NASA STI Repository (National Aeronautics and Space Administration) · 1975 · 51 citations · 0 references
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EngineeringComputational EngineeringComputational MechanicsFinite Element AnalysisFinite Element MethodsFinite Element FormulationShell AnalysisShell ElementsShell TheoryStrain AnalysisStructural Finite Element AnalysisCurved Shell ElementsCurved Shell Finite ElementsShell Finite Element AnalysisStiffness Matrix FormulationStrain EnergyThin Shell AnalysisThin Shell TheoryTriangular Shell Elements
The formulation of the linear stiffness matrix for a doubly-curved triangular thin shell element, using a modified potential energy principle, is described. The strain energy component of the potential energy is expressed in terms of displacements and displacement gradients by use of consistent Koiter strain-displacement equations. The element inplane and normal displacement fields are approximated by complete cubic polynomials. The interelement displacement admissibility conditions are met in the global representation by imposition of constraint conditions on the interelement boundaries; the constraints represent the modification of the potential energy. Errors due to the nonzero strains under rigid body motion are shown to be of small importance for practical grid refinements through performance of extensive comparison analyses.