SimcenterKnowledge

Laminate Composites > Solution and post processing > Laminate results

Simcenter 3D Multiphysics laminate results

Modeling object Output request Output result Results coordinate systems
Structural Output RequestsNOTE Force Solid element forces Native (element) coordinate system
Stress/Strain Ply stresses and strains Native (ply) coordinate system
Failure indices N/A
Strength ratiosNOTE N/A
Thermal Output Requests (Thermal page) Temperatures Ply temperatures N/A

Structural results locations

Ply results are located at the middle of the ply, the top and bottom of the ply, or the top, middle, and bottom of the ply. You request the location from the Composite Solid Ply Output list in Structural Output Requests dialog box.

Interlaminar results are located at the top and bottom of the ply.

Elemental, nodal output

Structural 3D element ply results are at the element centroid and at the element nodes depending on the option you select from the Location list in the Structural Output Requests dialog box.

  • When you select CENTER from the Location list, 3D element ply results are displayed at the element centroid and have the string Elemental in the results node name in the Post Processing Navigator.

  • When you select CORNER or SGAGE from the Location list, 3D element ply results are at both the element centroid and element nodes.The results at the element centroid have the string Elemental in the results node name in the Post Processing Navigator.The results at the element nodes have the string Elemental-Nodal in the results node name in the Post Processing Navigator.

The thermal solver outputs only Ply Temperatures - Elemental results per plies bacause the thermal solver solves for elemental results. Nodal results are interpolated from elemental results, thus nodal temperatures cannot be computed for each ply separately. Nodal temperatures are displayed using the Temperatures - Nodal result set.

How do I

View laminate physical properties for a selected element in post processing

Learn more

Nastran laminate results

ANSYS laminate results

Abaqus laminate results

Laminate results (Simcenter Samcef)

Look up more details

Shell stress resultant notations

Quick links

Command reference

Pre/Post video examples

Bulk Entry Descriptions

Simcenter 3D tutorials

Browse Simcenter 3D help by product area

Simcenter 3D Multiphysics laminate results, Simcenter 3D 2021.1 Series

© 2020 Siemens

The Nastran output format is PCOMPS.

PARAM,SRCOMPS = YES (default = NO)

window.mainLanguage="en_US"

window.delivId=""

window.projectId=""

MathJax.Hub.Config({ TeX: { extensions: ["autoload-all.js"] }, tex2jax: { displayMath: [ ] }, "SVG": { scale: 125 } });

Source: https://docs.sw.siemens.com/en-US/doc/289054037/PL20200601120302950.advanced/xid1185478 · retrieved 2026-07-17