To use the all-tetrahedral mesh generation capabilities existing today, we
have explored the creation of a computationally efficient eight-node tetrah
edral finite element (a four-node tetrahedral finite element enriched with
four mid-face nodal points). The derivation of the element's gradient opera
tor, studies in obtaining a suitable mass lumping and the element's perform
ance in applications are presented. In particular, we examine the eight-nod
e tetrahedral finite element's behavior in longitudinal plane wave propagat
ion, in transverse cylindrical wave propagation, and in simulating Taylor b
ar impacts. The element samples only constant strain states and, therefore,
has 12 hourglass modes. In this regard, it bears similarities to the eight
-node, mean-quadrature hexahedral finite element. Comparisons with the resu
lts obtained from the mean-quadrature eight-node hexahedral finite element
and the four-node tetrahedral finite element are included. Given automatic
all-tetrahedral meshing, the eight-node, mean-quadrature tetrahedral finite
element is a suitable replacement for the eight-node, mean-quadrature hexa
hedral finite element and meshes requiring an inordinate amount of user int
ervention and direction to generate. Copyright (C) 1999 John Wiley & Sons,
Ltd. This paper was produced under the auspices of the U.S. Government and
it is therefore not subject to copyright in the U.S.