This effort investigates the accuracy of some flux-split algorithms in high-speed viscous flows. Three methods are examined: (1) MacCormack and Candler's (MC) scheme, (2) the van Leer (vL) scheme and (3) the method of Roe. The problems studied include the blunt body flow at Mach 16 and the flow past a 240 compression corner at Mach 14. Higher order accuracy is obtained with the MUSCL approach. Viscous terms are centered in the full Navier-Stokes cell- centered implicit finite volume simulation. The results indicate a relative similarity of predicted surface pressure with all methods on both flows. However, considerable disparity exists in heat transfer prediction especially on the coarser meshes with van Leer's splitting exhibiting the most...
Van Leer's flux vector splitting scheme and Osher's flux difference splitting scheme are compared f...
A brief description of the work currently underway on hypersonic viscous flow computations, based on...
A new flux splitting scheme is proposed. The scheme is remarkably simple and yet its accuracy rivals...
A comparative study of five upwind schemes was performed to evaluate their ability accurately model ...
The interaction of an impinging shock with the bow-shock generated by a blunt geometry is examined n...
Thin-Layer Navier-Stokes equations in generalized body-fitted coordinate system and non-dimensional ...
Over the past three years a finite element based procedure for the solution of high speed viscous co...
The use of a new splitting scheme, the advection upstream splitting method, for model aerodynamic pr...
resolution schemes. A High-resolution Algorithm for all speed flows 2 A new collocated finite volume...
A review is given of computations for a series of nominally 2-D laminar viscous-inviscid interaction...
A numerical code has been developed to solve the Viscous Shock Layer (VSL) equations for chemically ...
An algorithm for laminar and turbulent viscous compressible two dimensional flows is presented. For ...
A numerical method for solving the parabolic approximation to the steady-state compressible Navier-S...
An efficient time-splitting, second-order accurate, numerical scheme is used to solve the complete N...
Copyright © 2022 The Author(s). Artificial compressibility methods intend to offer divergence-free f...
Van Leer's flux vector splitting scheme and Osher's flux difference splitting scheme are compared f...
A brief description of the work currently underway on hypersonic viscous flow computations, based on...
A new flux splitting scheme is proposed. The scheme is remarkably simple and yet its accuracy rivals...
A comparative study of five upwind schemes was performed to evaluate their ability accurately model ...
The interaction of an impinging shock with the bow-shock generated by a blunt geometry is examined n...
Thin-Layer Navier-Stokes equations in generalized body-fitted coordinate system and non-dimensional ...
Over the past three years a finite element based procedure for the solution of high speed viscous co...
The use of a new splitting scheme, the advection upstream splitting method, for model aerodynamic pr...
resolution schemes. A High-resolution Algorithm for all speed flows 2 A new collocated finite volume...
A review is given of computations for a series of nominally 2-D laminar viscous-inviscid interaction...
A numerical code has been developed to solve the Viscous Shock Layer (VSL) equations for chemically ...
An algorithm for laminar and turbulent viscous compressible two dimensional flows is presented. For ...
A numerical method for solving the parabolic approximation to the steady-state compressible Navier-S...
An efficient time-splitting, second-order accurate, numerical scheme is used to solve the complete N...
Copyright © 2022 The Author(s). Artificial compressibility methods intend to offer divergence-free f...
Van Leer's flux vector splitting scheme and Osher's flux difference splitting scheme are compared f...
A brief description of the work currently underway on hypersonic viscous flow computations, based on...
A new flux splitting scheme is proposed. The scheme is remarkably simple and yet its accuracy rivals...