Some design problems of thin shell structures

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dc.creator Johns, D. J. 2017-06-19T15:19:02Z 2017-06-19T15:19:02Z 1961-09 2022-05-09T10:07:09Z 2022-05-09T10:07:09Z
dc.description Simplified 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.
dc.language en
dc.publisher College of Aeronautics
dc.relation CoA/N-118
dc.relation 118
dc.title Some design problems of thin shell structures
dc.type Report

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