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Buckling analysis of anisotropic variable-curvature panels and shells
Authors:Navin Jaunky  Norman F. Knight Jr.   Damodar R. Ambur
Affiliation:

a Department of Aerospace Engineering, Old Dominion University, Norfolk, VA 23529-0247, USA

b Structural Mechanics Branch, NASA Langley Research Center, Hampton, VA 23681-0001, USA

Abstract:A buckling formulation for anisotropic variable-curvature panels is presented in this paper. The variable-curvature panel is assumed to consist of two or more panels of constant curvature where each panel may have a different curvature. Bezier functions are used as Ritz functions. Displacement (C0), and slope (C1) continuities between segments are imposed by manipulation of the Bezier control points. A first-order shear-deformation theory is used in the buckling formulation. Results obtained from the present formulation are compared with those from finite element simulations and are found to be in good agreement.
Keywords:
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