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dc.contributor.authorDíez, Pedro
dc.contributor.authorHuerta, Antonio
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Matemàtica Aplicada III
dc.date.accessioned2010-07-13T10:45:31Z
dc.date.available2015-04-22T07:14:57Z
dc.date.created2000-03
dc.date.issued2000-03
dc.identifier.citationDíez, P.; Huerta, A. "Revue européenne des élements finis". Març 2000.
dc.identifier.issn1250-6559
dc.identifier.urihttp://hdl.handle.net/2117/8145
dc.description.abstractThe finite element discretization of a shell structure introduces two kinds of errors: the error in the functional approximation and the error in the geometry approximation. The first is associated with the finite dimensional interpolation space and it is present in any finite element computation. The latter is associated with the piecewise polynomial approximation of a curved surface and is much more relevant in shell problems than in any other standard 2D or 3D computation. In the shells framework, formerly the quality control of the finite element solution has been carried out using flux projection a posteriori error estimators. This technique exhibits two main drawbacks: 1) the flux smoothing averages stress components over different elements that may have different physical meaning if the tangent planes are different and 2) the error estimation process uses only the approximate solution and hence, the discretized forces and the computational mesh: the data describing the real geometry and load is therefore not accounted for. In this work, a residual type error estimator introduced for standard 2D finite element analysis is generalized to shell problems. This allows to easily account for the real original geometry of the problem in the error estimation procedure and precludes the necessity of comparing generalized stress components between non coplanar elements. This estimator is based on approximating a reference error associated with a refined reference mesh. In order to build up the residual error equation the computed solution must be represented (projected) on the reference mesh. The use of thin shell finite elements requires a proper formulation in order to preclude shear locking. Following an idea of Donea and Lamain, the interpolation of the rotations is not unique and requires a particular technique to transfer the information from the computational mesh to the reference mesh. This technique is also developed in this work and may be used in any adaptive evolution problem where the solution must be transferred from one mesh to another.
dc.format.extent18 p.
dc.language.isoeng
dc.subjectÀrees temàtiques de la UPC::Matemàtiques i estadística::Anàlisi numèrica::Mètodes numèrics
dc.subjectÀrees temàtiques de la UPC::Enginyeria civil::Materials i estructures
dc.subject.lcshShells (Engineering)--Mathematical models
dc.subject.otherError estimation
dc.subject.otheradaptivity
dc.subject.otherThin shell elements
dc.subject.otherLocking free formulation
dc.titleError estimation for adaptive computations on shell structures
dc.typeArticle
dc.subject.lemacEstructures laminars -- Mètodes numèrics
dc.contributor.groupUniversitat Politècnica de Catalunya. LACÀN - Mètodes Numèrics en Ciències Aplicades i Enginyeria
dc.description.peerreviewedPeer Reviewed
dc.rights.accessOpen Access
local.identifier.drac672227
dc.description.versionPostprint (author’s final draft)
local.citation.authorDíez, P.; Huerta, A.
local.citation.publicationNameRevue européenne des élements finis
local.citation.volume9
local.citation.number1,2,3
local.citation.startingPage49
local.citation.endingPage66


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