This paper presents an analysis of the scalability and efficiency of a simulation framework based on the Vortex Particle Method (VPM). The code is applied for the numerical aerodynamic analysis of line-like structures. The numerical code runs on multicore CPU and GPU architectures using OpenCL framework. The focus of this paper is the analysis of the parallel efficiency and scalability of the method being applied to an engineering test case, namely the aero-elastic response of a long-span bridge girder. The target is to assess the optimal configuration and the required computer architecture, such that it becomes feasible to efficiently utilize the method within the computational resources available for a regular engineering office. The simulations a...
The authors present an accelerated aerodynamic computational model derived from the integration of t...
A method for the treatment of the evolution of the wake ofaerodynamic bodies has been implemented. A...
The accurate representation of aerodynamic forces is essential for a safe, yet reasonable design of ...
AbstractThe implementations of 2D vortex element method adapted to different types of parallel compu...
We present Vortex Methods implemented in massively parallel computer architectures for the Direct Nu...
We present Vortex Methods implemented in massively parallel computer architectures for the Direct Nu...
International audienceWe present a GPU accelerated solver for simulations of bluff body flows in 2D ...
The efficiency of a wind turbine depends largely on the wake of the upstream turbine. Seeking to con...
A novel parallel computing method for computational fluid dynamics research in engineering is presen...
International audienceThe study detailed in this paper aims to provide a solver able to simulate of ...
We develop a fast, user-friendly implementation of a potential flow solver based on the unsteady vor...
A parallel finite-volume CFD algorithm for modeling of incompressible flows on hybrid supercomputers...
A fast parallel oct-tree code originally developed for three-dimensional N-body gravitational simula...
[[abstract]]©1997 John Wiley & Sons-This paper addressed the implementation of vortex filament metho...
[[abstract]]This paper addressed the implementation of vortex filament methods on parallel machines ...
The authors present an accelerated aerodynamic computational model derived from the integration of t...
A method for the treatment of the evolution of the wake ofaerodynamic bodies has been implemented. A...
The accurate representation of aerodynamic forces is essential for a safe, yet reasonable design of ...
AbstractThe implementations of 2D vortex element method adapted to different types of parallel compu...
We present Vortex Methods implemented in massively parallel computer architectures for the Direct Nu...
We present Vortex Methods implemented in massively parallel computer architectures for the Direct Nu...
International audienceWe present a GPU accelerated solver for simulations of bluff body flows in 2D ...
The efficiency of a wind turbine depends largely on the wake of the upstream turbine. Seeking to con...
A novel parallel computing method for computational fluid dynamics research in engineering is presen...
International audienceThe study detailed in this paper aims to provide a solver able to simulate of ...
We develop a fast, user-friendly implementation of a potential flow solver based on the unsteady vor...
A parallel finite-volume CFD algorithm for modeling of incompressible flows on hybrid supercomputers...
A fast parallel oct-tree code originally developed for three-dimensional N-body gravitational simula...
[[abstract]]©1997 John Wiley & Sons-This paper addressed the implementation of vortex filament metho...
[[abstract]]This paper addressed the implementation of vortex filament methods on parallel machines ...
The authors present an accelerated aerodynamic computational model derived from the integration of t...
A method for the treatment of the evolution of the wake ofaerodynamic bodies has been implemented. A...
The accurate representation of aerodynamic forces is essential for a safe, yet reasonable design of ...