Ground Structures-Based Topology Optimization of a Morphing Wing Using a Metaheuristic Algorithm

This paper presents multi-objective topology and sizing optimization of a morphing wing structure. The purpose of this paper is to design a new aircraft wing structure with a tapered shape for ribs, spars, and skins including a torsion beam for external actuating torques, which is anticipated to mod...

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Vydáno v:	Metals (Basel ) Ročník 11; číslo 8; s. 1311
Hlavní autoři:	Winyangkul, Seksan, Wansaseub, Kittinan, Sleesongsom, Suwin, Panagant, Natee, Kumar, Sumit, Bureerat, Sujin, Pholdee, Nantiwat
Médium:	Journal Article
Jazyk:	angličtina
Vydáno:	Basel MDPI AG 01.08.2021
Témata:	Aeroelasticity Aircraft Aircraft design aircraft wing Algorithms Aluminum Buckling Design factors Design optimization Heuristic methods internal wing structure Investigations Lift Manufacturing metaheuristics Morphing multi-objective evolutionary algorithms Multiple objective analysis Optimization techniques Pareto optimization Thickness Topology optimization Wings (aircraft)
ISSN:	2075-4701, 2075-4701
On-line přístup:	Získat plný text
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