Failure Analysis of Composite Laminates with Free Edge
Journal of Composites Technology and Research1990Vol. 12(2), pp. 91–91
Citations Over TimeTop 15% of 1990 papers
Abstract
A failure theory which combines classical lamination theory with free-edge interlaminar stress was employed to predict the strength of laminates with free edges. Laminates studied were [±θ]2s angle-ply laminates, [±θ/90]s laminates, and fiber-dominated π/4 laminates. The present theory was capable of predicting failure loads for [±θ]2s and [±θ/90]s laminates as well as delamination on-set loads for π/4 laminates.
Related Papers
- → Delamination formation, evaluation and suppression during drilling of composite laminates: A review(2019)450 cited
- → XFEM simulation of delamination in composite laminates(2015)96 cited
- → Application of Scanning Acoustic Microscopy for Micro Delamination Detection(2015)1 cited
- XFEM simulation of delamination in composite laminates Part A Applied science and manufacturing(2016)
- → Effects of planimetric position of delamination on compressive failure of composite laminates(2022)