Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-3345
Publication type: Conference paper
Type of review: Not specified
Title: Numerical and experimental investigation of cooling concept for an electric propulsion system for aerobatic aircrafts
Authors: Liu, Xinying
Ferrari, Flavio
Manfriani, Leonardo
DOI: 10.21256/zhaw-3345
Proceedings: ICAS 2018 : congress proceedings, belo horizonte, brazil, september 09-14, 2018
Conference details: 31st Congress of the International Council of the Aeronautical Sciences, Belo Horizonte, Brazil, 9-14 September 2018
Issue Date: 2018
Publisher / Ed. Institution: ICAS
Publisher / Ed. Institution: Stockholm
ISBN: 978-3-932182-88-4
Language: English
Subjects: Electric propulsion; Aerobatic aircraft; Conjugate heat transfer analysis; Full scale wind tunnel test
Subject (DDC): 620: Engineering
Abstract: 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
Fulltext version: Published version
License (according to publishing contract): Licence according to publishing contract
Departement: School of Engineering
Organisational Unit: Centre for Aviation (ZAV)
Appears in collections:Publikationen School of Engineering

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