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- W2034386822 abstract "A method for computing skin-stiffener interface stresses in stiffened composite panels is developed. Both geometrically linear and nonlinear analyses are considered. Particular attention is given to the flange termination region where stresses are expected to exhibit unbounded characteristics. The method is based on a finite element analysis and an elasticity solution. The finite element analysis is standard, whereas the elasticity solution is based on an eigenvalue expansion of the stress functions. The eigenvalue expansion is assumed to be valid in the local flange termination region and is coupled with the finite element analysis using collocation of stresses on the local region boundaries. The results indicate that the inclusion of geometric nonlinearities is very important for an accurate determination of the interface stresses. Membrane flattening of the panel tends to reduce the tendency of the stiffener to separate." @default.
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- W2034386822 date "1992-04-01" @default.
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- W2034386822 title "Influence of geometric nonlinearities on skin-stiffener interface stresses" @default.
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- W2034386822 doi "https://doi.org/10.2514/3.11027" @default.
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