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  <title>DSpace Collection:</title>
  <link rel="alternate" href="http://dspace.univ-setif.dz:8888/jspui/handle/123456789/266" />
  <subtitle />
  <id>http://dspace.univ-setif.dz:8888/jspui/handle/123456789/266</id>
  <updated>2026-05-12T01:47:58Z</updated>
  <dc:date>2026-05-12T01:47:58Z</dc:date>
  <entry>
    <title>Comportement mécanique des composites à matrice céramique</title>
    <link rel="alternate" href="http://dspace.univ-setif.dz:8888/jspui/handle/123456789/267" />
    <author>
      <name>Fantozzi, G.</name>
    </author>
    <author>
      <name>Reynaud, P.</name>
    </author>
    <id>http://dspace.univ-setif.dz:8888/jspui/handle/123456789/267</id>
    <updated>2015-03-25T11:38:46Z</updated>
    <published>2011-01-01T00:00:00Z</published>
    <summary type="text">Titre: Comportement mécanique des composites à matrice céramique
Auteur(s): Fantozzi, G.; Reynaud, P.
Résumé: Ceramic-matrix composites (CMCs) are interesting materials for aeronautic applications because of 

their good mechanical properties at high temperatures even under air. Contrary to bulk ceramics, 

CMCs have a non-brittle mechanical behaviour due tothe high strength of fibres and to optimized 

fibre/matrix interactions after matrix multi-cracking. 

Interactions between fibres and matrix act mainly  at the interface level. When fibres and 

matrix are debonded, fibres slide with friction andenergy dissipation occurs. By using a shear-lag 

model, the energy dissipation can be calculated andthe evolution of the fibre/matrix interaction can be 

followed during fatigue.</summary>
    <dc:date>2011-01-01T00:00:00Z</dc:date>
  </entry>
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