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High-Performance High-Lift Design for Laminar Wings

Wild, Jochen (2017) High-Performance High-Lift Design for Laminar Wings. In: Aviation in Europe Innovating for Growth European Union. pp. 305-310. ISBN 978-92-79-59141-9.

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Abstract

The presentation summarizes the design of high-lift devices for laminar wings. Within the EC-project DeSIReH a natural laminar flow (NLF) wing was equipped with a high-performing high-lift system leading to a benefit of about 5% in fuel reduction on aircraft level. Within the EC-project AFLoNext this design has been adapted for the additional restrictions for use on a hybrid laminar flow control (HLFC) wing.

Item URL in elib:https://elib.dlr.de/113764/
Document Type:Book Section
Title:High-Performance High-Lift Design for Laminar Wings
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wild, Jochenjochen.wild (at) dlr.deUNSPECIFIED
Date:2017
Journal or Publication Title:Aviation in Europe Innovating for Growth
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2777/62810
Page Range:pp. 305-310
Editors:
EditorsEmail
Knörzer, DietrichUNSPECIFIED
Warsop, ClydeUNSPECIFIED
Diaconescu, CiprianUNSPECIFIED
Sanfourche, Jean-PierreUNSPECIFIED
Publisher:European Union
ISBN:978-92-79-59141-9
Status:Published
Keywords:High-lift, aerodynamics, laminar wing
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
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Seyfried, Beate
Deposited On:27 Sep 2017 08:40
Last Modified:31 Jul 2019 20:11

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