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![Decompositon of the original problem into t2o subproblems for {1} the matrix and {2}, the shell](thumbnails/s151.jpg) |
![Buckling pattern for: (a-c) nearly perfect interface bonding; (d-f) weak interface](thumbnails/s152.jpg) |
![Buckling of a large byperbolic paraboloid roof](thumbnails/s153.jpg) |
![Snapping of a bimetallic shallow shell as a function of temperature](thumbnails/s154.jpg) |
![Circumferentially corrugated shallow spherical shell](thumbnails/s155.jpg) |
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Decompositon of the original problem into t2o subproblems for {1} the matrix and {2}, the shell |
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Buckling pattern for: (a-c) nearly perfect interface bonding; (d-f) weak interface |
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Buckling of a large byperbolic paraboloid roof |
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Snapping of a bimetallic shallow shell as a function of temperature |
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Circumferentially corrugated shallow spherical shell |
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![Optimized shell of revolution with ribs: first buckling mode shape. Symmetry conditions are imposed at the large end. Buckling is between adjacent ribs near the large end.](thumbnails/s156.jpg) |
![ANSYS Finite element model of a Cassini shell of revolution](thumbnails/s157.jpg) |
![Buckling modes as a function of Cassini ovaloidal shape](thumbnails/s158.jpg) |
![Three stable states of an orthotropic shell. In this paper it is proved that untwisted, uniformly curved, orthotropic shells can have up to 3 stable equilibrium positions](thumbnails/s159.jpg) |
![Crushing a spherical shell](thumbnails/s160.jpg) |
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Optimized shell of revolution with ribs: first buckling mode shape. Symmetry conditions are imposed at the large end. Buckling is between adjacent ribs near the large end. |
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ANSYS Finite element model of a Cassini shell of revolution |
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Buckling modes as a function of Cassini ovaloidal shape |
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Three stable states of an orthotropic shell. In this paper it is proved that untwisted, uniformly curved, orthotropic shells can have up to 3 stable equilibrium positions |
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Crushing a spherical shell |
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![Reticulated dome with axisymmetric inward step pressure over the part of the surface near the apex (blue area)](thumbnails/s161.jpg) |
![Reticulated dome with axisymmetric inward step pressure near the apex (continued)](thumbnails/s162.jpg) |
![Deformation of blast-loaded circular sandwich panel: results from test and theory. The shock loading is applied to the lower face sheet of the initially flat specimen.](thumbnails/s163.jpg) |
![TOP: Hydro-explosive rig for forming a torispherical pressure vessel head; BOTTOM: A typical torispherical head. What is called](thumbnails/s164.jpg) |
![LS-DYNA simulation of the hydro-explosive forming of a torispherical head. In (f) notice the formation of wrinkles along the edge.](thumbnails/s165.jpg) |
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Reticulated dome with axisymmetric inward step pressure over the part of the surface near the apex (blue area) |
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Reticulated dome with axisymmetric inward step pressure near the apex (continued) |
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Deformation of blast-loaded circular sandwich panel: results from test and theory. The shock loading is applied to the lower face sheet of the initially flat specimen. |
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TOP: Hydro-explosive rig for forming a torispherical pressure vessel head; BOTTOM: A typical torispherical head. What is called "Blanket" in the top view is the test specimen. |
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LS-DYNA simulation of the hydro-explosive forming of a torispherical head. In (f) notice the formation of wrinkles along the edge. |
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