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    <subfield code="a">B-6208</subfield>
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    <subfield code="a">Onset of matrix cracking in angle-ply ceramic matrix composites</subfield>
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  <datafield tag="490" ind1="0" ind2=" ">
    <subfield code="v">International Journal of Mechanical Sciences, 44(10), p.2173-2187 , 2002</subfield>
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  <datafield tag="520" ind1="3" ind2=" ">
    <subfield code="a">The problem of initial damage in angle-ply [-m/0n/m]and [-/]ceramic matrix composites subjected to axial tension is considered in this paper. The damage is in the form of matrix cracks that may appear in either inclined (- and lamination angle)or longitudinal layers. As follows from the analysis, if the lamination angle of the inclined layers is small, the initial failure occurs in the 0-layers of [-m/0n/m]composites or in [-/]composites in the form of bridging cracks. However, if the inclined layers form a larger angle with the load direction, they fail due to tunneling cracks. It is shown that the boundary between two different modes of failure in a representative SiC/CAS composite corresponds to a lamination angle equal to 35&#xB0; in the case of [-m/0n/m]composites. In the case of [-/]laminates, the boundary value of the lamination angle is equal to 45&#xB0;, i.e. bridging cracks form if &lt;45&#xB0; and tunneling cracks appear if &gt;45&#xB0;</subfield>
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    <subfield code="a">CERAMIC MATRIX COMPOSITES</subfield>
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    <subfield code="a">MATRIX CRACKS</subfield>
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    <subfield code="a">Byrd, L.W.</subfield>
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    <subfield code="a">Birman, V.</subfield>
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    <subfield code="z">Para ver el documento ingresa a Google con tu cuenta: @cicy.edu.mx</subfield>
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    <subfield code="d">2025-06-25</subfield>
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    <subfield code="o">B-6208</subfield>
    <subfield code="r">2025-06-25 12:46:38</subfield>
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