Some design problems of thin shell structures

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dc.contributor.authorJohns, D. J.
dc.date.accessioned2017-06-19T15:19:02Z
dc.date.available2017-06-19T15:19:02Z
dc.date.issued1961-09
dc.description.abstractSimplified analyses are presented which illustrate some of the design problems of typical space vehicle structures, with the emphasis on thin, circular cylindrical shells. Amongst the problems considered are panel flutter, thermal buckling and buckling under axial compression.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/12056
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N-118en_UK
dc.relation.ispartofseries118en_UK
dc.titleSome design problems of thin shell structuresen_UK
dc.typeReporten_UK

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CoA. Notes (1952-1969)