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Development of a simplified procedure for cyclic structural analysisDevelopment was extended of a simplified inelastic analysis computer program (ANSYMP) for predicting the stress-strain history at the critical location of a thermomechanically cycled structure from an elastic solution. The program uses an iterative and incremental procedure to estimate the plastic strains from the material stress-strain properties and a plasticity hardening model. Creep effects can be calculated on the basis of stress relaxation at constant strain, creep at constant stress, or a combination of stress relaxation and creep accumulation. The simplified method was exercised on a number of problems involving uniaxial and multiaxial loading, isothermal and nonisothermal conditions, dwell times at various points in the cycles, different materials, and kinematic hardening. Good agreement was found between these analytical results and nonlinear finite-element solutions for these problems. The simplified analysis program used less than 1 percent of the CPU time required for a nonlinear finite-element analysis.
Document ID
19840012810
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaufman, A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1984
Subject Category
Structural Mechanics
Report/Patent Number
E-1855
NAS 1.60:2243
NASA-TP-2243
Report Number: E-1855
Report Number: NAS 1.60:2243
Report Number: NASA-TP-2243
Meeting Information
Meeting: ASME Intern. Gas Turbine Conf.
Location: Amsterdam
Start Date: June 3, 1984
End Date: June 7, 1984
Accession Number
84N20878
Funding Number(s)
PROJECT: RTOP 505-33-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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