Versenden
Drucken
Hasabnis, Apurva und Maseland, Hans und Moens, Frédéric und Prachar, Ales und Wild, Jochen (2024) Lessons Learnt from Chimera Method Application to a Deploying Krueger Device. In: Advanced Computational Methods and Design for Greener Aviation Computational Methods in Applied Sciences, 59. Springer Nature. Seiten 124-144. doi: 10.1007/978-3-031-61109-4_9. ISBN 978-3-031-61109-4.
Dieses Archiv kann nicht den Volltext zur Verfügung stellen.
Offizielle URL: https://link.springer.com/chapter/10.1007/978-3-031-61109-4_9
Kurzfassung
The Chimera method is an established method for simulation of overlapping grids. Meshing parts independently has made this method popular for complex geometries as well as moving bodies like propellers and rotors or control surfaces. It is thus a promising method to simulate deflecting high-lift systems. In the frame of the UHURA project, several partners applied their CFD capabilities based on Chimera in order to validate the method for this specific application in comparison to wind tunnel tests. The presentation outlines the different Chimera approaches ranging from structured/2D to hybrid/3D in steady and unsteady simulations for the different type of setups investigated, namely straight and swept wing with full-span and part-span Krueger flap. It summarizes common challenges and best practice for application of the Chimera approach for such a device.
| elib-URL des Eintrags: | https://elib.dlr.de/205807/ | ||||||||||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Dokumentart: | Beitrag im Sammelband | ||||||||||||||||||||||||
| Titel: | Lessons Learnt from Chimera Method Application to a Deploying Krueger Device | ||||||||||||||||||||||||
| Autoren: |
| ||||||||||||||||||||||||
| Datum: | 2024 | ||||||||||||||||||||||||
| Erschienen in: | Advanced Computational Methods and Design for Greener Aviation | ||||||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||||||
| Band: | 59 | ||||||||||||||||||||||||
| DOI: | 10.1007/978-3-031-61109-4_9 | ||||||||||||||||||||||||
| Seitenbereich: | Seiten 124-144 | ||||||||||||||||||||||||
| Herausgeber: |
| ||||||||||||||||||||||||
| Verlag: | Springer Nature | ||||||||||||||||||||||||
| Name der Reihe: | Computational Methods in Applied Sciences | ||||||||||||||||||||||||
| ISBN: | 978-3-031-61109-4 | ||||||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||||||
| Stichwörter: | Aerodynamics, Unsteady, High-Lift Systems, CFD, Chimera, Overset Methods | ||||||||||||||||||||||||
| 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: | Braunschweig | ||||||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Transportflugzeuge | ||||||||||||||||||||||||
| Hinterlegt von: | Wild, Dr.-Ing. Jochen | ||||||||||||||||||||||||
| Hinterlegt am: | 14 Okt 2024 10:26 | ||||||||||||||||||||||||
| Letzte Änderung: | 14 Okt 2024 12:38 |
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags
