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| Shell plate buckling eyed in box ship break-up |
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| DLR’s buckling test facility: left: axial compression configuration; right: compression-shear- configuration |
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| The small load, P1, creates an imperfection that reduces the carrying capacity of the axially compressed cylindrical shell |
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| Non-destructive test suggested by J.M.T Thompson for buckling of an axially compressed cylindrical shell |
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| Hydrostatically compressed cylindrical shell on a Pasternak foundation |
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| Some parts of a rocket that can buckle (DESICOS workshop: new robust DESign guideline for Imperfection sensitive COmposite launcher Structures) |
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| Assembly of micro/nanomaterials into complex, three-dimensional architectures by compressive buckling |
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| Buckling in 3D Structures investigated by the Bertoldi Group at Harvard University |
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| Schematic illustration of lamina being combined to form a laminate |
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| Buckling of axially compressed, curved composite shell containing tapered sections |
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| Detail of a tapered section including resin-rich layers |
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| Model used for the properties of a lamina in connection with multi-scale computational homogenization frameworks for the non-linear behavior of heterogeneous thin shells |
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| Finite element discretization of the lamina shown in the previous slide |
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| Building up a laminate consisting of layers modeled as displayed in the previous 2 slides |
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| Three modes of buckling of an axially compressed flat plate with a local delamination |
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