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

Structural and Systems Modelling of a Fluid-driven Morphing Winglet Trailing Edge

Vasista, Srinivas and Titze, Maik and Schäfer, Michael and Bertram, Oliver and Riemenschneider, Johannes and Monner, Hans Peter (2020) Structural and Systems Modelling of a Fluid-driven Morphing Winglet Trailing Edge. In: AIAA Scitech 2020 Forum. AIAA SciTech 2020 Forum, Adaptive Structures Conference, 2020-01-06 - 2020-01-10, Orlando, United States. doi: 10.2514/6.2020-2010. ISBN 978-162410595-1.

Full text not available from this repository.

Official URL: https://arc.aiaa.org/doi/abs/10.2514/6.2020-2010

Abstract

This paper presents structural and systems modeling of a control surface comprising fluid actuated morphing unit structures (FAMoUS). This control surface is intended to be used as a morphing winglet trailing edge for the primary purpose of load alleviation, and one key challenge in this region is the small installation space given the thin profile. The FAMoUS concept is based on reinforced elastomeric unit structures or "cells" that can elongate under pressurization, with either gas or hydraulic fluid. In this work, a control surface with uniform cross-section based on the thin winglet profile and hydraulic pressurization is investigated. Finite element analyses with three-dimensional structural and hydrostatic fluid elements are used to model the structural behavior and provide input for modeling and design of the systems architecture. These early results show that a thin control surface with FAMoUS is capable of carrying external loads and deflecting with sufficient magnitude though careful material design is also needed to ensure a balance between actuation power, material stress, stiffness, and deflection capability. Detailed design for manufacture and the comparison with pneumatic-based architectures is needed in future work, together with optimization of the various design parameters.

Item URL in elib:https://elib.dlr.de/133519/
Document Type:Conference or Workshop Item (Lecture)
Title:Structural and Systems Modelling of a Fluid-driven Morphing Winglet Trailing Edge
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Vasista, SrinivasUNSPECIFIEDhttps://orcid.org/0000-0002-7917-6740UNSPECIFIED
Titze, MaikUNSPECIFIEDhttps://orcid.org/0000-0001-5223-1538UNSPECIFIED
Schäfer, MichaelUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Bertram, OliverUNSPECIFIEDhttps://orcid.org/0000-0002-7732-9280140199315
Riemenschneider, JohannesUNSPECIFIEDhttps://orcid.org/0000-0001-5485-8326UNSPECIFIED
Monner, Hans PeterUNSPECIFIEDhttps://orcid.org/0000-0002-5897-2422UNSPECIFIED
Date:2020
Journal or Publication Title:AIAA Scitech 2020 Forum
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.2514/6.2020-2010
Series Name:AIAA
ISBN:978-162410595-1
Status:Published
Keywords:morphing wing, fluidic actuation
Event Title:AIAA SciTech 2020 Forum, Adaptive Structures Conference
Event Location:Orlando, United States
Event Type:international Conference
Event Start Date:6 January 2020
Event End Date:10 January 2020
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
Institute of Flight Systems > Safety Critical Systems&Systems Engineering
Deposited By: Vasista, Srinivas
Deposited On:15 Jan 2020 07:40
Last Modified:24 Apr 2024 20:36

Repository Staff Only: item control page

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