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Large-Displacement Wing Droop Nose Design

Nolte, Felix and Horst, Peter and Vasista, Srinivas and Monner, Hans Peter (2017) Large-Displacement Wing Droop Nose Design. Project Report. TU Braunschweig.

Full text not available from this repository.

Abstract

The following paper presents an overview of the work done on the morphing wing leading edge droop nose device in the second funding period of the Sonderforschungsbereich 880 project (SFB880). The device is composed of a hybrid composite skin including prepreg and elastomeric layers and conventional kinematic and compliant options for the internal mechanism. Prior manufacturing and experimental work showed the suitability of the skin concept and several optimization tools were developed and used to determine the best thickness distributions and internal mechanism architecture. Development of these optimization tools are ongoing and have been extended into 3D design. Industrial considerations such as possible solutions for system integration of lightning strike protection, an abrasion layer and a de-icing system have also been proposed and experimentally tested. A cyclic electrical de-icing system, which uses the given structure as resistive heating, is proposed and a demonstrator as proof of concept is built and experimentally investigated. Experimental tests are regularly performed and the data embedded in the optimization tools as the material development of the skin continues in order to characterize the multifunctional material behaviour appropriately in the numerical models.

Item URL in elib:https://elib.dlr.de/115874/
Document Type:Monograph (Project Report)
Title:Large-Displacement Wing Droop Nose Design
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Nolte, FelixTU BraunschweigUNSPECIFIED
Horst, Petertu braunschweigUNSPECIFIED
Vasista, Srinivassrinivas.vasista (at) dlr.dehttps://orcid.org/0000-0002-7917-6740
Monner, Hans Peterhans.monner (at) dlr.dehttps://orcid.org/0000-0002-5897-2422
Date:2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:93
Publisher:TU Braunschweig
ISBN:978-3-928628-90-7
Status:Published
Keywords:Morphing wing, droop nose, high-lift, hybrid composite
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 - Structures and Materials
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Adaptronics
Deposited By: Vasista, Srinivas
Deposited On:23 Nov 2017 14:48
Last Modified:23 Nov 2017 14:48

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