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Hybrid Wing Body as a Low-Noise Aircraft from a Multidisciplinary Point of View

Mößner, Michael and Bertsch, Lothar and Delfs, Jan Werner and Hasan, Yasim Julian and Hecken, Tobias and Iwanizki, Michael and Keller, Dennis and Moreau, Antoine and Schmidt, Florian Nils and Seitz, Arne (2026) Hybrid Wing Body as a Low-Noise Aircraft from a Multidisciplinary Point of View. In: Numerical Methods and Experimental Means for the Integration of Future Propulsion Systems Springer Aerospace Technology. Springer Cham. pp. 25-49. doi: 10.1007/978-3-031-97725-1_2. ISBN 978-3-031-97724-4. ISSN 1869-1730.

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

Abstract

One important goal when reducing the environmental impact of an aircraft is the reduction of noise. There is much potential for reducing noise when making it a major objective from the beginning of the design phase. Within this contribution a hybrid wing body concept as a mid-range aircraft will be presented together with detailed studies of different disciplines such as aerodynamics, acoustics, structure and also handling qualities. How much noise reduction can be achieved? What are the advantages, where are the difficulties and weaknesses of such an aircraft configuration?

Item URL in elib:https://elib.dlr.de/224762/
Document Type:Book Section
Title:Hybrid Wing Body as a Low-Noise Aircraft from a Multidisciplinary Point of View
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Mößner, MichaelMichael.Moessner (at) dlr.dehttps://orcid.org/0000-0002-6355-4436220114812
Bertsch, LotharLothar.Bertsch (at) dlr.dehttps://orcid.org/0000-0003-2780-2858UNSPECIFIED
Delfs, Jan WernerJan.Delfs (at) dlr.dehttps://orcid.org/0000-0001-8893-1747220114813
Hasan, Yasim JulianYasim.Hasan (at) dlr.dehttps://orcid.org/0000-0002-5081-223XUNSPECIFIED
Hecken, TobiasTobias.Hecken (at) dlr.dehttps://orcid.org/0009-0007-0030-7941220114814
Iwanizki, MichaelMichael.Iwanizki (at) dlr.deUNSPECIFIEDUNSPECIFIED
Keller, DennisDennis.Keller (at) dlr.dehttps://orcid.org/0000-0002-1471-9433220114816
Moreau, Antoineantoine.moreau (at) dlr.deUNSPECIFIEDUNSPECIFIED
Schmidt, Florian NilsF.Schmidt (at) dlr.dehttps://orcid.org/0000-0002-5537-7214220114817
Seitz, ArneArne.Seitz (at) dlr.deUNSPECIFIEDUNSPECIFIED
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:No
In ISI Web of Science:No
DOI:10.1007/978-3-031-97725-1_2
Page Range:pp. 25-49
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Boden, Fritzfritz.boden (at) dlr.dehttps://orcid.org/0000-0001-9653-3802220114818
Publisher:Springer Cham
Series Name:Springer Aerospace Technology
ISSN:1869-1730
ISBN:978-3-031-97724-4
Status:Published
Keywords:Low-noise aircraft, hybrid wing body, preliminary design
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: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Technical Acoustics
Institute for Aerodynamics and Flow Technology > Transport Aircraft
Institute for Aerodynamics and Flow Technology > Helicopter, GO
Institute of Flight Systems > Flight Dynamics and Simulation
Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Institute of Propulsion Technology > Engine Acoustic
Deposited By: Mößner, Michael
Deposited On:09 Jul 2026 08:11
Last Modified:20 Aug 2026 16:51

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