The results of numerical modeling of the flows in the near wake behind plane and axisymmetric bodies in a wide range of Mach and Reynolds numbers are presented. The problem solution was sought in the approximation of Favre-averaged Navier-Stokes equations for a compressible heat-conductive
gas complemented by a semi-empirical turbulence model, which were solved with the method of splitting into physical processes and space directions. The peculiarities of the laminar, transitional and turbulent flows have
been studied.
Author(s):
Kovenya Viktor MikhailovichDr. , Professor
Position: General Scientist
Office: Federal Research Center for Information and Computational Technologies
Address: 630090, Russia, Novosibirsk, academician M.A. Lavrentiev avenue, 6
Phone Office: (383) 330 61 68
E-mail: kovenya@ict.nsc.ru
Lebedev Aleksandr StepanovichPhD.
Position: Senior Research Scientist
Office: Institute of Computational Technologies SB RAS
Address: 630090, Russia, Novosibirsk, ac. Lavrentyev Ave. 6
Phone Office: (3832) 307373
E-mail: sasa@net.ict.nsc.ru
