elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Design of a smart leading edge device for low speed wind tunnel tests in the European project SA-DE

Kintscher, Markus and Wiedemann, Martin and Monner, Hans Peter and Heintze, Olaf and Kühn, Timo (2011) Design of a smart leading edge device for low speed wind tunnel tests in the European project SA-DE. International Journal of Structural Integrity, Vol. 2 (Iss: 4), pp. 383-405. Emerald Group Publishing Ltd.. DOI: 10.1108/17579861111183911 ISSN 1757-9864

Full text not available from this repository.

Abstract

The presented paper describes the pre-design and sizing of a smart leading edge section which is developed in the project SADE (Smart High Lift Devices for Next Generation Wings) which is part of the seventh framework program of the EU. SADE aims at a major step forward in the development and evaluation of the potential of morphing airframe technologies. The development of morphing technologies in SADE concentrates on the leading and trailing edge high-lift devices. At the leading edge a smart gap and step-less droop nose device is developed. For the landing flap a smart trailing edge of the flap is in the focus of the research activities. The main path in SADE follows the development of the leading edge section and the subsequent wind tunnel testing of a five meter span full-scale section with a chord length of three meters in the wind tunnel T-101 at the Russian central aero-hydrodynamic institute (TsAGI) in Moscow. The presented paper gives an overview over the desired performance and requirements of a smart leading edge device, its aerodynamic design for the wind tunnel tests and the structural pre-design and sizing of the full-scale leading edge section which will be tested in the wind tunnel.

Item URL in elib:https://elib.dlr.de/74559/
Document Type:Article
Title:Design of a smart leading edge device for low speed wind tunnel tests in the European project SA-DE
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kintscher, MarkusUNSPECIFIEDUNSPECIFIED
Wiedemann, MartinUNSPECIFIEDUNSPECIFIED
Monner, Hans PeterUNSPECIFIEDUNSPECIFIED
Heintze, OlafUNSPECIFIEDUNSPECIFIED
Kühn, TimoUNSPECIFIEDUNSPECIFIED
Date:2011
Journal or Publication Title:International Journal of Structural Integrity
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:Vol. 2
DOI :10.1108/17579861111183911
Page Range:pp. 383-405
Publisher:Emerald Group Publishing Ltd.
ISSN:1757-9864
Keywords:Morphing, Smart Droop Nose, High-Lift, Smart Leading Edge.
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Structures & Materials (old)
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Adaptronics
Deposited By: Böhringer-Thelen, Isolde
Deposited On:25 Jan 2012 09:07
Last Modified:06 Sep 2019 15:26

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.