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KIAM Preprint  98, Moscow, 2014
Authors: Davydov A. A., Lutsky A. E.
Numerical simulation of supersonic flows in the wing wake and its interaction with crossing shock waves
The results of numerical simulation of supersonic flow in the wing wake and its interaction with shock waves investigation are presented. The system of couple counter wedges with a sharp edge has been used for the formation of shock waves of varying intensity. Investigation of regular and Mach interaction of shock waves has been performed. Calculations have been performed on a multiprocessor computer system K-100 in KIAM RAS. Experiments were carried out in a supersonic wind tunnel T325 (ITAM SB RAS) at the Mach number 3.
wingtip vortices, shock waves, turbulent models, RANS, DES, WENO
Publication language: russian,  pages: 16
Research direction:
Mathematical modelling in actual problems of science and technics
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About authors:
  • Davydov Alexandr Alexandrovich, RAS
  • Lutsky Alexander Evgenievich, RAS