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Deflection Measurements of Laminated Thin Plates Using Electronic Speckle Pattern Interferometry
An adaptive Electronic speckle Pattern Interferometry (ESPI) system has been developed to measure out-of-plane deformation of laminates subjected to quasi-static loads. The system was installed and setup for calibration with aluminum specimens mounted to an optical breadboard. Several parameters of...
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Published in: | Journal of composites technology & research 2002, Vol.24 (4), p.215-223 |
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container_title | Journal of composites technology & research |
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creator | Golda, D Kedlaya, D Pelegri, AA |
description | An adaptive Electronic speckle Pattern Interferometry (ESPI) system has been developed to measure out-of-plane deformation of laminates subjected to quasi-static loads. The system was installed and setup for calibration with aluminum specimens mounted to an optical breadboard. Several parameters of the test fixture and system's geometry needed to be adjusted before usable fringe patterns were obtained, and the system's resolution and range were determined. The ESPI system was then reconfigured for use with composite specimens subjected to quasi-static loading. Results of fringe patterns, calibration curves and deformation patterns are presented for A1 and graphite/epoxy specimens. The ESPI resolution was estimated at 25 μm per fringe for the A1 surface, and 11 μm per fringe for the composite laminate. From the results, it can be concluded that the usable deflection range is limited at high system resolutions. |
doi_str_mv | 10.1520/CTR10927J |
format | article |
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The system was installed and setup for calibration with aluminum specimens mounted to an optical breadboard. Several parameters of the test fixture and system's geometry needed to be adjusted before usable fringe patterns were obtained, and the system's resolution and range were determined. The ESPI system was then reconfigured for use with composite specimens subjected to quasi-static loading. Results of fringe patterns, calibration curves and deformation patterns are presented for A1 and graphite/epoxy specimens. The ESPI resolution was estimated at 25 μm per fringe for the A1 surface, and 11 μm per fringe for the composite laminate. From the results, it can be concluded that the usable deflection range is limited at high system resolutions.</description><identifier>ISSN: 0884-6804</identifier><identifier>EISSN: 1945-7537</identifier><identifier>DOI: 10.1520/CTR10927J</identifier><identifier>CODEN: JCTRER</identifier><language>eng</language><publisher>Philadelphia, PA: American Society for Testing and Materials</publisher><subject>Applied sciences ; Exact sciences and technology ; Forms of application and semi-finished materials ; Laminates ; Polymer industry, paints, wood ; Technology of polymers</subject><ispartof>Journal of composites technology & research, 2002, Vol.24 (4), p.215-223</ispartof><rights>All rights reserved. This material may not be reproduced or copied, in whole or in part, in any printed, mechanical, electronic, film, or other distribution and storage media, without the written consent of the publisher.</rights><rights>2003 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a367t-f97105504a2ea8be4520fe76bde10957b6b176620e1d0dfa4db94f223b1d77473</citedby><cites>FETCH-LOGICAL-a367t-f97105504a2ea8be4520fe76bde10957b6b176620e1d0dfa4db94f223b1d77473</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,4024,9791,27923,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=14019835$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Golda, D</creatorcontrib><creatorcontrib>Kedlaya, D</creatorcontrib><creatorcontrib>Pelegri, AA</creatorcontrib><title>Deflection Measurements of Laminated Thin Plates Using Electronic Speckle Pattern Interferometry</title><title>Journal of composites technology & research</title><description>An adaptive Electronic speckle Pattern Interferometry (ESPI) system has been developed to measure out-of-plane deformation of laminates subjected to quasi-static loads. The system was installed and setup for calibration with aluminum specimens mounted to an optical breadboard. Several parameters of the test fixture and system's geometry needed to be adjusted before usable fringe patterns were obtained, and the system's resolution and range were determined. The ESPI system was then reconfigured for use with composite specimens subjected to quasi-static loading. Results of fringe patterns, calibration curves and deformation patterns are presented for A1 and graphite/epoxy specimens. The ESPI resolution was estimated at 25 μm per fringe for the A1 surface, and 11 μm per fringe for the composite laminate. From the results, it can be concluded that the usable deflection range is limited at high system resolutions.</description><subject>Applied sciences</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Laminates</subject><subject>Polymer industry, paints, wood</subject><subject>Technology of polymers</subject><issn>0884-6804</issn><issn>1945-7537</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2002</creationdate><recordtype>article</recordtype><recordid>eNptkLtOxDAURC0EEsuj4A_cgEQRsB0nTkq0vLWIFSy1cZJrMCROsJ0Cvh6vWLEFVHOLM3M1g9ABJSc0Y-R0unigpGTidgNNaMmzRGSp2EQTUhQ8yQvCt9GO92-E0IIJOkHP56BbqIPpLb4D5UcHHdjgca_xTHXGqgANXrwai-dtvD1-8sa-4IulyfXW1PhxgPq9BTxXIYCz-MZG0eD6DoL73ENbWrUe9le6i54uLxbT62R2f3UzPZslKs1FSHQpKMkywhUDVVTAYxkNIq8aiH0yUeUVFXnOCNCGNFrxpiq5ZiytaCMEF-kuOvrJHVz_MYIPsjO-hrZVFvrRSyZIyTkvInj8A9au996BloMznXKfkhK53FD-bhjZw1Wo8rVqtVO2Nn5t4ISWRZqtnysfOvnWj87Grv8Giv_ACEjGJZdfZvjrkkOj029y5I-Z</recordid><startdate>2002</startdate><enddate>2002</enddate><creator>Golda, D</creator><creator>Kedlaya, D</creator><creator>Pelegri, AA</creator><general>American Society for Testing and Materials</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>2002</creationdate><title>Deflection Measurements of Laminated Thin Plates Using Electronic Speckle Pattern Interferometry</title><author>Golda, D ; Kedlaya, D ; Pelegri, AA</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a367t-f97105504a2ea8be4520fe76bde10957b6b176620e1d0dfa4db94f223b1d77473</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2002</creationdate><topic>Applied sciences</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Laminates</topic><topic>Polymer industry, paints, wood</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Golda, D</creatorcontrib><creatorcontrib>Kedlaya, D</creatorcontrib><creatorcontrib>Pelegri, AA</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Journal of composites technology & research</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Golda, D</au><au>Kedlaya, D</au><au>Pelegri, AA</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Deflection Measurements of Laminated Thin Plates Using Electronic Speckle Pattern Interferometry</atitle><jtitle>Journal of composites technology & research</jtitle><date>2002</date><risdate>2002</risdate><volume>24</volume><issue>4</issue><spage>215</spage><epage>223</epage><pages>215-223</pages><issn>0884-6804</issn><eissn>1945-7537</eissn><coden>JCTRER</coden><abstract>An adaptive Electronic speckle Pattern Interferometry (ESPI) system has been developed to measure out-of-plane deformation of laminates subjected to quasi-static loads. The system was installed and setup for calibration with aluminum specimens mounted to an optical breadboard. Several parameters of the test fixture and system's geometry needed to be adjusted before usable fringe patterns were obtained, and the system's resolution and range were determined. The ESPI system was then reconfigured for use with composite specimens subjected to quasi-static loading. Results of fringe patterns, calibration curves and deformation patterns are presented for A1 and graphite/epoxy specimens. The ESPI resolution was estimated at 25 μm per fringe for the A1 surface, and 11 μm per fringe for the composite laminate. From the results, it can be concluded that the usable deflection range is limited at high system resolutions.</abstract><cop>Philadelphia, PA</cop><pub>American Society for Testing and Materials</pub><doi>10.1520/CTR10927J</doi><tpages>9</tpages></addata></record> |
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subjects | Applied sciences Exact sciences and technology Forms of application and semi-finished materials Laminates Polymer industry, paints, wood Technology of polymers |
title | Deflection Measurements of Laminated Thin Plates Using Electronic Speckle Pattern Interferometry |
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