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A Validation Program for Dynamic High-Lift System Aerodynamics

Wild, Jochen and Strüber, Henning and Moens, Frédéric and van Rooijen, Bart and Maseland, Hans (2024) A Validation Program for Dynamic High-Lift System Aerodynamics. In: Advanced Computational Methods and Design for Greener Aviation Computational Methods in Applied Sciences, 59. Springer Cham. pp. 145-157. doi: 10.1007/978-3-031-61109-4_10. ISBN 978-3-031-61109-4.

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Official URL: https://link.springer.com/chapter/10.1007/978-3-031-61109-4_10

Abstract

The feasibility of laminar flow control technology for future wing is bound to the development of a leading edge high-lift system that complies with the requirements on smooth surfaces to enable maintaining the laminar boundary layer flow, such as a Krueger flap. Although in principle the aerodynamic performance of a Krueger flap is known, the unsteady behaviour of the flow during deployment and retraction is completely unknown. This is as even more important as during deployment the Krueger flap is exposed to highly unfavourable positions perpendicular to the flow. To mitigate the risk of unfavourable aircraft behaviour, it is therefore expected that a Krueger flap has to be deflected significantly fast and may trigger unsteady aerodynamic effects. The European H2020 project UHURA, running from September 2018 to August 2022, has been focusing on the unsteady flow behaviour around such high-lift system and will first time deliver a deeper understanding of critical flow features at this type of high-lift device during their deployment and retraction together with a validated numerical procedure for its simulation. UHURA performed detailed experimental measurements in several wind tunnels to obtain a unique data set for validation purposes of Computational Fluid Dynamics (CFD) software, including detailed flow measurements by Particle Image Velocimetry (PIV) and other optical measurement technologies. Advanced CFD methods promising significant improvements in the design lead time have been applied and validated against this database to obtain efficient and reliable prediction methods for design. This first contribution within the Special Technology Session provides an overview on the project. While the simulation activities are detailed in the forthcoming presentations, this presentation focusses on the experiments conducted to obtain a unique database for the validation of simulation methods for this kind of unsteady flows. Finally, an outlook is given on the validation and exploitation methodology applied in the last period of the project.

Item URL in elib:https://elib.dlr.de/205808/
Document Type:Contribution to a Collection
Title:A Validation Program for Dynamic High-Lift System Aerodynamics
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Wild, JochenUNSPECIFIEDhttps://orcid.org/0000-0002-2303-3214UNSPECIFIED
Strüber, HenningAirbus Operations GmbH, Bremen, GermanyUNSPECIFIEDUNSPECIFIED
Moens, FrédéricONERA, Meudon, FranceUNSPECIFIEDUNSPECIFIED
van Rooijen, BartDNW, Marknese, The NetherlandsUNSPECIFIEDUNSPECIFIED
Maseland, HansRoyal NLR, Amsterdam, The NetherlandsUNSPECIFIEDUNSPECIFIED
Date:30 July 2024
Journal or Publication Title:Advanced Computational Methods and Design for Greener Aviation
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:59
DOI:10.1007/978-3-031-61109-4_10
Page Range:pp. 145-157
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Tuovinen, TeroUniversity of Jyväskylä of Applied Sciences, Jyväskylä, FinlandUNSPECIFIEDUNSPECIFIED
Periaux, JacquesInternational Centre for Numerical Methods in Engineering, CIMNE, Barcelona, SpainUNSPECIFIEDUNSPECIFIED
Knörzer, DietrichDK Aeronautics Consultant, Brussels, BelgiumUNSPECIFIEDUNSPECIFIED
Bugeda, GabrielInternational Center for Numerical Methods in Engineering (CIMNE), Barcelona, Spainhttps://orcid.org/0000-0002-9320-8729UNSPECIFIED
Pons-Prats, JordiInternational Center for Numerical Methods in Engineering (CIMNE), Barcelona, SpainUNSPECIFIEDUNSPECIFIED
Publisher:Springer Cham
Series Name:Computational Methods in Applied Sciences
ISBN:978-3-031-61109-4
Status:Published
Keywords:Aerodynamics, Unsteady, High-Lift Systems, CFD, Wind Tunnel, Validation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Aircraft and  Validation
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Transport Aircraft
Institute for Aerodynamics and Flow Technology > Experimental Methods, GO
Institute for Aerodynamics and Flow Technology > CASE, BS
Deposited By: Wild, Dr.-Ing. Jochen
Deposited On:20 Sep 2024 11:55
Last Modified:20 Sep 2024 12:21

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