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- W860596564 abstract "This paper investigates if corrosion pitting invalidates the fatigue lifeing method used by the Royal Australian Air Force to manage the structural integrity of its P-3C Orion aircraft. Fatigue life predictions made using the P-3C Service Life Assessment Program method were compared with those from an Equivalent Crack Size model for pitting corrosion. The data for this comparison came from a program of variable amplitude fatigue tests of high-kt specimens of 7075-T6. This testing was performed using two stress levels on both corroded and uncorroded specimens. Analysis of the results showed that the safe-life estimates made using the P-3 life assessment method were conservative in the presence of corrosion as they were above the 99.9th percentile of fatigue life predicted by the equivalent crack size method." @default.
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- W860596564 date "2015-09-01" @default.
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- W860596564 title "The effect of pitting corrosion on the safe-life prediction of the Royal Australian Air Force P-3C Orion aircraft" @default.
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- W860596564 doi "https://doi.org/10.1016/j.engfailanal.2015.05.020" @default.
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