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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Name affiliation
  1. National Research Council Canada. Aerospace
FormatText
TypeArticle
Journal titleFatigue and Fracture of Engineering Materials and Structures
ISSN8756-758X
Volume38
Issue5
Pages528539; # of pages: 12
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
Abstract
Publication date
PublisherWiley
Terms of use
LanguageEnglish
Peer reviewedYes
NPARC number21275715
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Record identifier675672da-b322-4bba-8651-716e824dc405
Record created2015-07-14
Record modified2016-05-09
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