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Thermo-mechanical design aspects for primary composite structures of large transport aircraft

Petersen, D. and Rolfes, R. and Zimmermann, R. (2001) Thermo-mechanical design aspects for primary composite structures of large transport aircraft. Aerospace Science and Technology, 5 (2), pp. 135-146.

Full text not available from this repository.

Abstract

Thermo-mechanical design aspects for primary carbon fibre reinforced plastics (CFRP) components, especially wings, of future large transport aircraft are discussed. Numerical simulations of the heating of a wing under intensive sun irradiation and of cooling during taxiing and take-off result in the recommendation of an appropriate design temperature. The study of flat stringer-stiffened panels reveals the influence of imperfections and boundary conditions on the buckling load under simultaneous thermal and mechanical loading.

Item URL in elib:https://elib.dlr.de/16575/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2001,
Title:Thermo-mechanical design aspects for primary composite structures of large transport aircraft
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Petersen, D.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Rolfes, R.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Zimmermann, R.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2001
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:5
Page Range:pp. 135-146
Status:Published
Keywords:thermo-mechanics, heat transfer, thermal analysis, thermally induced buckling, structural stability, composites, transport aircraft, wing, fuselage
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: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 16:09

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