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![Shell plate buckling eyed in box ship break-up](thumbnails/s106.jpg) |
![DLR’s buckling test facility: left: axial compression configuration; right: compression-shear- configuration](thumbnails/s107.jpg) |
![The small load, P1, creates an imperfection that reduces the carrying capacity of the axially compressed cylindrical shell](thumbnails/s108.jpg) |
![Non-destructive test suggested by J.M.T Thompson for buckling of an axially compressed cylindrical shell](thumbnails/s109.jpg) |
![Hydrostatically compressed cylindrical shell on a Pasternak foundation](thumbnails/s110.jpg) |
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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)](thumbnails/s111.jpg) |
![Assembly of micro/nanomaterials into complex, three-dimensional architectures by compressive buckling](thumbnails/s112.jpg) |
![Buckling in 3D Structures investigated by the Bertoldi Group at Harvard University](thumbnails/s113.jpg) |
![Schematic illustration of lamina being combined to form a laminate](thumbnails/s114.jpg) |
![Buckling of axially compressed, curved composite shell containing tapered sections](thumbnails/s115.jpg) |
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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](thumbnails/s116.jpg) |
![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](thumbnails/s117.jpg) |
![Finite element discretization of the lamina shown in the previous slide](thumbnails/s118.jpg) |
![Building up a laminate consisting of layers modeled as displayed in the previous 2 slides](thumbnails/s119.jpg) |
![Three modes of buckling of an axially compressed flat plate with a local delamination](thumbnails/s120.jpg) |
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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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