Add to ORKGA family of high order accurate compact upwind difference operators have been used, together with the split fluxes of the KFVS (kinetic flux vector splitting) scheme to obtain high order semidis-cretizations of the 2D Euler equations of inviscid gas dynamics in general coordinates. A TVD multistage Rungex2013;Kutta time stepping scheme is used to compute steady states for selected transonic/supersonic flow problems which indicate the higher accuracy and suitlow13; diffusion realizable in such schemes
Kinetic Flux Vector Splitting (KFVS) has been extensively used to compute inviscid as well as viscou...
Many problems arising in the aerodynamic design of aerospace vehicles require the numerical solution...
A global fourth-order solution method that incorporates compact differencing with Roe\u27s approxima...
A family of high order accurate compact upwind difference operators have been used, together with th...
Third order compact upwind operators have been used together with the split fluxes of the KFVS (Kine...
A compact upwind difference operator is used to generate formally third order accurate spatial discr...
This paper is mainly concerned with the development of a class of new upwind methods and a novel tre...
This paper is mainly concerned with the development of a class of new upwind methods and a novel tre...
In the present paper we consider second order compact upwind schemes with a space split time derivat...
A family of compact upwind schemes with formal orders of accuracy 3 to 5 have been developed. Flux l...
In the present paper we consider second order compact upwind schemes with a space split time derivat...
A comparative study of the performance of commonly used, TVD or non-7VD second order accurate numeri...
A comparative study of five upwind schemes was performed to evaluate their ability accurately model ...
A new upwind Boltzmann scheme termed peculiar velocity based Upwind (PVU) method is developed for so...
This thesis presents and verifies a numerical method for solving the compressible Euler equations. T...
Kinetic Flux Vector Splitting (KFVS) has been extensively used to compute inviscid as well as viscou...
Many problems arising in the aerodynamic design of aerospace vehicles require the numerical solution...
A global fourth-order solution method that incorporates compact differencing with Roe\u27s approxima...
A family of high order accurate compact upwind difference operators have been used, together with th...
Third order compact upwind operators have been used together with the split fluxes of the KFVS (Kine...
A compact upwind difference operator is used to generate formally third order accurate spatial discr...
This paper is mainly concerned with the development of a class of new upwind methods and a novel tre...
This paper is mainly concerned with the development of a class of new upwind methods and a novel tre...
In the present paper we consider second order compact upwind schemes with a space split time derivat...
A family of compact upwind schemes with formal orders of accuracy 3 to 5 have been developed. Flux l...
In the present paper we consider second order compact upwind schemes with a space split time derivat...
A comparative study of the performance of commonly used, TVD or non-7VD second order accurate numeri...
A comparative study of five upwind schemes was performed to evaluate their ability accurately model ...
A new upwind Boltzmann scheme termed peculiar velocity based Upwind (PVU) method is developed for so...
This thesis presents and verifies a numerical method for solving the compressible Euler equations. T...
Kinetic Flux Vector Splitting (KFVS) has been extensively used to compute inviscid as well as viscou...
Many problems arising in the aerodynamic design of aerospace vehicles require the numerical solution...
A global fourth-order solution method that incorporates compact differencing with Roe\u27s approxima...