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Manufacture and Testing of a Large-displacement Droop-Nose Morphing Wing Leading Edge

Vasista, Srinivas and Riemenschneider, Johannes and Monner, Hans Peter and Nolte, Felix and Horst, Peter (2019) Manufacture and Testing of a Large-displacement Droop-Nose Morphing Wing Leading Edge. In: AIAA SciTech 2019 Forum. AIAA Science and Technology Forum and Exposition SciTech 2019, 07-11 January 2019, San Diego, United States.

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/abs/10.2514/6.2019-1858

Abstract

The manufacture and ground testing of a 3D full-scale 1100 mm span morphing wing leading edge device or droop-nose is presented in this paper. The device allows the smooth, gapless and large (90 deg.) variation in leading edge camber angle to enable the generation of very high lift coefficients for the design of a future regional aircraft. The droop-nose structure is composed of a composite elastomer-fiberglass skin supported by two internal kinematic assemblies and driven by harmonic drive rotational actuators. Preliminary results of shape show in general good agreement with the expected response. Quantification of the shape errors is underway along with solutions to improve the correlation. Strain measurements from strain gauges and digital image correlation show reasonable values of strain that are within the failure limits. Further tests including spar bending tests are ongoing and will be compared quantitatively with finite element simulations in future work.

Item URL in elib:https://elib.dlr.de/126882/
Document Type:Conference or Workshop Item (Speech)
Title:Manufacture and Testing of a Large-displacement Droop-Nose Morphing Wing Leading Edge
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Vasista, SrinivasUNSPECIFIEDhttps://orcid.org/0000-0002-7917-6740
Riemenschneider, JohannesUNSPECIFIEDhttps://orcid.org/0000-0001-5485-8326
Monner, Hans PeterUNSPECIFIEDhttps://orcid.org/0000-0002-5897-2422
Nolte, FelixTechnische Universität BraunschweigUNSPECIFIED
Horst, PeterTU BraunschweigUNSPECIFIED
Date:2019
Journal or Publication Title:AIAA SciTech 2019 Forum
Refereed publication:Yes
Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:morphing wing, leading edge droop nose, hybrid composite
Event Title:AIAA Science and Technology Forum and Exposition SciTech 2019
Event Location:San Diego, United States
Event Type:international Conference
Event Dates:07-11 January 2019
Organizer:AIAA
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:29 Apr 2019 08:53
Last Modified:29 Apr 2019 08:53

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