SYNOPSISIn the present study, the prefailure damage processes of a series of short glass fiber/mica/ epoxy composites under three-point bending were elucidated using acoustic emission ( AE) coupled with in situ scanning electron microscopy ( SEM) observations. This study consisted of a detailed investigation of the damage tolerance of composite systems that had constant inorganic content of 75% by weight with a varying ratio of glass fibers to mica. The flexural strength was found to increase from 11 to 21 ksi as the glass fiber content increased (mica content decreased), while the flexural modulus decreased from 5.0 to 2.5 Msi. By monitoring the AE during flexural deformation of the glass fiber-to-mica ratio composites, it was determined that low amplitude (0-42 db) AE events, which occurred throughout the deformation process, were caused by matrix cracking, whereas the high-amplitude (43-100 db) AE events, which occurred just prior to failure, were caused by a fiber-related mechanism. In situ SEM observations of the composites during flexural deformation allowed a correlation between the AE and the damage mechanisms as a function of strain. In the all-mica composite, microcracking initiated in the linear region a t preexisting flaws, on the order of 10 pm, located at the mica interface. These microcracks grew along the mica contours over the majority of the deformation process, emitting low-amplitude events, until final fracture occurred at relatively low strains. In the glass fiber-containing composites, microcracking initiated in the linear region a t preexisting flaws and voids, on the order of 10 pm. These microcracks grew slowly, emitting low-amplitude events, as the strain increased, but were prevented from causing failure at low strains because of the toughening effect of the glass fibers. At sufficiently high strains, however, fiber breakage and fiber pull-out occurred that corresponded to the high-amplitude events detected by the AE. At strains just prior to failure, catastrophic crack growth occurred, producing a rapid increase in both low-and high-amplitude events, causing ultimate failure.
INTRODUCTIONComposites are finding increased usage as structural components, oftentimes replacing materials in which the damage and failure mechanisms are well understood. Since damage accumulation in composites is closely related to the actual strength, stiffness, and life of the materials, understanding of the failure mechanisms and damage accumulation are of utmost importance.' This, however, has proved difficult To whom correspondence should be addressed. Continuous fiber-epoxy composites have received an immense amount of attention in the literature because of their structural uses. These structural uses are, in part, due to the varied processing techniques, such as hand lay-up, filament winding, and pultrusion, which are available. Although the optimum processing technique is imperative to the successful use of these materials, even more critical is an understanding of their failure mechanisms. The evaluatio...