1.3.5 Axisymmetric solid elements with twist

Product: ABAQUS/Standard  

Elements tested

CGAX3    CGAX3H    CGAX3HT    CGAX3T    CGAX4    CGAX4H    CGAX4HT    CGAX4R    CGAX4RH    CGAX4RHT    CGAX4RT    CGAX4T    CGAX6    CGAX6H    CGAX6M    CGAX6MH    CGAX6MHT    CGAX6MT    CGAX8    CGAX8H    CGAX8HT    CGAX8R    CGAX8RH    CGAX8RHT    CGAX8RT    CGAX8T   

Problem description

Material:

Linear elastic, Young's modulus = 106, Poisson's ratio = 0.3.

Boundary conditions:

; ; .

Step 1

A concentrated moment loading equivalent to a distributed moment loading M of 6402 is applied on top face CD.

Analytical solution:

Twist

= 0.01 (on top face CD).

Stresses

.

Results and discussion

All elements yield the analytical solution.

The *SECTION FILE and *SECTION PRINT output requests are used in some of the input files to output accumulated quantities on the face CD. The area of the face is 3.142.

Input files

eca3gfs3.inp

CGAX3 elements.

eca3ghs3.inp

CGAX3H elements.

eca3hhs3.inp

CGAX3HT elements.

eca3hfs3.inp

CGAX3T elements.

eca4gfs3.inp

CGAX4 elements.

eca4ghs3.inp

CGAX4H elements.

eca4hhs3.inp

CGAX4HT elements.

eca4grs3.inp

CGAX4R elements.

eca4gys3.inp

CGAX4RH elements.

eca4hys3.inp

CGAX4RHT elements.

eca4hrs3.inp

CGAX4RT elements.

eca4hfs3.inp

CGAX4T elements.

eca6gfs3.inp

CGAX6 elements.

eca6ghs3.inp

CGAX6H elements.

eca6gks3.inp

CGAX6M elements.

eca6gls3.inp

CGAX6MH elements.

eca6hls3.inp

CGAX6MHT elements.

eca6hks3.inp

CGAX6MT elements.

eca8gfs3.inp

CGAX8 elements.

eca8ghs3.inp

CGAX8H elements.

eca8hhs3.inp

CGAX8HT elements.

eca8grs3.inp

CGAX8R elements.

eca8gys3.inp

CGAX8RH elements.

eca8hys3.inp

CGAX8RHT elements.

eca8hrs3.inp

CGAX8RT elements.

eca8hfs3.inp

CGAX8T elements.