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Prestraining and Its Influence on Subsequent Fatigue LifeAn experimental program was conducted to study the damaging effects of tensile and compressive prestrains on the fatigue life of nickel-base, Inconel 718 superalloy at room temperature. To establish baseline fatigue behavior, virgin specimens with a solid uniform gage section were fatigued to failure under fully-reversed strain-control. Additional specimens were prestrained to 2 percent, 5 percent, and 10 percent (engineering strains) in the tensile direction and to 2 percent (engineering strain) in the compressive direction under stroke-control, and were subsequently fatigued to failure under fully-reversed strain-control. Experimental results are compared with estimates of remaining fatigue lives (after prestraining) using three life prediction approaches: (1) the Linear Damage Rule; (2) the Linear Strain and Life Fraction Rule; and (3) the nonlinear Damage Curve Approach. The Smith-Watson-Topper parameter was used to estimate fatigue lives in the presence of mean stresses. Among the cumulative damage rules investigated, best remaining fatigue life predictions were obtained with the nonlinear Damage Curve Approach.
Document ID
19960002347
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Halford, Gary R.
(NASA Lewis Research Center Cleveland, OH, United States)
Mcgaw, Michael A.
(NASA Lewis Research Center Cleveland, OH, United States)
Kalluri, Sreeramesh
(NYMA, Inc. Brook Park, OH., United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1995
Subject Category
Structural Mechanics
Report/Patent Number
E-9517
NASA-TM-106881
NAS 1.15:106881
Report Number: E-9517
Report Number: NASA-TM-106881
Report Number: NAS 1.15:106881
Accession Number
96N12355
Funding Number(s)
PROJECT: RTOP 584-03-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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