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High-Performance High-Lift Design for Laminar Wings

Wild, Jochen (2015) High-Performance High-Lift Design for Laminar Wings. AeroDays 2015, 20.-23. Okt. 2015, London, United Kingdom.

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Official URL: http://www.aerodays2015.com/

Abstract

The presenatation summarizes teh 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 an hybrid laminar flow control (HLFC) wing.

Item URL in elib:https://elib.dlr.de/100802/
Document Type:Conference or Workshop Item (Speech)
Title:High-Performance High-Lift Design for Laminar Wings
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wild, Jochenjochen.wild (at) dlr.deUNSPECIFIED
Date:2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:high-lift, aerodynamics, laminar wing
Event Title:AeroDays 2015
Event Location:London, United Kingdom
Event Type:international Conference
Event Dates:20.-23. Okt. 2015
Organizer:European Commission
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 of Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Wild, Dr.-Ing. Jochen
Deposited On:14 Dec 2015 16:14
Last Modified:10 May 2016 23:38

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