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Structural Design of a Generic High Bypass Ration Fan

Ebel, Paul-Benjamin and Winkelmann, Peter and Schnell, Rainer and Schuff, Matthias (2026) Structural Design of a Generic High Bypass Ration Fan. In: Numerical Methods and Experimental Means for the Integration of Future Propulsion Systems Springer Aerospace Technology. Springer Cham. pp. 93-110. doi: 10.1007/978-3-031-97725-1_5.

Full text not available from this repository.

Official URL: https://link.springer.com/chapter/10.1007/978-3-031-97725-1_5

Abstract

Novel engine concepts for climate-friendly propulsion are accompanied by several deviations from today’s aero engine designs. Finding feasible propulsor designs for these concepts is a highly multidisciplinary task and has to unite, at least, aerodynamic goals with structural requirements. The presented work provides an insight into DLR’s approach on turbomachinery optimization and layout. The paper focuses on DLR’s multidisciplinary design process that is carried out for a generic ultra-high bypass ratio (UHBR) fan within the ASPIRE project as well as the lessons learned out of this, which have been incorporated into a new "Virtual Engine" approach.

Item URL in elib:https://elib.dlr.de/224371/
Document Type:Book Section
Title:Structural Design of a Generic High Bypass Ration Fan
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Ebel, Paul-Benjaminpaul.ebel (at) dlr.dehttps://orcid.org/0000-0002-7112-7653UNSPECIFIED
Winkelmann, PeterPeter.Winkelmann (at) dlr.deUNSPECIFIEDUNSPECIFIED
Schnell, RainerRainer.Schnell (at) dlr.deUNSPECIFIEDUNSPECIFIED
Schuff, MatthiasMatthias.Schuff (at) dlr.dehttps://orcid.org/0000-0003-3276-2539UNSPECIFIED
Date:2 May 2026
Journal or Publication Title:Numerical Methods and Experimental Means for the Integration of Future Propulsion Systems
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI:10.1007/978-3-031-97725-1_5
Page Range:pp. 93-110
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Boden, Fritzfritz.boden (at) dlr.dehttps://orcid.org/0000-0001-9653-3802215205200
Publisher:Springer Cham
Series Name:Springer Aerospace Technology
Status:Published
Keywords:aero engine, UHBR, Virtual Engine, multidisciplinary design, optimisation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Virtual Engine
Location: Göttingen , Köln-Porz , Stuttgart
Institutes and Institutions:Institute of Structures and Design > Design and Manufacture Technologies
Institute of Propulsion Technology > Fan and Compressor
Institute of Aeroelasticity > Aeroelastic Experiments
Deposited By: Ebel, Paul-Benjamin
Deposited On:08 Jun 2026 13:03
Last Modified:08 Jun 2026 14:34

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