Application package for computations of 3d flow of viscous gas through tur-bomachinery cascades
Abstract
The conception of the new CFD solver for the 3D turbomachinery viscous compressible flow simulation using the RANS equations is considered. Choice of turbulent flow models, turbulence models and numerical methods is grounded. Realisability constraints and suitable boundary conditions are shown to be important for adverse pressure gradient flows. User interface of new application package is shown briefly. The numerical results for some test and engineering cases of viscous flows are presented.
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Published
2012-09-28
Issue
Section
Aero- and hydrodynamics in energy machines
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Copyright (c) 2016 С. В. Ершов
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