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Application of an Energy-Based Life Prediction Model to Bithermal and Thermomechanical FatigueThe inelastic hysteresis energy applied to the material in a cycle is used as the basis for predicting nonisothermal fatigue life of a wrought cobalt-base superalloy, Haynes 188, from isothermal fatigue data. Damage functions that account for hold-time effects and time-dependent environmental phenomena such as oxidation and hot corrosion are proposed in terms of the inelastic hysteresis energy per cycle. The proposed damage functions are used to predict the bithermal and thermomechanical fatigue lives of Haynes 188 between 316 and 760 C from isothermal fatigue data. Predicted fatigue lives of all but two of the nonisothermal tests are within a factor of 1.5 of the experimentally observed lives.
Document ID
19950013763
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Radhakrishnan, V. M.
(Indian Inst. of Tech. Madras., United States)
Kalluri, Sreeramesh
(NYMA, Inc. Brook Park, OH., United States)
Halford, Gary R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
E-9038
NAS 1.15:106684
NASA-TM-106684
Report Number: E-9038
Report Number: NAS 1.15:106684
Report Number: NASA-TM-106684
Accession Number
95N20179
Funding Number(s)
CONTRACT_GRANT: NAS3-27186
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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