Abstract:
The technological aspects of the computing system “Potok-3” intended for
modeling of problems in aerodynamics and gas dynamics are considered. The
techniques and problems are discussed and investigated for global
parallelization of this computing system with respect to the main input
parameters. The $C$-, $L$- and $V$-type parallelizations of procedures in the
basic iteration kernel of the system for local acceleration of operations
are analyzed.
Keywords:parallel computing, aerodynamics, gas dynamics, application packages.