Preliminary Aircraft Design for Hybrid Electric Propulsion Architectures: A Focus on Critical Loss of Thrust
Hybrid electric propulsion architectures offer a promising solution for reducing fuel consumption and emissions in aviation. However, the introduction of dual-energy carriers adds complexity to preliminary aircraft design, particularly in terms of power distribution, failure analysis, and compliance...
| Published in: | Aerospace |
|---|---|
| Main Authors: | Jonas Mangold, Andreas Strohmayer |
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2025-03-01
|
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/12/4/275 |
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