Polymer watrix woven fabric composites subjected to low velocity impact. II - Effect of plate thickness

Polymer watrix woven fabric composites subjected to low velocity impact. II - Effect of plate thickness

Studies were carried out on the damage initiation behavior of polymer matrix woven fabric (WF) composite plates subjected to a transverse central low velocity point impact load. Specifically, the effect of composite plate thickness on the impact behavior was investigated with a square plate of 150 x...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Journal of reinforced plastics and composites 2000-09, Vol.19 (13), p.1031-1055
Hauptverfasser: Naik, N K, Meduri, Sailendra, Chandra Sekher, Y
Format: Artikel
Sprache:eng
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page 1055
container_issue 13
container_start_page 1031
container_title Journal of reinforced plastics and composites
container_volume 19
creator Naik, N K
Meduri, Sailendra
Chandra Sekher, Y
description Studies were carried out on the damage initiation behavior of polymer matrix woven fabric (WF) composite plates subjected to a transverse central low velocity point impact load. Specifically, the effect of composite plate thickness on the impact behavior was investigated with a square plate of 150 x 150 mm with thicknesses varying from 4.5 to 8.0 mm. The material systems considered are: E-glass/epoxy and T300/5208 carbon/epoxy. In-plane failure of the layers in the form of matrix cracking/lamina splitting and delaminations were the primary objectives of the study. The studies were carried out using an in-house Finite Element Analysis code. The in-plane failure functions and the interlaminar failure functions were predicted using quadratic failure criteria. General observations on the impact behavior of polymer matrix WF composites as a function of plate thickness are presented. (Author)
format Article
fullrecord <record><control><sourceid>proquest</sourceid><recordid>TN_cdi_proquest_miscellaneous_27664153</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>27664153</sourcerecordid><originalsourceid>FETCH-proquest_miscellaneous_276641533</originalsourceid><addsrcrecordid>eNqNyr0SwUAQAOArmPH7DlvpYhI5id4wdAq9OWePi0s2shvh7Sk8gOprvp4axnmaRNlK64EaMRdxvEi01kN1PVB4l9hAZ6TxL-joiRU4c268BUtlTewFGbg9F2gFLyAEgTp4YiDr5Q2-rI2VOez3EMHGue8CclAHIwhy8_ZeIfNE9Z0JjNOfYzXbbo7rXVQ39GiR5VR6thiCqZBaPi3yLNPJMk3_jh92oUn5</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>27664153</pqid></control><display><type>article</type><title>Polymer watrix woven fabric composites subjected to low velocity impact. II - Effect of plate thickness</title><source>SAGE Complete</source><creator>Naik, N K ; Meduri, Sailendra ; Chandra Sekher, Y</creator><creatorcontrib>Naik, N K ; Meduri, Sailendra ; Chandra Sekher, Y</creatorcontrib><description>Studies were carried out on the damage initiation behavior of polymer matrix woven fabric (WF) composite plates subjected to a transverse central low velocity point impact load. Specifically, the effect of composite plate thickness on the impact behavior was investigated with a square plate of 150 x 150 mm with thicknesses varying from 4.5 to 8.0 mm. The material systems considered are: E-glass/epoxy and T300/5208 carbon/epoxy. In-plane failure of the layers in the form of matrix cracking/lamina splitting and delaminations were the primary objectives of the study. The studies were carried out using an in-house Finite Element Analysis code. The in-plane failure functions and the interlaminar failure functions were predicted using quadratic failure criteria. General observations on the impact behavior of polymer matrix WF composites as a function of plate thickness are presented. (Author)</description><identifier>ISSN: 0731-6844</identifier><language>eng</language><ispartof>Journal of reinforced plastics and composites, 2000-09, Vol.19 (13), p.1031-1055</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780</link.rule.ids></links><search><creatorcontrib>Naik, N K</creatorcontrib><creatorcontrib>Meduri, Sailendra</creatorcontrib><creatorcontrib>Chandra Sekher, Y</creatorcontrib><title>Polymer watrix woven fabric composites subjected to low velocity impact. II - Effect of plate thickness</title><title>Journal of reinforced plastics and composites</title><description>Studies were carried out on the damage initiation behavior of polymer matrix woven fabric (WF) composite plates subjected to a transverse central low velocity point impact load. Specifically, the effect of composite plate thickness on the impact behavior was investigated with a square plate of 150 x 150 mm with thicknesses varying from 4.5 to 8.0 mm. The material systems considered are: E-glass/epoxy and T300/5208 carbon/epoxy. In-plane failure of the layers in the form of matrix cracking/lamina splitting and delaminations were the primary objectives of the study. The studies were carried out using an in-house Finite Element Analysis code. The in-plane failure functions and the interlaminar failure functions were predicted using quadratic failure criteria. General observations on the impact behavior of polymer matrix WF composites as a function of plate thickness are presented. (Author)</description><issn>0731-6844</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2000</creationdate><recordtype>article</recordtype><recordid>eNqNyr0SwUAQAOArmPH7DlvpYhI5id4wdAq9OWePi0s2shvh7Sk8gOprvp4axnmaRNlK64EaMRdxvEi01kN1PVB4l9hAZ6TxL-joiRU4c268BUtlTewFGbg9F2gFLyAEgTp4YiDr5Q2-rI2VOez3EMHGue8CclAHIwhy8_ZeIfNE9Z0JjNOfYzXbbo7rXVQ39GiR5VR6thiCqZBaPi3yLNPJMk3_jh92oUn5</recordid><startdate>20000901</startdate><enddate>20000901</enddate><creator>Naik, N K</creator><creator>Meduri, Sailendra</creator><creator>Chandra Sekher, Y</creator><scope>8FD</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>20000901</creationdate><title>Polymer watrix woven fabric composites subjected to low velocity impact. II - Effect of plate thickness</title><author>Naik, N K ; Meduri, Sailendra ; Chandra Sekher, Y</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-proquest_miscellaneous_276641533</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2000</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Naik, N K</creatorcontrib><creatorcontrib>Meduri, Sailendra</creatorcontrib><creatorcontrib>Chandra Sekher, Y</creatorcontrib><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of reinforced plastics and composites</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Naik, N K</au><au>Meduri, Sailendra</au><au>Chandra Sekher, Y</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Polymer watrix woven fabric composites subjected to low velocity impact. II - Effect of plate thickness</atitle><jtitle>Journal of reinforced plastics and composites</jtitle><date>2000-09-01</date><risdate>2000</risdate><volume>19</volume><issue>13</issue><spage>1031</spage><epage>1055</epage><pages>1031-1055</pages><issn>0731-6844</issn><abstract>Studies were carried out on the damage initiation behavior of polymer matrix woven fabric (WF) composite plates subjected to a transverse central low velocity point impact load. Specifically, the effect of composite plate thickness on the impact behavior was investigated with a square plate of 150 x 150 mm with thicknesses varying from 4.5 to 8.0 mm. The material systems considered are: E-glass/epoxy and T300/5208 carbon/epoxy. In-plane failure of the layers in the form of matrix cracking/lamina splitting and delaminations were the primary objectives of the study. The studies were carried out using an in-house Finite Element Analysis code. The in-plane failure functions and the interlaminar failure functions were predicted using quadratic failure criteria. General observations on the impact behavior of polymer matrix WF composites as a function of plate thickness are presented. (Author)</abstract></addata></record>
fulltext fulltext
identifier ISSN: 0731-6844
ispartof Journal of reinforced plastics and composites, 2000-09, Vol.19 (13), p.1031-1055
issn 0731-6844
language eng
recordid cdi_proquest_miscellaneous_27664153
source SAGE Complete
title Polymer watrix woven fabric composites subjected to low velocity impact. II - Effect of plate thickness
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-03T13%3A32%3A54IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Polymer%20watrix%20woven%20fabric%20composites%20subjected%20to%20low%20velocity%20impact.%20II%20-%20Effect%20of%20plate%20thickness&rft.jtitle=Journal%20of%20reinforced%20plastics%20and%20composites&rft.au=Naik,%20N%20K&rft.date=2000-09-01&rft.volume=19&rft.issue=13&rft.spage=1031&rft.epage=1055&rft.pages=1031-1055&rft.issn=0731-6844&rft_id=info:doi/&rft_dat=%3Cproquest%3E27664153%3C/proquest%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=27664153&rft_id=info:pmid/&rfr_iscdi=true