1.3.14 Verification of section forces for shells

Product: ABAQUS/Standard  

Elements tested

S4    S4R    S4R5    S8R    S8R5    S9R5    STRI3    STRI65   

Problem description

Material:

Linear elastic, 2.00313 × 107, 5.00783 × 105, 1.25296 × 105, 0.5 × 105, 0.5 × 105.

Boundary conditions:

Nodes along edge are clamped.

Loading:

0.5 at nodes B and C.

Orientations:

90° in the first layer and 0° in the second layer, with respect to the x-axis, rotated about the z-axis.

There are two elements with identical geometries in the model. The first element is defined via *SHELL SECTION, COMPOSITE and uses *ORIENTATION options. The second element is defined by *SHELL GENERAL SECTION, with the section stiffness matrix input directly, and is equivalent to the two-layer model presented above.

The section stiffness is:

Reference solution

Stress resultants: Moment = –1.0(10.0 – x).

Results and discussion

All elements yield acceptable solutions. The *EL FILE, DIRECTIONS=YES option is used in the input file with element type S8R5 (es58s2sc.inp).

Input files

ese4s2sc.inp

S4 elements.

esf4s2sc.inp

S4R elements.

es54s2sc.inp

S4R5 elements.

es68s2sc.inp

S8R elements.

es58s2sc.inp

S8R5 elements.

es59s2sc.inp

S9R5 elements.

es63s2sc.inp

STRI3 elements.

es56s2sc.inp

STRI65 elements.