Analyse aéroélastique d'une pale flexible composite : application au microdrone

Analyse aéroélastique d'une pale flexible composite : application au microdrone

The vision driving the work reported herein is to investigate the fluid-structure interac-tion (FSI) effects of the flexible laminated blades for tilt-body micro-air-vehicles (MAV)proprotors in hover and forward flight configurations. This is in order to exploit the po-tential of flexible-bladed pro...

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Bibliographic Details
Main Author: Mohd Zawawi, Fazila
Other Authors: Toulouse, ISAE
Language:en
Published: 2014
Subjects:
Micros-Trottoirs
Fluide-Structure-Itération
Anisotrope laminé composite
Faible nombre de Reynolds
Micro-Proprotor
Fluid-Scture-Itérationtructure-Interation (FSI)
Anisotropic Laminate Composite
Low Reynolds Number
629.4
Online Access:http://www.theses.fr/2014ESAE0027/document

Internet

http://www.theses.fr/2014ESAE0027/document

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