STP593: Concepts for Crack Arrestment in Composites

    Sendeckyj, GP
    Aerospace engineer, Air Force Flight Dynamics Laboratory, Wright-Patterson AFB, Ohio

    Pages: 12    Published: Jan 1975


    Abstract

    Crack arrestment criteria for composite panels containing buffer (or crack-arrestment) strips are derived for the cases of cracks within the primary and buffer-strip material. The criteria, which can be used to size the buffer strips to arrest cracks of given length, are in good agreement with the available experimental data on crack arrest in composite panels.

    Keywords:

    fracture properties, composite materials, stresses, laminates, crack propagation, crack arrest, damage control


    Paper ID: STP34800S

    Committee/Subcommittee: D30.04

    DOI: 10.1520/STP34800S


    CrossRef ASTM International is a member of CrossRef.