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    Compliance measurements of chevron notched four point bend specimen (1994)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The experimental stress intensity factors for various chevron notched four point bend specimens are presented. The experimental compliance is verified using the analytical solution for a straight through crack four point bend specimen and the boundary integral equation method for one chevron geometry. Excellent agreement is obtained between the experimental and analytical results. In this report, stress intensity factors, loading displacements and crack mouth opening displacements are reported for different crack lengths and different chevron geometries, under four point bend loading condition.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA-TM-106538 , E-8679 , NAS 1.15:106538
    Format: application/pdf
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