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Consistent linearization of the element-independent corotational formulation for the structural analysis of general shellsA consistent linearization is provided for the element-dependent corotational formulation, providing the proper first and second variation of the strain energy. As a result, the warping problem that has plagued flat elements has been overcome, with beneficial effects carried over to linear solutions. True Newton quadratic convergence has been restored to the Structural Analysis of General Shells (STAGS) code for conservative loading using the full corotational implementation. Some implications for general finite element analysis are discussed, including what effect the automatic frame invariance provided by this work might have on the development of new, improved elements.
Document ID
19880007694
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rankin, C. C.
(Lockheed Aircraft Corp. Palo Alto, CA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:178418
NASA-CR-178418
Report Number: NAS 1.26:178418
Report Number: NASA-CR-178418
Accession Number
88N17078
Funding Number(s)
CONTRACT_GRANT: NAS1-18101
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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