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- W6858319 abstract "AbstractThe need for lower cost and the emergence of new welding technologies has brought interest in large integral metallic structures for aircraft applications; however, new problems must be addressed, e.g. in integral structures, a crack approaching a stiffener propagates simultaneously in the skin and into the stiffener and breaks it. The use of manufacturing techniques such as high speed machining (HSM), laser beam welding (LBW) and friction stir welding (FSW) requires further experimental and numerical work concerning the fatigue behaviour of panels manufactured using those processes. This chapter is focused on an experimental test programme including fatigue crack growth rate characterization in panels fabricated using HSM, LBW and FSW. The work was developed in the frame of the European Union DaToN project. Data was obtained for panels tested in mode I crack propagation under load ratios (R) of 0.1 and 0.5. It was found that welded panels presented longer lives up to rupture. This result is associated to the residual stress fields existing in the welded panels, and also to the location of the initial artificial defect, placed in the skin midway the specimen’s two stiffeners.KeywordsFatigue CrackStress Intensity FactorFatigue LifeCrack Growth RateFriction Stir WeldingThese keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves." @default.
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- W6858319 date "2010-01-01" @default.
- W6858319 modified "2023-10-18" @default.
- W6858319 title "Lightweight Stiffened Panels Fabricated Using Emerging Fabrication Technologies: Fatigue Behaviour" @default.
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- W6858319 doi "https://doi.org/10.1007/8611_2010_49" @default.
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