Book Description

A new parallel numerical scheme for solving incompressible steady-state flows is presented. The algorithm uses a finite-difference approach to solving the Navier-Stokes equations. The algorithms are scalable and expandable. They may be used with only two processors or with as many processors as are available. The code is general and expandable. Any size grid may be used. Four processors of the NASA LeRC Hypercluster were used to solve for steady-state flow in a driven square cavity. The Hypercluster was configured in a distributed-memory, hypercube-like architecture. By using a 50-by-50 finite-difference solution grid, an efficiency of 74 percent (a speedup of 2.96) was obtained. Milner, Edward J. and Lin, Avi and Liou, May-Fun and Blech, Richard A. Glenn Research Center NASA-TM-4451, E-7345, NAS 1.15:4451 NASA ORDER C-99066-G; RTOP 505-62-52...