Exploring the Detached-Eddy Simulation for Main Rotor Flows

F. Dehaeze; G. N. Barakos; A. N. Kusyumov; S. A. Kusyumov; S. A. Mikhailov

doi:10.3103/S1068799818010063

Exploring the Detached-Eddy Simulation for Main Rotor Flows

Authors: Dehaeze F.¹, Barakos G.N.¹, Kusyumov A.N.², Kusyumov S.A.², Mikhailov S.A.²
Affiliations:
1. University of Glasgow, Glasgow G12 8QQ
2. Tupolev Kazan National Research Technical University, ul. Karla Marksa 10
Issue: Vol 61, No 1 (2018)
Pages: 37-44
Section: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
URL: https://journals.rcsi.science/1068-7998/article/view/230392
DOI: https://doi.org/10.3103/S1068799818010063
ID: 230392

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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.