Skip to main content

Currently Skimming:

Appendix E Survey of Some Computational Models for Failure, Damage, and Degradation in Composite Materials
Pages 56-63

The Chapter Skim interface presents what we've algorithmically identified as the most significant single chunk of text within every page in the chapter.
Select key terms on the right to highlight them within pages of the chapter.


From page 56...
... Laboratory Progressive Sleight of Langley Research Center. Failure in For further information, access the Laminated technical support package free online Composites at under materials category L-17660.
From page 57...
... MRLife, a damage model developed at Virginia Polytechnic Institute and State University. The damage model was incorporated into a subroutine linked to ANSYS, creating a life prediction system in which entire composite structures can be evaluated for damage using realistic geometry and loading.
From page 58...
... Dynamic This enhancement to LS-DYNA Commercial Composite enables the most effective and code Simulator accurate dynamic progressive failure module of modeling of composite structures LS-DYNA currently available. The integration of this module, known as MAT 161, into LS-DYNA allows users to account for progressive damage of various fiber, matrix, and interplay delamination failure modes.
From page 59...
... LAMPAT Finite element pre- and postprocessor for analyzing thick composite laminates. Integrates with PATRAN.
From page 60...
... continuous and discontinuous composite materials with arbitrary internal microstructures and reinforcement shapes. It enables the efficient analysis of composite structures subjected to complex thermomechanical load histories.
From page 61...
... RESTRAN This code is developed at the Army Laboratory (Residual Research Laboratory at Aberdeen Strength Proving Ground in Maryland. A general Analysis of predictive methodology for determining Impact residual strength in impact-damaged Damaged composite laminates has been Composite developed and incorporated into a Laminates)
From page 62...
... Structural failure as a result of sequential sublaminate buckling of delaminated layers is also accounted for. A progressive failure analysis is performed until ultimate structural failure is predicted, thereby yielding an estimate of the residual strength.
From page 63...
... dependent, nonlinear deformation and failure responses of composite materials in which the matrices are ductile polymers. Modified versions of the Ramaswamy-Stouffer constitutive equations of viscoplasticity, originally developed for metals, are used to represent deformation of a polymeric matrix.


This material may be derived from roughly machine-read images, and so is provided only to facilitate research.
More information on Chapter Skim is available.