A VORTEX MODEL OF A HELICOPTER ROTOR

A vortex model of a helicopter rotor is presented. Each blade of the rotor has three degrees of freedom: flapping, lagging and feathering. The motions after each degree of freedom are also known for all blades. The blade is modelled as a thin vortex surface. The wakes are free fluid surfaces. A syst...

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Bibliographic Details
Main Author: Valentin BUTOESCU
Format: Artigo
Language:Inglês
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2009-06-01
Series:INCAS Bulletin
Online Access:http://bulletin.incas.ro/files/valentin_butoescu_v1no1_full.pdf
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