The Riemann solver,flux difference splitting(FDS),is employed to estimate the numerical normal flux of variables including flow,momentum and pollutant concentration across the interface between cells.

The flux difference splitting(FDS) scheme was employed to calculate the numerical flux across the interface between cells in the framework of the finite volume method.

Calculations for the flowfield of helicopter rotors in forward flight based on high-order upwind flux-difference splitting scheme;

A high order accurate MmB difference scheme based on flux splitting;

It is based on flux splitting, piecewise linear cell-averaged reconstruction and upwind property in the spatial discretization.

A continuous flux splitting method for unsteady Euler equations based on time-dependent body fitted coordinates is given.

LU implicit timeformat and Van-Leer flux vector splitting format were applied in two-fluid model.

By the use of implicit flux vector splitting method, three dimensional dimensionless conservative parabolic navier stokes equation is solved in general curved coordinates system.

Based on flux vector splitting, a conservative and implicit defference scheme is presented for one dimensional shallow discontinuous water equations with arbitrary cross section.