A technique is suggested to estimate numerically values of surface fracture growth and stress intensity factors (SIF) for standard parts with complicated geometry. A module is developed basing on the ANSYS finite-element software package. This module allows to generate automatically a net of singular elements and to evaluate SIF distribution along the front of elliptic-shaped fracture. Numerical and experimental investigations are carried out for fracture growth duration in regard to structural elements of airliner high-lift devices. It is demonstrated that the proposed technique for finite-element SIF and crack growth resistance evaluation provides results, which are acceptable with respect to accuracy.
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