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High-Lift Concepts Compatible with Laminar Flow Wings

Keller, Dennis and Wild, Jochen (2014) High-Lift Concepts Compatible with Laminar Flow Wings. DLR-Interner Bericht. DLR-IB 124-2014/915, 17 S.

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Abstract

This report summarizes the design optimizations of several concepts of high-lift systems for laminar wing airfoils. The airfoil wing section used is the airfoil shape denoted LV1 taken form the laminar airfoil catalogue. The design was performed in a 2D normalized manner. Three concepts were investigated, one at the leading edge and two at the trailing edge. The designed high-lift concepts show suitable aerodynamic performance for the realisation of laminar wing technology at high-lift conditions.

Item URL in elib:https://elib.dlr.de/94069/
Document Type:Monograph (DLR-Interner Bericht)
Title:High-Lift Concepts Compatible with Laminar Flow Wings
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Keller, Dennisdennis.keller (at) dlr.deUNSPECIFIED
Wild, Jochenjochen.wild (at) dlr.deUNSPECIFIED
Date:2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:17
Status:Published
Keywords:Aerodynamik, Hochauftrieb, Optimierung, Entwurf
Institution:DLR Institut für Aerodynamik und Strömungstechnik
Department:Transportflugzeuge
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 14:13
Last Modified:06 Jan 2015 14:13

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