Mode I Interlaminar Fracture Toughness of Composites Using Slender Double Cantilevered Beam Specimens

Author:

Keary Paul E.1,Ilcewicz Larry B.1,Shaar Casey2,Trostle Jess3

Affiliation:

1. Boeing Commercial Airplane Company P.O. Box 3707 M/S 6C-11 Seattle, WA 98124

2. Photon Kinetics S W Cirrus Beaverton, OR 97075

3. Morton Thiokol Inc. P.O. Box 524 M/S 287E Brigham City, UT 84302

Abstract

The use of slender double cantilever beam specimens for measuring the mode I in terlaminar fracture toughness was critically evaluated. Experiments were performed with unidirectional composites to judge the validity of using data from multiple crack jumps on a single specimen. Three approaches for calculating the strain energy release rate were compared. These included an energy rate determination of the JI-integral, a compliance calibration procedure and an analytical equation based on linear beam bending. The fracture toughness was overestimated by the latter two approaches. Per manent deflection was seen to accumulate in the arms of the double cantilever beam specimens as the cracked surface area increased. This component of deflection must be accounted for in all forms of analysis with DCB specimens.

Publisher

SAGE Publications

Subject

Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

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