Flutter margin with non-linearities: real-time prediction of flutter onset speed

Casado Corpas, José and López Díez, Jesús (2008). Flutter margin with non-linearities: real-time prediction of flutter onset speed. "Journal of Aerospace Engineering", v. 222 (n. 6); pp. 921-929. ISSN 0954-4100. https://doi.org/10.1243/09544100JAERO251.

Descripción

Título: Flutter margin with non-linearities: real-time prediction of flutter onset speed
Autor/es:
  • Casado Corpas, José
  • López Díez, Jesús
Tipo de Documento: Artículo
Título de Revista/Publicación: Journal of Aerospace Engineering
Fecha: 1 Junio 2008
ISSN: 0954-4100
Volumen: 222
Número: 6
Materias:
ODS:
Palabras Clave Informales: flutter margin, non-linear, flight test
Escuela: E.T.S.I. Aeronáuticos (UPM) [antigua denominación]
Departamento: Materiales y Producción Aeroespacial
Licencias Creative Commons: Reconocimiento - Sin obra derivada - No comercial

Texto completo

[thumbnail of INVE_MEM_2008_155931.pdf]
Vista Previa
PDF (Portable Document Format) - Se necesita un visor de ficheros PDF, como GSview, Xpdf o Adobe Acrobat Reader
Descargar (662kB) | Vista Previa

Resumen

The present article shows a procedure to predict the flutter speed based on real-time tuning of a quasi non-linear aeroelastic model. A two-dimensional non-linear (freeplay) aeroeslastic model is implemented inMatLab/Simulink with incompressible aerodynamic conditions. A comparison with real compressible conditions is provided. Once the numerical validation is accomplished, a parametric aeroelastic model is built in order to describe the proposed procedure and contribute to reduce the number of flight hours needed to expand the flutter envelope.

Más información

ID de Registro: 22554
Identificador DC: https://oa.upm.es/22554/
Identificador OAI: oai:oa.upm.es:22554
URL Portal Científico: https://portalcientifico.upm.es/es/ipublic/item/5483228
Identificador DOI: 10.1243/09544100JAERO251
URL Oficial: http://pig.sagepub.com/content/222/6/921
Depositado por: Memoria Investigacion
Depositado el: 27 Mar 2014 14:43
Ultima Modificación: 12 Nov 2025 00:00