Evaluation of the fibre-matrix debond strength of a Ti-22Al-23Nb (AT.%)/trimarc metal matrix composite

J. L. LeBoeuf, C. J. Boehlert

    Research output: Contribution to journalArticle

    Abstract

    A methodology involving experimental testing using a cruciform specimen geometry has been developed which assists fibre/matrix debond strength calculations for continuously reinforced metal matrix composites (MMCs) [1-11]. Using this methodology the interfacial debond strength of a MMC consisting of a Ti-22Al-23Nb(at.%) matrix alloy embedded with Trimarc silicon-carbon fibres was evaluated. The fibre/matrix debond location was identified to be within the carbon layers at the fibre-matrix interface and the debond strength was found to be almost negligible.

    Original languageEnglish (US)
    Pages (from-to)17-21
    Number of pages5
    JournalAdvanced Composites Letters
    Volume19
    Issue number1
    StatePublished - Jan 2010

    Profile

    Enzyme Reactivators
    Abnormal Erythrocytes
    Fibers
    Composite materials
    Metals
    Blood Stains
    Community Psychiatry
    Geometry
    Carbon fibers
    Silicon
    Carbon
    Testing

    ASJC Scopus subject areas

    • Ceramics and Composites
    • Industrial and Manufacturing Engineering

    Cite this

    Evaluation of the fibre-matrix debond strength of a Ti-22Al-23Nb (AT.%)/trimarc metal matrix composite. / LeBoeuf, J. L.; Boehlert, C. J.

    In: Advanced Composites Letters, Vol. 19, No. 1, 01.2010, p. 17-21.

    Research output: Contribution to journalArticle

    LeBoeuf, J. L.; Boehlert, C. J. / Evaluation of the fibre-matrix debond strength of a Ti-22Al-23Nb (AT.%)/trimarc metal matrix composite.

    In: Advanced Composites Letters, Vol. 19, No. 1, 01.2010, p. 17-21.

    Research output: Contribution to journalArticle

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