Generalized curvature tailoring of bistable CFRP laminates by curing on a cylindrical tool-plate with misalignment
Inducing an initial curvature is advantageous for tailoring the curvature of bistable Carbon Fiber Reinforced Prepreg (CFRP) laminate because the final curvature of the laminate can be tailored without changing its mechanical properties, i.e., bending rigidity, thickness, and weight. However, curvat...
Gespeichert in:
Veröffentlicht in: | Composites science and technology 2014-10, Vol.103, p.127-133 |
---|---|
Hauptverfasser: | , , , , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 133 |
---|---|
container_issue | |
container_start_page | 127 |
container_title | Composites science and technology |
container_volume | 103 |
creator | Ryu, Junghyun Lee, Jong-Gu Kim, Seung-Won Koh, Je-Sung Cho, Kyu-Jin Cho, Maenghyo |
description | Inducing an initial curvature is advantageous for tailoring the curvature of bistable Carbon Fiber Reinforced Prepreg (CFRP) laminate because the final curvature of the laminate can be tailored without changing its mechanical properties, i.e., bending rigidity, thickness, and weight. However, curvature tailoring with initial curvature has been limited to tailoring the curvature of only one state of the two equilibrium states. In this study, we propose a curvature tailoring scheme which can tailor the curvatures of both equilibrium states by misaligning the laminate and the cylindrical tool-plate for curing. This method was verified by analysis with the Rayleigh–Ritz method and experiments. In addition, explicit equations to determine the misalignment angle and tool-plate curvature are derived for curvature tailoring of the bistable CFRP cross-ply laminates. These equations provide a simple engineering guideline for designers of bistable CFRP cross-ply laminate. The proposed curvature tailoring method gives the designer the ability to select the curvature of both equilibrium states without changing its mechanical properties, and increasing the functionality of bistable CFRP laminates. |
doi_str_mv | 10.1016/j.compscitech.2014.08.024 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_1642226950</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0266353814003133</els_id><sourcerecordid>1642226950</sourcerecordid><originalsourceid>FETCH-LOGICAL-c384t-846b7c3c4edea69e5305a589a157ec61a13e76f32c43d45902f0f9d5b7a974c33</originalsourceid><addsrcrecordid>eNqNkE9v1DAUxC0EUpe238EckLgk-H-cI1rRglQJhMrZcpyX1ivHXmxv0fLp8bIV4sjpXX4z82YQekNJTwlV73e9S-u-OF_BPfaMUNET3RMmXqAN1cPYUSLJS7QhTKmOS64v0OtSdoSQQY5sg_ItRMg2-F8wY3fIT7YeMuBqfUjZxwecFjz5Uu0UAG9vvn3Fwa4-2goFT8eT4g8UscXuGHycs3c24JpS6PahYfinr4949aVlPMQVYr1CrxYbClw_30v0_ebj_fZTd_fl9vP2w13nuBa100JNg-NOwAxWjSA5kVbq0VI5gFPUUg6DWjhzgs9CjoQtZBlnOQ12HITj_BK9O_vuc_pxgFJN-8JBCDZCOhRDlWCMqVGSho5n1OVUSobF7LNfbT4aSsxpZ7Mz_-xsTjsbok3buWnfPsfY0qov2Ubny18DpjWjROjGbc8ctM5PHrJpbhAdzD6Dq2ZO_j_SfgOB2ZuF</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1642226950</pqid></control><display><type>article</type><title>Generalized curvature tailoring of bistable CFRP laminates by curing on a cylindrical tool-plate with misalignment</title><source>Elsevier ScienceDirect Journals</source><creator>Ryu, Junghyun ; Lee, Jong-Gu ; Kim, Seung-Won ; Koh, Je-Sung ; Cho, Kyu-Jin ; Cho, Maenghyo</creator><creatorcontrib>Ryu, Junghyun ; Lee, Jong-Gu ; Kim, Seung-Won ; Koh, Je-Sung ; Cho, Kyu-Jin ; Cho, Maenghyo</creatorcontrib><description>Inducing an initial curvature is advantageous for tailoring the curvature of bistable Carbon Fiber Reinforced Prepreg (CFRP) laminate because the final curvature of the laminate can be tailored without changing its mechanical properties, i.e., bending rigidity, thickness, and weight. However, curvature tailoring with initial curvature has been limited to tailoring the curvature of only one state of the two equilibrium states. In this study, we propose a curvature tailoring scheme which can tailor the curvatures of both equilibrium states by misaligning the laminate and the cylindrical tool-plate for curing. This method was verified by analysis with the Rayleigh–Ritz method and experiments. In addition, explicit equations to determine the misalignment angle and tool-plate curvature are derived for curvature tailoring of the bistable CFRP cross-ply laminates. These equations provide a simple engineering guideline for designers of bistable CFRP cross-ply laminate. The proposed curvature tailoring method gives the designer the ability to select the curvature of both equilibrium states without changing its mechanical properties, and increasing the functionality of bistable CFRP laminates.</description><identifier>ISSN: 0266-3538</identifier><identifier>EISSN: 1879-1050</identifier><identifier>DOI: 10.1016/j.compscitech.2014.08.024</identifier><identifier>CODEN: CSTCEH</identifier><language>eng</language><publisher>Kidlington: Elsevier Ltd</publisher><subject>A. Carbon fibers ; Applied sciences ; B. Non-linear behavior ; C. Laminate theory ; C. Residual stress ; Carbon fiber reinforced plastics ; Curing ; Curvature ; Exact sciences and technology ; Forms of application and semi-finished materials ; Laminates ; Mathematical analysis ; Mechanical properties ; Misalignment ; Polymer industry, paints, wood ; Technology of polymers</subject><ispartof>Composites science and technology, 2014-10, Vol.103, p.127-133</ispartof><rights>2014</rights><rights>2015 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c384t-846b7c3c4edea69e5305a589a157ec61a13e76f32c43d45902f0f9d5b7a974c33</citedby><cites>FETCH-LOGICAL-c384t-846b7c3c4edea69e5305a589a157ec61a13e76f32c43d45902f0f9d5b7a974c33</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0266353814003133$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65306</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=28821048$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Ryu, Junghyun</creatorcontrib><creatorcontrib>Lee, Jong-Gu</creatorcontrib><creatorcontrib>Kim, Seung-Won</creatorcontrib><creatorcontrib>Koh, Je-Sung</creatorcontrib><creatorcontrib>Cho, Kyu-Jin</creatorcontrib><creatorcontrib>Cho, Maenghyo</creatorcontrib><title>Generalized curvature tailoring of bistable CFRP laminates by curing on a cylindrical tool-plate with misalignment</title><title>Composites science and technology</title><description>Inducing an initial curvature is advantageous for tailoring the curvature of bistable Carbon Fiber Reinforced Prepreg (CFRP) laminate because the final curvature of the laminate can be tailored without changing its mechanical properties, i.e., bending rigidity, thickness, and weight. However, curvature tailoring with initial curvature has been limited to tailoring the curvature of only one state of the two equilibrium states. In this study, we propose a curvature tailoring scheme which can tailor the curvatures of both equilibrium states by misaligning the laminate and the cylindrical tool-plate for curing. This method was verified by analysis with the Rayleigh–Ritz method and experiments. In addition, explicit equations to determine the misalignment angle and tool-plate curvature are derived for curvature tailoring of the bistable CFRP cross-ply laminates. These equations provide a simple engineering guideline for designers of bistable CFRP cross-ply laminate. The proposed curvature tailoring method gives the designer the ability to select the curvature of both equilibrium states without changing its mechanical properties, and increasing the functionality of bistable CFRP laminates.</description><subject>A. Carbon fibers</subject><subject>Applied sciences</subject><subject>B. Non-linear behavior</subject><subject>C. Laminate theory</subject><subject>C. Residual stress</subject><subject>Carbon fiber reinforced plastics</subject><subject>Curing</subject><subject>Curvature</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Laminates</subject><subject>Mathematical analysis</subject><subject>Mechanical properties</subject><subject>Misalignment</subject><subject>Polymer industry, paints, wood</subject><subject>Technology of polymers</subject><issn>0266-3538</issn><issn>1879-1050</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2014</creationdate><recordtype>article</recordtype><recordid>eNqNkE9v1DAUxC0EUpe238EckLgk-H-cI1rRglQJhMrZcpyX1ivHXmxv0fLp8bIV4sjpXX4z82YQekNJTwlV73e9S-u-OF_BPfaMUNET3RMmXqAN1cPYUSLJS7QhTKmOS64v0OtSdoSQQY5sg_ItRMg2-F8wY3fIT7YeMuBqfUjZxwecFjz5Uu0UAG9vvn3Fwa4-2goFT8eT4g8UscXuGHycs3c24JpS6PahYfinr4949aVlPMQVYr1CrxYbClw_30v0_ebj_fZTd_fl9vP2w13nuBa100JNg-NOwAxWjSA5kVbq0VI5gFPUUg6DWjhzgs9CjoQtZBlnOQ12HITj_BK9O_vuc_pxgFJN-8JBCDZCOhRDlWCMqVGSho5n1OVUSobF7LNfbT4aSsxpZ7Mz_-xsTjsbok3buWnfPsfY0qov2Ubny18DpjWjROjGbc8ctM5PHrJpbhAdzD6Dq2ZO_j_SfgOB2ZuF</recordid><startdate>20141028</startdate><enddate>20141028</enddate><creator>Ryu, Junghyun</creator><creator>Lee, Jong-Gu</creator><creator>Kim, Seung-Won</creator><creator>Koh, Je-Sung</creator><creator>Cho, Kyu-Jin</creator><creator>Cho, Maenghyo</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>20141028</creationdate><title>Generalized curvature tailoring of bistable CFRP laminates by curing on a cylindrical tool-plate with misalignment</title><author>Ryu, Junghyun ; Lee, Jong-Gu ; Kim, Seung-Won ; Koh, Je-Sung ; Cho, Kyu-Jin ; Cho, Maenghyo</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c384t-846b7c3c4edea69e5305a589a157ec61a13e76f32c43d45902f0f9d5b7a974c33</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2014</creationdate><topic>A. Carbon fibers</topic><topic>Applied sciences</topic><topic>B. Non-linear behavior</topic><topic>C. Laminate theory</topic><topic>C. Residual stress</topic><topic>Carbon fiber reinforced plastics</topic><topic>Curing</topic><topic>Curvature</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Laminates</topic><topic>Mathematical analysis</topic><topic>Mechanical properties</topic><topic>Misalignment</topic><topic>Polymer industry, paints, wood</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ryu, Junghyun</creatorcontrib><creatorcontrib>Lee, Jong-Gu</creatorcontrib><creatorcontrib>Kim, Seung-Won</creatorcontrib><creatorcontrib>Koh, Je-Sung</creatorcontrib><creatorcontrib>Cho, Kyu-Jin</creatorcontrib><creatorcontrib>Cho, Maenghyo</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>Ryu, Junghyun</au><au>Lee, Jong-Gu</au><au>Kim, Seung-Won</au><au>Koh, Je-Sung</au><au>Cho, Kyu-Jin</au><au>Cho, Maenghyo</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Generalized curvature tailoring of bistable CFRP laminates by curing on a cylindrical tool-plate with misalignment</atitle><jtitle>Composites science and technology</jtitle><date>2014-10-28</date><risdate>2014</risdate><volume>103</volume><spage>127</spage><epage>133</epage><pages>127-133</pages><issn>0266-3538</issn><eissn>1879-1050</eissn><coden>CSTCEH</coden><abstract>Inducing an initial curvature is advantageous for tailoring the curvature of bistable Carbon Fiber Reinforced Prepreg (CFRP) laminate because the final curvature of the laminate can be tailored without changing its mechanical properties, i.e., bending rigidity, thickness, and weight. However, curvature tailoring with initial curvature has been limited to tailoring the curvature of only one state of the two equilibrium states. In this study, we propose a curvature tailoring scheme which can tailor the curvatures of both equilibrium states by misaligning the laminate and the cylindrical tool-plate for curing. This method was verified by analysis with the Rayleigh–Ritz method and experiments. In addition, explicit equations to determine the misalignment angle and tool-plate curvature are derived for curvature tailoring of the bistable CFRP cross-ply laminates. These equations provide a simple engineering guideline for designers of bistable CFRP cross-ply laminate. The proposed curvature tailoring method gives the designer the ability to select the curvature of both equilibrium states without changing its mechanical properties, and increasing the functionality of bistable CFRP laminates.</abstract><cop>Kidlington</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.compscitech.2014.08.024</doi><tpages>7</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0266-3538 |
ispartof | Composites science and technology, 2014-10, Vol.103, p.127-133 |
issn | 0266-3538 1879-1050 |
language | eng |
recordid | cdi_proquest_miscellaneous_1642226950 |
source | Elsevier ScienceDirect Journals |
subjects | A. Carbon fibers Applied sciences B. Non-linear behavior C. Laminate theory C. Residual stress Carbon fiber reinforced plastics Curing Curvature Exact sciences and technology Forms of application and semi-finished materials Laminates Mathematical analysis Mechanical properties Misalignment Polymer industry, paints, wood Technology of polymers |
title | Generalized curvature tailoring of bistable CFRP laminates by curing on a cylindrical tool-plate with misalignment |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-07T22%3A36%3A30IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Generalized%20curvature%20tailoring%20of%20bistable%20CFRP%20laminates%20by%20curing%20on%20a%20cylindrical%20tool-plate%20with%20misalignment&rft.jtitle=Composites%20science%20and%20technology&rft.au=Ryu,%20Junghyun&rft.date=2014-10-28&rft.volume=103&rft.spage=127&rft.epage=133&rft.pages=127-133&rft.issn=0266-3538&rft.eissn=1879-1050&rft.coden=CSTCEH&rft_id=info:doi/10.1016/j.compscitech.2014.08.024&rft_dat=%3Cproquest_cross%3E1642226950%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1642226950&rft_id=info:pmid/&rft_els_id=S0266353814003133&rfr_iscdi=true |