1972
DOI: 10.1115/1.3422833
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Nonlinear Shell Theory With Finite Rotation and Stress-Function Vectors

Abstract: A general nonlinear theory for thin shells of arbitrary midsurface geometry is formulated in terms of a finite rotation vector and a stress-function vector. Compatibility equations, equilibrium equations, and boundary conditions are derived which are valid for shells undergoing arbitrarily large rotations and strains. For problems admitting a potential energy functional, a variational principle is formulated. The simplifications implied by small extensional strains are discussed. The theory contains, as specia… Show more

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Cited by 116 publications
(29 citation statements)
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“…The challenge has spawned numerous publications, for example [1,4,5,34,42,43,62,71,72]. For use of finite rotations in mathematical models, particularly shells, see [60,70,77]. There has been an Euromech Colloquium devoted entirely to that topic [61].…”
Section: Continuum Mechanics Sourcesmentioning
confidence: 99%
“…The challenge has spawned numerous publications, for example [1,4,5,34,42,43,62,71,72]. For use of finite rotations in mathematical models, particularly shells, see [60,70,77]. There has been an Euromech Colloquium devoted entirely to that topic [61].…”
Section: Continuum Mechanics Sourcesmentioning
confidence: 99%
“…Classical, minimum complementary energy-based, dimensionally reduced plate and shell models in terms of symmetric stresses can be derived using functional (8). In that case both the translational and rotational equilibrium equations, (13) and (16), should be satisÿed a priori. When dimensional reduction in terms of stresses is carried out, transverse variation of the stress components is approximated by polynomials of ÿnite degree in z. Equilibrium requirements (13) and (16) mean, however, that the polynomial dependence of the stress components on z cannot be arbitrary.…”
Section: Notation and Preliminariesmentioning
confidence: 99%
“…They were so far derived from Newton's law and Euler's theorem either by directly using the Cosserat model [36], [37], [38] or indirectly from 3D elasticity [12], [39]. When investigated by the direct approach, the dynamics of the directors t 3 are the most of the time, directly derived on S 2 through an alternative set of angular equations deduced from (80)-bottom (or (81)-bottom) by cross multiplying them on the right by t 3 .…”
Section: Reduction Of the Kinematic And Kinetic Modelsmentioning
confidence: 99%