3.2.6 Linear kinematics element tests

Product: ABAQUS/Explicit  

Elements tested

B21    B22    B31    B32    C3D8R    CPE4R    CPS4R    CAX4R    M3D4R    S4R    S4RS    S4RSW    SAX1    T2D2    T3D2   

Feature tested

The small-displacement deformation theory.

Problem description

This verification test consists of a set of single-element models for each element type in analyses that use the small-displacement theory (NLGEOM=NO on the *STEP option). All degrees of freedom are prescribed so that the results do not include any dynamic effects. Each element is subjected to all applicable fundamental modes of deformation. The total strains are large to show that the results are linear and remain unaffected by changes to the element's current configuration.

The material is linear elastic with a Young's modulus of 1.0 × 105, Poisson's ratio of .33, and density of 1000.

Results and discussion

All element types tested yield the appropriate results for their applicable fundamental modes of deformation. Results for the two-dimensional truss element are illustrated here.

There are two global modes of deformation for a two-dimensional truss: longitudinal and lateral. The longitudinal mode is driven by fixing one end of the truss and prescribing a longitudinal displacement at the other. The axial stresses in the truss element as a result of longitudinal deformation for both small-displacement theory (NLGEOM=NO) and large-displacement theory (NLGEOM=YES) are shown in Figure 3.2.6–1. As the strains become large, the results diverge because the large-displacement theory accounts for the thinning of the truss as it stretches. The global lateral mode is invoked by prescribing a lateral displacement at one end of the truss element while holding all other degrees of freedom fixed. Results for the lateral case are shown in Figure 3.2.6–2. The nonlinear geometric effect is accounted for only in the large-displacement analysis. The small-displacement analysis ignores the extension of the truss due to its rotation and, therefore, sees no extensional strain due to the prescribed lateral displacements.

Input files

lk_b21.inp

B21 elements.

lk_b22.inp

B22 elements.

lk_b31.inp

B31 elements.

lk_b32.inp

B32 elements.

lk_c3d8r.inp

C3D8R elements.

lk_c3d8r_orient.inp

C3D8R elements with *ORIENTATION.

lk_cax4r.inp

CAX4R elements.

lk_cax4r_orient.inp

CAX4R elements with *ORIENTATION.

lk_cpe4r.inp

CPE4R elements.

lk_cpe4r_orient.inp

CPE4R elements with *ORIENTATION.

lk_cps4r.inp

CPS4R elements.

lk_cps4r_orient.inp

CPS4R elements with *ORIENTATION.

lk_dashpota.inp

Dashpot elements.

lk_m3d4r.inp

M3D4R elements.

lk_m3d4r_orient.inp

M3D4R elements with *ORIENTATION.

lk_s4r.inp

S4R elements.

lk_s4r_gs.inp

S4R elements with the *SHELL GENERAL SECTION option.

lk_s4rs.inp

S4RS elements.

lk_s4rs_orient.inp

S4RS elements with *ORIENTATION.

lk_s4rs_gs.inp

S4RS elements with the *SHELL GENERAL SECTION option.

lk_s4rsw.inp

S4RSW elements.

lk_s4rsw_orient.inp

S4RSW elements with *ORIENTATION.

lk_s4rsw_gs.inp

S4RSW elements with the *SHELL GENERAL SECTION option.

lk_sax1.inp

SAX1 elements.

lk_sax1_gs.inp

SAX1 elements with the *SHELL GENERAL SECTION option.

lk_springa.inp

Spring elements.

lk_t2d2.inp

Two-dimensional truss elements.

lk_t3d2.inp

Three-dimensional truss elements.

Figures

Figure 3.2.6–1 Axial stress comparison for the extensional mode.

Figure 3.2.6–2 Axial stress comparison for the shear mode.