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  <titleInfo>
    <title>Local buckling strength of cylindrical shells with residual stress</title>
  </titleInfo>
  <name type="personal">
    <namePart>Methi Wecharatana</namePart>
    <role>
      <roleTerm authority="marcrelator" type="text">creator</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Usami, Tsutomu</namePart>
    <role>
      <roleTerm type="text">Chairperson</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Karasudhi, Pisidhi</namePart>
    <role>
      <roleTerm type="text">Examination Committee</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Panitan Lukkunaprasit</namePart>
    <role>
      <roleTerm type="text">Examination Committee</roleTerm>
    </role>
  </name>
  <name type="corporate">
    <namePart>The Government of the Federal Republic of Germany</namePart>
    <role>
      <roleTerm type="text">Scholarship Donor</roleTerm>
    </role>
  </name>
  <typeOfResource>text</typeOfResource>
  <originInfo>
    <place>
      <placeTerm type="code" authority="marccountry">th</placeTerm>
    </place>
    <place>
      <placeTerm type="text">Bangkok</placeTerm>
    </place>
    <publisher>Asian Institute of Technology</publisher>
    <dateIssued>1978</dateIssued>
    <issuance>monographic</issuance>
  </originInfo>
  <language>
    <languageTerm authority="iso639-2b" type="code">eng</languageTerm>
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    <extent>24 p.</extent>
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  <note>A thesis submitted in partial fulfillment of the requirements for the degree of Master of Engineering of the Asian Institute of Technology, Bangkok, Thailand</note>
  <note>A theoretical study is presented on the elastic and inelastic local  buckling strength of cylindrical shells under axial compression. The effect of residual stress due to the forming process of the cylindrical shell, is mainly given attention. The finite strip method is employed to obtain the stiffness and geometric matrices of a buckled cylindrical shell based on the deformation theory of plasticity. The analysis is  performed under the boundary condition that the cylindrical shells are simply supported at the loading edges. In the numerical study, the critical radius over thickness ratio of the cylindrical shells are calculated  and this is the major subject in this research.</note>
  <note>Thesis (M.Eng.) - Asian Institute of Technology, 1978</note>
  <subject authority="lcsh">
    <topic>Strains and stresses</topic>
  </subject>
  <subject authority="lcsh">
    <topic>Buckling (Mechanics)</topic>
  </subject>
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    <titleInfo>
      <title>Thesis ; no. 1342</title>
    </titleInfo>
    <name type="corporate">
      <namePart>Asian Institute of Technology.</namePart>
      <namePart/>
    </name>
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  <identifier type="uri">http://203.159.5.9/ait-thesis/detail.php?q=B22939</identifier>
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    <url displayLabel="Full-Text">http://203.159.5.9/ait-thesis/detail.php?q=B22939</url>
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    <recordCreationDate encoding="marc">250398</recordCreationDate>
    <recordChangeDate encoding="iso8601">20260818153625.0</recordChangeDate>
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