2019
DOI: 10.1016/j.compstruct.2019.111440
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Virtual testing of mechanical response of composite plates with normally distributed wrinkles

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Cited by 4 publications
(2 citation statements)
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“…According to the Equation (1), . The angle is one of the most important parameters describing the wrinkle [ 19 , 20 , 21 , 22 ]. When the ply deflects in the out-of-plane direction, the new compliance matrix of the wrinkle region is expressed as: where [ ] is the out-of-plane stiffness transformation, which is expressed as: …”
Section: Analytical Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…According to the Equation (1), . The angle is one of the most important parameters describing the wrinkle [ 19 , 20 , 21 , 22 ]. When the ply deflects in the out-of-plane direction, the new compliance matrix of the wrinkle region is expressed as: where [ ] is the out-of-plane stiffness transformation, which is expressed as: …”
Section: Analytical Modelmentioning
confidence: 99%
“…Garnich [ 21 ] established a micromechanical model of sinusoidal wrinkles and studied the equivalent elastic modulus and failure behavior of composite structure with wrinkles. Based on Takeda’s model, Shen [ 22 ] numerically transformed and applied the two-step homogenization of representative volume element theory on the MATLAB platform and proposed a three-dimensional stiffness finite element analysis method to study the macroscopic mechanical response of the wrinkle defects on the composite structures.…”
Section: Introductionmentioning
confidence: 99%