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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.
| Título: | Rapid Parametric CAx Tools for Modelling Morphing Wings of Micro Air Vehicles (MAVs) |
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| Autor/es: |
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| 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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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.
| ID de Registro: | 84980 |
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| 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 |
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