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Design and Testing a Full Scale Laminar Wing Leading Edge High-Lift System

Wild, Jochen and Palazzo, Salvatore and Brinza, Ionuts and van der Biest, Koen and Vervliet, Antoon and Schmitz, Holger (2021) Design and Testing a Full Scale Laminar Wing Leading Edge High-Lift System. 8th European Congress on Computational Methods in Applied Science and Engineering, 11.-15.Jan 2021, VIRTUAL EVENT.

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Official URL: https://www.wccm-eccomas2020.org/

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. Classical leading edge high-lift devices like slats are not suitable as they introduce disturbances in the very sensitive upper surface leading edge area. Krueger flaps, which are deflected from the lower side of the wing, are a good alternative as they additionally offer the capability to shield the wing against contamination by insects, water or dirt. Already in 1985, Boeing proposed a concept of a vented Krueger forming a gap flow between main wing and Krueger flap together with a folding bull nose. Although in principle the aerodynamic performance of a Krueger flap is less than for a slat, Rudolph proposed to further develop this kind of Krueger device to provide aerodynamic characteristics comparable to a slat device. Within the EC project DeSiReH a vented foldable bull nose Krueger was designed that showed comparable high-lift aerodynamics. Within the European AFLoNext project, a full scale HLFC leading edge demonstrator was designed and built that incorporated the vented foldable bull nose Krueger. In summer 2018 this demonstrator was wind tunnel tested in the CIRA Icing Wind Tunnel facility. Within this test the aerodynamic design was verified. Additionally, it was tested whether the Krueger device would need a distinct de-icing system. The contribution summarizes the design of the Kruger device together with the findings from the full scale wind tunnel test of the Krueger flap configuration.

Item URL in elib:https://elib.dlr.de/140191/
Document Type:Conference or Workshop Item (Speech)
Title:Design and Testing a Full Scale Laminar Wing Leading Edge High-Lift System
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Wild, JochenJochen.Wild (at) dlr.dehttps://orcid.org/0000-0002-2303-3214
Palazzo, SalvatoreCIRA, s.palazzo (at) cira.itUNSPECIFIED
Brinza, IonutsINCAS, ibrinza (at) incas.roUNSPECIFIED
van der Biest, KoenASCO Industries N.V.UNSPECIFIED
Vervliet, AntoonASCO Industries N.V.UNSPECIFIED
Schmitz, HolgerINVENT GmbHUNSPECIFIED
Date:January 2021
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hybrid Laminar Flow Control, High-Lift System, Krueger Flap, Wind Tunnel Test, Icing Test
Event Title:8th European Congress on Computational Methods in Applied Science and Engineering
Event Location:VIRTUAL EVENT
Event Type:international Conference
Event Dates:11.-15.Jan 2021
Organizer:ECCOMAS
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Wild, Dr.-Ing. Jochen
Deposited On:11 Jan 2021 07:28
Last Modified:11 Jan 2021 07:28

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