Linear buckling of an axially reinforced pressurised cylinder

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dc.contributor.authorHoughton, D. S.
dc.contributor.authorJohns, D. J.
dc.date.accessioned2017-06-19T14:32:16Z
dc.date.available2017-06-19T14:32:16Z
dc.date.issued1960-10
dc.description.abstractAn analysis is presented using small deflection theory for the buckling of a pressurised, axially reinforced cylinder, which is subjected to axial compression. Various approximations to the analysis are discussed and some results are presented which show the effects of internal pressure and various structural parameters on both panel buckling and overall buckling.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/12050
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N-110en_UK
dc.relation.ispartofseries110en_UK
dc.titleLinear buckling of an axially reinforced pressurised cylinderen_UK
dc.typeReporten_UK

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CoA. Notes (1952-1969)