H. Baier, R. Wehrle, T. Ungwattanapanit

Alternative concepts of aircraft fuselage structures are discussed. These are based on modified topology and arrangement of the stiffeners or stiffener frames, the use of steered fiber reinforcements in case of fiber composite fuselages, and also possible increase of window sizes to enhance passenger comfort. Results indicate that such improvements look feasible in the future and allow reduced weight or increased performance.

Deutscher Luft- und Raumfahrtkongress 2015, Rostock

Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn, 2015

Conference Paper

englisch

21,0 x 29,7 cm, 6 Seiten

urn:nbn:de:101:1-201510192299

Entwurfsoptimierung, Rumpfbauweisen

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19.10.2015