Abstract
Recently, laminate structures have been investigated as a method for enhancing the fracture resistance of discontinuously reinforced aluminum (DRA) materials. Laminated DRA materials have been constructed which contain alternating layers of DRA material and monolithic aluminum. Initiation in these laminates has been found to preferentially occur in the DRA layers. After initiation, stable crack growth is produced in the DRA material via a crack bridging mechanism in which the ductile aluminum ligaments in the crack wake serve to reduce the driving force for propagation in the DRA layer. In a manner similar to that of Kaufman and Goolsby, it was proposed that the initiation toughness of the DRA laminates may be improved if the thickness of the DRA layers was reduced. The goal of this study was to investigate the influence of thickness on the toughness of a DRA material based upon a transition from plane strain to plane stress conditions and how this transition may affect the fracture resistance of laminated DRA materials. The following sections document initial attempts to determine the influence of DRA thickness on toughness both in conventional DRA materials and laminated DRA materials.
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