Fatigue damage mechanics of composite materials part IV: prediction of post-fatigue stiffness
Spearing, S.M., Beaumont, P.W.R. and Smith, P.A. (1992) Fatigue damage mechanics of composite materials part IV: prediction of post-fatigue stiffness. Composites Science and Technology, 44, (4), 309-317. ( doi:10.1016/0266-3538(92)90068-E).
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A model has been developed for predicting the stiffness of cross-ply carbon fibre composite laminates containing a notch from which damage, in the form of matrix cracks, splits and delaminations, has grown. A combination of experimental and theoretical results have been used to deduce appropriate degraded stiffness properties for the damaged regions of the laminate. These degraded stiffnesses have then been incorporated into a finite element representation of the notched laminate to predict the overall stiffness. Agreement with experimental data is satisfactory.
|Keywords:||predicting post-fatigue stiffness, finite element analysis|
|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 12:26|
|Contributors:||Spearing, S.M. (Author)
Beaumont, P.W.R. (Author)
Smith, P.A. (Author)
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
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