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Development of a simplified analytical method for representing material cyclic responseDevelopment of a simplified method for estimating structural inelastic stress and strain response to cyclic thermal loading is presented. The method assumes that high temperature structural response is the sum of time independent plastic and time dependent elastic/creep components. The local structural stress and strain response predicted by linear elastic analysis is modified by the simplified method to predict the inelastic response. The results with simulations by a nonlinear finite element analysis and used time independent plasticity and unified time dependent material model are compared.
Document ID
19830013119
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Moreno, V.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:168100
PWA-5843-13
NASA-CR-168100
Report Number: NAS 1.26:168100
Report Number: PWA-5843-13
Report Number: NASA-CR-168100
Accession Number
83N21390
Funding Number(s)
CONTRACT_GRANT: NAS3-22821
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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