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Numerical analysis of the behavior of a three-layer honeycomb panel with interlayer defects under action of dynamic load
In: Structural Mechanics of Engineering Constructions and Buildings, Vol 17, Iss 4, Pp 357-365 (2021) (2021)
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Numerical analysis of layered composite panel behavior with interlaminar defects subject to dynamic loads
In: Structural Mechanics of Engineering Constructions and Buildings, Vol 15, Iss 2, Pp 127-134 (2019) (2019)
Abstract: Aims of research. Polymer unidirectional composite laminate panel behavior with interlaminate defects under action of different dynamic loads is consider. Methods. Normal modes and eigenvalues of rectangular composite panels in the presence multiple delamination different sizes ellipsoidal form are calculated. The dependences of the maximum deflections from the frequency of the stationary pressure field action are constructed. Distribution field of panels plies failure index under action of nonstationary pressure field by using different failure criteria for composites is determined. Results. Modeling methodology composite panels behavior in the presence multiple interlaminar defects under action of different dynamic loads is developed. Analysis of failure panel with the use of different failure criteria for composites is carried out.
Keyword: Architectural engineering. Structural engineering of buildings; composite failure criteria; composite panel; finite element method (FEM); interlaminar defect; nonstationary load; numerical modeling; TH845-895
URL: https://doi.org/10.22363/1815-5235-2019-15-2-127-134
https://doaj.org/article/b4d11e1e019f43a6937a7fa0ec2a8b5f
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