This paper describes contribution to solving the problem of non-linear truss system buckling. Matrix equations [[K] + γ [KG]]{R} = {0} are used in theory of linear buckling for solving of critical force. System's stiffness matrix [K] and geometrical stiffness matrix are independent on nodal displacement vector {R}. Critical parameter γ is solved from equation mentioned above using methods of numerical mathematics. Vector of critical load is determinated by equation {Fₖᵣ} = γ {Fₒ}. Vector {Fₒ} is used for solving of [KG]. Corresponding matrix [kg] of elements are linearized. The main topic of this contribution is the exchange of the matrix [kg] after removing of this linearization.
The paper provides an analysis of a membrane element with an additional rotational degree of freedom. Similar elements, the stiffness matrices obtained in an exact procedure, were investigated in other studies. The paper, however, analyses the membrane element stiffness matrix obtained in an approximate procedure with the use of reduced integration. Such an approach is an attempt at eliminating shear locking that occurs when a membrane element with additional rotational degrees of freedom is applied.
W prezentowanej pracy przeprowadzono analizę spektralną macierzy sztywności niestandardowych elementów skończonych. Niestandardowe elementy skończone to elementy tarczowe z dodatkowymi rotacyjnymi stopniami swobody w węźle. Zastosowane w modelowaniu umożliwiają połączenie podobszarów o różnych stopniach swobody. Dla każdej analizowanej macierzy sztywności zostały wyznaczone wartości i wektory własne, na podstawie których dokonano oceny poprawności sformułowania MES wymienionych elementów. Sprawdzono również wektor odkształceń e.
EN
In this paper, the spectral analysis was applied for evaluation of the non-standard finite elements. The finite non-standard element is based on the following assumptions: a rigid nodal point exists in the area of membrane. Three nodal displacements, two in plane translations and one rotation (drilling) are considered. Therefore, was one should also estimate the correctness of the non-standard elements formulation. In this paper, the research results of the correctness of the 2D & 3D transition elements with use of the test of eigenvalues and eigenvectors of stiffness matrix as well as verification of strains vector have been presented.
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