The Fracture Toughness of Adhesive-Bonded Joints

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Abstract
Fracture mechanics is related to adhesion theory and the testing of adhesive-bonded joints in the lap-shear configuration. The complexity of the stress field necessitates the strain energy release rate approach, which is followed to derive the relation for a lap-shear sample: Gc = Pc 2/4b (dC/da). Gc is the fracture toughness (critical strain energy release rate), Pc is the breaking or crack instability load, a and b are crack lengths and widths, respectively, and C is the sample compliance for the Tap-shear sample with a crack of these dimensions at each loading edge. It was found that Gc ranged from 1.18 to 1.42 with an average value of 1.34 in.-lb./in.2 for epoxy bonded aluminum strips (EPON 934 and Alcald 2024-T3). Evidence, in the form of photoelastic stress patterns, suggesting that crack extension occurs in the opening mode in lap-shear samples is presented and discussed.

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