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Numerical Aerodynamic Optimisation of 3D High-Lift Configurations

Brezillon, Joël and Dwight, Richard P. and Wild, Jochen (2009) Numerical Aerodynamic Optimisation of 3D High-Lift Configurations. CEAS 2009 European Air and Space Conference, 26-29 October 2009, Manchester, UK.

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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.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Numerical Aerodynamic Optimisation of 3D High-Lift Configurations
Authors:
AuthorsInstitution or Email of Authors
Brezillon, JoëlJoel.Brezillon@dlr.de
Dwight, Richard P.r.p.dwight@tudelft.nl
Wild, Jochenjochen.wild@dlr.de
Date:October 2009
Keywords:aerodynamic, high-lift, optimisation, evolutionary strategy, adjoint approach, mesh strategy
Event Title:CEAS 2009 European Air and Space Conference
Event Location:Manchester, UK
Event Type:international Conference
Event Dates:26-29 October 2009
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts & Integration
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Joel Brezillon
Deposited On:15 Dec 2009 13:29
Last Modified:15 Dec 2009 13:29

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