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MAAXIMUS D3.5.3 – Task 3.5.3 Numerical Methodology to Model High Velocity Impact on Preloaded Composite Panels
Schueler, Dominik and Toso, Nathalie (2012) MAAXIMUS D3.5.3 – Task 3.5.3 Numerical Methodology to Model High Velocity Impact on Preloaded Composite Panels. Project Report. DLR-IB 435-2012/22, 46 S.
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Abstract
This part of deliverable D3.5.3 presents a FE methodology to predict impact damage in composite panels using the detailed Ladevèze damage models implemented by DLR. Coupled implicit-explicit techniques are utilized to incorporate static preloads acting in panels subjected to HVI. A discretization method and a material model for ice projectiles are presented for further simulations involving hail impact in Abaqus/Explicit.
| Document Type: | Monograph (Project Report) | ||||||
|---|---|---|---|---|---|---|---|
| Title: | MAAXIMUS D3.5.3 – Task 3.5.3 Numerical Methodology to Model High Velocity Impact on Preloaded Composite Panels | ||||||
| Authors: |
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| Date: | January 2012 | ||||||
| Number of Pages: | 46 | ||||||
| Keywords: | Composites, High Velocity Impact, Preload, Damage, Delamination, Ice Model | ||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||
| HGF - Program: | Aeronautics | ||||||
| HGF - Program Themes: | L AR - Aircraft Research | ||||||
| DLR - Research area: | Aeronautics | ||||||
| DLR - Program: | L AR - Aircraft Research | ||||||
| DLR - Research theme (Project): | L - Structures & Materials | ||||||
| Location: | Stuttgart | ||||||
| Institutes and Institutions: | Institute of Structures and Design > Structural Integrity | ||||||
| Deposited By: | Dominik Schüler | ||||||
| Deposited On: | 23 Jul 2012 12:41 | ||||||
| Last Modified: | 23 Jul 2012 12:41 |
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