Finite element implementation of Koiter's initial post-buckling analysis
Thin-wall structures as the main components in the aircrafts, as well as in many other types of structures, such as automotive, trains, ships, etc., are exposed to complex loading conditions. For some parts of these structures, e.g. the upper surface of wings of aircrafts, buckling is the most commo...
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| Format: | Thesis (University of Nottingham only) |
| Language: | English |
| Published: |
2019
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| Online Access: | https://eprints.nottingham.ac.uk/55663/ |