Abstract:
A three-dimensional method for solving tridiagonal systems of linear
equations arising as a result of using the implicit technique of splitting
for the Euler and Navier-Stokes equations is considered. Several
approaches to construct parallel algorithms for numerical realization of
the method under consideration are proposed. This allows the researches
to transport numerical programs of solving aerodynamic problems to computers
of new architecture. The algorithms being proposed can be implemented for
multiprocessor computing systems with common memory. The work was supported
by the Russian Foundation for Basic Research (00-07-90297, 99-01-00514).