A simple matric formulation is developed for calculating the elastic buckling of a class of simply supported flat plates that arc simultaneously tapered in plan form and in thickness in one direction and subjected to biaxial loading that varies in each direction. Design curves are presented for the special case when the thickness taper is linear and the plate material is equally stressed in the direction of this thickness taper.
The Buckling of Tapered Plates in Compression
Compressive Buckling under Varying Loading of Simply Supported Plates Simultaneously Tapered in Plan Form and in Thickness
Aircraft Engineering and Aerospace Technology ; 28 , 12 ; 427-430
1956-12-01
4 pages
Article (Journal)
Electronic Resource
English
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