Prediction of unstable crack length in aluminium alloys

Date published

1960-10

Free to read from

Supervisor/s

Journal Title

Journal ISSN

Volume Title

Publisher

College of Aeronautics

Department

Type

Report

ISSN

Format

Citation

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.

Description

Software Description

Software Language

Github

Keywords

DOI

Rights

Relationships

Relationships

Resources

Funder/s