Thermal Management System Design for Electrified Aircraft Propulsion Concepts

This paper describes the development of thermal management systems (TMS) for three electrified aircraft propulsion (EAP) vehicle concepts released by NASA that span the UAM, regional, and single-aisle markets. For each EAP concept, a conventional TMS is designed for two electric component technology...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Chapman, Jeffryes, Hasseeb, Hashmatullah, Schnulo, Sydney
Format:	Other
Sprache:	eng
Schlagworte:	Aircraft Propulsion And Power
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!