32th Congress of the International Council of the Aeronautical Sciences

04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity

ITERATIVE GLOBAL/LOCAL NON-INTRUSIVE MODEL COUPLING METHOD FOR STRUCTURE FAILURE ANALYSIS

Y.J. Liuš, S.Q. Liangš, R.J. Sunš, M.Q. Li, China; šAVIC THE FIRST AIRCRAFT INSTITUTE, China

In this paper, based on the FE non-intrusive coupling framework, an innovative iterative global/local non-intrusive model coupling method was developed to analyze the local crack failure. Several acceleration strategies are studied to further reduce iterations. The FE simulation of a failure experiment of a joint structure is performed to verify the proposed method. Numerical results showed that the coupling results have very good convergence with experimental result.


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