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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Gädke, M.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Roudolff, F.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2000

Journal or Publication Title:

Aerospace Science and Technology

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Yes

Volume:

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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