Prediction of unstable crack length in aluminium alloys

dc.contributor.authorRyder, R. H.
dc.date.accessioned2017-06-19T14:28:34Z
dc.date.available2017-06-19T14:28:34Z
dc.date.issued1960-10
dc.description.abstractA 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.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/12049
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N-109en_UK
dc.relation.ispartofseries109en_UK
dc.titlePrediction of unstable crack length in aluminium alloysen_UK
dc.typeReporten_UK

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