Multidisciplinary structural optimization of novel high-aspect ratio composite aircraft wings

Novel high-aspect ratio airframe designs pave the way for a more sustainable aviation future. Such configurations enhance the aerodynamic efficiency of an aircraft through induced drag reduction mechanisms. Further performance gains, mainly in terms of structural mass, are accomplished via composite...

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Veröffentlicht in:	Structural and multidisciplinary optimization Jg. 66; H. 7; S. 150
Hauptverfasser:	Kilimtzidis, Spyridon, Kostopoulos, Vassilis
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Berlin/Heidelberg Springer Berlin Heidelberg 01.07.2023 Springer Nature B.V
Schlagworte:	Accuracy Aircraft Aircraft configurations Airframes Aspect ratio Composite materials Computational efficiency Computational Mathematics and Numerical Analysis Computing costs Configuration management Couplings Design optimization Drag reduction Engineering Engineering Design Geometric nonlinearity Induced drag Industrial Application Paper Optimization Software Structural response Theoretical and Applied Mechanics Wings (aircraft) Aircraft wings, Structural optimization, Composite materials, Computational aerodynamics
ISSN:	1615-147X, 1615-1488
Online-Zugang:	Volltext
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