Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-3345
Full metadata record
DC FieldValueLanguage
dc.contributor.authorLiu, Xinying-
dc.contributor.authorFerrari, Flavio-
dc.contributor.authorManfriani, Leonardo-
dc.date.accessioned2019-03-29T09:03:12Z-
dc.date.available2019-03-29T09:03:12Z-
dc.date.issued2018-
dc.identifier.isbn978-3-932182-88-4de_CH
dc.identifier.urihttps://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/preview/ICAS2018_0162.htmde_CH
dc.identifier.urihttps://digitalcollection.zhaw.ch/handle/11475/16437-
dc.description.abstractThis 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.de_CH
dc.language.isoende_CH
dc.publisherICASde_CH
dc.rightsLicence according to publishing contractde_CH
dc.subjectElectric propulsionde_CH
dc.subjectAerobatic aircraftde_CH
dc.subjectConjugate heat transfer analysisde_CH
dc.subjectFull scale wind tunnel testde_CH
dc.subject.ddc620: Ingenieurwesende_CH
dc.titleNumerical and experimental investigation of cooling concept for an electric propulsion system for aerobatic aircraftsde_CH
dc.typeKonferenz: Paperde_CH
dcterms.typeTextde_CH
zhaw.departementSchool of Engineeringde_CH
zhaw.organisationalunitZentrum für Aviatik (ZAV)de_CH
zhaw.publisher.placeStockholmde_CH
dc.identifier.doi10.21256/zhaw-3345-
zhaw.conference.details31st Congress of the International Council of the Aeronautical Sciences, Belo Horizonte, Brazil, 9-14 September 2018de_CH
zhaw.funding.euNode_CH
zhaw.originated.zhawYesde_CH
zhaw.publication.statuspublishedVersionde_CH
zhaw.publication.reviewNot specifiedde_CH
zhaw.title.proceedingsICAS 2018 : congress proceedings, belo horizonte, brazil, september 09-14, 2018de_CH
zhaw.webfeedAerodynamicsde_CH
Appears in collections:Publikationen School of Engineering

Files in This Item:
File Description SizeFormat 
ICAS2018_0162_paper.pdf1.26 MBAdobe PDFThumbnail
View/Open
Show simple item record
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.


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.