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  <titleInfo>
    <title>Dynamic analysis of large deformation shells</title>
  </titleInfo>
  <name type="personal">
    <namePart>Lomboy, Gilson Rescober</namePart>
    <role>
      <roleTerm authority="marcrelator" type="text">creator</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Kim, Kidu</namePart>
    <role>
      <roleTerm type="text">Chairperson</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Worsak Kanok-Nukulchai</namePart>
    <role>
      <roleTerm type="text">Examination Committee</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Barry, William Joseph</namePart>
    <role>
      <roleTerm type="text">Examination Committee</roleTerm>
    </role>
  </name>
  <name type="corporate">
    <namePart>Asian Institute of Technology (partial)</namePart>
    <role>
      <roleTerm type="text">Scholarship donor</roleTerm>
    </role>
  </name>
  <name type="corporate">
    <namePart>Mapua Institute of Technology (partial)</namePart>
    <role>
      <roleTerm type="text">Scholarship donor</roleTerm>
    </role>
  </name>
  <typeOfResource>text</typeOfResource>
  <genre authority="marc">series</genre>
  <genre authority="marc">technical report</genre>
  <originInfo>
    <place>
      <placeTerm type="code" authority="marccountry">th</placeTerm>
    </place>
    <place>
      <placeTerm type="text">Bangkok</placeTerm>
    </place>
    <publisher>Asian Institute of Technology</publisher>
    <dateIssued>2002</dateIssued>
    <issuance>continuing</issuance>
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  <language>
    <languageTerm authority="iso639-2b" type="code">eng</languageTerm>
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  <physicalDescription>
    <extent>48, 10 leaves</extent>
  </physicalDescription>
  <abstract>The Hilbur-Hughes-Taylor method is implemented in XFINAS to analyze nonlinear dynamic shell problems. Two types of shell elements were made available for this purpose, an eight node co-rotational element developed by Kim (2002) and a new four-node shell element, XSHELL24. Two new shell elements with explicit tangent stiffness and internal force vector are developed, XSHELL20 and its extension, XSHELL24. The first has five degrees of freedom per node and the other has six degrees of freedom per node. Mass matrices were formulated for XSHELL24. One type was formed by lumping masses at the nodes and neglecting rotational inertia and the other was formed by the use of interpolation functions. Validation of the new shell elements was made through the patch test and various linear and nonlinear benchmarks. The two new shell elements provide reasonable results to most problems when compared with some standard four-node shell elements. The weaknesses of the two shell elements are also discussed. </abstract>
  <note>A thesis submitted in partial fulfillment of the requirements for the degree of Master of Engineering, School of Civil Engineering</note>
  <note>Thesis (M.Eng.) - Asian Institute of Technology, 2002</note>
  <subject authority="lcsh">
    <topic>Shells</topic>
  </subject>
  <subject authority="lcsh">
    <topic>Nonlinear theories</topic>
  </subject>
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    <titleInfo>
      <title>Thesis ; no. ST-02-16</title>
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    <name type="corporate">
      <namePart>Asian Institute of Technology.</namePart>
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    </name>
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  <identifier type="uri">http://203.159.5.9/ait-thesis/detail.php?q=B07538</identifier>
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    <recordCreationDate encoding="marc">030207</recordCreationDate>
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