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<records>
  <record>
    <language>eng</language>
    <publisher>Science and Education Publishing</publisher>
    <journalTitle>Journal of Mechanical Design and Vibration</journalTitle>
    <eissn>2376-9572</eissn>
    <publicationDate>2017-05-17</publicationDate>
    <volume>5</volume>
    <issue>1</issue>
    <startPage>11</startPage>
    <endPage>20</endPage>
    <doi>10.12691/jmdv-5-1-2</doi>
    <publisherRecordId>JMDV2017512</publisherRecordId>
    <documentType>article</documentType>
    <title language="eng">Active Stiffness Method for High Cycle Fatigue Mitigation using Topical Thin Foil Shape Memory Alloy</title>
    <authors>
      <author>
        <name>Nicholas G. Garafolo</name>
        <email>nicholas.g.garafolo@uakron.edu</email>
        <affiliationId>1</affiliationId>
      </author>
      <author>
        <name>Rachel Collard</name>
        <affiliationId>1</affiliationId>
      </author>
    </authors>
    <affiliationsList>
      <affiliationName affiliationId="1">Department of Mechanical Engineering, The University of Akron, Akron, OH 44325, U.S.A.</affiliationName>
    </affiliationsList>
    <abstract language="eng">The strong need for high cycle fatigue mitigation has resulted in numerous techniques resulting in added weight, increased operational costs, and lower performance. The experimental investigation presented was a foundational effort towards mitigating HCF through the use of shape memory alloy in a composite system. The research objective was to quantify changes in eigenvalue, eigenvector, and amplitude of a vibrating cantilever beam with a thin SMA topical treatment; as quantified during SMA phase transformations and through comparison with a control. A composite beam consisting of a nitinol thin SMA foil adhered to an Aluminum Alloy 6061 substrate was designed and fabricated. The three configurations were utilized: (1) a full-span SMA treatment designed for maximum eigenvalue shift and maximum amplitude reduction, (2) a half-span SMA treatment designed for eigenvector shift, and (3) a full-span aluminum treatment for a control. Through a complete modal analysis, results illustrated that thin foil SMA treatments led to a significant shift in eigenvalue, up to 6.53%. Highlighting the reduction in amplitude was a 92% reduction in amplitude at second bending with constant excitation frequency with the full-span sample. Spanwise scans on the half-span sample with and without SMA actuation illustrated a 0.77% shift in node location.</abstract>
    <fullTextUrl format="pdf">http://pubs.sciepub.com/jmdv/5/1/2/jmdv-5-1-2.pdf</fullTextUrl>
    <keywords language="eng">
      <keyword>shape memory alloys</keyword>
      <keyword>thin foil</keyword>
      <keyword>vibration</keyword>
      <keyword>high cycle fatigue</keyword>
      <keyword>turbomachinery</keyword>
    </keywords>
  </record>
</records>