In this paper, a unified method is presented: (i) to model delaminated stiffened laminated composite shells; (ii) for synthesising accurate multiple post-buckling solution paths under compressive loading; and (iii) for predicting delamination growth. A multi-domain modelling technique is used for modelling the delaminated stiffened shell structures. Error-free geometrically nonlinear element formulations — a 2-noded curved stiffener element (BEAM2) and a 3-noded shell element (SHELL3) — are used for the finite element analysis. An accurate and simple automated solution strategy based on Newton type iterations is used for predicting the general geometrically nonlinear and postbuckling behaviour of structures. A simple method derived from the 3-dimensionalJ-integral is used for computing the pointwise energy release rate at the delamination front in the plate/shell models. Finally, the influence of post-buckling structural behaviour and the delamination growth on each other has been demonstrated.

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A computational model for analysing interactive buckling and delamination growth in composite structures

In this paper, a unified ethod is presented to model delaminated stiffened laminated composite shells, for synthesizing accurate multiple post-buckling solution paths under comprssive loading, and for predicting delamination growth in an a posteriori sense with reference to finite element applications. A multi-domain modeling technique is presented for modeling the delaminated stiffened shell structures. Error-free formulations axe presented for a 2-noded curved stiffener element and a 3-noded shell element for geometrically nonlinear applications. An accurate and simple automated solution strategy based on Newton type iterations is presented for predicting the general geometrically nonlinear and postbuckling behaviour of structures. Finally, a simple method is derived for predicting the delamination growth in terms of pointwise energy release rate at the delamination front from the 3-dimensional J-integral.

B P Naganarayana

Papers

Multi-Domain Modeling of Delaminated Stiffened Composite Shells