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Aerodynamic Design of a High-Lift System Compatible with a Natural Laminar Flow Wing within the DeSiReH Project

Strüber, Henning and Wild, Jochen (2014) Aerodynamic Design of a High-Lift System Compatible with a Natural Laminar Flow Wing within the DeSiReH Project. In: ICAS 2014 CD-Rom Proceedings, e300. 29th Congress of the International Council of the Aeronautical Sciences, 7.-12. Sep. 2014, St. Petersburg, Russia. ISBN 3-932182-80-4

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Official URL: http://www.icas.org/ICAS_ARCHIVE/ICAS2014/data/papers/2014_0300_paper.pdf

Abstract

The paper describes the aerodynamic design of a high lift system suitable for a Natural Laminar Flow wing. 2D & 3D numerical optimization has been used in the design process and the outcome has been tested at flight Reynolds Number in the European Transonic Windtunnel (ETW), where various measurement techniques have been applied. An analysis on aircraft level has been performed to assess Natural Laminar Flow (NLF) wing’s drag benefits.

Item URL in elib:https://elib.dlr.de/90822/
Document Type:Conference or Workshop Item (Speech)
Title:Aerodynamic Design of a High-Lift System Compatible with a Natural Laminar Flow Wing within the DeSiReH Project
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Strüber, HenningAirbus Operations GmbHUNSPECIFIED
Wild, Jochenjochen.wild (at) dlr.deUNSPECIFIED
Date:2014
Journal or Publication Title:ICAS 2014 CD-Rom Proceedings
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:e300
Editors:
EditorsEmail
UNSPECIFIEDThe International Council of the Aeronautical Sciences
ISBN:3-932182-80-4
Status:Published
Keywords:high-lift, aerodynamics, design, laminar wing, wind tunnel testing
Event Title:29th Congress of the International Council of the Aeronautical Sciences
Event Location:St. Petersburg, Russia
Event Type:international Conference
Event Dates:7.-12. Sep. 2014
Organizer:ICAS
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:06 Jan 2015 14:11
Last Modified:06 Jan 2015 14:11

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