The paper describes a solver for the compressible inviscid flow equations which is based on a flux vector splitting strategy able to deal with chemical reaction effects. The methodology here adopted is based on a modification of the Flux Vector Splitting technique due to van Leer. 11 The scheme operates on completely unstructured grids and has been coupled with an adaptive remeshing procedure to compute high speed flows. Solutions for two-dimensional problems for non-reactive and reactive air in thermodynamic equilibrium are presented
Recent progress in flux vector splitting is reviewed with the aim to obtain high resolution and robu...
An upwinding flux difference splitting method has been used to solve the Euler equations for compre...
The numerical simulation of hypersonic reacting 3D flows is one of the key tools for the design of r...
The paper describes a solver for the compressible inviscid flow equations which is based on a flux v...
A method for computing inviscid hypersonic flow over complex configurations using unstructured meshe...
A method for computing inviscid hypersonic flow over complex configurations using unstructured meshe...
Several flux-splitting methods for the inviscid terms of the compressible-flow equations are derived...
An unstructured grid Euler solver for reactive compressible flow applications is presented. The meth...
A two-dimensional, axisymmetric, full Navier-Stokes solver has been developed with equilibrium and n...
A CFD solver, using Residual Distribution Schemes on unstructured grids, has been extended to deal w...
The synthesis of physical models for gas chemistry and turbulence from the structured grid codes LAU...
In this collaborative work, an unstructured grid generation technique, based upon the Delaunay trian...
Accurate and easy to handle simulation tools are needed for the design and development of future spa...
A novel high order compact scheme for solving the compressible Navier-Stokes equations has been deve...
Abstract: A comparison of five different spatial discretization schemes is performed considering a t...
Recent progress in flux vector splitting is reviewed with the aim to obtain high resolution and robu...
An upwinding flux difference splitting method has been used to solve the Euler equations for compre...
The numerical simulation of hypersonic reacting 3D flows is one of the key tools for the design of r...
The paper describes a solver for the compressible inviscid flow equations which is based on a flux v...
A method for computing inviscid hypersonic flow over complex configurations using unstructured meshe...
A method for computing inviscid hypersonic flow over complex configurations using unstructured meshe...
Several flux-splitting methods for the inviscid terms of the compressible-flow equations are derived...
An unstructured grid Euler solver for reactive compressible flow applications is presented. The meth...
A two-dimensional, axisymmetric, full Navier-Stokes solver has been developed with equilibrium and n...
A CFD solver, using Residual Distribution Schemes on unstructured grids, has been extended to deal w...
The synthesis of physical models for gas chemistry and turbulence from the structured grid codes LAU...
In this collaborative work, an unstructured grid generation technique, based upon the Delaunay trian...
Accurate and easy to handle simulation tools are needed for the design and development of future spa...
A novel high order compact scheme for solving the compressible Navier-Stokes equations has been deve...
Abstract: A comparison of five different spatial discretization schemes is performed considering a t...
Recent progress in flux vector splitting is reviewed with the aim to obtain high resolution and robu...
An upwinding flux difference splitting method has been used to solve the Euler equations for compre...
The numerical simulation of hypersonic reacting 3D flows is one of the key tools for the design of r...