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Measurement and analysis of critical crack tip processes during fatigue crack growthThe mechanics of fatigue crack growth under constant-amplitudes and variable-amplitude loading were examined. Critical loading histories involving relatively simple overload and overload/underload cycles were studied to provide a basic understanding of the underlying physical processes controlling crack growth. The material used for this study was 7091-T7E69, a powder metallurgy aluminum alloy. Local crack-tip parameters were measured at various times before, during, and after the overloads, these include crack-tip opening loads and displacements, and crack-tip strain fields. The latter were useed, in combination with the materials cyclic and monotonic stress-strain properties, to compute crack-tip residual stresses. The experimental results are also compared with analytical predictions obtained using the FAST-2 computer code. The sensitivity of the analytical model to constant-amplitude fatigue crack growth rate properties and to through-thickness constrain are studied.
Document ID
19850024029
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Davidson, D. L.
(Southwest Research Inst. San Antonio, TX, United States)
Hudak, S. J.
(Southwest Research Inst. San Antonio, TX, United States)
Dexter, R. J.
(Southwest Research Inst. San Antonio, TX, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1985
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-172597
NAS 1.26:172597
Report Number: NASA-CR-172597
Report Number: NAS 1.26:172597
Accession Number
85N32342
Funding Number(s)
PROJECT: RTOP 505-33-23-02
CONTRACT_GRANT: NAS1-17641
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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