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Progressive failure analysis of thin-walled composite structure with open cross-section
Author(s) -
Patryk Różyło,
H. Dębski
Publication year - 2019
Publication title -
aip conference proceedings
Language(s) - English
Resource type - Conference proceedings
eISSN - 1551-7616
pISSN - 0094-243X
DOI - 10.1063/1.5092010
Subject(s) - materials science , finite element method , epoxy , structural engineering , numerical analysis , composite material , composite number , cross section (physics) , compression (physics) , engineering , mathematics , physics , mathematical analysis , quantum mechanics
The subject of study was thin-walled profile made of carbon-epoxy laminate. Specimen had an open cross-section with a symmetrical arrangement of the laminate layers. In presented work, experimental and numerical tests of the axial compression process were carried out up to the loss of load-carrying capacity. Numerical study was carried out using nonlinear analysis of construction stability - Newton-Raphson method. The results of numerical analysis were confronted with the experimental study, which provided the same quality of prepared FEM model.The subject of study was thin-walled profile made of carbon-epoxy laminate. Specimen had an open cross-section with a symmetrical arrangement of the laminate layers. In presented work, experimental and numerical tests of the axial compression process were carried out up to the loss of load-carrying capacity. Numerical study was carried out using nonlinear analysis of construction stability - Newton-Raphson method. The results of numerical analysis were confronted with the experimental study, which provided the same quality of prepared FEM model.

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