Abstract
The development of a virtual testing environment, as a cost-effective industrial design
tool in the design and analysis of composite structures, requires the need to create models
efficiently, as well as accelerate the analysis by reducing the number of degrees of freedom,
while still satisfying the need for accurately tracking the evolution of a debond, delamination
or crack front. The eventual aim is to simulate both damage initiation and propagation
in components with realistic geometrical features, where crack propagation paths are not
trivial.
Meshless approaches, and the Element-Free Galerkin (EFG) method, are particularly
suitable for problems involving changes in topology and have been successfully applied to
simulate damage in homogeneous materials and concrete. In this work, the method is
utilized to model initiation and mixed-mode propagation of cracks in composite laminates,
and to simulate experimentally-observed crack migration which is difficult to model using
standard finite element analysis.
N
| Original language | English |
|---|---|
| Title of host publication | 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2009 |
| Publisher | American Institute of Aeronautics and Astronautics |
| Number of pages | 11 |
| ISBN (Electronic) | 9781600869754 |
| ISBN (Print) | 9781615671380 |
| DOIs | |
| Publication status | Published - 07 May 2009 |
| Event | 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference - Palm Springs, United States Duration: 04 May 2009 → 07 May 2009 |
Conference
| Conference | 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference |
|---|---|
| Country/Territory | United States |
| City | Palm Springs |
| Period | 04/05/2009 → 07/05/2009 |
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