Fibre-matrix interfacial adhesion in ®bre-reinforced composites plays an important role in controlling the mechanical properties and overall performance of composites. There are many different micromechanical tests that are used for characterizing the composite interface properties. Within these methods, the single-®bre pull-out test [1], microbond test [2], the single-®bre fragmentation test [3, 4], and the micro-indentation test [5, 6] are becoming more popular among these numerous test methods and are widely used for measuring the interfacial properties in composites. This paper describes the basics, concerns, and sensitivity of using the microbond pull-out test and micro-indentation test. Four types of Owens Corning glass ®bre with different surface treatments were investigated in this study. D.E.R. 331 epoxy resin from Dow Chemicals Company had Lindride 66 curing agent from Lindau Chemicals Inc., were selected as the matrix material which is commonly used in ®lament winding. The resin to curing agent mixing ratio was 100:85 by weight. Both microdroplet samples for microbond pull-out test and composite laminates for microindentation test, were prepared under the same curing cycles: 2 h at 120 8C and 2 h postcure at 180 8C. Table I summarizes a list of ®bre sample identi®cations used for composite laminates that were used in this study. The microbond pull-out test, considered as a modi®ed single-®bre pull-out test, consists of a single ®lament embedded in a polymer matrix. This experiment involves the deposition of a small amount of resin onto the ®bre surface in the form of a droplet which forms concentrically around the ®bre in the shape of an ellipsoid. A single microdroplet of the resin system with a dimension of 50±80 im embedded length was controlled to each ®bre specimen. In the test, a small aluminium microvise with two parallel shearing plates was attached to the base of a vertical Instron testing machine. Prior to the experiment, the shearing plates are positioned just above the sample microdroplet, and the two plates closed to slightly touch the ®bre surface. The plates then move downward and exert a shearing force to create a debonding between the matrix and the ®bre. Load-extension curves were recorded for each specimen, and a suf®cient number of tests were carried out to provide 40 interfacial shear strength values for each ®bre system, from which the mean and standard deviations were calculated. Upon debonding, the pull-out force is recorded, and the interfacial shear strength o is calculated using the equation
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