Abstract A novel modular multistep algorithm is proposed for multi-criteria analysis of fracture of aircraft structures with complex geometries. In order to evaluate the algorithm, the crack growth analysis is realized by the following three criteria, namely, the stress intensity factor, the strain energy release rate, and the J-integral. The algorithm implementation by the finite element method is considered and prospects of alternative implementation based on the meshfree methods are assigned.
Multi-criteria analysis of aircraft structures fracture
Russian Aeronautics (Iz VUZ) ; 58 , 4 ; 370-375
2015-10-01
6 pages
Article (Journal)
Electronic Resource
English
Multi-criteria analysis of aircraft structures fracture
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