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A Validation Program for Dynamic High-Lift System Aerodynamics

Wild, Jochen und Strüber, Henning und Moens, Frédéric und van Rooijen, Bart und Maseland, Hans (2022) A Validation Program for Dynamic High-Lift System Aerodynamics. In: 8th European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS Congress 2022, Seiten 1-15. SciPedia. ECCOMAS Congress 2022, 2022-06-05 - 2022-06-09, Oslo, Norwegen. doi: 10.23967/eccomas.2022.033. ISSN 2696-6999.

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Offizielle URL: https://www.scipedia.com/public/Wild_et_al_2022a

Kurzfassung

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.

elib-URL des Eintrags:https://elib.dlr.de/187410/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:A Validation Program for Dynamic High-Lift System Aerodynamics
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Wild, JochenJochen.Wild (at) dlr.dehttps://orcid.org/0000-0002-2303-3214NICHT SPEZIFIZIERT
Strüber, HenningAirbus Operations GmbH, Bremen, GermanyNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Moens, FrédéricONERA, Meudon, FranceNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
van Rooijen, BartDNW, Marknese, The NetherlandsNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Maseland, HansRoyal NLR, Amsterdam, The NetherlandsNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:7 Juni 2022
Erschienen in:8th European Congress on Computational Methods in Applied Sciences and Engineering, ECCOMAS Congress 2022
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Nein
DOI:10.23967/eccomas.2022.033
Seitenbereich:Seiten 1-15
Verlag:SciPedia
ISSN:2696-6999
Status:veröffentlicht
Stichwörter:Aerodynamics, Unsteady, High-Lift Systems, CFD, Wind Tunnel, Validation
Veranstaltungstitel:ECCOMAS Congress 2022
Veranstaltungsort:Oslo, Norwegen
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:5 Juni 2022
Veranstaltungsende:9 Juni 2022
Veranstalter :ECCOMAS
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Effizientes Luftfahrzeug
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L EV - Effizientes Luftfahrzeug
DLR - Teilgebiet (Projekt, Vorhaben):L - Virtuelles Flugzeug und Validierung
Standort: Braunschweig , Göttingen
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Transportflugzeuge
Institut für Aerodynamik und Strömungstechnik > Experimentelle Verfahren, GO
Institut für Aerodynamik und Strömungstechnik > CASE, BS
Hinterlegt von: Wild, Dr.-Ing. Jochen
Hinterlegt am:07 Dez 2022 11:04
Letzte Änderung:24 Apr 2024 20:48

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