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

Autor: Friedmann, Felix, Rienecker, Hannes, Dexl, Florian, Hauffe, Andreas, Wolf, Klaus
Předmět:
Zdroj: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering; Dec2023, Vol. 237 Issue 15, p3369-3381, 13p
Abstrakt: 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. [ABSTRACT FROM AUTHOR]
Databáze: Complementary Index