Abstract This paper applies the Detached-Eddy Simulation (DES) method to resolve a larger part of the flow spectrum around rotor blades in hover and forward flight. A comparison between DES and Unsteady Reynolds–Averaged Navier–Stokes simulation was carried out for the case of a forward flying rotor suggesting that DES has great potential for rotor applications.
Exploring the Detached-Eddy Simulation for Main Rotor Flows
Russian Aeronautics ; 61 , 1 ; 37-44
2018-01-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Exploring the Detached-Eddy Simulation for Main Rotor Flows
Online Contents | 2018
|Detached-Eddy-Simulation of Supersonic Jet Flows
AIAA | 2006
|Delayed Detached Eddy Simulation of Projectile Flows
AIAA | 2015
|Detached eddy simulation of massively separated flows
AIAA | 2001
|