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International Journal of Fluid Mechanics Research
ESCI SJR: 0.206 SNIP: 0.446 CiteScore™: 0.5

ISSN Druckformat: 2152-5102
ISSN Online: 2152-5110

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International Journal of Fluid Mechanics Research

DOI: 10.1615/InterJFluidMechRes.2017020125
pages 553-563

INFLUENCE OF GEOMETRIC PARAMETERS AND CHEMICAL KINETICS MODEL ON COMBUSTION IN A SUPERSONIC FLOW

Alexander M. Molchanov
Aerospace Heating Engineering Department,Moscow Aviation Institute (National Research University) "MAI", Volokolamskoe shosse, d. 4, 125993, Moscow, Russia
Leonid V. Bykov
Aerospace Heating Engineering Department, Moscow Aviation Institute (National Research University) "MAI", Volokolamskoe shosse, d. 4, 125993, Moscow, Russia
Ivan M. Platonov
Aerospace Heating Engineering Department,Moscow Aviation Institute (National Research University) "MAI", Volokolamskoe shosse, d. 4, 125993, Moscow, Russia
Dmitry S. Yanyshev
Aerospace Heating Engineering Department,Moscow Aviation Institute (National Research University) "MAI", Volokolamskoe shosse, d. 4, 125993, Moscow, Russia

ABSTRAKT

This paper presents a mathematical model which describes the process of hydrogen combustion in a supersonic flow. The simulations were carried out to investigate the dependence of combustion from geometric parameters of the inlet, the combustion chamber, and the nozzle. Dependence on chemical and thermal non-equilibrium models, as well as a turbulence model, was shown.


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