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- W1578483412 endingPage "1183" @default.
- W1578483412 startingPage "1177" @default.
- W1578483412 abstract "Bolted joints are very common in aerospace structural components, nevertheless, their behaviour is not yet fully understood, especially if a crack is present when defect tolerance is requested. Stress intensity factor solutions (mode I) of a cracked iso-metric bolt derived from a three dimensional F.E. model are presented. In the F.E. model the crack shape has been modelled with special isoparametric singular elements. Four different crack lengths (depths) have been considered in the analysis starting from 0.5 mm up to 1, 2, 3, mm. Three different loading conditions have been assumed in order to assess the influence on the stress intensity factor solutions of the pressure load acting on the bolt thread. Comparison with existing data has been carried out." @default.
- W1578483412 created "2016-06-24" @default.
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- W1578483412 date "1984-01-01" @default.
- W1578483412 modified "2023-10-14" @default.
- W1578483412 title "STRESS INTENSITY FACTOR SOLUTIONS FOR A CRACKED BOLT" @default.
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- W1578483412 doi "https://doi.org/10.1016/b978-1-4832-8440-8.50101-0" @default.
- W1578483412 hasPublicationYear "1984" @default.
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