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Relation of cyclic loading pattern to microstructural fracture in creep fatigueCreep-fatigue-environment interaction is discussed using the 'strainrange partitioning' (SRP) framework as a basis. The four generic SRP strainrange types are studied with a view of revealing differences in micromechanisms of deformation and fatigue degradation. Each combines in a different manner the degradation associated with slip-plane sliding, grain-boundary sliding, migration, cavitation, void development and environmental interaction; hence the approch is useful in delineating the relative importance of these mechanisms in the different loadings. Micromechanistic results are shown for a number of materials, including 316 SS, wrought heat resistant alloys, several nickel-base superalloys, and a tantalum base alloy, T-111. Although there is a commonality of basic behavior, the differences are useful in delineation several important principles of interpretation. Some quantitative results are presented for 316 SS, involving crack initiation and early crack growth, as well as the interaction of low-cycle fatigue with high-cycle fatigue.
Document ID
19830026078
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Manson, S. S.
(Case Western Reserve Univ. Cleveland, OH, United States)
Halford, G. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Oldrieve, R. E.
(NASA Lewis Research Center)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-83473
E-1787
NAS 1.15:83473
Report Number: NASA-TM-83473
Report Number: E-1787
Report Number: NAS 1.15:83473
Meeting Information
Meeting: Fatigue 84 The 2nd Intern. Conf. on Fatigue and Fatigue Thresholds
Location: Birmingham
Start Date: September 3, 1984
End Date: September 7, 1984
Accession Number
83N34349
Funding Number(s)
PROJECT: RTOP 505-33-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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