- The results are automatically loaded into Autodesk Nastran In-CAD.
- You will now look at various composite results.
-
COMP MAX PLY FAILURE INDEX
- Right-click on
von Mises under
Results and choose
Edit.
- Select
COMP MAX PLY FAIL INDEX for the
Results Data under
Contour Options. Make sure
Deform and
Contour are selected.
- Change the
Data Type drop-down to
Centroidal, the
Contour Type drop-down to
Elemental, and check the
No Averaging checkbox.
- Uncheck
Max/Min under
Display Options.
- Click
Display.
- Click
OK.
This result output vector shows you the maximum occurring failure index (calculated using the Hill composite failure theory) on each element. When the failure index is over 1.0, first ply failure is predicted, meaning at least one ply has failed. When the failure index is less than 1.0, no failure is predicted to occur.
-
COMP MAX FAILURE INDEX PLY
- Right-click on
Displacement and select
Edit.
- Change the
Result Data to
COMP MAX FAILURE INDEX PLY.
- Change
Levels from
24 to
12.
- Change
Rendering to
Fringe.
- Uncheck
Max/Min under
Display Options.
- Click
Display.
- Click
OK.
COMP MAX FAILURE INDEX PLY indicates what ply is most critical and has the highest failure index.
-
COMP PLY 1 NORMAL-1
- Right-click on
Displacement and select
Edit.
- Change the
Result Data to
COMP PLY 1 NORMAL-1 STRESS.
- Change the
Levels from
12 to
24 and
Rendering to
Continuous.
- Click
Display.
- Click
OK.
COMP PLY 1 NORMAL–1 STRESS is the stress along the fiber direction for ply 1. COMP PLY 1 NORMAL-2 STRESS is the stress in the transverse fiber direction for ply 1.
This concludes Using Composite Materials in a Bike Frame Section.
The following summarizes the main topics covered:
- Running an analysis with a composite material.
- How to set up a laminate physical property.
- How to configure a material orientation.
- How to use shell modeling.
- How to extract the maximum failure index.
- How to extract the ply where the maximum failure index is occurring.
- How to interpret ply normal stresses.