Special finite elements for the analysis of flaw growth and fracture in fiber composites
β Scribed by S.S Wang; J.F Mandell; F.J McGarry
- Publisher
- Elsevier Science
- Year
- 1976
- Tongue
- English
- Weight
- 59 KB
- Volume
- 8
- Category
- Article
- ISSN
- 0013-7944
No coin nor oath required. For personal study only.
β¦ Synopsis
In this paper, comparisons of fracture stress values obtained in graphite/epoxy composites with the predictions of the model are made. The experimental results of Brinson and Yeow[l] on unidirectionsl composites using double edge notch tensile coupons were used. The calculations are performed usinp the results of finite-ekment calculations on double edge notch specimens with various crack length to specimen width ratios and crack angles. From these results, the displacement held to be imposed at the outer bouodaries of the LHR is determined. Then, separate LHR calculations are performed for each experiment of interest. By forcing the computational result to match one experiment, the critical energy icvel for crack growth can be established. This value is then used to predict the failure loads in other cases. REFERENCE [I] H. F. Brinson and Y. T. Ycow, An investigation of the failure and fracture behavior of graphite/epoxy laminates. VPEE-75-23, Sept. 1975.
π SIMILAR VOLUMES
## Abstract The finite element analysis of delamination in laminated composites is addressed using interface elements and an interface damage law. The principles of linear elastic fracture mechanics are indirectly used by equating, in the case of singleβmode delamination, the area underneath the tr
The analysis of the free-edge stress distributions in composite laminates under uniaxial tension is approached by a finite element technique based on a multi-layer higher-order laminate theory. Several finite elements corresponding to different through-thickness assumed distributions of the displac
## Us&act-It is shown that the singularity of stresses near the tip of crack in an elastii: bi-material can be obtained by using degenerate triangular elements, the shape functions of which are derived from those classical isoparametric elements. A four node triangular element is tested on two dif