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Pozycja Wpływ modułu sprężystości postaciowej na stateczność płyt trójwarstwowych(Katedra Wytrzymałości Materiałów i Konstrukcji, Politechnika Łódzka, 2003) Mania, R.W pracy podano wyniki analizy stateczności globalnej płyt trójwarstwowych w kształcie trapezu równoramiennego swobodnie podpartych na całym obwodzie, poddanych osiowemu ściskaniu. Omówiono szczególny wpływ materiału rdzenia - jego modułu odkształcenia postaciowego - na wybór modelu płyty dla rozwiązania zagadnienia stateczności oraz na poziom obciążenia krytycznego płyty. Zamieszczono i omówiono wyniki rozwiązania analitycznego i rozwiązania numerycznego metodą elementów skończonych.Pozycja Element Birth and Death Method Application to Lamellar Crack Analysis(Wydawnictwo Politechniki Łódzkiej ; Katedra Dynamiki Maszyn - Wydział Mechaniczny Politechniki Łódzkiej, 2015) Jaroniek, Mieczysław; Niezgodziński, TadeuszLoad structure, the maximum permissible load is usually determined by the strength calculation (bearing data. Yield stress or strength of the material), or the parameters of fracture mechanics. The paper analyzes the calculations lamellar cracks formed in the lower crane girders steel belts. These cracks are formed in rolled sheets of non-metallic inclusions. The determination of the cracks in the existing designs are extremely difficult. It requires testing metallographic, ultrasonic or acoustic methods. Based on typical images of metallographic steel plates specified place of occurrence of cracks lamellar and sampling, and has subsequently been adopted for the calculation of numerical models of material structure and distribution of artificial joints. In order to analyze the propagation of cracks and formation of lamellar phase slots and destruction was carried out modeling studies and numerical methods cracking process.Pozycja Numerical Model of CAI Test for Fibre-Reinforced Polymer Plate.(Lodz University of Technology. Faculty of Mechanical Engineering. Department Division of Dynamics., 2016) Baszczyński, Piotr; Dziomdziora, Sebastian; Naze, Rafał; Kubiak, TomaszThis article presents numerical simulations of laminates subjected to Compression After Impact (CAI) testing including delamination modelling. Different model of impact damages of laminate were considered. Progressive damage analysis have been employed and different failure criteria have been applied. For each simulation failure load has been estimated as same as the position of damages at destroyed layer. Finally, obtained numerical results were compared with experimental data from referential paper.Pozycja Local Buckling of Thin-Walled Column of Square Cross-Section Made of In-Plane Coupled Laminate.(Lodz University of Technology. Faculty of Mechanical Engineering. Department Division of Dynamics., 2016) Kołakowski, Zbigniew; Teter, Andrzej; Pasierbiewicz, DamianThe non–symmetric, general laminate exhibits different types of coupling between the extension, shearing, bending and twisting. For practical reasons, the in–plane coupled laminate is a particularly interesting. In this case, the coupling between shearing andextension takes place. Details calculations were performed for a short columns of square cross-section made of in–plane coupled and fully uncoupled laminate under uniform compression. Finite element method (FEM) and analytical–numerical method (ANM) were performed. In FEM analyses, the eigenbuckling problem has been solved using the Lanczos method, whereas the nonlinear buckling analysis were performed using the Newton– Raphson method and the Ritz method. In ANM analyses, the Koiter’s asymptotic theory is applied. The relationship between forces/moments and deformations/curvature were described using classical lamination theory (CLT). The coupling between in–plane shearing and extension has a significant influence on the behavior of thin–walled structures under compression.Pozycja Element Birth and Death Method Application to Lamellar Crack Analysis.(Lodz University of Technology. Faculty of Mechanical Engineering. Department Division of Dynamics., 2015) Jaroniek, Mieczysław; Niezgodziński, TadeuszLoad structure, the maximum permissible load is usually determined by the strength calculation (bearing data. Yield stress or strength of the material), or the parameters of fracture mechanics. The paper analyzes the calculations lamellar cracks formed in the lower crane girders steel belts. These cracks are formed in rolled sheets of non–metallic inclusions. The determination of the cracks in the existing designs are extremely difficult. It requires testing metallographic, ultrasonic or acoustic methods. Based on typical images of metallographic steel plates specified place of occurrence of cracks lamellar and sampling, and has subsequently been adopted for the calculation of numerical models of material structure and distribution of artificial joints. In order to analyze the propagation of cracks and formation of lamellar phase slots and destruction was carried out modeling studies and numerical methods cracking process.