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  <titleInfo>
    <title>Application of a turbulence model to an oscillatory boundary layer</title>
  </titleInfo>
  <name type="personal">
    <namePart>Arain, Ahmad Sana</namePart>
    <role>
      <roleTerm authority="marcrelator" type="text">creator</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Tanaka, Hitoshi</namePart>
    <role>
      <roleTerm type="text">Chairperson</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Suphat Vongvisessomjai</namePart>
    <role>
      <roleTerm type="text">Examination Committee</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Tawatchai Tingsanchali</namePart>
    <role>
      <roleTerm type="text">Examination Committee</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Sutat Weesakul</namePart>
    <role>
      <roleTerm type="text">Examination committee</roleTerm>
    </role>
  </name>
  <name type="corporate">
    <namePart>Government of Denmark</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>1992</dateIssued>
    <issuance>monographic</issuance>
  </originInfo>
  <language>
    <languageTerm authority="iso639-2b" type="code">eng</languageTerm>
  </language>
  <physicalDescription>
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    <extent>113 leaves</extent>
  </physicalDescription>
  <abstract>The most popular low Reynolds' number model is applied to steady flow, wave motion and  wave-current coexistent motion. In doing so, the model equations are non dimensionalized and then finite  difference equations are derived using an implicit finite difference scheme.  A computer program is developed in FORTRAN 77 to solve these finite difference equations  simultaneously. A variety of numerical experiments is performed for steady and unsteady flows.  The transitional flow is successfully predicted for the first time by k - E model. The computed results  are compared with the available experimental data and good agreement is found.</abstract>
  <note>A thesis submitted in partial fulfillment of the requirements for the degree of Master of Engineering, School of Engineering and Technology</note>
  <note>Thesis (M.Eng.) - Asian Institute of Technology, 1992</note>
  <subject authority="lcsh">
    <topic>Turbulence</topic>
    <topic>Mathematical models</topic>
  </subject>
  <subject authority="lcsh">
    <topic>Boundary layer</topic>
  </subject>
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    <titleInfo>
      <title>Thesis ; no. WA-92-1</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=B17241</identifier>
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    <url displayLabel="Full-Text">http://203.159.5.9/ait-thesis/detail.php?q=B17241</url>
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