2.3.8 Twisted ribbon test for shells

Product: ABAQUS/Standard  

Problem description

The original problem description and the benchmark solutions can be found in Batoz (1982).

The length of the plate is varied from 2.0 to 10.0 to study aspect ratio effects. The material is linear elastic with a Young's modulus of 1 × 107 and a Poisson's ratio of 0.25. Nodes along edge are clamped. The plate is twisted by applying a force of –1.0 at node , and an equal and opposite force at node . Gauss integration is used for the shell cross-section for the S9R5 element.

Results and discussion

The vertical displacement at node is found as a function of the plate's aspect ratio. Since the plate's width is 1.0, the aspect ratio is equal to the length, . Figure 2.3.8–2 plots vertical displacement at versus the length of the plate. All elements give reasonable numerical predictions compared with the reference solution; see Batoz (1982).

Input files

ese4sxsa.inp

S4 elements.

esf4sxsa.inp

S4R elements.

es54sxsa.inp

S4R5 elements.

es68sxsa.inp

S8R elements.

es58sxsa.inp

S8R5 elements.

es59sxsa.inp

S9R5 elements.

es63sxsa.inp

STRI3 elements.

es56sxsa.inp

STRI65 elements.

Reference

Figures

Figure 2.3.8–1 Model of plate.

Figure 2.3.8–2 Comparison of results.