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Passive loads alleviation through aeroelastic tailoring

De Breuker, Roeland and Krüger, Wolf R. (2021) Passive loads alleviation through aeroelastic tailoring. AIAA Scitech 2021 Forum, 11.–15. Jan. 2021 + 19.–21. Jan. 2021, Virtual Event.

Full text not available from this repository.

Abstract

The presentation covered work performed by TU Delft and DLR on a hybrid aeroelastic tailoring process, in the framework of the European 7FP Smart Fixed Wing Aircraft (SFWA) project. Aim of the work package 'Adaptive Wing' in SFWA was to create design processes and solutions for aircraft wings giving optimal response with respect to loads, comfort and performance by the introduction of passive and active concepts. Central activity of the work was the design and optimization of adaptive wing structures, for complete wings as well as for special components. The design is performed with respect to loads, comfort and performance. This process, often called "aeroelastic tailoring" for passive solutions and "aeroservoelastic tailoring" for solutions including control devices and an active control loop, formed the backbone of the work package.

Item URL in elib:https://elib.dlr.de/140656/
Document Type:Conference or Workshop Item (Speech)
Title:Passive loads alleviation through aeroelastic tailoring
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
De Breuker, RoelandAerospace Structures, Delft University of Technologyhttps://orcid.org/0000-0002-7882-2173
Krüger, Wolf R.Wolf.Krueger (at) dlr.dehttps://orcid.org/0000-0002-7949-1169
Date:15 January 2021
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:aeroelastic tailoring, load control, wing design
Event Title:AIAA Scitech 2021 Forum
Event Location:Virtual Event
Event Type:international Conference
Event Dates:11.–15. Jan. 2021 + 19.–21. Jan. 2021
Organizer:AIAA - American Institute of Aeronautics and Astronautics
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 - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity
Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Krüger, Prof. Dr.-Ing. Wolf R.
Deposited On:27 Jan 2021 16:52
Last Modified:27 Jan 2021 16:52

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