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...
Guardat en:
| Autors principals: | , , , , |
|---|---|
| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
MDPI AG
2018-10-01
|
| Col·lecció: | Aerospace |
| Matèries: | |
| Accés en línia: | http://www.mdpi.com/2226-4310/5/4/105 |
| Etiquetes: |
Sense etiquetes, Sigues el primer a etiquetar aquest registre!
|