Volume 7, Issue 3 (September 1985)

    A Damage Tolerant Design Parameter for Graphite/Epoxy Laminated Composites

    CODEN: CTROAD

      Format Pages Price  
    PDF Version 5 $25   ADD TO CART


    Abstract

    The results of an extensive experimental investigation of the fracture behavior of notched graphite/epoxy laminates are presented. Twenty-seven laminates with different stacking sequences and laminate thicknesses have been studied. The data presented herein suggest that a damage tolerant design parameter exists that is relatively independent of ply stacking sequence and laminate thickness.


    Author Information:

    Harris, CE
    Assistant professor, Texas A&M University, College Station, TX

    Morris, DH
    Professor, Virginia Polytechnic Institute and State University, Blacksburg, VA


    Stock #: CTR10301J

    ISSN: 0884-6804

    DOI: 10.1520/CTR10301J

    ASTM International is a member of CrossRef.

    Author
    Title A Damage Tolerant Design Parameter for Graphite/Epoxy Laminated Composites
    Symposium , 0000-00-00
    Committee D30