| タイトル | Convergence of strain energy release rate components for edge-delaminated composite laminates |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870011944 |
| 著者（英） | Raju, I. S.; Aminpour, M. A.; Crews, J. H., Jr. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1987-04-01 |
| 言語 | eng |
| 内容記述 | Strain energy release rates for edge delaminated composite laminates were obtained using quasi 3 dimensional finite element analysis. The problem of edge delamination at the -35/90 interfaces of an 8-ply composite laminate subjected to uniform axial strain was studied. The individual components of the strain energy release rates did not show convergence as the delamination tip elements were made smaller. In contrast, the total strain energy release rate converged and remained unchanged as the delamination tip elements were made smaller and agreed with that calculated using a classical laminated plate theory. The studies of the near field solutions for a delamination at an interface between two dissimilar isotropic or orthotropic plates showed that the imaginary part of the singularity is the cause of the nonconvergent behavior of the individual components. To evaluate the accuracy of the results, an 8-ply laminate with the delamination modeled in a thin resin layer, that exists between the -35 and 90 plies, was analyzed. Because the delamination exists in a homogeneous isotropic material, the oscillatory component of the singularity vanishes. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 87N21377
NAS 1.15:89135
NASA-TM-89135 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/151028 |
