Loading...
Please wait, while we are loading the content...
Similar Documents
Comparison of Damage Path Predictions for Composite Laminates by Explicit and Standard Finite Element Analysis Tools
| Content Provider | Semantic Scholar |
|---|---|
| Author | Bogert, Philip B. Satyanarayana, A. Chunchu, Prasad B. |
| Copyright Year | 2006 |
| Abstract | Splitting, ultimate failure load and the damage path in center notched composite specimens subjected to in-plane tension loading are predicted using progressive failure analysis methodology. A 2-D Hashin-Rotem failure criterion is used in determining intra-laminar fiber and matrix failures. This progressive failure methodology has been implemented in the Abaqus/Explicit and Abaqus/Standard finite element codes through user written subroutines “VUMAT” and “USDFLD” respectively. A 2-D finite element model is used for predicting the intra-laminar damages. Analysis results obtained from the Abaqus/Explicit and Abaqus/Standard code show good agreement with experimental results. The importance of modeling delamination in progressive failure analysis methodology is recognized for future studies. The use of an explicit integration dynamics code for simple specimen geometry and static loading establishes a foundation for future analyses where complex loading and nonlinear dynamic interactions of damage and structure will necessitate it. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20060017017.pdf |
| Alternate Webpage(s) | https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20060017017.pdf |
| Language | English |
| Access Restriction | Open |
| Subject Keyword | Biological specimen CDISC SEND Biospecimens Terminology Code Delamination - medical device material degradation Failure analysis Finite element method Futures studies Interaction Nonlinear Dynamics Nonlinear system Subroutine Tension Tissue fiber Ultimate failure |
| Content Type | Text |
| Resource Type | Article |
