Fatigue crack growth in 7249-T76511 aluminium alloy under constant-amplitude and spectrum loading

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1111/ffe.12253
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  1. National Research Council of Canada. Aerospace
FormatText, Article
SubjectAlloys; Aluminum; Aluminum alloys; Amplitude modulation; Crack closure; Crack propagation; Fatigue crack propagation; Fatigue of materials; Fatigue testing; Strain; Stress analysis; Stress intensity factors; Wings; Compression pre crackings; Constant amplitude; Constraint factor; Crack mouth opening displacement; Effective stress intensity factor range; Fatigue-crack-growth tests; Full-scale fatigue test; Spectrum loading; Cracks
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Peer reviewedYes
NPARC number21275715
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Record identifier675672da-b322-4bba-8651-716e824dc405
Record created2015-07-14
Record modified2020-04-22
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