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- W130567019 abstract "Abstract : Fatigue life data were obtained for four different types of fatigue life enhancing (FLE) fasteners installed in new uncracked holes and in reworked, pre-cracked holes. The first condition represented a new design where the FLE fasteners are installed during production. The second condition represented a structural rework in which fastener holes are reamed to a larger size to remove fatigue or fretting damage but might still contain a small undetected crack. Results showed that the FLE fasteners produced approximately the same overall fatigue life in the new design and the rework condition and provided a significant increase in life compared to conventional non-FLE fasteners. Tests were performed with 7075-T6 aluminum alloy under spectrum loading typical of a Navy fighter/attack type of aircraft. For the rework condition, the pre-crack size was limited to .03 inch (.76mm). Flush head fasteners were used in all tests. Keywords: Crack-growth; Fasteners; Structural rework; Joints." @default.
- W130567019 created "2016-06-24" @default.
- W130567019 creator A5078235084 @default.
- W130567019 date "1985-02-28" @default.
- W130567019 modified "2023-09-27" @default.
- W130567019 title "Effectiveness of Fatigue Life Enhancing Fasteners in the Design and Rework of Aircraft Structures" @default.
- W130567019 doi "https://doi.org/10.21236/ada159676" @default.
- W130567019 hasPublicationYear "1985" @default.
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