Titlebook: Composite Structures 4; Volume 2 Damage Asse I. H. Marshall Book 19871st edition Elsevier Applied Science Publishers Ltd 1987 alloy.composi

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Considerations for Designing with Metal Matrix Composite Materialseneral design considerations of technical criteria and operational and cost criteria are discussed briefly. Relevant MMC material properties equations are given in a table. The structural indices that are used to calculate ratios between MMC and conventional material to compare weight to strength, i

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A Causal Approach to Effective Dynamic Moduli of Random Compositestly, large-scale structures made of these materials possess the absorption capability because of energy transfer to incoherent motions. This chapter presents some of the recently established theories of these phenomena and their implications to predictions of effective dynamic moduli. It is shown th

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The Effects of Combined Shear and Direct Loads on the Damping Behaviour of Unidirectional FRPsof unidirectionally reinforced FRPs..A theoretical model based on the energy being dissipated in the resin only is derived using equivalent strain analyses previously developed for isotropic materials. The model was applied to two different combined loading situations and predictions compared with e

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Effects of Shear Deformation on the Onset of Flexural Failure in Symmetric Cross-ply Laminated Rectample higher-order shear deformation plate theory (HSDT) and simple lamina and interlaminar shear failure criteria. Initial failure pressures and associated plate centre deflections are computed for CFRP plates. The computed values are compared with corresponding values derived from classical laminat

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Micromechanical Failure Analysis of Elliptic, Cross-ply Laminates under Flexural Loads laminates under a uniformly distributed load are treated. The effects of fibre type and content, voids and hygrothermal conditions are investigated on the failure load and its location by means of micromechanical relations from which elastic and strength properties of the composite are computed. Nu

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