Data for: Effect of Design Parameters on the Mass of a Variable-span Morphing Wing Based on Finite Element Structural Analysis and Optimization

Published: 6 August 2018| Version 2 | DOI: 10.17632/x9nd3y6cyh.2
Contributors:
Pedro Santos, Pedro Gamboa, Yifan Zhao, Diogo Sousa

Description

Supplemental data: Aerodynamic loading values for all wing configurations and aeroplane MTOWs; complete parametric study results of the fixed wing and variable-span wing.

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Categories

Optimization (Algorithms), Aerospace, Morphing, Unmanned Aerial Vehicle (Space Vehicle), Finite-Element

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