0000000000761552

AUTHOR

Masaki Hojo

showing 3 related works from this author

Empirical model for stress ratio effect on fatigue delamination growth rate in composite laminates

2004

An empirical model is proposed for the stress ratio effect on the fatigue delamination growth rate in composite laminates under single-mode loading, intending to provide a simple and accurate description tool in engineering application. The model is based on heuristic considerations of damage accumulation ahead of the crack. Linear cumulative assumption is used for damage estimation. Comparison of the prediction based on the proposed model with the test results for different carbon, glass, and alumina fibre-reinforced composites at several stress ratios shows reasonable agreement.

Materials scienceStress ratioMechanical EngineeringDelaminationComposite laminatesIndustrial and Manufacturing EngineeringdelaminationStress (mechanics)fatigue crack growthMechanics of MaterialsModeling and Simulationpolymer matrix compositesfatigue modellingGeneral Materials ScienceGrowth rateComposite materialINTERNATIONAL JOURNAL OF FATIGUE
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Glass fibre strength distribution determined by common experimental methods

2002

The tensile strength of brittle fibres is routinely described by the Weibull distribution. The parameters of the distribution can be obtained from tests on single fibres and fibre bundles or from model composite tests. However, there is growing evidence that the distribution parameters obtained by different experimental techniques differ systematically. In order to investigate the possible causes of such discrepancies, single-fibre tension, fibre bundle, and single-fibre fragmentation tests are employed in this study to obtain strength distribution of commercial E-glass fibres. The results reveal parameter dependence on the approach used to extract the distribution parameters from experimen…

Materials scienceTension (physics)glass fibresComposite numberGlass fiberGeneral EngineeringShape parameterMathematics::Algebraic GeometryBrittlenessstatisticsfragmentationUltimate tensile strengthCeramics and CompositesFiber bundleComposite materialstrengthweibull distributionWeibull distributionComposites Science and Technology
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Model of delamination propagation in brittle-matrix composites under cyclic loading

2001

A model of interlaminar fatigue crack growth based on damage accumulation ahead of the crack is proposed. Linear cumulative assumption is used for damage estimation, and a quadratic failure criterion is applied for complex interlaminar loading. Model parameters are determined from mode I and mode II fatigue tests, and used to predict mixed-mode delamination propagation rate. Comparison of theoretical prediction with mixed-mode test results for different brittle graphite FRP at several mode- and load ratios show reasonable agreement.

Materials sciencePolymers and PlasticsMechanical EngineeringDelaminationMode (statistics)laminated compositeFracture mechanics02 engineering and technologyParis' lawFibre-reinforced plastic021001 nanoscience & nanotechnologyFatigue limitdelaminationMatrix (mathematics)020303 mechanical engineering & transportsBrittleness0203 mechanical engineeringMechanics of MaterialsMaterials ChemistryCeramics and CompositesComposite material0210 nano-technologycyclic loadingJOURNAL OF REINFORCED PLASTICS AND COMPOSITES
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