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

Heald, W. R.

dc.contributor.author	Heald, W. R.
dc.date.accessioned	2012-06-19T14:29:33Z
dc.date.available	2012-06-19T14:29:33Z
dc.date.issued	1951-04
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7251
dc.description.abstract	A 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.language.iso	en	en_UK
dc.publisher	College of Aeronautics, Cranfield.	en_UK
dc.relation.ispartofseries	College Report	en_UK
dc.relation.ispartofseries	45	en_UK
dc.title	Tests on the general instability of a stiffened metal cylinder under axial compression	en_UK
dc.type	Report	en_UK