Prediction of unstable crack length in aluminium alloys

Date

1960-10

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College of Aeronautics

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Report

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Free to read from

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Abstract

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.

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Github

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