Tests on the general instability of a stiffened metal cylinder under axial compression

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dc.contributor.authorHeald, W. R.
dc.date.accessioned2012-06-19T14:29:33Z
dc.date.available2012-06-19T14:29:33Z
dc.date.issued1951-04
dc.description.abstractA thin stiffened metal cylinder liable to General Instability was tested under axial compression and an investigation was made into possible methods of predicting the critical load from non-destructive tests. Particular attention was paid to the perturbation loading technique. The cylinder was finally tested to destruction and the actual failing load compaired with the values given by various theories and empirical relationships.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7251
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfield.en_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries45en_UK
dc.titleTests on the general instability of a stiffened metal cylinder under axial compressionen_UK
dc.typeReporten_UK

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