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  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Applied composite materials 4 (1997), S. 121-132 
    ISSN: 1573-4897
    Keywords: textile composites ; design of 3D braided preforms ; yarn structures ; composite properties ; close-loop design optimization
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract This paper outlines a method which links the following analytically simulated events in sequence: (1) braiding of a 3D preform of tubular cross-section – characterized by a set of braiding parameters defining the braiding setup and braiding steps; (2) geometric description of the yarn topology in the braided preform – in explicit terms of a set of topological parameters defined by the preform shape and the braiding parameters; (3) description of the exact yarn distribution after preform consolidation with a binding matrix – the values of the topological parameters are related to the exterior dimensions and surface features of the consolidated preform; and (4) forecasting the mechanical properties in the final composite – via a suitable micromechanics model that takes into account the spatial yarn distribution in the composite and properties of the constituents. It is shown that these sequential events form a closed-loop linkage which connects the properties of the final composite all the way to the initial preform braiding setup design; the analytically derived interrelationships in each link can provide for design simulations of three dimensionally braided, complex-shaped and property-specific composite articles. In order to obtain explicit interrelationships, the 4-step 1×1 braiding procedure is utilized in the analytical development. For the same reason, a graphite yarn and an epoxy resin with known properties are used in illustrative examples. There can be more than one braiding setup design for a preform to have the same shape and overall dimensions; but the yarn structure and properties in the final composite can differ widely if different braiding setups are used. Hence an optimization for a composite shape to meet the prescribed requirements may be conducted using the developed closed-loop.
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    Springer
    Computational mechanics 14 (1994), S. 84-99 
    ISSN: 1432-0924
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract This paper presents a local-global matching method to effectively determine the detail spatial structure and magnitude of the locally singular stress field as well as the complete global stress distribution in the single fiber pullout model. The motivation to solve for the local stress field is the belief that these accentuated stresses, strains and energy are likely to induce damage. The local-global matching method consists of three components: a local analysis, a global analysis, and proper matching of the local asymptotic field to the global complete stress field. The method as developed is applicable for various fiber-matrix interfacial conditions: namely perfectly bonded interface, partially debonded interface with interfacial crack, or debonded interface with frictional interfacial sliding. In this paper, results for perfectly bonded fiber-matrix interface are presented to illustrate key features of the local-global matching method. For this problem, the local stress field is asymptotically singular at the location where the fiber protrudes from the matrix. A local analysis at the fiber protrusion point reveals that, when the fiber is stiffer than the matrix, the most dominant singular stresses are of the from: $$\sigma _{ij} (\rho ,\theta ) = K\rho ^\lambda \tilde \sigma _{_{ij} } (\theta )$$ where the exponent λ is real-valued and λ〈0. The local analysis can solve for the spatial structure of the local field: its radial dependence ρλ and angular variations $$\tilde \sigma _{ij} (\theta )$$ . The actual magnitude of the local stress field is scaled by the amplitude factor K which depends upon externally applied load and global boundary conditions. The global analysis, performed using a finite element model, can be subjected to arbitrary fiber-pulling load and/or thermal load. With solutions from both the local analysis and global analysis, a local-global matching method based on angular variation of stresses is developed to accurately determine K. In local-global matching, a proper region is selected in which the angular variation of stresses of the local field is scaled to match the angular variation of the finite-element computed full-field stresses. Several monitoring parameters are developed to measure the quality of the matching and to determine the region of dominance of the local asymptotic field. The local analysis shows that in many composite material systems, there are two singular terms in the local field: $$\sigma _{ij} K = \rho ^{\lambda _1 } \tilde \sigma _{ij}^1 (\lambda ;{\text{ }}\theta ) + K_2 \rho ^{\lambda 2} \tilde \sigma _{ij}^2 (\lambda ;{\text{ }}\theta ), - 1 〈 \lambda _1 〈 \lambda _2 〈 0$$ . Hence, local-global matching procedures have been developed for both one-term field and two-term field. The matching method is further generalized to determine complex-valued K for composites having complex-valued λ. The local-global matching method may also be applied to problems with material nonlinearity.
    Type of Medium: Electronic Resource
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  • 3
    Electronic Resource
    Electronic Resource
    Springer
    International journal of fracture 47 (1991), S. 1-24 
    ISSN: 1573-2673
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract This paper presents a fracture analysis for a bent crack in an infinite orthotropic plate subjected to a far-field uniform tensile stress. To determine parameters relevant to the mixed-mode fracture conditions at the tip of the bent crack, the problem is formulated in terms of singular integral equations with generalized Cauchy kernels. The resulting system of equations is then solved numberically employing a Gaussian quadrature and the collocation method. Stress intensity factors, k1 and k2, and the strain energy release rates, GI and GII at the tip of the bent crack are obtained for various values of fibres direction θ and L2/L1 ratios. Extensive results for a graphite-epoxy unidirectional composite laminate are presented.
    Type of Medium: Electronic Resource
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  • 4
    Publication Date: 1991-01-01
    Print ISSN: 0376-9429
    Electronic ISSN: 1573-2673
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Published by Springer
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  • 5
    Publication Date: 2011-08-16
    Description: Consideration of coupled stress waves generated by an impulsive load applied at one end of a semiinfinite plate. For the field equations governing the one-dimensional coupled waves a hyperbolic system of equations is obtained in which a strong coupling in the second derivatives exists. The method of characteristics described by Chou and Mortimer (1967) is extended to cover the case of strong coupling, and a study is made of the transient stress waves in a semiinfinite plate subjected to an initial step input. Coupled discontinuity fronts are found to propagate at different velocities. The normal plate stress and the bending moment at different time regimes are illustrated by graphs.
    Keywords: STRUCTURAL MECHANICS
    Type: AIAA Journal; 10; Aug. 197
    Format: text
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  • 6
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2013-08-29
    Description: Material defects may be introduced willingly or unwillingly during material manufacturing and structural component fabrication stages. Their presence in the material plays a dominant role in determining the material's strength and the associate failure mechanisms. In the sense that the size and the number of defects may increase with the volume of the material, the effect of dimensional scaling may manifest itself in the dependence of material strength on volume. Or, alternatively, there may exist a scaling effect of material defects. In fiber-reinforced composites, manufacturing or fabrication defects may come in several forms: matrix voids, matrix microcracks, fiber misalignment, broken fibers, or interface disbonds, just to mention a few. These are interacting and competing defects in the sense that one type of defect may become dominant under one stress condition and another type of defect may become dominant under a different stress condition. This happens because the fiber reinforcement network, together with the distribution of defects, constitutes the prime microstructure of the composite, and there exist continued interactions between the evolving microstructure and the distribution of defects. In the process, the scaling effects of defects are complicated by this interaction. In this presentation, the scaling effects of defects in fiber-reinforced composites will be briefly discussed with the introduction of the concept of effective defects. It is then shown with the aid of some actual experimental and analysis results that the scaling effects are very much present, but they are regulated by the characteristic dimension of the composite microstructure due to the aforementioned microstructure-defect interaction effect.
    Keywords: STRUCTURAL MECHANICS
    Type: NASA. Langley Research Center, Workshop on Scaling Effects in Composite Materials and Structures; p 179-195
    Format: text
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