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KIAM Preprint № 97, Moscow, 2017
Authors: Vlasenko V.V., Zhukov V. T., Novikova N.D., Feodoritova O. B.
Numerical simulation of different regimes of high-speed combustion chamber
The flows in a model combustion chamber of a ramjet/scramjet engine with supersonic flow at the inlet are considered. The influence of the hydrocarbon fuel consumption on the combustion processes is studied based on Navier-Stokes equations of a reacting multicomponent flows. Numerical 2D simulation is performed on the K-100 supercomputer by means of OpenFOAM. It is obtained that depending on the fuel consumption the stationary and pulsating combustion processes are possible. The results agree qualitatively with known calculated and experimental data.
mathematical simulation, high-speed combustor; hydrocarbon fuel, OpenFOAM
Publication language: russian,  pages: 32
Research direction:
Mathematical modelling in actual problems of science and technics
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About authors:
  • Vlasenko Vladimir Victorovich,  ,  Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского
  • Zhukov Victor Timofeevich, RAS
  • Novikova Natalia Dmitrievna, RAS
  • Feodoritova Olga Borisovna, RAS