1997
DOI: 10.1016/s0266-3538(97)00030-4
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Analytical method for micromechanics of textile composites

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Cited by 94 publications
(63 citation statements)
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“…The effective properties of each angled unit cell were estimated through the transformation matrix. A similar approach has been proposed in the literature for estimating effective properties of braided (Ayranci and Carey 2008), short fibre (Laspalas et al 2008) and woven (Sankar and Marrey 1997;Shrotriya and Sottos 2005;Vandeurzen et al 1996) composites. For panels with mixed species, a species distribution function in addition to orientation distribution function may be defined to incorporate the effect of different species.…”
Section: Orientation Distributionmentioning
confidence: 99%
“…The effective properties of each angled unit cell were estimated through the transformation matrix. A similar approach has been proposed in the literature for estimating effective properties of braided (Ayranci and Carey 2008), short fibre (Laspalas et al 2008) and woven (Sankar and Marrey 1997;Shrotriya and Sottos 2005;Vandeurzen et al 1996) composites. For panels with mixed species, a species distribution function in addition to orientation distribution function may be defined to incorporate the effect of different species.…”
Section: Orientation Distributionmentioning
confidence: 99%
“…This represents an extension of the micromechanical models used to predict the strength of textile composites [28][29][30][31][32] The significance of including the analysis of moment terms is further illustrated in and 2-1c, the non-uniformity of applied loading leads directly to an appreciable moment term, which must be included in the analysis. In fact, in some cases it is possible that the net force resultant is zero while the effective moment resultant is non-zero, in which case conventional analysis techniques cannot be employed.…”
Section: Finite Element Micromechanical Methodsmentioning
confidence: 99%
“…Physics-based computational models play a key role in predicting damage initiation and propagation as a result of mechanical and thermal loading conditions, simulating the interaction of elastic and electromagnetic waves with the predicted damage, and assessing the current condition of the structure. Because of the complexities associated with aerospace materials, in particular fiber-reinforced composites, damage prediction and quantification studies are often limited to two-dimensional (2D) geometries, linearly elastic constitutive models, prescribed damage initiation location and progression path, and ordered microstructures (Murthy and Chamis, 1986;Freund, 1990;Sankar and Marrey, 1997;Lee and Staszewski, 2003;Swaminathan, Ghosh, and Pagano, 2006;Skoček, Zeman, and Šejnoha, 2008). These assumptions can lead to oversimplification of the problem, and therefore, often result in poor prediction of the critical behavior of these materials.…”
Section: Motivation and Backgroundmentioning
confidence: 99%