The helicopter main rotor in forward flight is considered in this paper. The results for rigid blades and elastic blades are compared by the method of coupled simulation. The influence of the structural damping coefficient on the blade in-flight deformation is also considered
The article considers the problem of the flow around the helicopter main rotor taking into account b...
A framework is described and demonstrated for CFD analysis of helicopter rotors in hover and forward...
Abstract: Aerodynamic characteristics of a 5-seater helicopter with different rotor configuration (i...
The helicopter main rotor in forward flight is considered in this paper. The results for rigid blade...
A loosely coupled simulation is presented for a helicopter rotor in forward flight. The aeromechanic...
This paper presents a combination of an analysis between a computational structural dynamics (CSD) a...
This work presents a computational study of the aerodynamic interactions that arise between the comp...
This thesis is devoted to the study of rotor flows. A literature survey suggested that possible impr...
State-of-the-art helicopter rotor simulations reveal that the prediction accuracy of aerodynamic and...
A weak coupling procedure for coupling the rotor simulation code S4 and the Euler/Navier-Stokes solv...
In this paper, helicopter rotor blades are analysed in hover using computational fluid dynamics (CFD...
Results of calculation of the helicopter main rotor loads and deformations of rotor blades are prese...
Coupled fluid-structure simulations of high fidelity tools enable an accurate prediction of the aero...
Blade-vortex interaction (BVI) is one of the main sources of noise and vibrations in helicopters. Th...
A weak coupling procedure for coupling the rotor simulation code S4 and the Euler/Navier-Stokes solv...
The article considers the problem of the flow around the helicopter main rotor taking into account b...
A framework is described and demonstrated for CFD analysis of helicopter rotors in hover and forward...
Abstract: Aerodynamic characteristics of a 5-seater helicopter with different rotor configuration (i...
The helicopter main rotor in forward flight is considered in this paper. The results for rigid blade...
A loosely coupled simulation is presented for a helicopter rotor in forward flight. The aeromechanic...
This paper presents a combination of an analysis between a computational structural dynamics (CSD) a...
This work presents a computational study of the aerodynamic interactions that arise between the comp...
This thesis is devoted to the study of rotor flows. A literature survey suggested that possible impr...
State-of-the-art helicopter rotor simulations reveal that the prediction accuracy of aerodynamic and...
A weak coupling procedure for coupling the rotor simulation code S4 and the Euler/Navier-Stokes solv...
In this paper, helicopter rotor blades are analysed in hover using computational fluid dynamics (CFD...
Results of calculation of the helicopter main rotor loads and deformations of rotor blades are prese...
Coupled fluid-structure simulations of high fidelity tools enable an accurate prediction of the aero...
Blade-vortex interaction (BVI) is one of the main sources of noise and vibrations in helicopters. Th...
A weak coupling procedure for coupling the rotor simulation code S4 and the Euler/Navier-Stokes solv...
The article considers the problem of the flow around the helicopter main rotor taking into account b...
A framework is described and demonstrated for CFD analysis of helicopter rotors in hover and forward...
Abstract: Aerodynamic characteristics of a 5-seater helicopter with different rotor configuration (i...
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