Bitte benutzen Sie diese Kennung, um auf die Ressource zu verweisen:
https://doi.org/10.21256/zhaw-3345| Publikationstyp: | Konferenz: Paper |
| Art der Begutachtung: | Keine Angabe |
| Titel: | Numerical and experimental investigation of cooling concept for an electric propulsion system for aerobatic aircrafts |
| Autor/-in: | Liu, Xinying Ferrari, Flavio Manfriani, Leonardo |
| DOI: | 10.21256/zhaw-3345 |
| Tagungsband: | ICAS 2018 : congress proceedings, belo horizonte, brazil, september 09-14, 2018 |
| Angaben zur Konferenz: | 31st Congress of the International Council of the Aeronautical Sciences, Belo Horizonte, Brazil, 9-14 September 2018 |
| Erscheinungsdatum: | 2018 |
| Verlag / Hrsg. Institution: | ICAS |
| Verlag / Hrsg. Institution: | Stockholm |
| ISBN: | 978-3-932182-88-4 |
| Sprache: | Englisch |
| Schlagwörter: | Electric propulsion; Aerobatic aircraft; Conjugate heat transfer analysis; Full scale wind tunnel test |
| Fachgebiet (DDC): | 620: Ingenieurwesen |
| Zusammenfassung: | This paper presents the development of a cooling concept for an electric propulsion system of an aerobatic aircraft. The numerical part of this paper focuses on the battery cooling performance requirements, the internal design of the cooling duct and their influence on heat transfer efficiency, using conjugate heat transfer (CHT) simulation. The analysis was performed with the computational fluid dynamics (CFD) code Ansys CFX, using a Shear Stress Transport (SST) model. It is planned to prove the cooling concept in a full scale wind tunnel test. The test preparation is also described in this paper. |
| URI: | https://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/preview/ICAS2018_0162.htm https://digitalcollection.zhaw.ch/handle/11475/16437 |
| Volltext Version: | Publizierte Version |
| Lizenz (gemäss Verlagsvertrag): | Lizenz gemäss Verlagsvertrag |
| Departement: | School of Engineering |
| Organisationseinheit: | Zentrum für Aviatik (ZAV) |
| Enthalten in den Sammlungen: | Publikationen School of Engineering |
Dateien zu dieser Ressource:
| Datei | Beschreibung | Größe | Format | |
|---|---|---|---|---|
| ICAS2018_0162_paper.pdf | 1.26 MB | Adobe PDF |  Öffnen/Anzeigen |
Zur Langanzeige
Liu, X., Ferrari, F., & Manfriani, L. (2018). Numerical and experimental investigation of cooling concept for an electric propulsion system for aerobatic aircrafts. ICAS 2018 : Congress Proceedings, Belo Horizonte, Brazil, September 09-14, 2018. https://doi.org/10.21256/zhaw-3345
Liu, X., Ferrari, F. and Manfriani, L. (2018) ‘Numerical and experimental investigation of cooling concept for an electric propulsion system for aerobatic aircrafts’, in ICAS 2018 : congress proceedings, belo horizonte, brazil, september 09-14, 2018. Stockholm: ICAS. Available at: https://doi.org/10.21256/zhaw-3345.
X. Liu, F. Ferrari, and L. Manfriani, “Numerical and experimental investigation of cooling concept for an electric propulsion system for aerobatic aircrafts,” in ICAS 2018 : congress proceedings, belo horizonte, brazil, september 09-14, 2018, 2018. doi: 10.21256/zhaw-3345.
LIU, Xinying, Flavio FERRARI und Leonardo MANFRIANI, 2018. Numerical and experimental investigation of cooling concept for an electric propulsion system for aerobatic aircrafts. In: ICAS 2018 : congress proceedings, belo horizonte, brazil, september 09-14, 2018 [online]. Conference paper. Stockholm: ICAS. 2018. ISBN 978-3-932182-88-4. Verfügbar unter: https://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/preview/ICAS2018_0162.htm
Liu, Xinying, Flavio Ferrari, and Leonardo Manfriani. 2018. “Numerical and Experimental Investigation of Cooling Concept for an Electric Propulsion System for Aerobatic Aircrafts.” Conference paper. In ICAS 2018 : Congress Proceedings, Belo Horizonte, Brazil, September 09-14, 2018. Stockholm: ICAS. https://doi.org/10.21256/zhaw-3345.
Liu, Xinying, et al. “Numerical and Experimental Investigation of Cooling Concept for an Electric Propulsion System for Aerobatic Aircrafts.” ICAS 2018 : Congress Proceedings, Belo Horizonte, Brazil, September 09-14, 2018, ICAS, 2018, https://doi.org/10.21256/zhaw-3345.
Alle Ressourcen in diesem Repository sind urheberrechtlich geschützt, soweit nicht anderweitig angezeigt.