Fatigue damage mechanics of composite materials II: a damage growth model
Spearing, S.M., Beaumont, P.W.R. and Ashby, M.F. (1992) Fatigue damage mechanics of composite materials II: a damage growth model. Composites Science and Technology, 44, (2), 169-177. (doi:10.1016/0266-3538(92)90110-O).
Full text not available from this repository.
A fatigue model has been developed for damage growth at a notch tip in carbon fibre/epoxy laminates. The damage is modelled as a series of interacting matrix cracks in various forms: splitting, delamination and transverse ply cracking. The extent of fatigue damage can be successfully predicted for a family of (90i/0j)ns and (90/±45/0)s laminates. In this second paper of four, a damage-based model is proposed which can explain the effect of cyclic tensile loading on the post-fatigue strength and stiffness of a notched laminate.
|Keywords:||damage prediction, fatigue damage model, notches|
|Subjects:||T Technology > T Technology (General)
Q Science > Q Science (General)
|Divisions:||University Structure - Pre August 2011 > School of Engineering Sciences
|Date Deposited:||30 Jan 2007|
|Last Modified:||02 Mar 2012 12:46|
|Contributors:||Spearing, S.M. (Author)
Beaumont, P.W.R. (Author)
Ashby, M.F. (Author)
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
Actions (login required)