Aerodynamic optimization of a VTOL drone using winglets

In this work, an aerodynamic optimization of a VTOL drone wing has been carried out by implementing winglets. A dual methodology has been used employing a CFD study with the open source code OpenFOAM and applying the Vortex Lattice Method with the open source tool XFLR5 for different configurations...

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Main Authors: Marina Prieto, Mara S. Escarti-Guillem, Sergio Hoyas
Format: Article
Language:English
Published: Elsevier 2023-03-01
Series:Results in Engineering
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2590123022005254
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author Marina Prieto
Mara S. Escarti-Guillem
Sergio Hoyas
author_facet Marina Prieto
Mara S. Escarti-Guillem
Sergio Hoyas
author_sort Marina Prieto
collection DOAJ
description In this work, an aerodynamic optimization of a VTOL drone wing has been carried out by implementing winglets. A dual methodology has been used employing a CFD study with the open source code OpenFOAM and applying the Vortex Lattice Method with the open source tool XFLR5 for different configurations and wingtips: the original wing, raked wingtips, and blended winglets. A comparison between the two software has been conducted to determine the validity of XFLR5 and to quantify the error in calculating the aerodynamic coefficients and the bending moment. XFLR5 offers the same trends as RANS at a fraction of the cost, allowing the use of XFLR5 for the first stages of design.
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spelling doaj.art-79a341c61694498eb514eadb1f00baab2023-01-05T04:32:37ZengElsevierResults in Engineering2590-12302023-03-0117100855Aerodynamic optimization of a VTOL drone using wingletsMarina Prieto0Mara S. Escarti-Guillem1Sergio Hoyas2Instituto Universitario de Matemática Pura y Aplicada, Universitat Politècnica de València, 46022, Valencia, SpainInstituto Universitario de Matemática Pura y Aplicada, Universitat Politècnica de València, 46022, Valencia, Spain; Comet Ingeniería, Convento Carmelitas, 2, 46010, Valencia, SpainInstituto Universitario de Matemática Pura y Aplicada, Universitat Politècnica de València, 46022, Valencia, Spain; Corresponding author.In this work, an aerodynamic optimization of a VTOL drone wing has been carried out by implementing winglets. A dual methodology has been used employing a CFD study with the open source code OpenFOAM and applying the Vortex Lattice Method with the open source tool XFLR5 for different configurations and wingtips: the original wing, raked wingtips, and blended winglets. A comparison between the two software has been conducted to determine the validity of XFLR5 and to quantify the error in calculating the aerodynamic coefficients and the bending moment. XFLR5 offers the same trends as RANS at a fraction of the cost, allowing the use of XFLR5 for the first stages of design.http://www.sciencedirect.com/science/article/pii/S2590123022005254CFDUAVAerodynamicsWingletVLM
spellingShingle Marina Prieto
Mara S. Escarti-Guillem
Sergio Hoyas
Aerodynamic optimization of a VTOL drone using winglets
Results in Engineering
CFD
UAV
Aerodynamics
Winglet
VLM
title Aerodynamic optimization of a VTOL drone using winglets
title_full Aerodynamic optimization of a VTOL drone using winglets
title_fullStr Aerodynamic optimization of a VTOL drone using winglets
title_full_unstemmed Aerodynamic optimization of a VTOL drone using winglets
title_short Aerodynamic optimization of a VTOL drone using winglets
title_sort aerodynamic optimization of a vtol drone using winglets
topic CFD
UAV
Aerodynamics
Winglet
VLM
url http://www.sciencedirect.com/science/article/pii/S2590123022005254
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AT marasescartiguillem aerodynamicoptimizationofavtoldroneusingwinglets
AT sergiohoyas aerodynamicoptimizationofavtoldroneusingwinglets