Numerical solutions of Euler equations using simplified flux vector splitting
Abstract
A numerical method for solving the twodimensional steady Euler equations using flux vector splitting is developed. The equations are expressed in curvilinear coordinates and the finite volume approach is used. The energy equation is omitted since only steady state solutions are required. A simple implicit procedure is employed to increase the stability limits of the present method. Present numerical results are compared with predictions obtained by other authors.
 Publication:

AIAA, SAE, ASME, and ASEE, 21st Joint Propulsion Conference
 Pub Date:
 July 1985
 Bibcode:
 1985jpmc.confR....V
 Keywords:

 Cascade Flow;
 Computational Fluid Dynamics;
 Euler Equations Of Motion;
 Finite Volume Method;
 Supersonic Flow;
 Two Dimensional Flow;
 Computational Grids;
 Outlet Flow;
 Steady Flow;
 Transonic Flow;
 Vectors (Mathematics);
 Fluid Mechanics and Heat Transfer