
The limit state of two polymer layered composite elements was studied using a numerical-analytical method, employing the finite element method during their deformation, damage, and failure. Stress intensity factors for normal separation were determined for developed complex-shaped models with initial imperfections in the form of cracks, simulating defects in the composite structure. A comparative analysis of the obtained calculated values of critical load with the experimental studies and adaptation of the developed methodology were conducted.
finite element method, коефіцієнт інтенсивності напружень, fracture theory, crack, граничний стан, stress intensity factor, limit state, метод скінченних елементів, composite material, композиційний матеріал, тріщина, теорія руйнування
finite element method, коефіцієнт інтенсивності напружень, fracture theory, crack, граничний стан, stress intensity factor, limit state, метод скінченних елементів, composite material, композиційний матеріал, тріщина, теорія руйнування
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