The buckling of plates tapered in planform

Show simple item record G. G. Pope en_US 2014-10-21T15:55:52Z 2014-10-21T15:55:52Z 1962 en_US
dc.identifier.other ARC/R&M-3324 en_US
dc.description.abstract An analysis is given of the buckling of a plate of constant thickness tapered symmetrically in planform and subjected to uniform compressive loading on the parallel ends. Two cases are considered. (1) Different uniform loads applied normal to the ends, equilibrium being maintained by shear flows along the sides. (2) Equal uniform stresses applied normal to the ends, with displacement of the sides prevented normal to the direction of taper. Opposite pairs of edges are either simply-supported or clamped. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title The buckling of plates tapered in planform en_US

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