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Adaptive Finite Element Technology in Integrated Design and AnalysisAn assessment of the potential impact of adaptive finite element technology on the analysis part of the aircraft structural synthesis process is presented. The main conclusion is that adaptive application of the p-version of the finite element method based on indirect error estimation procedures results in substantial cost reduction and increased reliability of the computed data. Adaptivity based on direct a posteriori error estimation has the potential for additional savings.
Document ID
19810020272
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Szabo, B. A.
(Washington Univ. Saint Louis, MO, United States)
Basu, P. K.
(Washington Univ. Saint Louis, MO, United States)
Dunavant, D. A.
(Washington Univ. Saint Louis, MO, United States)
Vasilopoulos, D.
(Washington Univ. Saint Louis, MO, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Numerical Analysis
Report/Patent Number
NASA-CR-164560
WU/CCM-81/1
Report Number: NASA-CR-164560
Report Number: WU/CCM-81/1
Accession Number
81N28810
Funding Number(s)
CONTRACT_GRANT: NSG-1640
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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