Numerical study of the flow around spacecraft model
Abstract:
The paper is devoted to a numerical study of the flow around spacecraft model using developed software for simulation three-dimensional turbulent flows of a viscous compressible gas. A comparative analysis of the influence of the choice of Spalart-Allmaras or Menter SST turbulent models on the flow is presented. Numerical results are compared with published experimental data.
Keywords:
URANS equations, Spalart-Allmaras turbulent model, SST turbulent model, re-entering body
Publication language:russian, pages:19
Research direction:
Mathematical modelling in actual problems of science and technics
