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| Various shear deformation models |
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| Error in central deflection of rectangular (b = 3a) composite 0/90/0 plate for changing length/thickness ratio a/h |
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| (a) Various models for in-plane displacements through the thickness of a multi-layered shell wall and (b) improved transverse shear stress distribution |
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| Layerwise model of a shell wall |
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| Shell wall modeling: Continuum-based shell elements; Degenerated solid approach |
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| Various approximations in which the 3-dimensional shell wall is reduced to a surface |
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| Relative amounts of bending versus membrane strain energy as functions of radius-to-thickness of a clamped externally pressureized hemispherical shell |
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| The Southwell plot: A non-destructive way of determining the buckling load Pcr |
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| Residual stress distributions in edge-welded plates |
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| Relationships between stress and strain in a loaded plate containing residual stresses |
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| Typical aircraft wing internal structure |
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| Positive, negative and zero Gaussian curvature of a shell |
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| Deformation from corotated to deformed configuration of a finite element |
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| Performance of thin shell 16-node finite element |
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| TRIC element model for large deflection of a cylindrical panel with inward-directed concentrated load |
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