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
State-of-the-art helicopter rotor simulations reveal that the prediction accuracy of aerodynamic and...
Actuator Disks (AD) can provide characterizations of rotor wakes while reducing computational expens...
In this work Computational Fluid Dynamics is used as a tool for rotor outwash evaluation. The paper ...
This thesis is devoted to the study of rotor flows. A literature survey suggested that possible impr...
The helicopter main rotor in forward flight is considered in this paper. The results for rigid blade...
The flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains ma...
This paper presents numerical simulations of different rotor designs using high-fidelity CFD method...
The effect of turbulence models in the off-body grids on the accuracy of solutions for rotor flows i...
http://e-university.tu-sofia.bg/e-publ/files/882_BulTrans_12_Velkova.pdfThe aim of the computational...
This study presents the outcomes of a series of computational fluid dynamics analyses conducted to o...
AbstractA hybrid Euler/full potential/Lagrangian wake method, based on single-blade simulation, for ...
The presented work is dedicated to the numerical study of the aerodynamic characteristics of the hel...
An overset grid thin-layer Navier-Stokes code has been extended to include dynamic motion of helicop...
http://e-university.tu-sofia.bg/e-publ/files/882_BulTrans_12_Velkova.pdfInternational audienceThe ai...
Detached-Eddy Simulation (DES) is a hybrid turbulence modeling strategy, combining Reynolds-Averaged...
State-of-the-art helicopter rotor simulations reveal that the prediction accuracy of aerodynamic and...
Actuator Disks (AD) can provide characterizations of rotor wakes while reducing computational expens...
In this work Computational Fluid Dynamics is used as a tool for rotor outwash evaluation. The paper ...
This thesis is devoted to the study of rotor flows. A literature survey suggested that possible impr...
The helicopter main rotor in forward flight is considered in this paper. The results for rigid blade...
The flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains ma...
This paper presents numerical simulations of different rotor designs using high-fidelity CFD method...
The effect of turbulence models in the off-body grids on the accuracy of solutions for rotor flows i...
http://e-university.tu-sofia.bg/e-publ/files/882_BulTrans_12_Velkova.pdfThe aim of the computational...
This study presents the outcomes of a series of computational fluid dynamics analyses conducted to o...
AbstractA hybrid Euler/full potential/Lagrangian wake method, based on single-blade simulation, for ...
The presented work is dedicated to the numerical study of the aerodynamic characteristics of the hel...
An overset grid thin-layer Navier-Stokes code has been extended to include dynamic motion of helicop...
http://e-university.tu-sofia.bg/e-publ/files/882_BulTrans_12_Velkova.pdfInternational audienceThe ai...
Detached-Eddy Simulation (DES) is a hybrid turbulence modeling strategy, combining Reynolds-Averaged...
State-of-the-art helicopter rotor simulations reveal that the prediction accuracy of aerodynamic and...
Actuator Disks (AD) can provide characterizations of rotor wakes while reducing computational expens...
In this work Computational Fluid Dynamics is used as a tool for rotor outwash evaluation. The paper ...
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