2022
DOI: 10.1177/00219983221117216
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Design allowables of composite laminates: A review

Abstract: The design and certification process of composite structures relies on the building-block approach, which starts from the mechanical characterization of the material at coupon-level. The certification of composite laminates is thus the first challenge and requires the definition of the design allowables, which are statistically defined as established by the Composite Material Handbook. These quantities are strength or strain values indicated as A- or B-basis and an accurate estimation is needed in order to gua… Show more

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Cited by 9 publications
(3 citation statements)
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“…The mechanical analysis of anisotropic and isotropic materials has the same equilibrium equations, geometric equations, coordination equations, and boundary conditions, and the main difference is that the constitutive equations of stress and strain are different. When analyzing the mechanical properties of composites, the following conditions are often assumed to hold [ 41 , 42 , 43 ]: (1) Assume that the laminate is continuous; (2) Assumed that the unidirectional laminates are homogeneous; (3) Assumed that the unidirectional laminates are orthotropic anisotropic; (4) Assume that the laminates are linearly elastic; and (5) Assumed that the deformation of laminate is very small.…”
Section: Basic Theory Of Composite Mechanicsmentioning
confidence: 99%
“…The mechanical analysis of anisotropic and isotropic materials has the same equilibrium equations, geometric equations, coordination equations, and boundary conditions, and the main difference is that the constitutive equations of stress and strain are different. When analyzing the mechanical properties of composites, the following conditions are often assumed to hold [ 41 , 42 , 43 ]: (1) Assume that the laminate is continuous; (2) Assumed that the unidirectional laminates are homogeneous; (3) Assumed that the unidirectional laminates are orthotropic anisotropic; (4) Assume that the laminates are linearly elastic; and (5) Assumed that the deformation of laminate is very small.…”
Section: Basic Theory Of Composite Mechanicsmentioning
confidence: 99%
“…This dictates the need for failure characterization at all three length scales namely: micro, meso and macro scales respectively [9]. FEA models are usually too simple to characterize failure at all three-length scales and experimental testing on its own can also be prohibitively expensive [10].…”
Section: Introductionmentioning
confidence: 99%
“…Applying traditional reverse-design methods to composites, which are inherently anisotropic and vary in their material elastic modulus, layer thickness, lamination angle, and stacking sequence, presents significant challenges [10]. The accurate analysis of materials in laminated composites requires iterative experimental procedures, such as cyclic load tests, cross-sectional evaluations, and fiber volume ratio assessments.…”
Section: Introductionmentioning
confidence: 99%