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ORCID: https://orcid.org/0000-0002-1690-1634, Sanz Andres, Angel Pedro
ORCID: https://orcid.org/0000-0001-5890-6065 and Barrero Gil, Antonio
ORCID: https://orcid.org/0000-0002-3509-5076
(2010).
A panel method free-wake code for aeroelastic rotor predictions.
"Wind Energy", v. 13
(n. 4);
pp. 357-371.
ISSN 1095-4244.
https://doi.org/10.1002/we.358.
| Título: | A panel method free-wake code for aeroelastic rotor predictions |
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| Autor/es: |
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| Tipo de Documento: | Artículo |
| Título de Revista/Publicación: | Wind Energy |
| Fecha: | Mayo 2010 |
| ISSN: | 1095-4244 |
| Volumen: | 13 |
| Número: | 4 |
| Materias: | |
| ODS: | |
| Escuela: | E.U.I.T. Aeronáutica (UPM) [antigua denominación] |
| Departamento: | Vehículos Aeroespaciales [hasta 2014] |
| Licencias Creative Commons: | Reconocimiento - Sin obra derivada - No comercial |
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A panel method free-wake model to analyse the rotor flapping is presented. The aerodynamic model consists of a panel method, which takes into account the three-dimensional rotor geometry, and a free-wake model, to determine the wake shape. The main features of the model are the wake division into a near-wake sheet and a far wake represented by a single tip vortex, and the modification of the panel method formulation to take into account this particular wake description. The blades are considered rigid with a flap degree of freedom. The problem solution is approached using a relaxation method, which enforces periodic boundary conditions. Finally, several code validations against helicopter and wind turbine experimental data are performed, showing good agreement
| ID de Registro: | 39626 |
|---|---|
| Identificador DC: | https://oa.upm.es/39626/ |
| Identificador OAI: | oai:oa.upm.es:39626 |
| URL Portal Científico: | https://portalcientifico.upm.es/es/ipublic/item/5484896 |
| Identificador DOI: | 10.1002/we.358 |
| URL Oficial: | http://onlinelibrary.wiley.com/doi/10.1002/we.358/... |
| Depositado por: | Biblioteca ETSI Aeronauticos |
| Depositado el: | 09 Mar 2016 11:45 |
| Ultima Modificación: | 12 Nov 2025 00:00 |
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