Buckling due to thermal stress of cylindrical shells subjected to axial temperature distributions

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dc.contributor.authorJohns, D. J.
dc.contributor.authorHoughton, D. S.
dc.contributor.authorWebber, J. P. H.
dc.date.accessioned2014-12-04T09:40:34Z
dc.date.available2014-12-04T09:40:34Z
dc.date.issued1961-05
dc.description.abstractThermal stress distributions in uniform circular cylindrical shells due to axial temperature distributions are investigated. The discontinuity effect due to the presence of a cooler stiffening bulkhead is considered, and the possibility of thermal buckling of the shell due to the circumferential discontinuity stress is examined. The buckling analysis is based on Donnell's shell equation, and particular attention is given to shells having clamped edges. An experimental investigation of this buckling problem is discussed, and the results obtained are seen to agree reasonably well with theory.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/8847
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCollege of Aeronautics Reportsen_UK
dc.relation.ispartofseries147en_UK
dc.relation.ispartofseriesCOA/147en_UK
dc.titleBuckling due to thermal stress of cylindrical shells subjected to axial temperature distributionsen_UK
dc.typeReporten_UK

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