| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 1719092 | Aerospace Science and Technology | 2006 | 9 Pages |
Abstract
A numerical and experimental analysis comparing the influence of specimen geometry, material composition and loading conditions on the crushing response of truncated conical shells is presented. The analysis is based on a new multi-layered numerical modelling composed of shell and solid elements. A material model appropriate for balanced fabrics has been developed including in-plane failure, delamination failure and resulting degradation models.
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