Rapid Parametric CAx Tools for Modelling Morphing Wings of Micro Air Vehicles (MAVs)

Rodríguez Sevillano, Ángel Antonio ORCID: https://orcid.org/0000-0003-0685-3875, Casati Calzada, María Jesús ORCID: https://orcid.org/0000-0003-0893-4177, Bardera Mora, Rafael ORCID: https://orcid.org/0000-0002-5157-9935, Nieto Centenero, Javier, Matías García, Juan Carlos ORCID: https://orcid.org/0000-0001-6049-6421 and Barroso Barderas, Estela ORCID: https://orcid.org/0000-0001-6694-3990 (2023). Rapid Parametric CAx Tools for Modelling Morphing Wings of Micro Air Vehicles (MAVs). "Aerospace", v. 10 (n. 5); ISSN 22264310. https://doi.org/10.3390/aerospace10050467.

Descripción

Título: Rapid Parametric CAx Tools for Modelling Morphing Wings of Micro Air Vehicles (MAVs)
Autor/es:
Tipo de Documento: Artículo
Título de Revista/Publicación: Aerospace
Fecha: 17 Mayo 2023
ISSN: 22264310
Volumen: 10
Número: 5
Materias:
Palabras Clave Informales: airfoil parameterization; CST (class-shape transformation); micro air vehicles (MAVs); PythonOCC; airfoil parameterization; CST (class-shape transformation); Design; micro air vehicles (MAVs); Morphing wings; PythonOCC
Escuela: E.T.S. de Ingeniería Aeronáutica y del Espacio (UPM)
Departamento: Aeronaves y Vehículos Espaciales
Licencias Creative Commons: Reconocimiento - Sin obra derivada - No comercial

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Resumen

This paper shows a series of tools that help in the research of morphing micro air vehicles (MAVs). These tools are aimed at generating parametric CAD models of wings in a few seconds that can be used in aerodynamic studies, either via CFD directly using the model obtained or via wind tunnel through rapid prototyping with 3D printers. It also facilitates the analysis of morphing wings by allowing for the continuous parametric deformation of the airfoils and the wing geometry. In addition, one of the tools greatly simplifies the purely experimental design of this type of vehicle, allowing the transfer of experimental measurements to the computer, generating virtual models with the same deformation as the physical model. This software has two fundamental parts. The first one is the parameterization of the airfoils, for which the CST (Class-Shape Transformation) method will be used. CST coefficients can be modified according to the actuator variable that changes the wing geometry. The second part is the generation of a three-dimensional parametric model of the wing. We used OpenCASCADE technology in its Python version called PythonOCC, which enables the generation of geometries with good surface quality for typical and non-standard wing shapes. Finally, the use of this software for the study of a morphing aircraft will be shown, as well as improvements that could be incorporated in the future to increase its capabilities for the design and analysis of MAVs.

Más información

ID de Registro: 84980
Identificador DC: https://oa.upm.es/84980/
Identificador OAI: oai:oa.upm.es:84980
URL Portal Científico: https://portalcientifico.upm.es/es/ipublic/item/10083281
Identificador DOI: 10.3390/aerospace10050467
URL Oficial: https://www.mdpi.com/2226-4310/10/5/467
Depositado por: iMarina Portal Científico
Depositado el: 23 Nov 2024 20:13
Ultima Modificación: 03 Mar 2025 16:55