"Parallelization in the vortex method for solving aerodynamic problems"
Aparinov A.A., Setukha A.V.

A software implementation of a parallel algorithm realizing the vortex method is considered for the case of solving 3D aerodynamic problems on multiprocessor platforms. The main computing costs are analyzed. A number of new problem classes are described. The numerical results illustrating the efficiency of the new algorithm are discussed.

Keywords: vortex methods, parallel computing, fast matrix algorithms, aerodynamics, incompressible fluid

Aparinov A.A., e-mail: andrey.aparinov@gmail.com – Research Institute of Parachute Design and Production; ulitsa Irkutskaya 2, Moscow, 107241, Russia
Setukha A.V., e-mail: setuhaav@rambler.ru – Research Computing Center, Lomonosov Moscow State University; Leninskiye Gory, Moscow, 119991, Russia