Pre-tension section

This problem contains basic test cases for one or more Abaqus elements and features.

This page discusses:

ProductsAbaqus/Standard

Elements tested

  • B21
  • B31
  • C3D6
  • C3D8
  • C3D8IH
  • C3D8R
  • C3D10
  • C3D10M
  • C3D20
  • C3D27H
  • CAX4
  • CAX4RH
  • CAX8R
  • CAX4T
  • CPE3
  • CPE3H
  • CPE4
  • CPE4R
  • CPE8
  • CPE8RT
  • CPS4R
  • CPS6M
  • CPS8
  • T2D2
  • T3D2
  • T3D3

Features tested

Applying a prescribed assembly load on a variety of structures by means of a pre-tension section is tested.

Problem description

This set of tests verifies that the proper prescribed assembly load is applied to a structure using a pre-tension section. Loading is done by enforcing either a concentrated force (pre-tension load) or a displacement (tightening) at the pre-tension node (see Prescribed Assembly Loads for a description of this option). The structure is preloaded in the first step. In most cases it is further loaded in the second step, ensuring that the tightening is maintained.

The majority of the models are two-element meshes with boundary conditions that allow for uniform stretching of the cross-section. Thus, results verification is straightforward. Some input files have several two-element meshes with different element types set up in parallel.

In the first input file the total force in the defined pre-tension sections is output (see Output to the Data and Results Files). The total force results in the direction perpendicular to the sections match the reaction forces at the reference nodes associated with the pre-tension sections exactly.

The analyses include a submodel run (with the pre-tension section fully enclosed by the submodel boundary) and a substructure run (where the substructure's retained degrees of freedom belong to the pre-tension section).

Results and discussion

Analysis results indicate that the prescribed force or displacement is always established across the pre-tension section. Uniform sections yield a uniform axial stress given the analysis boundary conditions. Results after subsequent loading in the second step also indicate that the prescribed tightening of the section is maintained properly.

A full example that makes use of this feature is included in Axisymmetric analysis of bolted pipe flange connections.

Input files

xptssib2a.inp

Tests in parallel, multiple element types; SECTION FILE tests.

xptspit3.inp

Linear static perturbation.

xptsse23.inp

Tests in parallel, multiple element types.

xptssh2a3.inp

Hyperelastic material.

xptsri2.inp

Static analysis, Riks method.

xptsdib.inp

Dynamic analysis.

xptsdea.inp

Dynamic analysis with orthotropic material.

xptsdh2.inp

Direct-integration and subspace-based steady-state dynamics with hyperelastic material.

xptsti2a.inp

Coupled temperature-displacement.

xptsfit.inp

Natural frequency extraction with steady-state dynamics.

xptssi3.inp

C3D10 mixed with C3D20 elements; automatic midface node generation.

xptssh3.inp

TRANSFORM used on section nodes.

xptssi23.inp

User-defined section normal; degenerate elements.

xptssi2z.inp

Static analysis with substructures.

xptssi2.inp

Submodeling, global analysis.

xptssi2s.inp

Submodeling, local analysis.