1 Ocak 2018 Konferans bildirisi Açık Erişim

Kaya, G.; Soutis, C.; Potluri, P.

DataCite XML

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  <identifier identifierType="URL">https://aperta.ulakbim.gov.tr/record/29693</identifier>
  <creators>
    <creator>
      <creatorName>Kaya, G.</creatorName>
      <givenName>G.</givenName>
      <familyName>Kaya</familyName>
      <affiliation>Kahramanmaras Sutcu Imam Univ, Dept Text Engn, TR-46040 Kahramanmaras, Turkey</affiliation>
    </creator>
    <creator>
      <creatorName>Soutis, C.</creatorName>
      <givenName>C.</givenName>
      <familyName>Soutis</familyName>
    </creator>
    <creator>
      <creatorName>Potluri, P.</creatorName>
      <givenName>P.</givenName>
      <familyName>Potluri</familyName>
      <affiliation>Univ Manchester, Northwest Composites Ctr, Manchester M13 9PL, Lancs, England</affiliation>
    </creator>
  </creators>
  <titles>
    <title>Tensile Properties Of A Novel Graphene Pattern Stitched Carbon/Epoxy 3D Composite</title>
  </titles>
  <publisher>Aperta</publisher>
  <publicationYear>2018</publicationYear>
  <dates>
    <date dateType="Issued">2018-01-01</date>
  </dates>
  <resourceType resourceTypeGeneral="Text">Conference paper</resourceType>
  <alternateIdentifiers>
    <alternateIdentifier alternateIdentifierType="url">https://aperta.ulakbim.gov.tr/record/29693</alternateIdentifier>
  </alternateIdentifiers>
  <relatedIdentifiers>
    <relatedIdentifier relatedIdentifierType="DOI" relationType="IsIdenticalTo">10.1088/1757-899X/460/1/012015</relatedIdentifier>
  </relatedIdentifiers>
  <rightsList>
    <rights rightsURI="http://www.opendefinition.org/licenses/cc-by">Creative Commons Attribution</rights>
    <rights rightsURI="info:eu-repo/semantics/openAccess">Open Access</rights>
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  <descriptions>
    <description descriptionType="Abstract">The focus of this study is on the tensile properties of a novel graphene pattern stitched carbon/epoxy 3D composite which could be considered in aerospace industry applications. Tensile modulus and strength are reduced by18-25% due to filament breakage during stitching; this reduction varies with stitching density. Fabrication induced voids and resin rich regions also contribute. However, extensive delamination observed in the tension loaded unstitched laminate is constrained by the graphene pattern stitching and the proposed 3D reinforced composite is expected to be more damage resistant under lateral impact loading.</description>
  </descriptions>
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