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Damage tolerance of composite structures for large transport aircraft

Gädke, M. and Roudolff, F. (2000) Damage tolerance of composite structures for large transport aircraft. Aerospace Science and Technology, 4 (1), pp. 23-32.

Full text not available from this repository.

Abstract

Damage of composite materials is studied at a coupon level from both a fracture mechanics and a damage mechanics point of view. Methods developed are applied to sub-elements and sub-structures with the objective of decreasing the amount of testing needed in certification procedures of composite structures.

Item URL in elib:https://elib.dlr.de/16473/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2000,
Title:Damage tolerance of composite structures for large transport aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gädke, M.UNSPECIFIEDUNSPECIFIED
Roudolff, F.UNSPECIFIEDUNSPECIFIED
Date:2000
Journal or Publication Title:Aerospace Science and Technology
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:Yes
Volume:4
Page Range:pp. 23-32
Status:Published
Keywords:composite structures, damage tolerance, numerical methods, coupons, sub-elements, sub-structures
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: Wolff, Sibylle
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 15:57

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