Abstract: A simple method is presented for the creation of vorticity from a solid boundary in the form of discrete vortex blobs. These vortices have uniform-vorticity cores and are released from a number of points distributed around the body surface at a small distance away from the surface. Their strengths are obtained by satisfying the no-slip condition at the midpoints of the corresponding vortex sheets. The dynamics of these vortices is then considered by including the effect of viscous diffusion by random walk approach. The method is applied to the starting flow past a circular cylinder. A detailed parametric study shows that viscosity has the most significant effect on the computed results and, in order to obtain meaningful results, i...
Abstract: The vortex particle method is an easy and attractive tool to analyze flow phenomena by inv...
Vortex methods use a Lagrangian (particle based) approach to flow simulation by concentrating on the...
A vortex method has been developed at the Department of Aerospace Engineering, University of Glasgo...
A simple method is presented for the creation of vorticity from a solid boundary in the form of disc...
A simple method is presented for the creation of vorticity from a solid boundary in the form of disc...
The viscous, incompressible and laminar flow around bluff bodies is analysed via a random vortex met...
Incompressible, viscous, two-dimensional unsteady flows over bluff bodies are simulated via the use ...
A Discrete Vortex Method has been developed at the Department of Aerospace Engineering, University ...
Bluff body flows controlled in various manners are simulated with a high-resolution, gridless vortex...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
In this thesis a parallel discrete vortex method is developed in order to investigate the long-time ...
Vortex methods offer an alternative way for the numerical simulation of problems regarding incompres...
THESIS 6795The random vortex method is a Lagrangian technique which involves solving the stream func...
This report presents details of a new mathematical model of viscous, incompressible, unsteady flow ...
The discrete vortex method has certain advantages over its counterparts, namely, finite difference, ...
Abstract: The vortex particle method is an easy and attractive tool to analyze flow phenomena by inv...
Vortex methods use a Lagrangian (particle based) approach to flow simulation by concentrating on the...
A vortex method has been developed at the Department of Aerospace Engineering, University of Glasgo...
A simple method is presented for the creation of vorticity from a solid boundary in the form of disc...
A simple method is presented for the creation of vorticity from a solid boundary in the form of disc...
The viscous, incompressible and laminar flow around bluff bodies is analysed via a random vortex met...
Incompressible, viscous, two-dimensional unsteady flows over bluff bodies are simulated via the use ...
A Discrete Vortex Method has been developed at the Department of Aerospace Engineering, University ...
Bluff body flows controlled in various manners are simulated with a high-resolution, gridless vortex...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
In this thesis a parallel discrete vortex method is developed in order to investigate the long-time ...
Vortex methods offer an alternative way for the numerical simulation of problems regarding incompres...
THESIS 6795The random vortex method is a Lagrangian technique which involves solving the stream func...
This report presents details of a new mathematical model of viscous, incompressible, unsteady flow ...
The discrete vortex method has certain advantages over its counterparts, namely, finite difference, ...
Abstract: The vortex particle method is an easy and attractive tool to analyze flow phenomena by inv...
Vortex methods use a Lagrangian (particle based) approach to flow simulation by concentrating on the...
A vortex method has been developed at the Department of Aerospace Engineering, University of Glasgo...