Asymmetric Shielding in Interfacial Fracture Under In-Plane Shear

[+] Author and Article Information
K. M. Liechti, Y. S. Chai

Department of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, Austin, TX 78712

J. Appl. Mech 59(2), 295-304 (Jun 01, 1992) (10 pages) doi:10.1115/1.2899520 History: Received March 12, 1990; Revised March 15, 1991; Online March 31, 2008


The toughness of a glass/epoxy interface was measured over a wide range of mode mixes. A toughening effect was associated with increasing positive and negative inplane shear components. Optical interference measurements of normal crack opening displacements near the crack front and complementary finite element analyses were used to examine near-front behavior during crack initiation. Estimates of the toughening based on plastic dissipation, bulk viscoelastic dissipation, and interface asperity shielding did not fully account for the measured values. The results suggest that the inelastic behavior of the epoxy, frictional, and, perhaps, three-dimensional effects should be considered.

Copyright © 1992 by The American Society of Mechanical Engineers
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