The Roe flux difference splitting method was extended to treat 2-D viscous flows with nonequilibrium chemistry. The derivations have avoided unnecessary assumptions or approximations. For spatial discretization, the second-order Roe upwind differencing is used for the convective terms and central differencing for the viscous terms. An upwind-based TVD scheme is applied to eliminate oscillations and obtain a sharp representation of discontinuities. A two-state Runge-Kutta method is used to time integrate the discretized Navier-Stokes and species transport equations for the asymptotic steady solutions. The present method is then applied to two types of flows: the shock wave/boundary layer interaction problems and the jet in cross flows
We present Numerical Viscosity Functions, or NVFs, for use with Riemann-problem based shock-capturin...
A flux splitting scheme is proposed for the general nonequilibrium flow equations with an aim at rem...
In this paper, a gas-kinetic solver is developed to solve Reynolds Averaged Navier-Stokes (RANS) equ...
A thin-layer Navier-Stokes has been developed for solving high Reynolds number, turbulent flows past...
An algorithm for laminar and turbulent viscous compressible two dimensional flows is presented. For ...
The viscous-shock-layer equations for hypersonic laminar and turbulent flows of radiating or nonradi...
Steady flow over the leading portion of a multicomponent airfoil section is studied using computatio...
Thin-Layer Navier-Stokes equations in generalized body-fitted coordinate system and non-dimensional ...
An approach is described to decouple the species continuity equations from the mixture continuity, m...
A single step second-order accurate flux-difference-splitting method has been developed for solving ...
The use of a new splitting scheme, the advection upstream splitting method, for model aerodynamic pr...
Under this grant, two numerical algorithms were developed to predict the flow of viscous, hypersonic...
This paper describes the development of a gas-kinetic solver to compute laminar viscous flows in two...
Ce travail de thèse porte sur le simulation d’écoulements diphasiques compressibles, visqueux et con...
This effort investigates the accuracy of some flux-split algorithms in high-speed viscous flows. Thr...
We present Numerical Viscosity Functions, or NVFs, for use with Riemann-problem based shock-capturin...
A flux splitting scheme is proposed for the general nonequilibrium flow equations with an aim at rem...
In this paper, a gas-kinetic solver is developed to solve Reynolds Averaged Navier-Stokes (RANS) equ...
A thin-layer Navier-Stokes has been developed for solving high Reynolds number, turbulent flows past...
An algorithm for laminar and turbulent viscous compressible two dimensional flows is presented. For ...
The viscous-shock-layer equations for hypersonic laminar and turbulent flows of radiating or nonradi...
Steady flow over the leading portion of a multicomponent airfoil section is studied using computatio...
Thin-Layer Navier-Stokes equations in generalized body-fitted coordinate system and non-dimensional ...
An approach is described to decouple the species continuity equations from the mixture continuity, m...
A single step second-order accurate flux-difference-splitting method has been developed for solving ...
The use of a new splitting scheme, the advection upstream splitting method, for model aerodynamic pr...
Under this grant, two numerical algorithms were developed to predict the flow of viscous, hypersonic...
This paper describes the development of a gas-kinetic solver to compute laminar viscous flows in two...
Ce travail de thèse porte sur le simulation d’écoulements diphasiques compressibles, visqueux et con...
This effort investigates the accuracy of some flux-split algorithms in high-speed viscous flows. Thr...
We present Numerical Viscosity Functions, or NVFs, for use with Riemann-problem based shock-capturin...
A flux splitting scheme is proposed for the general nonequilibrium flow equations with an aim at rem...
In this paper, a gas-kinetic solver is developed to solve Reynolds Averaged Navier-Stokes (RANS) equ...