-6596/2822/1/012114 |
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Due to the low-frequency signals required for measuring large thickness plates and the large wavelength of the low-frequency signals, the size of composite plates is highly required. Therefore, it is considered to use the first order symmetric (S1) mode wave to increase the signal frequency and reduce the wavelength. The effects of elastic constants on the phase velocities of the S1 mode are investigated. The phase velocity of the S1 mode depends only on the equivalent tensile elastic modulus and in-plane Poisson’s ratio in the low-dispersive frequency-thickness product regime. Moreover, the in-plane Poisson’s ratio of cross-ply laminates changes sufficiently small to neglect its effect on the phase velocities of the S1 mode. Therefore, the tensile elastic moduli of the cross-ply laminated plates can be estimated using the S1 mode, and the mapping relations between the phase velocities of S1 mode and the elastic moduli are established. The proposed approach has been numerically and experimentally tested on cross-ply glass fiber reinforced laminates with large thickness, and validated by theoretical values and conventional tensile tests.</description><identifier>ISSN: 1742-6588</identifier><identifier>EISSN: 1742-6596</identifier><identifier>DOI: 10.1088/1742-6596/2822/1/012114</identifier><language>eng</language><publisher>Bristol: IOP Publishing</publisher><subject>Composite structures ; Elastic properties ; Equivalence ; Glass fibers ; Lamb waves ; Laminates ; Measurement methods ; Modulus of elasticity ; Orthotropic plates ; Phase velocity ; Tensile tests ; Thickness measurement</subject><ispartof>Journal of physics. Conference series, 2024-09, Vol.2822 (1), p.012114</ispartof><rights>Published under licence by IOP Publishing Ltd</rights><rights>Published under licence by IOP Publishing Ltd. This work is published under https://creativecommons.org/licenses/by/4.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://iopscience.iop.org/article/10.1088/1742-6596/2822/1/012114/pdf$$EPDF$$P50$$Giop$$Hfree_for_read</linktopdf><link.rule.ids>314,776,780,27901,27902,38845,38867,53815,53842</link.rule.ids></links><search><creatorcontrib>Zeng, Jiaqi</creatorcontrib><creatorcontrib>Liu, Yaolu</creatorcontrib><creatorcontrib>Jiang, Youqiang</creatorcontrib><creatorcontrib>Wang, Yunlin</creatorcontrib><creatorcontrib>Hu, Ning</creatorcontrib><title>Equivalent tensile elastic modulus measurement of cross-ply composite plates using S1 mode of Lamb wave</title><title>Journal of physics. Conference series</title><addtitle>J. Phys.: Conf. Ser</addtitle><description>This paper proposes a simple and effective Lamb wave-based measurement method for the elastic moduli of cross-ply composite plates with large thickness, considered equivalent to a single-layer orthotropic plate with nine independent elastic constants. Due to the low-frequency signals required for measuring large thickness plates and the large wavelength of the low-frequency signals, the size of composite plates is highly required. Therefore, it is considered to use the first order symmetric (S1) mode wave to increase the signal frequency and reduce the wavelength. The effects of elastic constants on the phase velocities of the S1 mode are investigated. The phase velocity of the S1 mode depends only on the equivalent tensile elastic modulus and in-plane Poisson’s ratio in the low-dispersive frequency-thickness product regime. Moreover, the in-plane Poisson’s ratio of cross-ply laminates changes sufficiently small to neglect its effect on the phase velocities of the S1 mode. Therefore, the tensile elastic moduli of the cross-ply laminated plates can be estimated using the S1 mode, and the mapping relations between the phase velocities of S1 mode and the elastic moduli are established. The proposed approach has been numerically and experimentally tested on cross-ply glass fiber reinforced laminates with large thickness, and validated by theoretical values and conventional tensile tests.</description><subject>Composite structures</subject><subject>Elastic properties</subject><subject>Equivalence</subject><subject>Glass fibers</subject><subject>Lamb waves</subject><subject>Laminates</subject><subject>Measurement methods</subject><subject>Modulus of elasticity</subject><subject>Orthotropic plates</subject><subject>Phase velocity</subject><subject>Tensile tests</subject><subject>Thickness measurement</subject><issn>1742-6588</issn><issn>1742-6596</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><sourceid>O3W</sourceid><sourceid>BENPR</sourceid><recordid>eNpFkFtLwzAUgIMoOKe_wYDPtTlJ2qSPMuYFBj6ozyHt0pGRNl3TTPz3NkzmeTkHzncufAjdA3kEImUOgtOsLKoyp5LSHHICFIBfoMW5c3mupbxGNyHsCWFziAXarQ_RHrUz_YQn0wfrDDZOh8k2uPPb6GLAndEhjqZLjG9xM_oQssH94MZ3gw92MnhwejIBx2D7Hf6ANGoSu9Fdjb_10dyiq1a7YO7-8hJ9Pa8_V6_Z5v3lbfW0yez8Nc8YbyrN67otCl4DsHJ-lG7LCmpgkjWkFkzSVnAhqpY2puW6qmTByy2IwoiSsSV6OO0dRn-IJkxq7-PYzycVmy8UsyJezhQ7UdYP_wAQlYyq5EolbyoZVaBORtkvwPxogw</recordid><startdate>20240901</startdate><enddate>20240901</enddate><creator>Zeng, Jiaqi</creator><creator>Liu, Yaolu</creator><creator>Jiang, Youqiang</creator><creator>Wang, Yunlin</creator><creator>Hu, Ning</creator><general>IOP Publishing</general><scope>O3W</scope><scope>TSCCA</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>H8D</scope><scope>HCIFZ</scope><scope>L7M</scope><scope>P5Z</scope><scope>P62</scope><scope>PIMPY</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope></search><sort><creationdate>20240901</creationdate><title>Equivalent tensile elastic modulus measurement of cross-ply composite plates using S1 mode of Lamb wave</title><author>Zeng, Jiaqi ; Liu, Yaolu ; Jiang, Youqiang ; Wang, Yunlin ; Hu, Ning</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-i1214-34c9a4bbf554b11360032d691b1383c0b7382f74779f2cef4a998546d175e7633</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Composite structures</topic><topic>Elastic properties</topic><topic>Equivalence</topic><topic>Glass fibers</topic><topic>Lamb waves</topic><topic>Laminates</topic><topic>Measurement methods</topic><topic>Modulus of elasticity</topic><topic>Orthotropic plates</topic><topic>Phase velocity</topic><topic>Tensile tests</topic><topic>Thickness measurement</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zeng, Jiaqi</creatorcontrib><creatorcontrib>Liu, Yaolu</creatorcontrib><creatorcontrib>Jiang, Youqiang</creatorcontrib><creatorcontrib>Wang, Yunlin</creatorcontrib><creatorcontrib>Hu, Ning</creatorcontrib><collection>Open Access: IOP Publishing Free Content</collection><collection>IOPscience (Open Access)</collection><collection>Technology Research Database</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>ProQuest Central (Alumni)</collection><collection>ProQuest Central UK/Ireland</collection><collection>Advanced Technologies & Aerospace Database (1962 - current)</collection><collection>ProQuest Central Essentials</collection><collection>AUTh Library subscriptions: ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central</collection><collection>Aerospace Database</collection><collection>SciTech Premium Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>ProQuest advanced technologies & aerospace journals</collection><collection>ProQuest Advanced Technologies & Aerospace Collection</collection><collection>Publicly Available Content Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><jtitle>Journal of physics. Conference series</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zeng, Jiaqi</au><au>Liu, Yaolu</au><au>Jiang, Youqiang</au><au>Wang, Yunlin</au><au>Hu, Ning</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Equivalent tensile elastic modulus measurement of cross-ply composite plates using S1 mode of Lamb wave</atitle><jtitle>Journal of physics. Conference series</jtitle><addtitle>J. Phys.: Conf. Ser</addtitle><date>2024-09-01</date><risdate>2024</risdate><volume>2822</volume><issue>1</issue><spage>012114</spage><pages>012114-</pages><issn>1742-6588</issn><eissn>1742-6596</eissn><abstract>This paper proposes a simple and effective Lamb wave-based measurement method for the elastic moduli of cross-ply composite plates with large thickness, considered equivalent to a single-layer orthotropic plate with nine independent elastic constants. Due to the low-frequency signals required for measuring large thickness plates and the large wavelength of the low-frequency signals, the size of composite plates is highly required. Therefore, it is considered to use the first order symmetric (S1) mode wave to increase the signal frequency and reduce the wavelength. The effects of elastic constants on the phase velocities of the S1 mode are investigated. The phase velocity of the S1 mode depends only on the equivalent tensile elastic modulus and in-plane Poisson’s ratio in the low-dispersive frequency-thickness product regime. Moreover, the in-plane Poisson’s ratio of cross-ply laminates changes sufficiently small to neglect its effect on the phase velocities of the S1 mode. Therefore, the tensile elastic moduli of the cross-ply laminated plates can be estimated using the S1 mode, and the mapping relations between the phase velocities of S1 mode and the elastic moduli are established. The proposed approach has been numerically and experimentally tested on cross-ply glass fiber reinforced laminates with large thickness, and validated by theoretical values and conventional tensile tests.</abstract><cop>Bristol</cop><pub>IOP Publishing</pub><doi>10.1088/1742-6596/2822/1/012114</doi><tpages>14</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Composite structures Elastic properties Equivalence Glass fibers Lamb waves Laminates Measurement methods Modulus of elasticity Orthotropic plates Phase velocity Tensile tests Thickness measurement |
title | Equivalent tensile elastic modulus measurement of cross-ply composite plates using S1 mode of Lamb wave |
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