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A Coupled Global-Local Optimization Process for Fuselage Structures

Sinha, Kautuk and Klimmek, Thomas (2021) A Coupled Global-Local Optimization Process for Fuselage Structures. Deutscher Luft- und Raumfahrt Kongress 2021, 31 Aug 2021 - 2 Sept 2021, Bremen (virtuell).

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The aeroelastic loads and design processes at DLR-AE in the framework of multi-disciplinary optimization are constantly evolving. New developments have been made in the in-house model generation tool ModGen which allow us to create fuselage models for preliminary design. As a part of the subsequent developments to integrate the fuselage structure in our aeroelastic design process, a new framework for optimizing the fuselage structure has been developed. The process is based on a multi-level optimization approach which follows a coupled global-local optimization methodology to simplify a very large optimization problem. In this paper, we present a physical sub-structure grouping process which enables reduced number of panel optimizations and saves considerable computational effort with little compromise in the solution accuracy.

Item URL in elib:https://elib.dlr.de/144168/
Document Type:Conference or Workshop Item (Speech)
Title:A Coupled Global-Local Optimization Process for Fuselage Structures
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Sinha, KautukKautuk.Sinha (at) dlr.deUNSPECIFIED
Klimmek, ThomasThomas.Klimmek (at) dlr.deUNSPECIFIED
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:multi-level optimization, fuselage sizing, aeroelastic design
Event Title:Deutscher Luft- und Raumfahrt Kongress 2021
Event Location:Bremen (virtuell)
Event Type:national Conference
Event Dates:31 Aug 2021 - 2 Sept 2021
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Components and Systems
DLR - Research area:Aeronautics
DLR - Program:L CS - Components and Systems
DLR - Research theme (Project):L - Structural Materials and Design
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Sinha, Kautuk
Deposited On:11 Oct 2021 16:06
Last Modified:26 Sep 2022 09:05

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