The Van Leer flux splitting is known to produce excessive numerical dissipation for Navier-Stokes calculations. Researchers attempt to remedy this deficiency by introducing a higher order polynomial expansion (HOPE) for the mass flux. In addition to Van Leer's splitting, a term is introduced so that the mass diffusion error vanishes at M equals 0. Several splittings for pressure are proposed and examined. The effectiveness of the HOPE scheme is illustrated for 1-D hypersonic conical viscous flow and 2-D supersonic shock-wave boundary layer interactions. Also, the authors give the weakness of the scheme and suggest areas for further investigation
To resolve many flow features accurately, like accurate capture of suction peak in subsonic flows an...
breed of upwind schemes have been produced since the beginning of the 90s. To be practically useful,...
Die von Liou und Steffen entwickelte Upwind-Diskretisierung (Advection Upstream Splitting Method, AU...
The Van Leer flux splitting is known to produce excessive numerical dissipation for Navier-Stokes ca...
Maximizing both accuracy and efficiency has been the primary objective in designing a numerical algo...
A new flux splitting scheme is proposed. The scheme is remarkably simple and yet its accuracy rivals...
The use of a new splitting scheme, the advection upstream splitting method, for model aerodynamic pr...
A flux splitting scheme is proposed for the general nonequilibrium flow equations with an aim at rem...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76141/1/AIAA-1991-1566-857.pd
Among the various numerical schemes developed since the '80s for the computation of the compressible...
While enjoying demonstrated improvement in accuracy, efficiency, and robustness over existing scheme...
A novel high order compact scheme for solving the compressible Navier-Stokes equations has been deve...
Van Leer's flux vector splitting scheme and Osher's flux difference splitting scheme are compared f...
This effort investigates the accuracy of some flux-split algorithms in high-speed viscous flows. Thr...
To resolve many flow features accurately, like accurate capture of suction peak in subsonic flows an...
To resolve many flow features accurately, like accurate capture of suction peak in subsonic flows an...
breed of upwind schemes have been produced since the beginning of the 90s. To be practically useful,...
Die von Liou und Steffen entwickelte Upwind-Diskretisierung (Advection Upstream Splitting Method, AU...
The Van Leer flux splitting is known to produce excessive numerical dissipation for Navier-Stokes ca...
Maximizing both accuracy and efficiency has been the primary objective in designing a numerical algo...
A new flux splitting scheme is proposed. The scheme is remarkably simple and yet its accuracy rivals...
The use of a new splitting scheme, the advection upstream splitting method, for model aerodynamic pr...
A flux splitting scheme is proposed for the general nonequilibrium flow equations with an aim at rem...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76141/1/AIAA-1991-1566-857.pd
Among the various numerical schemes developed since the '80s for the computation of the compressible...
While enjoying demonstrated improvement in accuracy, efficiency, and robustness over existing scheme...
A novel high order compact scheme for solving the compressible Navier-Stokes equations has been deve...
Van Leer's flux vector splitting scheme and Osher's flux difference splitting scheme are compared f...
This effort investigates the accuracy of some flux-split algorithms in high-speed viscous flows. Thr...
To resolve many flow features accurately, like accurate capture of suction peak in subsonic flows an...
To resolve many flow features accurately, like accurate capture of suction peak in subsonic flows an...
breed of upwind schemes have been produced since the beginning of the 90s. To be practically useful,...
Die von Liou und Steffen entwickelte Upwind-Diskretisierung (Advection Upstream Splitting Method, AU...