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Investigations of passive wing technologies for load reduction

Krüger, Wolf R. and Dillinger, Johannes and De Breuker, Roeland and Haydn, Katharina (2019) Investigations of passive wing technologies for load reduction. CEAS Aeronautical Journal, 10 (4), pp. 977-993. Springer. DOI: 10.1007/s13272-019-00393-2 ISSN 1869-5590

Full text not available from this repository.

Official URL: https://link.springer.com/article/10.1007/s13272-019-00393-2

Abstract

Wings of modern aircraft have to be designed to give optimal response with respect to loads, comfort and performance. An essential part of the wing development is thus a design process which can take all these aspects into consideration. In the 'Adaptive Wing' work package of the CleanSky 'Smart Fixed Wing Aircraft' project, a multi-fidelity wing design method using aeroelastic tailoring has been developed. In the article, the process is presented in detail. The approach is based on a parametric wing design approach. Both beam models and shell models are derived and optimized in separate optimization environments. Investigations of the use of unbalanced laminates in aeroelastic tailoring are presented, employing the optimization of lamination parameters. The applications are demonstrated on two aircraft configurations, a long range and a short range transport aircraft. Further developments presented in the article include the introduction of CFD-based aerodynamics in the tailoring process, and a process extension to assess the influence of aeroelastic tailoring on fatigue.

Item URL in elib:https://elib.dlr.de/127471/
Document Type:Article
Title:Investigations of passive wing technologies for load reduction
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Krüger, Wolf R.Wolf.Krueger (at) dlr.dehttps://orcid.org/0000-0002-7949-1169
Dillinger, JohannesJohannes.Dillinger (at) dlr.dehttps://orcid.org/0000-0002-7522-7555
De Breuker, RoelandAerospace Structures, Delft University of Technologyhttps://orcid.org/0000-0002-7882-2173
Haydn, KatharinaFraunhofer-Institut für Betriebsfestigkeit und Systemzuverlässigkeit, DarmstadtUNSPECIFIED
Date:May 2019
Journal or Publication Title:CEAS Aeronautical Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:10
DOI :10.1007/s13272-019-00393-2
Page Range:pp. 977-993
Publisher:Springer
ISSN:1869-5590
Status:Published
Keywords:load analysis, load reduction, parametric model design, aeroelastic tailoring
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Institute of Aeroelasticity
Deposited By: Krüger, Prof. Dr.-Ing. Wolf R.
Deposited On:29 May 2019 16:01
Last Modified:14 Feb 2020 12:04

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