This report presents a simplified large-deflexion theory for thin flat plates subjected to normal loading. The theory is applicable to plates in which the loading is resisted primarily by the flexural rigidity of the plate. The middle surface of the plate is assumed to be inextensional so that the mode of deformation is a developable surface. There is good agreement with experiment.
A Large-Deflexion Theory for Thin Plates
A Theory based on the Assumption of an Inextensional Middle Surface of the Plate
Aircraft Engineering and Aerospace Technology ; 27 , 4 ; 102-108
1955-04-01
7 pages
Article (Journal)
Electronic Resource
English
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