2018
DOI: 10.1016/j.compstruct.2017.12.042
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Dynamic instability of variable angle tow composite plates with delamination

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Cited by 15 publications
(3 citation statements)
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References 43 publications
(109 reference statements)
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“…A study [4] showed that the general anisotropic property and the variable in-plane stiffness property inherent in composites create significant challenges in the static and dynamic analysis of these new types of variable stiffness composite structures. Therefore, it is important to develop mechanical models and calculation methods for composite lamellar-shell structures of variable stiffness to understand their complex mechanical mechanisms and promote their further application in aerospace engineering.…”
Section: Introductionmentioning
confidence: 99%
“…A study [4] showed that the general anisotropic property and the variable in-plane stiffness property inherent in composites create significant challenges in the static and dynamic analysis of these new types of variable stiffness composite structures. Therefore, it is important to develop mechanical models and calculation methods for composite lamellar-shell structures of variable stiffness to understand their complex mechanical mechanisms and promote their further application in aerospace engineering.…”
Section: Introductionmentioning
confidence: 99%
“…The bending behavior of anisotropic composite laminates was analyzed by Wang et al [ 5 ] with the assistance of the strip element method as well as the governing equation was deduced by using classical laminated theory. The dynamic instability of the delaminated composite plates on the basis of the composite plate's buckling properties and its fundamental frequencies were analytically modeled with the aid of the classical laminated plate theory by Chen et al [ 6 ] Lopez et al [ 7 ] presented an optimization study of the hybrid laminated composite structures with the different design variables (fiber angle orientations, material properties and the number of plies) through genetic algorithm technique. The Tsai‐Wu failure criteria, pluck failure criteria (PFC) were utilized in this study to estimate the maximum stress components of the laminates.…”
Section: Introductionmentioning
confidence: 99%
“…The strip element was presented in the form of a square laminated composite plate with many boundary situations and load conditions to compare with a Rayleigh-Ritz method, and received an excellent agreement. Chen [20] studied a rectangular single delamination behavior of dynamic instability using analytical modeling of CLPT by applying the potential energy-based principles. He examined the effect of composite delamination on a natural frequency, buckling, and dynamic instability by using numerical examples.…”
Section: Introductionmentioning
confidence: 99%