1. , 2, 3,J-1 and 1.81i, 6 - E given for a11 i = 2, 3,1-1. The quantity ( 5 : 6 - E represents the flux of change that c osses the top mesh boundary. If this boundary is located in the far flowfield or if the mesh is stretched so that AT satisfies the local explicit stability condition (22)at the mesh points near the boundary, as in the case of the test problems to be discussed later, this flux is set equal to zero. Otherwise,it should be suitably specified from the boundary conditions.
2. Following Ref. 5, the solution algorithm may now be summarized for each i and for j = J-1, 5-2,3,2in the following seven steps: