| dc.creator | Hemp, W. S. | |
| dc.date | 2017-02-28T13:02:00Z | |
| dc.date | 2017-02-28T13:02:00Z | |
| dc.date | 1957-05 | |
| dc.date.accessioned | 2022-05-09T10:07:05Z | |
| dc.date.available | 2022-05-09T10:07:05Z | |
| dc.identifier | http://dspace.lib.cranfield.ac.uk/handle/1826/11510 | |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/4425 | |
| dc.description | This note derives the mathematical equations for the analysis of the shear buckling of a plate, in the case where the initial stresses exceed the elastic limit of the material. It is hoped at a later stage to apply this theory to test results, which are being obtained using rectangular torsion boxes. | |
| dc.language | en | |
| dc.publisher | College of Aeronautics | |
| dc.relation | CoA/N-64 | |
| dc.relation | 64 | |
| dc.title | Plastic buckling of a plate in shear | |
| dc.type | Report |
| Files | Size | Format | View |
|---|---|---|---|
| COA_N_64_1957.pdf | 412.7Kb | application/pdf |
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