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Integration of Wing-Mounted Over-Wing Engines on a Mid-Range Aircraft

Wegener, Patrick und Lange-Schmuckall, Fabian (2022) Integration of Wing-Mounted Over-Wing Engines on a Mid-Range Aircraft. In: AIAA SciTech 2022 Forum, Seiten 1-19. American Institute of Aeronautics and Astronautics Inc, AIAA. AIAA SCITECH 2022 Forum, 2022-01-03 - 2022-01-07, San Diego, USA. doi: 10.2514/6.2022-2563. ISBN 978-162410631-6.

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Offizielle URL: https://dx.doi.org/10.2514/6.2022-2563

Kurzfassung

Ultra-High Bypass Ratio (UHBR) engines are an important technology for improving the efficiency of future aircraft. However, their large diameter poses a major challenge for their use in conventional under-wing mounted engine configurations due to limited space. A configuration with engines mounted above the wing is not subject to these limitations and therefore offers the potential for improvements in overall aircraft efficiency and performance. Another advantage of this configuration is the acoustic shielding effect of the fan noise toward the ground by the wing. Configurations with this type of engine layout were investigated as part of the German LuFo V project AVACON (AdVanced Aircraft CONcepts). This paper describes the investigated variant of engine integration via a vertical pylon between nacelle lower side and main spar of the wing. To investigate the complex aerodynamic interactions between the engine and the wing, RANS CFD simulations were performed using the DLR code TAU. By optimizing twist and upper surface shape, the wing geometry was adapted to the flow conditions resulting from the engine integration to reduce detrimental aerodynamic installation effects. In general, the influence of the geometric shape of the wing and engine as well as their relative geometric position on the overall drag is more pronounced in such a configuration than in a under-wing engine design. The use of advanced optimization methods is therefore crucial for a successful design.

elib-URL des Eintrags:https://elib.dlr.de/188989/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Integration of Wing-Mounted Over-Wing Engines on a Mid-Range Aircraft
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Wegener, PatrickPatrick.Wegener (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Lange-Schmuckall, FabianFabian.Lange (at) dlr.dehttps://orcid.org/0000-0001-5854-2345NICHT SPEZIFIZIERT
Datum:3 Januar 2022
Erschienen in:AIAA SciTech 2022 Forum
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Nein
DOI:10.2514/6.2022-2563
Seitenbereich:Seiten 1-19
Verlag:American Institute of Aeronautics and Astronautics Inc, AIAA
Name der Reihe:Conference Proceedings
ISBN:978-162410631-6
Status:veröffentlicht
Stichwörter:Aerodynamics; Aviation; Bypass ratio; Computational fluid dynamics; Efficiency; Integration; Machine design; Wings
Veranstaltungstitel:AIAA SCITECH 2022 Forum
Veranstaltungsort:San Diego, USA
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:3 Januar 2022
Veranstaltungsende:7 Januar 2022
Veranstalter :American Institute of Aeronautics and Astronautics
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Umweltschonender Antrieb
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L CP - Umweltschonender Antrieb
DLR - Teilgebiet (Projekt, Vorhaben):L - Triebwerkskonzepte und -integration
Standort: Braunschweig
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Transportflugzeuge
Hinterlegt von: Wegener, Patrick
Hinterlegt am:02 Nov 2022 12:05
Letzte Änderung:24 Apr 2024 20:50

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