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Error estimation and adaptive mesh refinement for parallel analysis of shell structuresThe formulation and application of element-level, element-independent error indicators is investigated. This research culminates in the development of an error indicator formulation which is derived based on the projection of element deformation onto the intrinsic element displacement modes. The qualifier 'element-level' means that no information from adjacent elements is used for error estimation. This property is ideally suited for obtaining error values and driving adaptive mesh refinements on parallel computers where access to neighboring elements residing on different processors may incur significant overhead. In addition such estimators are insensitive to the presence of physical interfaces and junctures. An error indicator qualifies as 'element-independent' when only visible quantities such as element stiffness and nodal displacements are used to quantify error. Error evaluation at the element level and element independence for the error indicator are highly desired properties for computing error in production-level finite element codes. Four element-level error indicators have been constructed. Two of the indicators are based on variational formulation of the element stiffness and are element-dependent. Their derivations are retained for developmental purposes. The second two indicators mimic and exceed the first two in performance but require no special formulation of the element stiffness mesh refinement which we demonstrate for two dimensional plane stress problems. The parallelizing of substructures and adaptive mesh refinement is discussed and the final error indicator using two-dimensional plane-stress and three-dimensional shell problems is demonstrated.
Document ID
19950011077
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Keating, Scott C.
(Colorado Univ. Boulder, CO, United States)
Felippa, Carlos A.
(Colorado Univ. Boulder, CO, United States)
Park, K. C.
(Colorado Univ. Boulder, CO, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-197500
CU-CAS-94-23
NAS 1.26:197500
Report Number: NASA-CR-197500
Report Number: CU-CAS-94-23
Report Number: NAS 1.26:197500
Accession Number
95N17492
Funding Number(s)
CONTRACT_GRANT: NAS1-756
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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