Development of dry film lubricants for highly loaded contacts
This thesis motivated by concerns over fretting damage in the aerospace engine disc dovetail joint in Ti6Al4V. The dovetail joint behaviour was investigated using a cylinder-on-flat contact geometry setup and fretting amplitude of 300 µm, a frequency of 2.5 Hz and load of 575 N was used. The thesis...
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| Format: | Thesis (University of Nottingham only) |
| Language: | English |
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2016
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| Online Access: | https://eprints.nottingham.ac.uk/35850/ |