Design studies for a light aircraft wing with highly integrated load-bearing hydrogen tanks using multi-objective optimization methods
Publikation: Beitrag in Fachzeitschrift › Forschungsartikel › Beigetragen › Begutachtung
Beitragende
Abstract
To enable emission-free flight, the use of hydrogen as an energy carrier in aircraft is one possible solution. However, hydrogen storage is a challenging task. The current paper presents a design study for a light aircraft wing with highly integrated load-bearing hydrogen tanks using an automated optimization method by means of Evolutionary Algorithms. With this method, both preliminary investigations and a more detailed design of structural wing concepts with highly integrated hydrogen vessels were carried out.
Details
Originalsprache | Englisch |
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Seiten (von - bis) | 3369-3381 |
Seitenumfang | 13 |
Fachzeitschrift | Proceedings of the Institution of Mechanical Engineers / Part G, Journal of aerospace engineering |
Jahrgang | 237 |
Ausgabenummer | 15 |
Frühes Online-Datum | 24 Feb. 2023 |
Publikationsstatus | Veröffentlicht - Dez. 2023 |
Peer-Review-Status | Ja |
Externe IDs
Mendeley | 8479c95a-2c88-39ab-bfbe-9b4c286dd4f1 |
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Scopus | 85148937191 |
Schlagworte
ASJC Scopus Sachgebiete
Schlagwörter
- evolutionary optimization, high pressure vessel, integral hydrogen tanks, light aircraft wing, structural optimization