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

Flexible-Wing Design Process for TU-FLEX Demonstrator

Gonzáles, Pedro J. and Shahi, Hikmat and Meddaikar, Muhammad Yasser and Krüger, Wolf R. and Silvestre, Flavio J. (2022) Flexible-Wing Design Process for TU-FLEX Demonstrator. International Forum on Aeroelasticity and Structural Dynamics (IFASD) 2022, 13.-17. Jun. 2022, Madrid, Spanien.

This is the latest version of this item.

[img] PDF - Only accessible within DLR


This research presents the conceptual and preliminary design process of the TU-Flex wing. This vehicle has been designed as a subscale-flying aeroelastic demonstrator with a transport aircraft configuration. The most flexible version of this vehicle should show a coupling between structural and rigid body dynamics during operation. In this paper, the reference wing for this aircraft was designed, such that a given level of structural flexibility and generally lower modal frequencies could be reached. Design boundary conditions included flexibility, operational, sensor, facility, and environmental requirements. The design flow allowed flexibility to evaluate multiple structural configurations, airfoils, materials, and load cases. A trend study was completed on a conventional wing-box design and a load-carrying closed skin shell. The selected wing is capable of displaying deformations above 10% for the 2g flight condition while meeting our construction feasibility requirements. The selected wing will proceed to the detailed design phase and subsequently to the construction process.

Item URL in elib:https://elib.dlr.de/188009/
Document Type:Conference or Workshop Item (Speech)
Title:Flexible-Wing Design Process for TU-FLEX Demonstrator
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Gonzáles, Pedro J.TU BerlinUNSPECIFIED
Shahi, Hikmathikmat.shahi (at) dlr.deUNSPECIFIED
Meddaikar, Muhammad YasserMuhammad.Meddaikar (at) dlr.dehttps://orcid.org/0000-0001-9580-7023
Krüger, Wolf R.Wolf.Krueger (at) dlr.dehttps://orcid.org/0000-0002-7949-1169
Silvestre, Flavio J.TU BerlinUNSPECIFIED
Date:June 2022
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:flexible wing, wing design process, aeroelasticity, UAV
Event Title:International Forum on Aeroelasticity and Structural Dynamics (IFASD) 2022
Event Location:Madrid, Spanien
Event Type:international Conference
Event Dates:13.-17. Jun. 2022
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Aircraft and  Validation
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Krüger, Prof. Dr.-Ing. Wolf R.
Deposited On:29 Aug 2022 09:44
Last Modified:29 Aug 2022 09:44

Available Versions of this Item

  • Flexible-Wing Design Process for TU-FLEX Demonstrator. (deposited 29 Aug 2022 09:44) [Currently Displayed]

Repository Staff Only: item control page

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