Determination of the maximum strains experienced by composite structures using metal coated optical fiber sensors
A determination technique for the maximum strains experienced by composites is proposed using the permanent deformation characteristics of elasto-plastic metal-coated optical fiber sensors (OFSs). In order to confirm their feasibility, both analytical and experimental approaches were undertaken. In...
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Veröffentlicht in: | Composites science and technology 2013-04, Vol.78, p.48-55 |
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creator | Kim, Sang-Woo Jeong, Min-Soo Lee, In Kim, Eun-Ho Kwon, Il-Bum Hwang, Tae-Kyung |
description | A determination technique for the maximum strains experienced by composites is proposed using the permanent deformation characteristics of elasto-plastic metal-coated optical fiber sensors (OFSs). In order to confirm their feasibility, both analytical and experimental approaches were undertaken. In the analysis, a theoretical model for a surface-mounted OFS on the composite was proposed, and the strain transfer relations were derived. Moreover, novel numerical methods were implemented in order to evaluate the residual strain distribution. The analytical results were validated through a finite element analysis (FEA) using the ABAQUS software. We found that the residual strain increases as the coating thickness and external strain increase. In addition, the required gauge length for the given bonding length of the OFSs is proposed. In the experiment, fiber Bragg grating (FBG) sensors were applied to carbon fiber reinforced polymer (CFRP) composite specimens in order to verify the proposed technique. The trends of the residual strain, which are corresponding to the maximum strains experienced by the composite specimens, were consistent with those obtained in the analysis. |
doi_str_mv | 10.1016/j.compscitech.2013.01.010 |
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In order to confirm their feasibility, both analytical and experimental approaches were undertaken. In the analysis, a theoretical model for a surface-mounted OFS on the composite was proposed, and the strain transfer relations were derived. Moreover, novel numerical methods were implemented in order to evaluate the residual strain distribution. The analytical results were validated through a finite element analysis (FEA) using the ABAQUS software. We found that the residual strain increases as the coating thickness and external strain increase. In addition, the required gauge length for the given bonding length of the OFSs is proposed. In the experiment, fiber Bragg grating (FBG) sensors were applied to carbon fiber reinforced polymer (CFRP) composite specimens in order to verify the proposed technique. The trends of the residual strain, which are corresponding to the maximum strains experienced by the composite specimens, were consistent with those obtained in the analysis.</description><identifier>ISSN: 0266-3538</identifier><identifier>EISSN: 1879-1050</identifier><identifier>DOI: 10.1016/j.compscitech.2013.01.010</identifier><identifier>CODEN: CSTCEH</identifier><language>eng</language><publisher>Kidlington: Elsevier Ltd</publisher><subject>A. Coating ; Applied sciences ; B. Plastic deformation ; C. Stress transfer ; Carbon fiber reinforced plastics ; D. 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In order to confirm their feasibility, both analytical and experimental approaches were undertaken. In the analysis, a theoretical model for a surface-mounted OFS on the composite was proposed, and the strain transfer relations were derived. Moreover, novel numerical methods were implemented in order to evaluate the residual strain distribution. The analytical results were validated through a finite element analysis (FEA) using the ABAQUS software. We found that the residual strain increases as the coating thickness and external strain increase. In addition, the required gauge length for the given bonding length of the OFSs is proposed. In the experiment, fiber Bragg grating (FBG) sensors were applied to carbon fiber reinforced polymer (CFRP) composite specimens in order to verify the proposed technique. The trends of the residual strain, which are corresponding to the maximum strains experienced by the composite specimens, were consistent with those obtained in the analysis.</description><subject>A. Coating</subject><subject>Applied sciences</subject><subject>B. Plastic deformation</subject><subject>C. Stress transfer</subject><subject>Carbon fiber reinforced plastics</subject><subject>D. Non-destructive testing</subject><subject>Exact sciences and technology</subject><subject>Finite element method</subject><subject>Forms of application and semi-finished materials</subject><subject>Laminates</subject><subject>Mathematical analysis</subject><subject>Mathematical models</subject><subject>Optical fibers</subject><subject>Polymer industry, paints, wood</subject><subject>Sensors</subject><subject>Strain</subject><subject>Strain distribution</subject><subject>Technology of polymers</subject><issn>0266-3538</issn><issn>1879-1050</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2013</creationdate><recordtype>article</recordtype><recordid>eNqNkU9r3DAQxUVpINtNvoN6CPTi7Uiy_OcYNk1TCPTSnIUsjxMta8urkUPy7avthpJbCyOE4Kf3mPcY-yxgI0BUX3cbF8aZnE_onjYShNqAyAMf2Eo0dVsI0PCRrUBWVaG0as7ZJ6IdANS6lSt2uMGEcfSTTT5MPAw8PSEf7Ysfl5FTitZPxPFlxuhxctjz7pUfLQNlyyOwuLREJL6Qnx75iMnuM2BTRsOcvMvPwXcYOeFEIdIFOxvsnvDy7V6zh9tvv7Z3xf3P7z-21_eFK3WZClla6XpdKd3bvu1cV0rRq1brbnDSWWsloKrbrpW1zKcbhLYOhe6ggbrppVqzLyfdOYbDgpTM6Mnhfm8nDAsZoaFSjYZW_xsty6aGpqrLjLYn1MVAFHEwc_Sjja9GgDk2YnbmXSPm2IgBkQfy36s3G0s5liHayXn6K5AXkaCkytz2xGGO59ljNFntT_g-okumD_4_3H4D9l-qKg</recordid><startdate>20130401</startdate><enddate>20130401</enddate><creator>Kim, Sang-Woo</creator><creator>Jeong, Min-Soo</creator><creator>Lee, In</creator><creator>Kim, Eun-Ho</creator><creator>Kwon, Il-Bum</creator><creator>Hwang, Tae-Kyung</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>7SR</scope><scope>8FD</scope><scope>JG9</scope><scope>L7M</scope></search><sort><creationdate>20130401</creationdate><title>Determination of the maximum strains experienced by composite structures using metal coated optical fiber sensors</title><author>Kim, Sang-Woo ; Jeong, Min-Soo ; Lee, In ; Kim, Eun-Ho ; Kwon, Il-Bum ; Hwang, Tae-Kyung</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c454t-24a2cd5635dad9bcb421d3955bfc2caaa20e379b9272927bf15ace15b08078d23</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2013</creationdate><topic>A. Coating</topic><topic>Applied sciences</topic><topic>B. Plastic deformation</topic><topic>C. Stress transfer</topic><topic>Carbon fiber reinforced plastics</topic><topic>D. Non-destructive testing</topic><topic>Exact sciences and technology</topic><topic>Finite element method</topic><topic>Forms of application and semi-finished materials</topic><topic>Laminates</topic><topic>Mathematical analysis</topic><topic>Mathematical models</topic><topic>Optical fibers</topic><topic>Polymer industry, paints, wood</topic><topic>Sensors</topic><topic>Strain</topic><topic>Strain distribution</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Kim, Sang-Woo</creatorcontrib><creatorcontrib>Jeong, Min-Soo</creatorcontrib><creatorcontrib>Lee, In</creatorcontrib><creatorcontrib>Kim, Eun-Ho</creatorcontrib><creatorcontrib>Kwon, Il-Bum</creatorcontrib><creatorcontrib>Hwang, Tae-Kyung</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Composites science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Kim, Sang-Woo</au><au>Jeong, Min-Soo</au><au>Lee, In</au><au>Kim, Eun-Ho</au><au>Kwon, Il-Bum</au><au>Hwang, Tae-Kyung</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Determination of the maximum strains experienced by composite structures using metal coated optical fiber sensors</atitle><jtitle>Composites science and technology</jtitle><date>2013-04-01</date><risdate>2013</risdate><volume>78</volume><spage>48</spage><epage>55</epage><pages>48-55</pages><issn>0266-3538</issn><eissn>1879-1050</eissn><coden>CSTCEH</coden><abstract>A determination technique for the maximum strains experienced by composites is proposed using the permanent deformation characteristics of elasto-plastic metal-coated optical fiber sensors (OFSs). In order to confirm their feasibility, both analytical and experimental approaches were undertaken. In the analysis, a theoretical model for a surface-mounted OFS on the composite was proposed, and the strain transfer relations were derived. Moreover, novel numerical methods were implemented in order to evaluate the residual strain distribution. The analytical results were validated through a finite element analysis (FEA) using the ABAQUS software. We found that the residual strain increases as the coating thickness and external strain increase. In addition, the required gauge length for the given bonding length of the OFSs is proposed. In the experiment, fiber Bragg grating (FBG) sensors were applied to carbon fiber reinforced polymer (CFRP) composite specimens in order to verify the proposed technique. The trends of the residual strain, which are corresponding to the maximum strains experienced by the composite specimens, were consistent with those obtained in the analysis.</abstract><cop>Kidlington</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.compscitech.2013.01.010</doi><tpages>8</tpages></addata></record> |
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subjects | A. Coating Applied sciences B. Plastic deformation C. Stress transfer Carbon fiber reinforced plastics D. Non-destructive testing Exact sciences and technology Finite element method Forms of application and semi-finished materials Laminates Mathematical analysis Mathematical models Optical fibers Polymer industry, paints, wood Sensors Strain Strain distribution Technology of polymers |
title | Determination of the maximum strains experienced by composite structures using metal coated optical fiber sensors |
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