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Procedures for characterizing an alloy and predicting cyclic life with the total strain version of Strainrange PartitioningProcedures are presented for characterizing an alloy and predicting cyclic life for isothermal and thermomechanical fatigue conditions by using the total strain version of strainrange partitioning (TS-SRP). Numerical examples are given. Two independent alloy characteristics are deemed important: failure behavior, as reflected by the inelastic strainrange versus cyclic life relations; and flow behavior, as indicated by the cyclic stress-strain-time response (i.e., the constitutive behavior). Failure behavior is characterized by conducting creep-fatigue tests in the strain regime, wherein the testing times are reasonably short and the inelastic strains are large enough to be determined accurately. At large strainranges, stress-hold, strain-limited tests are preferred because a high rate of creep damage per cycle is inherent in this type of test. At small strainranges, strain-hold cycles are more appropriate. Flow behavior is characterized by conducting tests wherein the specimen is usually cycled far short of failure and the wave shape is appropriate for the duty cycle of interest. In characterizing an alloy pure fatigue, or PP, failure tests are conducted first. Then depending on the needs of the analyst a series of creep-fatigue tests are conducted. As many of the three generic SRP cycles are featured as are required to characterize the influence of creep on fatigue life (i.e., CP, PC, and CC cycles, respectively, for tensile creep only, compressive creep only, and both tensile and compressive creep). Any mean stress effects on life also must be determined and accounted for when determining the SRP inelastic strainrange versus life relations for cycles featuring creep. This is particularly true for small strainranges. The life relations thus are established for a theoretical zero mean stress condition.
Document ID
19890016114
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Saltsman, James F.
(NASA Lewis Research Center Cleveland, OH, United States)
Halford, Gary R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1989
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-4102
NAS 1.15:4102
E-4457
Report Number: NASA-TM-4102
Report Number: NAS 1.15:4102
Report Number: E-4457
Accession Number
89N25485
Funding Number(s)
PROJECT: RTOP 505-66-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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