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    <marc:controlfield tag="008">240328e198812uubccad   obt  f000 0 eng d</marc:controlfield>
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      <marc:subfield code="a">CaOODSP</marc:subfield>
      <marc:subfield code="b">eng</marc:subfield>
      <marc:subfield code="e">rda</marc:subfield>
      <marc:subfield code="c">CaOODSP</marc:subfield>
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      <marc:subfield code="a">n-cn---</marc:subfield>
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      <marc:subfield code="a">DR52-11/4-1988E-PDF</marc:subfield>
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      <marc:subfield code="a">Russell, Alan J., </marc:subfield>
      <marc:subfield code="e">author.</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="245" ind1="1" ind2="2">
      <marc:subfield code="a">A damage tolerance assessment of bonded repairs to CF-18 composite components : </marc:subfield>
      <marc:subfield code="b">part I: adhesive properties / </marc:subfield>
      <marc:subfield code="c">A.J. Russell.</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="264" ind1=" " ind2="1">
      <marc:subfield code="a">Victoria, B.C. : </marc:subfield>
      <marc:subfield code="b">Defence Research Establishment Pacific = Centre de recherches pour la défense pacifique : </marc:subfield>
      <marc:subfield code="b">Research and Development Branch, Department of National Defence Canada, </marc:subfield>
      <marc:subfield code="c">December 1988</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="300" ind1=" " ind2=" ">
      <marc:subfield code="a">1 online resource (27, [2] pages) : </marc:subfield>
      <marc:subfield code="b">illustrations, charts</marc:subfield>
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    <marc:datafield tag="336" ind1=" " ind2=" ">
      <marc:subfield code="a">text</marc:subfield>
      <marc:subfield code="b">txt</marc:subfield>
      <marc:subfield code="2">rdacontent</marc:subfield>
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    <marc:datafield tag="337" ind1=" " ind2=" ">
      <marc:subfield code="a">computer</marc:subfield>
      <marc:subfield code="b">c</marc:subfield>
      <marc:subfield code="2">rdamedia</marc:subfield>
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    <marc:datafield tag="338" ind1=" " ind2=" ">
      <marc:subfield code="a">online resource</marc:subfield>
      <marc:subfield code="b">cr</marc:subfield>
      <marc:subfield code="2">rdacarrier</marc:subfield>
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    <marc:datafield tag="490" ind1="1" ind2=" ">
      <marc:subfield code="a">Technical memorandum ; </marc:subfield>
      <marc:subfield code="v">88-25</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="500" ind1=" " ind2=" ">
      <marc:subfield code="a">Title from cover page.</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="500" ind1=" " ind2=" ">
      <marc:subfield code="a">Digitized edition from print [produced by Defence Research and Development Canada].</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="504" ind1=" " ind2=" ">
      <marc:subfield code="a">Includes bibliographical references (page 27).</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="520" ind1="3" ind2=" ">
      <marc:subfield code="a">"The damage tolerance properties of three epoxy adhesives used in the manufacture and repair of the composite structure on the CF-18 aircraft are assessed. The resistance to both static fracture and fatigue crack growth are evaluated. Experimental variables include the mode of fracture (tension and shear), the fatigue load ratio, the test temperature and the method of bonding. Both the static and fatigue tests were found to rank the adhesives in the same order, viz. FM-300K superior to FM-300 superior to EA-9321. The fatigue testing revealed a tendency for delamination type failures to occur at low temperature, a situation likely to lead to non-conservative joint designs. The fatigue crack growth rate data are explained in terms of the failure mechanisms observed. The implication of these findings to the selection of repair adhesives for composite aircraft structure is discussed."--abstract.</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="650" ind1=" " ind2="0">
      <marc:subfield code="a">Graphite composites</marc:subfield>
      <marc:subfield code="x">Testing.</marc:subfield>
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    <marc:datafield tag="650" ind1=" " ind2="0">
      <marc:subfield code="a">Adhesive joints</marc:subfield>
      <marc:subfield code="x">Testing.</marc:subfield>
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    <marc:datafield tag="650" ind1=" " ind2="0">
      <marc:subfield code="a">Airframes</marc:subfield>
      <marc:subfield code="x">Fatigue.</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="650" ind1=" " ind2="6">
      <marc:subfield code="a">Composites de graphite</marc:subfield>
      <marc:subfield code="x">Tests.</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="650" ind1=" " ind2="6">
      <marc:subfield code="a">Assemblages collés</marc:subfield>
      <marc:subfield code="x">Tests.</marc:subfield>
    </marc:datafield>
    <marc:datafield tag="650" ind1=" " ind2="6">
      <marc:subfield code="a">Cellules (Aéronautique)</marc:subfield>
      <marc:subfield code="x">Fatigue.</marc:subfield>
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      <marc:subfield code="a">Technical reports</marc:subfield>
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      <marc:subfield code="a">Rapports techniques</marc:subfield>
      <marc:subfield code="2">rvmgf</marc:subfield>
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      <marc:subfield code="a">Defence Research Establishment Pacific, </marc:subfield>
      <marc:subfield code="e">issuing body.</marc:subfield>
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      <marc:subfield code="a">Canada. </marc:subfield>
      <marc:subfield code="b">Department of National Defence. </marc:subfield>
      <marc:subfield code="b">Research and Development Branch, </marc:subfield>
      <marc:subfield code="e">issuing body.</marc:subfield>
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      <marc:subfield code="a">Technical memorandum (Defence Research Establishment Pacific)</marc:subfield>
      <marc:subfield code="v">88-25.</marc:subfield>
      <marc:subfield code="w">(CaOODSP)9.936067</marc:subfield>
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      <marc:subfield code="q">PDF</marc:subfield>
      <marc:subfield code="s">924 KB</marc:subfield>
      <marc:subfield code="u">https://publications.gc.ca/collections/collection_2024/rddc-drdc/DR52-11-4-1988-eng.pdf</marc:subfield>
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      <marc:subfield code="a">DREP-TM-88-25</marc:subfield>
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