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The Benefits of the Passive and Active Design of Aircraft Structures

Hönlinger, H.G. and Hutin, P.M. and Pendleton, E.W. (1997) The Benefits of the Passive and Active Design of Aircraft Structures. In: Optimization in Industry, Vol. 1, pp. 259-281. Optimization in Industry, Palm Coast, Florida, 23.-27.03.97.

Full text not available from this repository.

Abstract

Increasing performance requirements and the economical pressure to reduce the Direct Operational Costs of new aircraft designs can no longer be met by traditional and sequential design strategies. Especially in the field of aeroelasticity, multidisciplinary design concepts must be applied during the early design stage to develop flutter-free structures and to guarantee excellent multi-point design characteristics, e.g. for wing flight shape, control efficiencies, etc. This paper describes aeroelastic design methods like stiffness optimization, mass balance, and the aeroelastic tailoring of the composite structures of primary structures in order to maximize aeroelastic performance and to minimize weight penalties.

Item URL in elib:https://elib.dlr.de/14133/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999,
Title:The Benefits of the Passive and Active Design of Aircraft Structures
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hönlinger, H.G.UNSPECIFIEDUNSPECIFIED
Hutin, P.M.ONERAUNSPECIFIED
Pendleton, E.W.WLUNSPECIFIED
Date:1997
Journal or Publication Title:Optimization in Industry
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 1
Page Range:pp. 259-281
Editors:
EditorsEmail
The American Society of Mechanical Engineers, UNSPECIFIED
Status:Published
Keywords:aeroelasticity, multidisciplinary design and optimization, aeroelastic tailoring, concurrent engineering
Event Title:Optimization in Industry, Palm Coast, Florida, 23.-27.03.97
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: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 21:27

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