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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:
AuthorsInstitution or Email of Authors
Zimmermann, R.UNSPECIFIED
Rolfes, R.UNSPECIFIED
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 (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
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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