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  <titleInfo>
    <title>Spline approximation as applied to aeronautical problems</title>
  </titleInfo>
  <name type="personal">
    <namePart>Ramamoorthy, P.</namePart>
    <role>
      <roleTerm authority="marcrelator" type="text">creator</roleTerm>
    </role>
  </name>
  <name type="personal">
    <namePart>Narayana, C. L.</namePart>
    <role>
      <roleTerm type="text">joint author.</roleTerm>
    </role>
  </name>
  <typeOfResource>text</typeOfResource>
  <genre authority="marc">bibliography</genre>
  <originInfo>
    <place>
      <placeTerm type="code" authority="marccountry">ii</placeTerm>
    </place>
    <place>
      <placeTerm type="text">Bangalore</placeTerm>
    </place>
    <publisher>National Aeronautical Laboratory</publisher>
    <dateIssued>1969</dateIssued>
    <issuance>monographic</issuance>
  </originInfo>
  <language>
    <languageTerm authority="iso639-2b" type="code">eng</languageTerm>
  </language>
  <physicalDescription>
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    <extent>i, 5 p. 29 cm.</extent>
  </physicalDescription>
  <note type="statement of responsibility">by P. Ramamoorthy &amp; C. L. Narayana.</note>
  <note>Bibliography: p. 5.</note>
  <subject authority="lcsh">
    <topic>Airplanes</topic>
    <topic>Wings</topic>
    <topic>Testing</topic>
  </subject>
  <subject authority="lcsh">
    <topic>Spline theory</topic>
  </subject>
  <subject authority="lcsh">
    <topic>Pressure</topic>
  </subject>
  <classification authority="lcc">TL504 .B35 TN-20</classification>
  <classification authority="lcc">TL574.P7</classification>
  <classification authority="ddc">629.13/008 s 629.134/32</classification>
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    <titleInfo>
      <title>NAL Technical note, TN-20</title>
    </titleInfo>
    <name type="corporate">
      <namePart>Bangalore, India (City).</namePart>
      <namePart>National Aeronautical Laboratory.</namePart>
      <namePart/>
    </name>
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  <identifier type="lccn">sa 68019765 //r82</identifier>
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