Add to ORKGIn this collaborative work, an unstructured grid generation technique, based upon the Delaunay triangulation, has been combined with an upwind kinetic flux vector splitting high resolution flow algorithm to simulate inviscid compressible flows for aeronautical applications
A method for simulating two-dimensional, high-Reynolds-number, compressible flows about complex geom...
Steady and unsteady flowfields around an airfoil are simulated numerically using a compressible Navi...
A simple and efficient dynamic grid deformation technique is proposed for computing unsteady flow pr...
In this collaborative work, an unstructured grid generation technique, based upon the Delaunay trian...
Abstract:-The unsteady and inviscid compressible flow around a circular cylinder and airfoil has bee...
The paper describes a solver for the compressible inviscid flow equations which is based on a flux v...
An upwinding flux difference splitting method has been used to solve the Euler equations for compre...
A method of efficiently computing turbulent compressible flow over complex two-dimensional configura...
The inviscid flow over a Williams two element airfoil (configuration A) is computed using an Euler c...
In this paper we present the work on the latest developments of a grid free method for computing inv...
Computational Fluid Dynamics is beginning to play a major role in the design of aerospace vehicles. ...
A grid generation and flow solution algorithm for the Euler equations on unstructured grids is prese...
This document contains a detailed review of works performed at INRIA related to the MUSCL-FEM upwind...
The application of an unstructured grid methodology on a three-dimensional high-lift configuration i...
The overall objective of the research carried out over the last two years was the development of new...
A method for simulating two-dimensional, high-Reynolds-number, compressible flows about complex geom...
Steady and unsteady flowfields around an airfoil are simulated numerically using a compressible Navi...
A simple and efficient dynamic grid deformation technique is proposed for computing unsteady flow pr...
In this collaborative work, an unstructured grid generation technique, based upon the Delaunay trian...
Abstract:-The unsteady and inviscid compressible flow around a circular cylinder and airfoil has bee...
The paper describes a solver for the compressible inviscid flow equations which is based on a flux v...
An upwinding flux difference splitting method has been used to solve the Euler equations for compre...
A method of efficiently computing turbulent compressible flow over complex two-dimensional configura...
The inviscid flow over a Williams two element airfoil (configuration A) is computed using an Euler c...
In this paper we present the work on the latest developments of a grid free method for computing inv...
Computational Fluid Dynamics is beginning to play a major role in the design of aerospace vehicles. ...
A grid generation and flow solution algorithm for the Euler equations on unstructured grids is prese...
This document contains a detailed review of works performed at INRIA related to the MUSCL-FEM upwind...
The application of an unstructured grid methodology on a three-dimensional high-lift configuration i...
The overall objective of the research carried out over the last two years was the development of new...
A method for simulating two-dimensional, high-Reynolds-number, compressible flows about complex geom...
Steady and unsteady flowfields around an airfoil are simulated numerically using a compressible Navi...
A simple and efficient dynamic grid deformation technique is proposed for computing unsteady flow pr...