A Hybrid Non-Linear Unsteady Vortex Lattice-Vortex Particle Method for Rotor Blades Aerodynamic Simulations

A Hybrid Non-Linear Unsteady Vortex Lattice-Vortex Particle Method for Rotor Blades Aerodynamic Simulations

This study presents a hybrid non-linear unsteady vortex lattice method-vortex particle method (NL UVLM-VPM) to investigate the aerodynamics of rotor blades hovering in and out of ground effect. The method is of interest for the fast aerodynamic prediction of helicopter and smaller rotor blades. UVLM...

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Bibliographic Details
Main Authors: Vincent Proulx-Cabana, Minh Tuan Nguyen, Sebastien Prothin, Guilhem Michon, Eric Laurendeau
Format: Article
Language:English
Published: MDPI AG 2022-02-01
Series:Fluids
Subjects:
unsteady vortex lattice method
Lagrangian method
vortex particle method
large eddy simulation
non-linear viscous-inviscid coupling
helicopter aerodynamics
Online Access:https://www.mdpi.com/2311-5521/7/2/81

Internet

https://www.mdpi.com/2311-5521/7/2/81

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