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View article: 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 Open
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…