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Krüger, Wolf R. und Klimmek, Thomas (2026) Parametric Structural Modelling for Aeroelastic and Aeroacoustic Analyses of an Aircraft Fuselage. In: Numerical Methods and Experimental Means for the Integration of Future Propulsion Systems Springer. Seiten 111-123. doi: 10.1007/978-3-031-97725-1. ISBN 978-3-031-97724-4. ISSN 1869-1730.
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Offizielle URL: https://link.springer.com/book/10.1007/978-3-031-97725-1
Kurzfassung
The chapter describes results of work in the Cross-DemonstratorCapabilities (XDC) activities in the project Large Passenger Aircraft on modelling and load analysis. As a result of this work, a simulation model of a 150-seat aircraft, used as a reference configuration in several investigations in the work package, has become available. The data includes a structural (finite-element) model and an aerodynamic (VLM/DLM) model. The model has been distributed to project partners for studies of aeroelastic stability and vibroacoustics. In this chapter, the modelling process is described and the simulation model is presented along with selected results.
| elib-URL des Eintrags: | https://elib.dlr.de/224330/ | ||||||||||||
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| Dokumentart: | Beitrag im Sammelband | ||||||||||||
| Titel: | Parametric Structural Modelling for Aeroelastic and Aeroacoustic Analyses of an Aircraft Fuselage | ||||||||||||
| Autoren: |
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| Datum: | 2026 | ||||||||||||
| Erschienen in: | Numerical Methods and Experimental Means for the Integration of Future Propulsion Systems | ||||||||||||
| Referierte Publikation: | Ja | ||||||||||||
| Open Access: | Nein | ||||||||||||
| Gold Open Access: | Nein | ||||||||||||
| In SCOPUS: | Nein | ||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||
| DOI: | 10.1007/978-3-031-97725-1 | ||||||||||||
| Seitenbereich: | Seiten 111-123 | ||||||||||||
| Herausgeber: |
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| Verlag: | Springer | ||||||||||||
| ISSN: | 1869-1730 | ||||||||||||
| ISBN: | 978-3-031-97724-4 | ||||||||||||
| Status: | veröffentlicht | ||||||||||||
| Stichwörter: | Structural modelling, Aeroelasticity, Vibroacoustic analysis, Parametric modelling | ||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||
| HGF - Programmthema: | Effizientes Luftfahrzeug | ||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||
| DLR - Forschungsgebiet: | L EV - Effizientes Luftfahrzeug | ||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Virtuelles Flugzeug und Validierung | ||||||||||||
| Standort: | Göttingen | ||||||||||||
| Institute & Einrichtungen: | Institut für Aeroelastik > Lastanalyse und Entwurf | ||||||||||||
| Hinterlegt von: | Krüger, Prof. Dr.-Ing. Wolf R. | ||||||||||||
| Hinterlegt am: | 06 Jul 2026 13:48 | ||||||||||||
| Letzte Änderung: | 06 Jul 2026 13:48 |
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