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

Hemp, W. S.; Griffin, K. H.

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