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Numerical Aerodynamic Optimisation of 3D High-Lift Configurations

Brezillon, Joel and Dwight, Richard and Wild, Jochen (2008) Numerical Aerodynamic Optimisation of 3D High-Lift Configurations. 26th Congress Of The International Council Of The Aeronautical Sciences, 2008-09-14 - 2008-09-19, Anchorage, AK (USA). ISBN 0-9533991-9-2

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Abstract

The paper presents the numerical optimisation activity carried out at DLR-IAS for the design of wing-body aircrafts in high-lift configuration. The purpose of the study is to assess the high-fidelity methods and tools needed to optimise the flap and slat settings of 3D configurations in a limited turn-around time. The selected key technologies are successfully applied for the optimisations of 2 different high-lift configurations.

Item URL in elib:https://elib.dlr.de/55295/
Document Type:Conference or Workshop Item (Paper)
Title:Numerical Aerodynamic Optimisation of 3D High-Lift Configurations
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Brezillon, JoelUNSPECIFIEDUNSPECIFIED
Dwight, RichardUNSPECIFIEDUNSPECIFIED
Wild, JochenUNSPECIFIEDUNSPECIFIED
Date:14 September 2008
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
ISBN:0-9533991-9-2
Status:Accepted
Keywords:high-lift, optimisation, evolutionary strategy, adjoint approach, mesh strategy
Event Title:26th Congress Of The International Council Of The Aeronautical Sciences
Event Location:Anchorage, AK (USA)
Event Type:international Conference
Event Dates:2008-09-14 - 2008-09-19
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts & Integration (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Brezillon, Joel
Deposited On:25 Sep 2008
Last Modified:31 Jul 2019 19:22

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