The buckling in compression of panels with square top-hat section stringers

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dc.contributor.author Hemp, W. S.
dc.contributor.author Griffin, K. H.
dc.date.accessioned 2012-05-15T14:48:26Z
dc.date.available 2012-05-15T14:48:26Z
dc.date.issued 1949-06
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/7154
dc.description.abstract A simplified panel model is described, together with a number of assumptions about the mode of its bucking. The approach to the calculation of the buckling stress is by splitting the panel into a number of flat plates and treating these by the ordinary plate theory. Use of the boundary conditions between these plates leads to a relation between the buckling stress and the variables of the panel geometry. The results thus obtained are compared with two sets of recent experimental work; and an appendix is included to show the effect of initial panel irregularities on the experimental determination of buckling stresses. 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 29 en_UK
dc.title The buckling in compression of panels with square top-hat section stringers en_UK
dc.type Report en_UK


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