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Life prediction of thermal-mechanical fatigue using strain-range partitioningThe applicability is described of the method of Strainrange Partitioning to the life prediction of thermal-mechanical strain-cycling fatigue. An in-phase test on 316 stainless steel is analyzed as an illustrative example. The observed life is in excellent agreement with the life predicted by the method using the recently proposed Step-Stress Method of experimental partitioning, the Interation Damage Rule, and the life relationships determined at an isothermal temperature of 705 C. Implications of the study are discussed relative to the general thermal fatigue problem.
Document ID
19760005310
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Halford, G. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Manson, S. S.
(Case Western Reserve Univ.)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
E-8537
NASA-TM-X-71829
Report Number: E-8537
Report Number: NASA-TM-X-71829
Meeting Information
Meeting: Symp. on Thermal Fatigue of Mater. and Components
Location: New Orleans, LA
Country: United States
Start Date: November 17, 1975
End Date: November 18, 1975
Sponsors: ASTM
Accession Number
76N12398
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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