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CFRP Fuselage Structures - Postbuckling Permitted
Zimmermann, R. and Rolfes, R. (2001) CFRP Fuselage Structures - Postbuckling Permitted. Air & Space Europe, (2001), 3 (3/4), pp. 129-131.
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Abstract
CFRP (carbon fibre reinforced plastics) fuselage structures are expected to be realized with future generations of aircraft. Going into the postbuckling regime with these structures requires improved, fast and reliable procedures for analysis and design of stiffened fibre composite panels. The EC project POSICOSS, which was started in the year 2000, develops such procedures. This article deals with the main objectives of the project, the theoretical and experimental work to be carried out, and with first results.
| Document Type: | Article | ||||||
|---|---|---|---|---|---|---|---|
| Additional Information: | LIDO-Berichtsjahr=2001, | ||||||
| Title: | CFRP Fuselage Structures - Postbuckling Permitted | ||||||
| Authors: |
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| Date: | 2001 | ||||||
| Journal or Publication Title: | Air & Space Europe, (2001) | ||||||
| Refereed publication: | Yes | ||||||
| In ISI Web of Science: | Yes | ||||||
| Volume: | 3 | ||||||
| Page Range: | pp. 129-131 | ||||||
| Status: | Published | ||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||
| HGF - Program: | Aeronautics | ||||||
| HGF - Program Themes: | L - no assignement | ||||||
| DLR - Research area: | Aeronautics | ||||||
| DLR - Program: | L ST - Starrflüglertechnologien | ||||||
| DLR - Research theme (Project): | UNSPECIFIED | ||||||
| Location: | Braunschweig | ||||||
| Institutes and Institutions: | Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik | ||||||
| Deposited By: | Sibylle Wolff | ||||||
| Deposited On: | 16 Sep 2005 | ||||||
| Last Modified: | 14 Jan 2010 16:17 |
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