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Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels
Authors:Navin Jaunky  Norman F Knight Jr  Damodar R Ambur
Affiliation:Department of Aerospace Engineering, Old Dominion University, Norfolk, VA 23529-0247, USA;Structural Mechanics Branch, NASA Langley Research Center, Hampton, VA 23681-0001, USA
Abstract:An improved smeared stiffener theory for stiffened panels is presented that includes skin-stiffener interaction effects. The neutral surface profile of the skin-stiffener combination is developed analytically using the minimum potential energy principle and statics conditions. The skin-stiffener interaction is accounted for by computing the bending and coupling stiffness due to the stiffener and the skin in the skin-stiffener region about a shift in the neutral axis at the stiffener. Buckling load results for axially stiffened, orthogrid, and general grid-stiffened panels are obtained using the smeared stiffness combined with a Rayleigh-Ritz method and are compared with results from detailed finite element analyses.
Keywords:stiffened composite panels  smeared stiffener theory  buckling
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