Thermal Management System Optimization for a Parallel Hybrid Aircraft Considering Mission Fuel Burn

Electrified aircraft propulsion enables new aircraft designs with fewer emissions. One challenge of electrified architectures is handling the electrical components’ waste heat. This is because batteries and other electrical components are sensitive to high temperatures and accumulate heat within the...

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Bibliographic Details
Main Authors: Eytan J. Adler, Benjamin J. Brelje, Joaquim R. R. A. Martins
Format: Article
Language:English
Published: MDPI AG 2022-04-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/9/5/243