MATEC Web Conf.
Volume 346, 2021International Conference on Modern Trends in Manufacturing Technologies and Equipment (ICMTMTE 2021)
|Number of page(s)||6|
|Published online||26 October 2021|
Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle
1 Department of Aerospace Composite Construction, Bauman Moscow State Technical University, Moscow 105005, Russia.
2 Department of Higher Mathematics, Plekhanov Russian University of Economics, Moscow 117997, Russia.
* Corresponding author: firstname.lastname@example.org
This paper describes the optimizing results of structural elements of the composite wing of an unmanned aerial vehicle. The thickness and composite lay-up structure of load-bearing elements and wing skin are determined using the ANSYS software package. The optimal structure is presented using the Pareto set method of the “ideal center” basing on four criteria: minimum mass, deflection, normal stress, and maximum safety factor of the wing. Verification calculations were carried out to determine the safety factor of the load-bearing wing structure using a geometrically nonlinear model in FEMAP software.
© The Authors, published by EDP Sciences, 2021
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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