| dc.creator | Ryder, R. H. | |
| dc.date | 2017-06-19T14:28:34Z | |
| dc.date | 2017-06-19T14:28:34Z | |
| dc.date | 1960-10 | |
| dc.date.accessioned | 2022-05-09T10:07:08Z | |
| dc.date.available | 2022-05-09T10:07:08Z | |
| dc.identifier | http://dspace.lib.cranfield.ac.uk/handle/1826/12049 | |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/4469 | |
| dc.description | A method was set down for predicting the unstable length of a crack in a flat sheet of aluminium alloy subjected to a steady tensile stress. The basis of the method was to take the work done to failure in the 'neck' region of a tensile test specimen and apply it, with a suitable constraint factor, to the flat sheet to give the work rate required to propagate the crack. Experimental evidence is produced in support of the method. | |
| dc.language | en | |
| dc.publisher | College of Aeronautics | |
| dc.relation | CoA/N-109 | |
| dc.relation | 109 | |
| dc.title | Prediction of unstable crack length in aluminium alloys | |
| dc.type | Report |
| Files | Size | Format | View |
|---|---|---|---|
| COA_N_109_1960.pdf | 1.294Mb | application/pdf |
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