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Effects of loading sequence for notched specimens under high-low two-step fatigue loadingThe effects of loading sequence on crack-initiation period were investigated for notched aluminum-alloy specimens under high-low two-step loading with special emphasis on local cyclic stresses and strains at the notch root. Local stress and strain were determined by a procedure based on an equation proposed by Neuber which relates elastoplastic stress and strain at a notch. Local stress and strain were also measured experimentally to verify the Neuber equation. The effects of initial high load on the crack-initiation periods were demonstrated with notched specimens and were simulated in unnotched specimens fatigue tested with local stress sequences. An analysis of the results indicated that sequence effects were not caused solely by local residual stresses, as is usually assumed; the existence of a damaging effect, resulting from the high local strain cycles, was demonstrated. The sequence effects observed with notched specimens were interpreted as the combined result of residual stresses and high local strain cycles.
Document ID
19720004153
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Crews, J. H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1971
Subject Category
Structural Mechanics
Report/Patent Number
L-7915
NASA-TN-D-6558
Report Number: L-7915
Report Number: NASA-TN-D-6558
Accession Number
72N11802
Funding Number(s)
PROJECT: RTOP 134-03-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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