Abstract
The effects of low velocity impact on laminated composite panels are presented in this paper. In the experimental program, 16 ply, 32 ply and 48 ply quasi-isotropic laminated composite panels were subjected to low velocity impact loads. The laminates were held in a special fixture, which was designed to simulate simply supported boundaries. Impact experiments were conducted in a Dynatup low velocity testing machine where a drop-weight system was used to strike each panel at 90 degrees incidence under controlled conditions of impact velocity. The impactor used was of a constant weight and tip diameter, the impact height and hence the velocity and energy were used as variables in the study.
| Original language | English |
|---|---|
| Pages (from-to) | 67-73 |
| Number of pages | 7 |
| Journal | American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP |
| Volume | 269 |
| State | Published - Dec 1 1993 |
| Event | Proceedings of the 1993 ASME Winter Annual Meeting - New Orleans, LA, USA Duration: Nov 28 1993 → Dec 3 1993 |
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