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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
Abstract:
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.
Keywords:
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
Russian source text:
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About authors:
  • Borisov Vitaly Evgenyevich,  orcid.org/0000-0003-4448-7474KIAM RAS
  • Davydov Alexandr Alexandrovich,  orcid.org/0000-0001-5662-817XKIAM RAS
  • Kostantinovskaya Tatiana Vitalievna,  orcid.org/0000-0002-1127-503XKIAM RAS
  • Lutsky Alexander Evgenievich,  orcid.org/0000-0002-4442-0571KIAM RAS
  • Shevchenko Andrey Mihailovich, 
  • Shmakov Andrey Sergeevich,