Preliminary Performance Analysis of Medium-Range Liquid Hydrogen-Powered Box-Wing Aircraft
This paper proposes a performance analysis of a medium-range airliner powered by liquid hydrogen (LH<sub>2</sub>) propulsion. The focus is on operating performance in terms of achievable payload and range. A non-conventional box-wing architecture was selected to maximize operating perfor...
| Published in: | Aerospace |
|---|---|
| Main Authors: | , , |
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2024-05-01
|
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/11/5/379 |
