Finite element crack propagation analysis of shear loaded buckling panels

Abstract

Purpose -In former work, test results of cracks in aluminium panels under cyclic shear buckling showed that cracks in the tensile stress field of a buckle propagate. The main influencing factor for the crack growth rate is the maximum principle stress. A simplified approach for crack propagation analyses based on this finding showed limitations for application on larger cracks because it disregarded the increasing out-of-plane deformation for larger cracks as well as stress redistributions. The purpose of this paper is to improve the results of the simplified approach with the help of finite element method (FEM). Design/methodology/approach -An approach for crack propagation based on FEM is presented taking into account the mutual interaction of cracks and buckling. The finite element (FE) model, which is described in detail, respects the boundary conditions of the test-set-up. Different initial crack positions, loads and panel thicknesses are analyzed. Results of the stress intensity factors KI calculated by the ABAQUS w FE model provide a function which is used to run a crack propagation analysis based on Forman law. Findings -The results of the FE-based crack propagation solution are in good agreement with test results and improve the prediction of the simplified approach. It is not restricted in terms of panel thickness, crack position or applied shear load. Research limitations/implications -Limitations of the FE-based crack propagation solution compared to the experimental results are discussed. These are, the sensitivity of crack propagation analyses to initial crack length and deviations of the experimental settings from the ideal FE model. Originality/value -The interaction of cracks and buckling in aluminium shells is mainly disregarded both in research and industrial work, but can be of interest considering, accidental damages in fuselage side shells. Cracks propagate under shear load as it was shown in former work. The FE modeling of the tests presented in this paper proves the mutual interactions of crack propagation and buckling deformation.

Numerical buckling analysis of cracked Bi-material thin plates

“…Recently, several numerical and experimental studies were carried out using the finite element method to analyze buckling strength for cracked panels under different load cases. 4,5 The critical load multiplier may be determined by varying certain parameters, such as the length of the crack, the Poisson’s ratio, and the orientation of the crack. AV Raviprakash et al 6 worked on the critical buckling load for a thin square plate with center or edge cracks, and subjected to axial compression.…”

The significance of the interaction of stability and damage propagation in metallic and composite panels

“…All data shown in this section are taken from Bierbaum's PhD thesis. Basic data on the material and the exact type of tests, etc., may be found in Bierbaum and Horst (2013).…”