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Numerical Modeling of Subsonic Axisymmetric Reacting Gas Flows Full article

Conference 6th All-Russian Conference on Thermophysics and Physical Hydrodynamics
22-29 Aug 2021 , Севастополь
Journal Journal of Physics: Conference Series
ISSN: 1742-6588 , E-ISSN: 1742-6596
Output data Year: 2021, Volume: 2057, Number: 1, Article number : 012071, Pages count : 7 DOI: 10.1088/1742-6596/2057/1/012071
Tags Mach number; Navier Stokes equations; Pyrolysis
Authors Peskova E.E. 1,2
Affiliations
1 Ogarev Mordovia State University, 68 Bolshevistskaya Street, Saransk, 430005, Russia
2 Boreskov Institute of Catalysis SB RAS, 5 Lavrentyev Avenue, Novosibirsk, 630090, Russia

Funding (1)

1 Russian Science Foundation 21-19-00429

Abstract: A numerical algorithm is developed and implemented for modelling axisymmetric subsonic reacting gas flows based on a previously created program for plane flows. The system of Navier-Stokes equations in the low Mach number limit is used as a mathematical model. Calculations of ethane pyrolysis for axisymmetric and plane flow of mixture at heat supply from the reactor's walls are carried out. Through the interplay of the developed code and the code for plane flows it becomes possible to identify the geometric factor role at the presence of a large number of nonlinear physicochemical processes. We found that diffusion of synthesized molecular hydrogen mainly influences heat supply from the reactor's walls to gas and pyrolysis products distribution along its length.
Cite: Peskova E.E.
Numerical Modeling of Subsonic Axisymmetric Reacting Gas Flows
Journal of Physics: Conference Series. 2021. V.2057. N1. 012071 :1-7. DOI: 10.1088/1742-6596/2057/1/012071 Scopus РИНЦ OpenAlex
Dates:
Published print: Nov 8, 2021
Published online: Nov 8, 2021
Identifiers:
Scopus: 2-s2.0-85119623403
Elibrary: 47533449
OpenAlex: W3212766611
Citing:
DB Citing
Scopus 7
Elibrary 12
OpenAlex 8
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