Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle

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 Pa...

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Autores principales:	Aung Naing Lin, Tatarnikov Oleg, Aung Phyo Wai
Formato:	article
Lenguaje:	EN FR
Publicado:	EDP Sciences 2021
Materias:	Engineering (General). Civil engineering (General) TA1-2040
Acceso en línea:	https://doaj.org/article/7fc0927c1b0a402fa41f9c232d582c59
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spelling	oai:doaj.org-article:7fc0927c1b0a402fa41f9c232d582c592021-11-08T15:20:33ZParametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle2261-236X10.1051/matecconf/202134603093https://doaj.org/article/7fc0927c1b0a402fa41f9c232d582c592021-01-01T00:00:00Zhttps://www.matec-conferences.org/articles/matecconf/pdf/2021/15/matecconf_icmtmte2021_03093.pdfhttps://doaj.org/toc/2261-236XThis 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.Aung Naing LinTatarnikov OlegAung Phyo WaiEDP SciencesarticleEngineering (General). Civil engineering (General)TA1-2040ENFRMATEC Web of Conferences, Vol 346, p 03093 (2021)
institution	DOAJ
collection	DOAJ
language	EN FR
topic	Engineering (General). Civil engineering (General) TA1-2040
spellingShingle	Engineering (General). Civil engineering (General) TA1-2040 Aung Naing Lin Tatarnikov Oleg Aung Phyo Wai Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle
description	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.
format	article
author	Aung Naing Lin Tatarnikov Oleg Aung Phyo Wai
author_facet	Aung Naing Lin Tatarnikov Oleg Aung Phyo Wai
author_sort	Aung Naing Lin
title	Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle
title_short	Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle
title_full	Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle
title_fullStr	Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle
title_full_unstemmed	Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle
title_sort	parametric optimization of load bearing elements for composite wing of an unmanned aerial vehicle
publisher	EDP Sciences
publishDate	2021
url	https://doaj.org/article/7fc0927c1b0a402fa41f9c232d582c59
work_keys_str_mv	AT aungnainglin parametricoptimizationofloadbearingelementsforcompositewingofanunmannedaerialvehicle AT tatarnikovoleg parametricoptimizationofloadbearingelementsforcompositewingofanunmannedaerialvehicle AT aungphyowai parametricoptimizationofloadbearingelementsforcompositewingofanunmannedaerialvehicle
_version_	1718441765190500352

Parametric Optimization of Load Bearing Elements for Composite Wing of an Unmanned Aerial Vehicle

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