Composites
New Features
- Post-Processing
- For the Abaqus solver interface, mapping section point results to actual plies and their corresponding recovery planes allows much more effective post-processing of results with layers. For details, see the Post release notes.
Enhancements
- Composite Stress Toolbox
- Composite Analysis Result viewer selection behavior for material and ply engineering constants calculation is now in line with the behavior of other analyses.
Resolved Issues
- Composite Stress Toolbox
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- When deactivating plies/composites in the Entity State Browser, the deactivated plies are no longer used in composite stress toolbox calculations.
- Previously, in rare cases with no failure criteria selected in the first ply failure method for load response failure calculations, a failure index was reported regardless. This is now prevented by a different initialization routine.
Known Issues
- Composite Stress Toolbox
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- MATF PUCK3D, TSAI3D, and HASH3 failure criteria only support reading the allowables, but not the additional parameters (W1, W2, W3). Standard set for those parameters for glass fiber and carbon fiber is used as per ESAComp documentation for PUCK. F12 is used for TSAI3D. W1=alpha=1 is used for HASH3D.
- Pre-Processing
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- Performance of laminate realization and graphics shift selection of plies for large models.
- FE Absorb Plies produces an incorrect result if input zone properties do not have global names/IDs and there are ply drops on top and bottom layers across properties to be absorbed.
- Comprehensive support of LS-DYNA material orientation review is not available.