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Large-Displacement Morphing Wing Leading Edge Droop Nose: Optimization, Manufacture and Instrumentation

Vasista, Srinivas and Riemenschneider, Johannes and Monner, Hans Peter and Keimer, Ralf and Nolte, Felix and Horst, Peter (2020) Large-Displacement Morphing Wing Leading Edge Droop Nose: Optimization, Manufacture and Instrumentation. In: Fundamentals of High Lift for Future Civil Aircraft Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer. pp. 153-164. doi: 10.1007/978-3-030-52429-6_10.

Full text not available from this repository.

Official URL: https://link.springer.com/chapter/10.1007%2F978-3-030-52429-6_10

Abstract

This paper provides an overview of research into a morphing wing leading edge allowing smooth and continuous shape changes. Together with high-lift technologies investigated in the Collaborative Research Center 880 over the past nine years, the morphing droop nose has the potential to generate very high lift coefficients with low noise. Multiple design strategies were explored over the course of research and summarized here. Design features include novel, multifunctional, hybrid tailored composites comprising fiberglass and elastomeric materials, integral stringers to facilitate the flow of internal and external forces, and the use of optimization chains to synthesize the numerous design variables. The results of experimental tests show in general the suitability of the design methods, as well as a number of lessons learned, including the need for tighter aerodynamic-structural coupling, that are useful for future work.

Item URL in elib:https://elib.dlr.de/137561/
Document Type:Book Section
Title:Large-Displacement Morphing Wing Leading Edge Droop Nose: Optimization, Manufacture and Instrumentation
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Vasista, SrinivasSrinivas.Vasista (at) dlr.dehttps://orcid.org/0000-0002-7917-6740
Riemenschneider, JohannesJohannes.Riemenschneider (at) dlr.dehttps://orcid.org/0000-0001-5485-8326
Monner, Hans PeterHans.Monner (at) dlr.dehttps://orcid.org/0000-0002-5897-2422
Keimer, RalfRalf.Keimer (at) dlr.dehttps://orcid.org/0000-0001-9638-4413
Nolte, FelixTU BraunschweigUNSPECIFIED
Horst, PeterTU BraunschweigUNSPECIFIED
Date:2020
Journal or Publication Title:Fundamentals of High Lift for Future Civil Aircraft
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.1007/978-3-030-52429-6_10
Page Range:pp. 153-164
Editors:
EditorsEmailEditor's ORCID iD
Radespiel, RolfTechnische Universität Braunschweig, Institut für StrömungsmechanikUNSPECIFIED
Semaan, RichardTechnische Universität BraunschweigUNSPECIFIED
Publisher:Springer
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Status:Published
Keywords:Morphing wing, leading edge, droop nose, high lift
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 (old)
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Adaptronics
Deposited By: Vasista, Srinivas
Deposited On:16 Nov 2020 09:41
Last Modified:23 Nov 2020 08:21

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