2010
DOI: 10.1016/j.compstruct.2010.04.016
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An analytical method for calculating stiffness of two-dimensional tri-axial braided composites

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Cited by 53 publications
(40 citation statements)
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“…Table 1 shows for the longitudinal Young's modulus E x , that the maximum average error is shown for the iso-strain model with 11.1%. It should be noticed that in previous studies [26,27,32], the iso-strain model shows good predictions for E x when modeling 2D woven and braided composites, while it suffers with 3D angle interlock woven composites with errors exceeding the 20% [31]. Very good agreement is shown with the MOC, the Ruan and Chou and the 3SHM models with an average error under the 7% margin and better than that obtained by the AEHM.…”
Section: Comparative Studysupporting
confidence: 54%
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“…Table 1 shows for the longitudinal Young's modulus E x , that the maximum average error is shown for the iso-strain model with 11.1%. It should be noticed that in previous studies [26,27,32], the iso-strain model shows good predictions for E x when modeling 2D woven and braided composites, while it suffers with 3D angle interlock woven composites with errors exceeding the 20% [31]. Very good agreement is shown with the MOC, the Ruan and Chou and the 3SHM models with an average error under the 7% margin and better than that obtained by the AEHM.…”
Section: Comparative Studysupporting
confidence: 54%
“…Then, averaging the stiffness over the volume or length of curved yarns under an iso-strain assumption is easy and straightforward. The iso-strain model, which provides an evaluation of all in-plane and out of plane elastic properties, proves relative effectiveness in modeling 2D and 3D braided composites [26,27,32] and 3D orthogonal woven composites [30]. Even to its simplicity, easy to use and applicability on all textiles architectures, the main disadvantage of the model remains in the assumption of only an iso-strain condition.…”
Section: Discussionmentioning
confidence: 98%
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“…The tensile properties were obtained based on ASTM standard D3039, while the in-plane shear properties were conducted according to ASTM standard D3518. The predicted effective elastic modulus and strength are listed in Table 5 and compared with the test results of Chen [26], and the numerical results using Quek model [29] and Shokrieh model [30]. The numbers in the parentheses illustrate the error percent between these models and experimental results.…”
Section: Configuration Bmentioning
confidence: 99%
“…The relation between fiber stress σf and matrix stress σm in a fiber‐reinforced composite is usually established by a bridging model . As is shown in Fig.…”
Section: Theoretical Backgroundsmentioning
confidence: 99%