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

Progress in Efficient Active High-Lift

Kauth, Felix and Narjes, Gerrit and Müller, Jan and Seume, Joerg R. and Vasista, Srinivas and Müller, Thomas and François, Daniela G. and El Sayed, Yosef and Semaan, Richard and Behr, Christian and Schwerter, Martin and Leester-Schädel, Monika and Nolte, Felix and Giesecke, Daniel and Atalayer, Çaǧlar and Radespiel, Rolf (2017) Progress in Efficient Active High-Lift. In: 35th AIAA Applied Aerodynamics Conference. 35th AIAA Applied Aerodynamics Conference, AIAA AVIATION Forum, 5-9 June 2017, Denver, Colorado, United States. doi: 10.2514/6.2017-3559.

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/abs/10.2514/6.2017-3559


This paper presents some of the progress in research on efficient high-lift systems for future civil aircraft achieved by the Coordinated Research Centre CRC 880 sponsored by the German Research Foundation. Several new approaches to increasing the lift are applied as part of the design of a reference aircraft with short take-off and landing capability: The numerically predicted positive effect of Coanda jet blowing at the trailing edge flap is validated in water tunnel experiments. Robust miniature pressure and hot-fi�lm sensors are developed for the closed-loop control of a piezo-actuated blowing lip. A flexible leading-edge device utilizes composite materials, for which new structural designs are developed. Additionally, a potential de-icing system, as well as a lightning-strike protection are presented. A high power-density electrically driven compressor with a broad operating range is designed to provide the blowing air ow. Different propulsion systems for the reference aircraft are evaluated. An ultra-high bypass ratio engine is considered to be most promising, and thus a preliminary fan stage design process is established. The rotor dynamic influences of the engine on the aircraft structure are investigated through a hybrid approach using a multibody model and modal reduction.

Item URL in elib:https://elib.dlr.de/115829/
Document Type:Conference or Workshop Item (Speech)
Title:Progress in Efficient Active High-Lift
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Kauth, FelixLeibniz Universität HannoverUNSPECIFIED
Narjes, GerritLeibniz Universität HannoverUNSPECIFIED
Müller, JanLeibniz Universität HannoverUNSPECIFIED
Seume, Joerg R.leibniz universität hannover, tfdUNSPECIFIED
Vasista, SrinivasUNSPECIFIEDhttps://orcid.org/0000-0002-7917-6740
Müller, ThomasGerman Aerospace CenterUNSPECIFIED
François, Daniela G.technische universität braunschweig, institut für strömungsmechanikUNSPECIFIED
El Sayed, YosefTechnische Universität BraunschweigUNSPECIFIED
Semaan, RichardTechnische Universität BraunschweigUNSPECIFIED
Behr, ChristianTechnische Universität BraunschweigUNSPECIFIED
Schwerter, MartinTechnische Universität BraunschweigUNSPECIFIED
Leester-Schädel, MonikaTechnische Universität BraunschweigUNSPECIFIED
Nolte, FelixTechnische Universität BraunschweigUNSPECIFIED
Giesecke, DanielTechnische Universität BraunschweigUNSPECIFIED
Atalayer, ÇaǧlarTechnische Universität BraunschweigUNSPECIFIED
Radespiel, Rolftu braunschweigUNSPECIFIED
Journal or Publication Title:35th AIAA Applied Aerodynamics Conference
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:High-lift, Coanda, Blowing, Morphing
Event Title:35th AIAA Applied Aerodynamics Conference, AIAA AVIATION Forum
Event Location:Denver, Colorado, United States
Event Type:international Conference
Event Dates:5-9 June 2017
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 - Concepts and Integration (old), L - Structures and Materials (old), L - Turbine Technologies (old), L - Fan and Compressor Technologies (old), L - Simulation and Validation (old)
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Adaptronics
Institute of Aeroelasticity > Aeroelastic Simulation
Deposited By: Vasista, Srinivas
Deposited On:23 Nov 2017 14:44
Last Modified:23 Nov 2017 14:44

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.