Interface strength effects on the compressive-flexural/shear failure mode transition of composites subjected to four-point bending |
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Authors: | G C Shih L J Ebert |
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Affiliation: | (1) Delsen Testing Laboratories, Inc., 91201 Glendale, California, USA;(2) Department of Metallurgy and Materials Science, Case Western Reserve University, 44106 Cleveland, Ohio, USA |
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Abstract: | Wang's microbuckling model 1] has been extended to oriented fibre composites loaded in four-point bending. The modified model
shows that when any internal parameter (e.g. the interface strength) is changed, the resultant change of the interlaminar
shear strength and that of the compressive strength are always of the same sense. Additionally, the degree of change of the
shear strength is always larger than that of the compressive strength. As a consequence of this conclusion, a four-point bend
test piece which normally fails in the flexural compressive mode may fail in the shear mode upon interface degradation. This
was rationalized with the aid of the failure-mode transition diagram 2]. This diagram has been used to explain the change
in bend failure mode resulting from a change of the external parameters, such as the span-to-thickness ratio, and the fibre
fraction. Experiments were conducted to verify such a failure-mode transition behaviour for fibreglass composites of different
interface conditions, when the flexural compressive failure mechanism was of the microbuckling type. |
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