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. DLR Institut für Aerodynamik und Strömungstechnik. 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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Keller, Dennis	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Wild, Jochen	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

2014

Refereed publication:

Open Access:

Number of Pages:

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 (old)

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:

20 Jun 2021 15:46

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