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- W2017078640 abstract "Abstract Flight simulation fatigue tests were carried out on specimens of two aluminium alloys to investigate the effect of differing gust load experiences on fatigue crack propagation in 7075-T6 and the effect of gust load alleviation on 2024-T3. Two gust spectra were used: the Fokker F-27 spectrum for 7075-T6; and the reference spectrum TWIST for 2024-T3. There was a large systematic effect of gust severity on crack propagation rates in 7075-T6, and this effect correlated with the stress intensity factor for the root mean square of the gust amplitudes. Gust alleviation increased the crack initiation and total lives for 2024-T3, but decreased the crack propagation lives owing to a lessening of crack growth retardation following severe flights." @default.
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- W2017078640 date "1979-07-01" @default.
- W2017078640 modified "2023-10-17" @default.
- W2017078640 title "Gust severity effects on fatigue crack propagation in aluminium alloy sheet materials" @default.
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- W2017078640 doi "https://doi.org/10.1016/0142-1123(79)90001-x" @default.
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