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Aircraft rudder optimization - A multi-level and knowledge-enabled approach

de Wit, A.J. and Lammen, W.F. and Vankan, W.J. and Timmermans, H. and van der Laan, T. and Ciampa, Pier Davide (2020) Aircraft rudder optimization - A multi-level and knowledge-enabled approach. Progress in Aerospace Sciences, 119, p. 100650. Elsevier. doi: 10.1016/j.paerosci.2020.100650. ISSN 0376-0421.

Full text not available from this repository.

Official URL: http://www.sciencedirect.com/science/article/pii/S0376042120300622

Abstract

In the AGILE project, advanced technologies for optimization, multi-disciplinary collaboration and knowledge-enabled engineering are developed and applied to conceptual and preliminary aircraft design in various representative use cases of some conventional and unconventional configurations (like strut-braced wing, box-wing and blended-wing). This paper describes the application of a multi-level optimization (MLO) strategy based on analytical target cascading (ATC) to aircraft rudder design. As a reference a traditional nested optimization method is applied as well. Both methods arrive at the same design optima. In the case of ATC the amount of interaction between the global and the local level is reduced. The MLO is illustrated by applying surrogate models that were derived from aircraft and rudder design analysis competences available from AGILE. The surrogate models are deployed through a specific repository that facilitates a knowledge-enabled approach. The rudder design case illustrates that applying MLO provides insight into the coupled design problem both for the OEM and for the supplier. Development time is reduced by minimizing the number of interaction events, providing a common understanding of the design problem, establishing interfaces in the design process and therefore reducing the risk of late changes.

Item URL in elib:https://elib.dlr.de/137463/
Document Type:Article
Title:Aircraft rudder optimization - A multi-level and knowledge-enabled approach
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
de Wit, A.J.NLR - Royal Netherlands Aerospace CentreUNSPECIFIED
Lammen, W.F.NLR - Royal Netherlands Aerospace CentreUNSPECIFIED
Vankan, W.J.NLR - Royal Netherlands Aerospace CentreUNSPECIFIED
Timmermans, H.NLR - Royal Netherlands Aerospace CentreUNSPECIFIED
van der Laan, T.GKN Fokker AerostructuresUNSPECIFIED
Ciampa, Pier DavidePier.Ciampa (at) dlr.dehttps://orcid.org/0000-0003-1652-4899
Date:November 2020
Journal or Publication Title:Progress in Aerospace Sciences
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:119
DOI :10.1016/j.paerosci.2020.100650
Page Range:p. 100650
Publisher:Elsevier
ISSN:0376-0421
Status:Published
Keywords:multi-level optimization (MLO), multi-disciplinary design optimization (MDO), analytical target cascading (ATC), global-local design
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L - no assignment
DLR - Research theme (Project):L - no assignment
Location: Hamburg
Institutes and Institutions:Institute of System Architectures in Aeronautics > Aircraft Design and System Integration
Deposited By: Ciampa, Pier Davide
Deposited On:07 Dec 2020 09:23
Last Modified:07 Dec 2020 09:23

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