Comparison of turbulence models for a supersonic tip vortex simulation
Abstract:
In the paper the turbulence models SA, SST and DES based on SA are compared for simulation of supersonic tip vortex at incoming flow Mach number M? = 3 and wing generator attack angles of 10 and 20 degrees. The simulations were carried out on the hybrid supercomputer system K-60 at the Keldysh Institute of Applied Mathematics RAS.
Keywords:
supersonic tip vortex, turbulence models, vortex flow visualization methods
Publication language:russian, pages:24
Research direction:
Mathematical modelling in actual problems of science and technics
