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Optimization Tool Assessment for a Large-displacement Compliant Morphing Wing Leading Edge

Vasista, Srinivas and Rose, Michael and Monner, Hans Peter (2016) Optimization Tool Assessment for a Large-displacement Compliant Morphing Wing Leading Edge. In: 27th International Conference on Adaptive Structures and Technologies (ICAST 2016), pp. 1-12. ICAST 2016, 3.-5. Okt. 2016, Lake George, USA. (In Press)

Full text not available from this repository.

Abstract

The design of a mandatory droop-nose morphing device for a new type of passenger aircraft is presented in this work. This work forms one of the subprojects of the Collaborative Research Center 880 in Braunschweig, Germany. The leading edge displacement requires large curvature changes against high external loads and a novel anisotropic hybrid material comprising fiberglass and an elastomer is considered to allow large chordwise displacement and high spanwise stiffness. A number of optimization tools have been developed, such as a skin optimization tool, topology optimization compliant mechanism design tool, and a heuristic genetic algorithm based method. Amongst these approaches, the design philosophies of using conventional or compliant mechanisms are considered. The tools have their advantages and disadvantages, and numerical issues have prevented the further development of the topology optimization tool. Planned demonstrator manufacture and testing of the various design philosophies will provide an insight into which philosophy is more effective.

Item URL in elib:https://elib.dlr.de/107370/
Document Type:Conference or Workshop Item (Speech)
Title:Optimization Tool Assessment for a Large-displacement Compliant Morphing Wing Leading Edge
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Vasista, SrinivasSrinivas.Vasista (at) dlr.deUNSPECIFIED
Rose, Michaelmichael.rose (at) dlr.deUNSPECIFIED
Monner, Hans PeterHans.Monner (at) dlr.deUNSPECIFIED
Date:2016
Journal or Publication Title:27th International Conference on Adaptive Structures and Technologies (ICAST 2016)
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-12
Status:In Press
Keywords:droop nose, leading edge, morphing wing, load path optimization
Event Title:ICAST 2016
Event Location:Lake George, USA
Event Type:international Conference
Event Dates:3.-5. Okt. 2016
Organizer:Rensselaer Polytechnic Institute, USA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Earth Observation
DLR - Research area:Raumfahrt
DLR - Program:R EO - Earth Observation
DLR - Research theme (Project):R - Aircraft SAR
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Adaptronics
Deposited By: Rose, Dr.rer.nat. Michael
Deposited On:09 Nov 2016 09:46
Last Modified:09 Nov 2016 09:46

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