Computational analysis of helicopter main rotor blades in ground effect

Computational analysis of helicopter main rotor blades in ground effect

Numerical investigation of an isolated representative helicopter main rotor has been performed in ANSYS FLUENT 16.2. In general, flow field around the rotor is unsteady, three-dimensional, complex and vortical. Such a simulation requires substantial computational resources. Ground effect, which impr...

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Bibliographic Details
Main Authors:	Trivković Zorana, Svorcan Jelena, Baltić Marija, Komarov Dragan, Fotev Vasko
Format:	Article
Language:	English
Published:	Military Technical Institute, Belgrade 2016-01-01
Series:	Scientific Technical Review
Subjects:	helicopter helicopter rotor blades flow field navier-stokes equations reynolds number aerodynamic coefficients ground effect
Online Access:	https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2016/1820-02061604052T.pdf

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