Add to ORKGUnsteady turbulent transonic flows over oscillating airfoils are investigated by using a novel third-order accurate scheme on block-structured meshes. Two turbulence models ( algebraic and two-transport equation models) are studied in order to generate flow fields in agreement with experimental data. Numerical results are presented for 2-D problems related to helicopter rotors in forward flight, including shock-stall phenomena. The advantages of using a high-order accurate method and a suitable turbulence model for this kind of applications are demonstrated
Two dimensional quasi-three dimensional Navier-Stokes solvers were used to predict the static and dy...
Two dimensional problems are solved using numerical techniques. Navier-Stokes equations are studied ...
A numerical procedure is presented for computing the unsteady transonic flow field about three dimen...
A two-dimensional model of the aerodynamics of rotor blades in forward flight is proposed in which ...
International audienceThe prediction of shock-induced oscillations over transonic rigid airfoils is ...
Full seven-equation Reynolds stress turbulence models are promising tools for todays aerospace techn...
Unsteady flowfields of a two-dimensional oscillating airfoil are calculated using an implicit, finit...
This paper presents a description and verification of RVC3D (rotor viscous code 3-D) which provides ...
A finite-difference solution to the Navier-Stokes equations combined with a time-varying grid-genera...
In the last two decades there have been extensive developments in computational unsteady transonic a...
In recent years codes that use the Navier-Stokes equations to compute aerodynamic flows have evolved...
This paper concerns the implementation and evaluation of high-order reconstruction schemes for predi...
A code developed for simulating high Reynolds number transonic flow fields of arbitrary configuratio...
Employing the advection–diffusion–reaction equation as a model problem, a multiscale stable finite e...
A phase 2 research and development effort was conducted in area transonic, compressible, inviscid fl...
Two dimensional quasi-three dimensional Navier-Stokes solvers were used to predict the static and dy...
Two dimensional problems are solved using numerical techniques. Navier-Stokes equations are studied ...
A numerical procedure is presented for computing the unsteady transonic flow field about three dimen...
A two-dimensional model of the aerodynamics of rotor blades in forward flight is proposed in which ...
International audienceThe prediction of shock-induced oscillations over transonic rigid airfoils is ...
Full seven-equation Reynolds stress turbulence models are promising tools for todays aerospace techn...
Unsteady flowfields of a two-dimensional oscillating airfoil are calculated using an implicit, finit...
This paper presents a description and verification of RVC3D (rotor viscous code 3-D) which provides ...
A finite-difference solution to the Navier-Stokes equations combined with a time-varying grid-genera...
In the last two decades there have been extensive developments in computational unsteady transonic a...
In recent years codes that use the Navier-Stokes equations to compute aerodynamic flows have evolved...
This paper concerns the implementation and evaluation of high-order reconstruction schemes for predi...
A code developed for simulating high Reynolds number transonic flow fields of arbitrary configuratio...
Employing the advection–diffusion–reaction equation as a model problem, a multiscale stable finite e...
A phase 2 research and development effort was conducted in area transonic, compressible, inviscid fl...
Two dimensional quasi-three dimensional Navier-Stokes solvers were used to predict the static and dy...
Two dimensional problems are solved using numerical techniques. Navier-Stokes equations are studied ...
A numerical procedure is presented for computing the unsteady transonic flow field about three dimen...