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

Internet

https://scindeks-clanci.ceon.rs/data/pdf/1820-0206/2016/1820-02061604052T.pdf

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