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Please use this identifier to cite or link to this item: http://dspace.lib.cranfield.ac.uk/handle/1826/7154

Document Type: Report
Title: The buckling in compression of panels with square top-hat section stringers
Authors: Hemp, W. S.
Griffin, K. H.
Issue Date: Jun-1949
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.
URI: http://dspace.lib.cranfield.ac.uk/handle/1826/7154
Appears in Collections:College of Aeronautics Reports

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