Composite Materials: Testing, Design, and Acceptance by ASTM International

By ASTM International

STP 1416 gains 17 peer-reviewed papers masking a number of features of checking out, layout, and recognition standards for composite fabrics. issues disguise: • NDT evaluate • fabric Qualification • Full-Scale Structural trying out • toughness • try process improvement • Micromechanics • harm Resistance and Tolerance • impression • Bucking viewers: STP is a useful study software for either the civil engineering infrastructure and aerospace groups

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Groves, "On the Finite Strain Invariant Failure Criterion for Composites," Journal of Composite Materials, Vol. 25, No. 1, 1991, pp. 88-100. , "Failure Criteria for Unidirectional Fiber Composites," J. Applied Mechanics, Vol. 47, 1980, pp. 329-334. , "The Strength of Orthotropic Materials," J. of Composite Materials, Vol. 1, 1967, pp. 200-206. , Yasunaga, T. , "Failure Criterion of Angle Ply Laminate of Fiber Reinforced Plastic and Applications to Optimize the Strength," Fiber Science & Technology, Vol.

2 mm thick, G10 tabs, combined loading). Effect of Tab Thickness The effect o f tab thickness was investigated for square tabs o f each material, and for G10 tabs with different taper angles. All cases had combined loading. For the case o f square tabs, the effects o f tab thickness and tab material on the peak stresses were evaluated simultaneously in Figures 25-27. Also included in these three figures for comparison are the peak stresses for an untabbed specimen, as well as the results from an analysis, that included the adhesive layer but no tab.

Because this error was insignificant and the modelling procedure was more straightforward for point loads, all o f the numerical results discussed below were generated using an applied force boundary condition to model the clamping action o f the D 6641 CLC fixture. 5 P .... 1 I .... 5 f .... 2 J .... 5 I .... 3 I .... evaluated slip loads for G10 tab material~. J 5 --~ 5 0 0 0 ~ Z 40005 3000! 5 , i ' 4000 Total ' Normal ' i . . . 6000 8000 Force i ' 10000 (N) Figure 7 - Analysis of friction in grip surfaces.

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Composite Materials: Testing, Design, and Acceptance by ASTM International
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