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KIAM Preprint  50, Moscow, 2018
Authors: Borisov V. E., Davydov A. A., Kostantinovskaya T.V., Lutsky A. E., Shevchenko A.M., Shmakov A.S.
Simulation of supersonic flow in the wake behind a wing at M = 24
The structure of a supersonic vortex and its features depending on the Mach number M are described in this paper. The investigations are performed both in the near and far regions. Numerical and experimental data are compared. Numerical simulations were carried out in Keldysh Institute of Applied Mathematics RAS using parallel algorithms for turbulent flows simulating. The experimental part was carried out in Khristianovich Institute of Theoretical and Applied Mechanics SB RAS.
wingtip vortex, vortex wake, supersonic flow, numerical simulation, experimental investigation, URANS, LES
Publication language: russian,  pages: 19
Research direction:
Mathematical modelling in actual problems of science and technics
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About authors:
  • Borisov Vitaly Evgenyevich, RAS
  • Davydov Alexandr Alexandrovich, RAS
  • Kostantinovskaya Tatiana Vitalievna, RAS
  • Lutsky Alexander Evgenievich, RAS
  • Shevchenko Andrey Mihailovich, 
  • Shmakov Andrey Sergeevich,