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On local total strain redistribution using a simplified cyclic inelastic analysis based on an elastic solutionStrain redistribution corrections were developed for a simplified inelastic analysis procedure to economically calculate material cyclic response at the critical location of a structure for life prediction purposes. The method was based on the assumption that the plastic region in the structure is local and the total strain history required for input can be defined from elastic finite element analyses. Cyclic stress-strain behavior was represented by a bilinear kinematic hardening model. The simplified procedure has been found to predict stress-strain response with reasonable accuracy for thermally cycled problems but needs improvement for mechanically load cycled problems. This study derived and incorporated Neuber type corrections in the simplified procedure to account for local total strain redistribution under cyclic mechanical loading. The corrected simplified method was exercised on a mechanically load cycled benchmark notched plate problem. Excellent agreement was found between the predicted material response and nonlinear finite element solutions for the problem. The simplified analysis computer program used 0.3 percent of the CPU time required for a nonlinear finite element analysis.
Document ID
19850013380
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hwang, S. Y.
(South Carolina State Coll. Cleveland, OH, United States)
Kaufman, A.
(NASA Lewis Research Center)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Structural Mechanics
Report/Patent Number
E-2406
NAS 1.15:86913
NASA-TM-86913
Report Number: E-2406
Report Number: NAS 1.15:86913
Report Number: NASA-TM-86913
Meeting Information
Meeting: Joint Propulsion Conf.
Location: Monterey, CA
Country: United States
Start Date: July 9, 1985
End Date: July 11, 1985
Sponsors: ASME, AIAA, SAE
Accession Number
85N21690
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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