Efficient structural optimisation of composite materials aircraft wings
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TL;DR: In this paper , the structural representation of the numerical model is based on the well-established equivalent-plate methodology, capable of reducing the size and computational cost of the associated problem.
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About: This article is published in Composite Structures. The article was published on 01 Oct 2022. and is currently open access. The article focuses on the topics: Spar & Aeroelasticity.
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