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 performance. An op...
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| Fformat: | Artigo |
| Iaith: | Inglês |
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MDPI AG
2024-05-01
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| Cyfres: | Aerospace |
| Pynciau: | |
| Mynediad Ar-lein: | https://www.mdpi.com/2226-4310/11/5/379 |
| Tagiau: |
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