NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Cyclic creep analysis from elastic finite-element solutionsA uniaxial approach was developed for calculating cyclic creep and stress relaxation at the critical location of a structure subjected to cyclic thermomechanical loading. This approach was incorporated into a simplified analytical procedure for predicting the stress-strain history at a crack initiation site for life prediction purposes. An elastic finite-element solution for the problem was used as input for the simplified procedure. The creep analysis includes a self-adaptive time incrementing scheme. Cumulative creep is the sum of the initial creep, the recovery from the stress relaxation and the incremental creep. The simplified analysis was exercised for four cases involving a benchmark notched plate problem. Comparisons were made with elastic-plastic-creep solutions for these cases using the MARC nonlinear finite-element computer code.
Document ID
19860016350
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaufman, A.
(NASA Lewis Research Center Cleveland, OH, United States)
Hwang, S. Y.
(South Carolina State Coll. Orangeburg, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:87213
E-2872
NASA-TM-87213
Report Number: NAS 1.15:87213
Report Number: E-2872
Report Number: NASA-TM-87213
Meeting Information
Meeting: Southeastern Conference on Theoretical and Applied Mechanics
Location: Columbia, SC
Country: United States
Start Date: April 17, 1986
End Date: April 18, 1986
Accession Number
86N25822
Funding Number(s)
PROJECT: RTOP 533-04-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available