Design studies for a light aircraft wing with highly integrated load-bearing hydrogen tanks using multi-objective optimization methods

Publikation: Beitrag in FachzeitschriftForschungsartikelBeigetragenBegutachtung

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

OriginalspracheEnglisch
Seiten (von - bis)3369-3381
Seitenumfang13
FachzeitschriftProceedings of the Institution of Mechanical Engineers / Part G, Journal of aerospace engineering
Jahrgang237
Ausgabenummer15
Frühes Online-Datum24 Feb. 2023
PublikationsstatusVeröffentlicht - Dez. 2023
Peer-Review-StatusJa

Externe IDs

Mendeley 8479c95a-2c88-39ab-bfbe-9b4c286dd4f1
Scopus 85148937191

Schlagworte

Schlagwörter

  • evolutionary optimization, high pressure vessel, integral hydrogen tanks, light aircraft wing, structural optimization