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  <title>DSpace Collection:</title>
  <link rel="alternate" href="http://localhost:8080/xmlui/handle/123456789/2707" />
  <subtitle />
  <id>http://localhost:8080/xmlui/handle/123456789/2707</id>
  <updated>2026-06-23T06:33:34Z</updated>
  <dc:date>2026-06-23T06:33:34Z</dc:date>
  <entry>
    <title>EXPERIMENTAL INVESTIGATION AND VALIDATION OF NATURAL FREQUENCY OF RECTANGULAR PLATES AND LAP JOINTS</title>
    <link rel="alternate" href="http://localhost:8080/xmlui/handle/123456789/2708" />
    <author>
      <name>Sonawane, A. R.</name>
    </author>
    <author>
      <name>Nichit, V. D.</name>
    </author>
    <id>http://localhost:8080/xmlui/handle/123456789/2708</id>
    <updated>2020-02-06T07:44:02Z</updated>
    <published>2018-03-03T00:00:00Z</published>
    <summary type="text">Title: EXPERIMENTAL INVESTIGATION AND VALIDATION OF NATURAL FREQUENCY OF RECTANGULAR PLATES AND LAP JOINTS
Authors: Sonawane, A. R.; Nichit, V. D.
Abstract: This paper deals with experimental investigation and validation of rectangular plates and&#xD;
lap joint using modal analysis. The purpose of the study is to analyze the dynamic behavior of&#xD;
structures like a rectangular plate, bolted lap joint, and single lap epoxy adhesive joint subjected to&#xD;
impact or shock loads using Finite Element Analysis (FEA) and experimental modal analysis. The&#xD;
various factors that affect the response of single rectangular plate, bolted and adhesive joint&#xD;
structures are studied, such as, mode shapes, damping ratio, natural frequencies etc. The purpose of&#xD;
this paper is to deliver effective techniques using software analysis for the calculation of the vibrant&#xD;
reply of single rectangular plate with rectangular plate lap joints and to validate the predictions by&#xD;
experimental modal analysis and FEA. The FEA method is used to validate the mode shapes, natural&#xD;
frequencies, and frequency response roles of the beams. The three different specimens are used&#xD;
which consist of aluminum material. The initial case study is focused on a simple rectangular plate of&#xD;
cantilever beam subjected to impact force. The second case study is focused on bolted lap joint and&#xD;
single lap adhesive joint. The core objective of this work is to determine the natural frequency and&#xD;
mode shape of all three specimens at cantilever beam condition and first to compare the result of all&#xD;
joints with the single rectangular plate and then compare it with experimental modal analysis. In&#xD;
practical application this kind of modal analysis can be used to analyze various structures to find&#xD;
natural frequency &amp; mode shapes such as cantilever bridge, frame of bicycle, automobile product,&#xD;
Industrial robots (manipulator), building structures, heavy machineries and aircraft industry etc.</summary>
    <dc:date>2018-03-03T00:00:00Z</dc:date>
  </entry>
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