July 30, 2020 Journal article Open Access

Suhail Khaliq; R.R Ghadge

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  <identifier identifierType="URL">https://zenodo.org/record/5852260</identifier>
  <creators>
    <creator>
      <creatorName>Suhail Khaliq</creatorName>
      <affiliation>,School of Mechanical Engineering ,MITWPU,,Pune  Maharashtra,India</affiliation>
    </creator>
    <creator>
      <creatorName>R.R Ghadge</creatorName>
      <affiliation>School of Mechanical Engineering ,MITWPU,,Pune  Maharashtra,India</affiliation>
    </creator>
  </creators>
  <titles>
    <title>Fatigue Behavior of Epoxy Bonded Composite  Lap Joints</title>
  </titles>
  <publisher>Zenodo</publisher>
  <publicationYear>2020</publicationYear>
  <subjects>
    <subject>Adhesive, Composite, Epoxy adhesive, Fatigue, FEA</subject>
    <subject subjectScheme="issn">2277-3878</subject>
    <subject subjectScheme="handle">B3167079220/2020©BEIESP</subject>
  </subjects>
  <contributors>
    <contributor contributorType="Sponsor">
      <contributorName>Blue Eyes Intelligence Engineering  and Sciences Publication(BEIESP)</contributorName>
      <affiliation>Publisher</affiliation>
    </contributor>
  </contributors>
  <dates>
    <date dateType="Issued">2020-07-30</date>
  </dates>
  <language>en</language>
  <resourceType resourceTypeGeneral="JournalArticle"/>
  <alternateIdentifiers>
    <alternateIdentifier alternateIdentifierType="url">https://zenodo.org/record/5852260</alternateIdentifier>
  </alternateIdentifiers>
  <relatedIdentifiers>
    <relatedIdentifier relatedIdentifierType="ISSN" relationType="IsCitedBy" resourceTypeGeneral="JournalArticle">2277-3878</relatedIdentifier>
    <relatedIdentifier relatedIdentifierType="DOI" relationType="IsIdenticalTo">10.35940/ijrte.B3167.079220</relatedIdentifier>
  </relatedIdentifiers>
  <rightsList>
    <rights rightsURI="https://creativecommons.org/licenses/by/4.0/legalcode">Creative Commons Attribution 4.0 International</rights>
    <rights rightsURI="info:eu-repo/semantics/openAccess">Open Access</rights>
  </rightsList>
  <descriptions>
    <description descriptionType="Abstract">&lt;p&gt;Laminated composites are rapidly finding uses in different engineering applications like Aviation, Sports equipment, Marine technology, Aerospace and Electronics. This is due to their versatile engineering properties. Bolting and Bonding are the widely used joining techniques in composites. However bonding has added advantages over bolting in terms of weight reduction and strength .This paper explores the fatigue strength of single lap epoxy bonded joint between composite laminates. The experimental results are compared with FEA (Finite Element Analysis) results.&lt;/p&gt;</description>
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