Expressions for critical timesteps are provided for an explicit finite element method for plane elastodynamic problems in isotropic, linear elastic solids. Both 4-node and 8-node quadrilateral elements are considered. The method involves solving for the eigenvalues directly from the eigenvalue problem at the element level. The characteristic polynomial is of order 8 for 4-node elements and 16 for 8-node elements. Due to the complexity of these equations, direct solution of these polynomials had not been attempted previously. The commonly used critical time-step estimates in the literature were obtained by reducing the characteristic equation for 4-node elements to a second-order equation involving only the normal strain modes of deformation. Furthermore, the results appear to be valid only for lumped-mass 4-node elements. In this paper, the characteristic equations are solved directly for the eigenvalues using Mathematica and critical time-step estimates are provided for both lumped and consistent mass matrix formulations. For lumped-mass method, both full and reduced integration are considered. In each case, the natural modes of deformation are obtained and it is shown that when Poisson's ratio is below a certain transition value, either shear-mode or hourglass mode of deformation dominates depending on the formulation. And when Poisson's ratio is above the transition value, in all the cases, the uniform normal strain mode dominates. Consequently, depending on Poisson's ratio the critical time-step also assumes two different expressions. The approach used in this work also has a definite pedagogical merit as the same approach is used in obtaining time-step estimates for simpler problems such as rod and beam elements.
IntroductionIt is well known known that the critical time-step estimates in fully-discretized standard Galerkin formulations of undamped structural dynamics problems obey the relationwhere x max is the largest natural frequency of any element in the finite element mesh and is obtained by solving the eigenvalue problem at the element level. The characteristic equation resulting from the eigenvalue problem is of the same order as the number of degrees of freedom (DOF)s per element. For problems such as axial loading of bars, beam bending and scalar wave propagation, when lower order elements are used, the maximum eigenvalue can be found readily in symbolic terms since the order of the polynomial characteristic equation is manageable [2]. However, for more complicated problems such as elastic wave propagation in two and three-dimensional media, the characteristic equations tend to be very complicated and hence roots cannot easily be found. For example, in the case of plane elastodynamic problems, the characteristic equation is, of order 8 when 4-node quadrilateral elements (Q4) are used and of order 16 when 8-node quadrilaterals (Q8) are used. To the authors' knowledge and as implied in [2], these equations have not been solved previously for the eigenvalues. However, conservative estimate for stable t...