Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
7212303 | Composites Part B: Engineering | 2018 | 30 Pages |
Abstract
The paper deals with experimental and numerical investigations of the composite plate subjected to low velocity impact (LVI). The discussed plates were made of eight-layer Glass Fiber Reinforced Polymer (GFRP) laminate with quasi-isotropic ply system and are predefined to conduct the impact and the Compression After Impact (CAI) tests. The numerical analyses were performed in Ansys® environment. Three numerical models were prepared. The implicit analyses were conducted with and without the implementation of the progressive failure algorithm and the application of the bilinear traction-separation law. The analyzed problem demonstrated the influence of the element-level time-incrementation, damping and time integration method (Newmark and Hilber-Hughes-Taylor) on agreement with the experimental results. The advantages of using impact constraints for modeling contact in a nonlinear transient dynamic analysis were shown. High consistency of numerical and experimental results was achieved. Application of the Hashin's criterion lead to a valid prediction of the fiber failure areas and to overestimation of the matrix failure areas.
Related Topics
Physical Sciences and Engineering
Engineering
Engineering (General)
Authors
Adrian Gliszczynski,