Buckling of simply supported GLARE cylindrical panels subjected to uniform compression
نویسندگان
چکیده
In this article, the elastic buckling behaviour of cylindrical GLARE (GLAss REinforced) panels with classically simply supported boundary conditions under uniaxial compression is investigated using finite element method (FEM) and eigenvalue analysis. The coefficient-curvature parameter diagrams five grades are obtained studied along two glass-fiber composites monolithic 2024-T3 aluminum, validated FEM models. It found that aluminium has a stronger impact on than composite layers. From constructed coefficient - curvature in double logarithmic scale it there an approximately linear relation between panels. Based finding, appropriate regressions implemented order to derive approximate analytical formulas as function for considered materials.
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ژورنال
عنوان ژورنال: MATEC web of conferences
سال: 2021
ISSN: ['2261-236X', '2274-7214']
DOI: https://doi.org/10.1051/matecconf/202134901004