We present the coupling of a vortex particle-mesh method with immersed lifting lines. The method relies on the Lagrangian discretization of the Navier-Stokes equations in vorticity- velocity formulation. Advection is handled by the particles while the mesh allows the evaluation of the differential operators and the use of fast Poisson solvers. We use a Fourier-based fast Poisson solver which simultaneously allows unbounded directions and inlet/outlet boundaries. A lifting line approach models the vorticity sources in the flow. Its immersed treatment efficiently captures the development of vorticity from thin sheets into a three-dimensional field. We apply this approach to the simulation of a wind turbine wake at very high Reynolds number. T...
The efficiency of a wind turbine depends largely on the wake of the upstream turbine. Seeking to con...
The aerodynamics of Vertical Axis Wind Turbines (VAWTs) is inherently unsteady, which leads to vorti...
We present the Direct Numerical Simulations of high Reynolds numbers aircraft wakes employing vortex...
We present the coupling of a vortex particle-mesh method with immersed lifting lines. The method rel...
AbstractWe present the treatment of lifting lines with a Vortex Particle-Mesh (VPM) methodology. The...
A Vortex Particle-Mesh (VPM) method with immersed lifting lines has been developed and validated. Th...
A Vortex Particle-Mesh (VPM) method with immersed lifting lines has been developed and validated. Ba...
A vortex particle-mesh (VPM) method with immersed lifting lines has been developed and validated. B...
The numerical study of the wake of full-scale slender devices such as aircraft wings and wind turbin...
A Vortex Particle-Mesh (VPM) method with immersed lifting lines (ILL) has been developed and validat...
This talk provides a brief introduction to vortex methods and specifically, their state-of-the-art v...
The present work joins a global effort in the development of efficient and accurate numerical tools ...
A method for the treatment of the evolution of the wake ofaerodynamic bodies has been implemented. A...
Recent development of a multi-dimensional upwind-based finite volume scheme for the vorticity transp...
Midway between a vortex method and a grid-based CFD, the Vortex Particle-Mesh method with Immersed L...
The efficiency of a wind turbine depends largely on the wake of the upstream turbine. Seeking to con...
The aerodynamics of Vertical Axis Wind Turbines (VAWTs) is inherently unsteady, which leads to vorti...
We present the Direct Numerical Simulations of high Reynolds numbers aircraft wakes employing vortex...
We present the coupling of a vortex particle-mesh method with immersed lifting lines. The method rel...
AbstractWe present the treatment of lifting lines with a Vortex Particle-Mesh (VPM) methodology. The...
A Vortex Particle-Mesh (VPM) method with immersed lifting lines has been developed and validated. Th...
A Vortex Particle-Mesh (VPM) method with immersed lifting lines has been developed and validated. Ba...
A vortex particle-mesh (VPM) method with immersed lifting lines has been developed and validated. B...
The numerical study of the wake of full-scale slender devices such as aircraft wings and wind turbin...
A Vortex Particle-Mesh (VPM) method with immersed lifting lines (ILL) has been developed and validat...
This talk provides a brief introduction to vortex methods and specifically, their state-of-the-art v...
The present work joins a global effort in the development of efficient and accurate numerical tools ...
A method for the treatment of the evolution of the wake ofaerodynamic bodies has been implemented. A...
Recent development of a multi-dimensional upwind-based finite volume scheme for the vorticity transp...
Midway between a vortex method and a grid-based CFD, the Vortex Particle-Mesh method with Immersed L...
The efficiency of a wind turbine depends largely on the wake of the upstream turbine. Seeking to con...
The aerodynamics of Vertical Axis Wind Turbines (VAWTs) is inherently unsteady, which leads to vorti...
We present the Direct Numerical Simulations of high Reynolds numbers aircraft wakes employing vortex...