4.2.4 LE4: Axisymmetric hyperbolic shell under uniform internal pressure

Product: ABAQUS/Standard  

Elements tested

SAX1    SAX2    SAXA11    SAXA21   

Problem description

Mesh:

A coarse and a fine mesh are tested for each element.

Material:

Linear elastic, Young's modulus = 210 GPa, Poisson's ratio = 0.3.

Boundary conditions:

At point , .

Loading:

Uniform internal pressure of 1 MPa.

Gauss integration is used for the shell cross-section for the SAXA11 elements.

Reference solution

This is a test recommended by the National Agency for Finite Element Methods and Standards (U.K.): Test LE4 from NAFEMS publication TNSB, Rev. 3, “The Standard NAFEMS Benchmarks,” October 1990.

Target solution: On the midsurface at point the meridional stress, , is –50.0 MPa and the hoop stress, , is 50.0 MPa.

Results and discussion

The results are shown in the following table. The values enclosed in parentheses are percentage differences with respect to the reference solution.

Element Type
SAX1 (Coarse)–49.69 (–0.62%)49.99 (–0.02%)
SAX1 (Fine)–49.99 (–0.02%)49.92 (–0.16%)
SAX2 (Coarse)–50.09 (0.18%)48.33 (–3.3%)
SAX2 (Fine)–50.02 (0.04%)48.34 (–3.3%)
SAXA11 (Coarse)–49.69 (–0.62%)49.92 (–0.16%)
SAXA11 (Fine)–49.99 (–0.02%)49.20 (–1.6%)
SAXA21 (Coarse)–50.09 (0.18%)48.33 (–3.3%)
SAXA21 (Fine)–50.02 (0.04%)48.34 (–3.3%)

Input files

Coarse mesh tests:


esa2smsf.inp

SAX1 elements.

esa3smsf.inp

SAX2 elements.

esnssmsf.inp

SAXA11 elements.

esnwsmsf.inp

SAXA21 elements.

Fine mesh tests:


esa2sfsf.inp

SAX1 elements.

esa3sfsf.inp

SAX2 elements.

esnssfsf.inp

SAXA11 elements.

esnwsfsf.inp

SAXA21 elements.