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Chapter 17: Design, Structural Optimization and Loads Assessment for a Flying Wing

Voß, Arne and Klimmek, Thomas and Bramsiepe, Kjell (2020) Chapter 17: Design, Structural Optimization and Loads Assessment for a Flying Wing. Other. STO-TR-AVT-251. NATO Science and Technology Organization. doi: 10.14339/STO-TR-AVT-251. (In Press)

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Abstract

This paper presents a summary of the evolution of aeroelastic models for flying wing configurations. Two different flying wing configurations have been studied and synergies with other DLR projects have been used to validate important parts of the loads process. A newly developed in-house software for aircraft loads extends the aeroelastic design process in combination with a parametric model generation software and a structural optimization sequence. During the progress from the DLR-F19-S towards the MULDICON, the numerical methods evolved as well, mainly aiming for higher fidelity to ensure a thorough and sophisticated design. Design and loads related studies were performed with national and international partners from industry and academia. This paper gives an overview on aspect and modeling strategies that distinguish flying wings from classical wing-fuselage-empennage configurations. Finally, an outlook is given on the next steps and on ongoing work.

Item URL in elib:https://elib.dlr.de/136218/
Document Type:Monograph (Other)
Title:Chapter 17: Design, Structural Optimization and Loads Assessment for a Flying Wing
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Voß, ArneArne.Voss (at) dlr.dehttps://orcid.org/0000-0003-2266-7853
Klimmek, ThomasThomas.Klimmek (at) dlr.deUNSPECIFIED
Bramsiepe, KjellKjell.Bramsiepe (at) dlr.deUNSPECIFIED
Date:2020
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.14339/STO-TR-AVT-251
Publisher:NATO Science and Technology Organization
Series Name:STO Technical Report
ISBN:978-92-837-2244-1
Status:In Press
Keywords:flying wing, aeroelastic modeling, structural optimization, loads analysis, MULDICON
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 > Loads Analysis and Aeroelastic Design
Deposited By: Voß, Arne
Deposited On:12 Oct 2020 16:12
Last Modified:12 Oct 2020 16:12

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