| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 7225782 | Procedia Engineering | 2018 | 7 Pages |
Abstract
The assessment of service life of composite thermo-structural parts is a primary issue for the aeronautic industry. To this end, a unified damage model for woven composites undergoing both static and fatigue loadings is presented here. Its specificity resides in its rate damage evolution law, which enables to predict the behaviour of the material under cyclic or random fatigue loadings.
Related Topics
Physical Sciences and Engineering
Engineering
Engineering (General)
Authors
Orianne Sally, Cédric Julien, Frédéric Laurin, Rodrigue Desmorat, Florent Bouillon,