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Buckling of CFRP plates with partly detached stringers

Rohwer, K. and Albat, A. and Steck, E. (1994) Buckling of CFRP plates with partly detached stringers. Zeitschrift für Flugwissenschaften und Weltraumforschung, 18, pp. 271-277.

Full text not available from this repository.

Abstract

So far, research in the field of stringer detachment has predominantly been focussed on conditions for its initiation and propagation. As an alternative this study assumes a certain detachment size and asks for its effect on the buckling strength. Standard finite elements are applied to determine buckling modes and the corresponding loads for CFRP plates with a single blade stiffener. The influence of the detachment length on the buckling load varies with cross sectional dimensions and plate stacking. Designs are identified which tolerate relatively large detachments without too serious a buckling load reduction. Unfortunately, an improved damage tolerance often has to be payed for by a lower buckling strength. However, considering more +45- layers in the plate stacking has a positive effect on the - damage tolerance as well as on the buckling load.

Document Type:Article
Additional Information: LIDO-Berichtsjahr=1994,
Title:Buckling of CFRP plates with partly detached stringers
Authors:
AuthorsInstitution or Email of Authors
Rohwer, K.UNSPECIFIED
Albat, A.TU Braunschweig
Steck, E.TU Braunschweig
Date:1994
Journal or Publication Title:Zeitschrift für Flugwissenschaften und Weltraumforschung
Refereed publication:Yes
In ISI Web of Science:Yes
Volume:18
Page Range:pp. 271-277
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: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 11:59

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