Impact of Battery Performance on the Initial Sizing of Hybrid-Electric General Aviation Aircraft-Reference-Cited by-同舟云学术

Impact of Battery Performance on the Initial Sizing of Hybrid-Electric General Aviation Aircraft

Published:2020-05 Issue:3 Volume:33 Page:04020007
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Finger D. Felix¹^ORCID,Braun Carsten²^ORCID,Bil Cees³

Affiliation:

1. Ph.D. Student, Dept. of Aerospace Engineering and Aviation, Royal Melbourne Institute of Technology Univ., Plenty Rd., Bundoora, VIC 3083, Australia; Research Engineer, Dept. of Aerospace Engineering, FH Aachen UAS, Hohenstaufenallee 6, 52064 Aachen, Germany (corresponding author). ORCID: .

2. Professor for Aircraft Design, Dept. of Aerospace Engineering, FH Aachen UAS, Hohenstaufenallee 6, 52064 Aachen, Germany. ORCID: .

3. Professor for Aircraft Design, Dept. of Aerospace Engineering and Aviation, Royal Melbourne Institute of Technology Univ., Plenty Rd., Bundoora, VIC 3083, Australia.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001113

Reference35 articles.

1. Borer N. K. M. D. Patterson J. K. Viken M. D. Moore J. Bevirt A. M. Stoll and A. R. Gibson. 2016. “Design and performance of the NASA SCEPTOR distributed electric propulsion flight demonstrator.” In Proc. 16th AIAA Aviation Technology Integration and Operations Conf. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2016-3920.

2. Chin J. C. S. L. Schnulo and A. D. Smith. 2017. “Transient thermal analyses of passive systems on SCEPTOR X-57.” In Proc. 17th AIAA Aviation Technology Integration and Operations Conf. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-3784.

3. Dean T. S. G. E. Wroblewski and P. J. Ansell. 2018. Mission analysis and component-level sensitivity study of hybrid-electric general-aviation propulsion systems. In Proc. AIAA Aerospace Sciences Meeting. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/1.C034635.

4. de Vries R. M. Hoogreef and R. Vos. 2019. “Preliminary sizing of a hybrid-electric passenger aircraft featuring over-the-wing distributed-propulsion.” In Proc. AIAA Scitech 2019 Forum. Reston VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2019-1811.

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