Development of a Lumped Parameter Model for an Aeronautic Hybrid Electric Propulsion System

Development of a Lumped Parameter Model for an Aeronautic Hybrid Electric Propulsion System

This paper describes a case study for applying a hybrid electric propulsion system for general aviation aircraft. The work was performed by a joint team from the Centro Italiano Ricerche Aerospaziali (CIRA) and the Department of Industrial Engineering of the University of Naples Federico II. The use...

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Bibliographic Details
Main Authors: Emma Frosina, Adolfo Senatore, Luka Palumbo, Giuseppe Di Lorenzo, Ciro Pascarella
Format: Article
Language:English
Published: MDPI AG 2018-10-01
Series:Aerospace
Subjects:
lumped parameter simulation
aircraft hybrid propulsion
fuel economy
propulsion and propellant systems
Online Access:http://www.mdpi.com/2226-4310/5/4/105

Internet

http://www.mdpi.com/2226-4310/5/4/105

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