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- W2028990010 abstract "Abstract This paper describes a randomized flight-by-flight loading sequence for the L 410 commuter airplane. Principles of the sequence and the scope of simulated load cases are presented in the first part of the paper. The second part deals with effects of a low-load omission of airborne spectra in terms of fatigue crack growth. M(T) specimens made of 2124-T851 and 7475-T7351 aluminum alloys were used for the investigation. Each alloy was tested using a full and a shortened (i.e. with applied omission) loading sequence." @default.
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- W2028990010 date "2015-01-01" @default.
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- W2028990010 title "Randomized Loading Sequence for L 410 Airplane" @default.
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- W2028990010 doi "https://doi.org/10.1016/j.proeng.2015.02.063" @default.
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