Abstract
A numerical method is presented for the elastic, post-buckling behaviour of a simply supported, mild-steel circular plate loaded in uniform compression around the edge of the plate. Such a procedure obviates the solution of the orthodox von Kármán large deflection equations, substituting, instead, a step-by-step integration of the differential equations of equilibrium and testing at each step to satisfy prescribed boundary conditions. The equations are programmed for a high-speed digital computer and the overall behaviour of the plate is obtained in terms of the applied edge load and the central deflection. The programme is evaluated for various plate sizes, and the edge load and central deflection are related through contours of moment and thrust at the centre of the plate.
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