Add to ORKGThe article presents details of a URANS simulation of the flow field near a hovering model of the Caradonna and Tung (1981) helicopter rotor [1]. The CFD code SPARC [2] proves to be capable of capturing the aerodynamics of a two-bladed rotor in high-speed transonic hover conditions. A comparison of the simulation results with the experimental data is acceptable, hence the described methodology might be used with confidence in future numerical studies of application of noise-reducing devices on helicopter blades
Two mathematical models are used in this work to estimate the acoustics of a hovering main rotor. Th...
The flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains ma...
Two numerical methods (the DLR code FLOWer and the ONERA code CANARI), based on the resolution of th...
Abstract: The article presents details of a URANS simulation of the flow field near a hovering model...
Hover computations were undertaken for a helicopter model rotor using Computational Fluid Dynamics (...
Reynolds-averaged thin-layer compressible Navier-Stokes steady simulations are presented for the Car...
The flow around rotor is numerical simulated in hover and forward flight based on multi-structured g...
In this paper, helicopter rotor blades are analysed in hover using computational fluid dynamics (CFD...
The computation of rotor flowfields is a challenging problem in theoretical aerodynamics and essent...
Abstract: Aerodynamic characteristics of a 5-seater helicopter with different rotor configuration (i...
The article presents results of simulations concerning possibilities of rotorcraft performance enhan...
A computational fluid dynamics model of a hovering helicopter main rotor is developed to examine air...
A study was performed with the objective of predicting the time-varying flow in the vicinity of a he...
This paper presents the results from an experimental study of the aerodynamic performance and effici...
This article presents a comparative study of three numerical algorithms for computation of the flow-...
Two mathematical models are used in this work to estimate the acoustics of a hovering main rotor. Th...
The flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains ma...
Two numerical methods (the DLR code FLOWer and the ONERA code CANARI), based on the resolution of th...
Abstract: The article presents details of a URANS simulation of the flow field near a hovering model...
Hover computations were undertaken for a helicopter model rotor using Computational Fluid Dynamics (...
Reynolds-averaged thin-layer compressible Navier-Stokes steady simulations are presented for the Car...
The flow around rotor is numerical simulated in hover and forward flight based on multi-structured g...
In this paper, helicopter rotor blades are analysed in hover using computational fluid dynamics (CFD...
The computation of rotor flowfields is a challenging problem in theoretical aerodynamics and essent...
Abstract: Aerodynamic characteristics of a 5-seater helicopter with different rotor configuration (i...
The article presents results of simulations concerning possibilities of rotorcraft performance enhan...
A computational fluid dynamics model of a hovering helicopter main rotor is developed to examine air...
A study was performed with the objective of predicting the time-varying flow in the vicinity of a he...
This paper presents the results from an experimental study of the aerodynamic performance and effici...
This article presents a comparative study of three numerical algorithms for computation of the flow-...
Two mathematical models are used in this work to estimate the acoustics of a hovering main rotor. Th...
The flowfield around a helicopter rotor in forward flight is intrinsically unsteady and contains ma...
Two numerical methods (the DLR code FLOWer and the ONERA code CANARI), based on the resolution of th...